command: ./cs_solver --mpi --param setup.xml *************************************************************** (R) Code_Saturne Version 5.2.0 Copyright (C) 1998-2018 EDF S.A., France revision 5.2.0 build Mon Apr 30 15:01:18 2018 MPI version 3.1 (MPICH 3.2) 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: Sun May 6 22:38:43 2018 System: Linux 3.0.101-0.46.1_1.0502.8871-cray_ari_c Machine: nid00027 Processor: model name : Intel(R) Xeon(R) CPU E5-2697 v2 @ 2.70GHz Memory: 64523 MB Directory: /fs3/e01/e01/yyan/rans/0018turbine/case1les/RESU/20180506-2238 MPI ranks: 192 (appnum attribute: 0) OpenMP threads: 1 Processors/node: 1 I/O read method: collective MPI-IO (explicit offsets) I/O write method: collective MPI-IO (explicit offsets) I/O rank step: 1 External libraries for partitioning: ParMETIS 4.0.3 Reading metadata from file: "mesh_input" =============================================================== CALCULATION PREPARATION ======================= =========================================================== @ @@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@ @ @ @@ WARNING : WHEN READING INPUT DATA @ ========= @ CHOICE OF TIME-SCHEME @ @ TIME-SCHEME FOR VELOCITY IS SECOND ORDER @ (THETAV = 0.50E+00) @ CERTAIN TERMS ARE HOWEVER FIRST ORDER IN TIME WITH @ THE FOLLOWING SETTINGS: @ @ parameters ISTMPF ISNO2T ISTO2T IROEXT IVIEXT ICPEXT @ Values entered 2 1 0 0 0 0 @ @ computation will go on. @ @ Check the input data given through the User Interface @ or in cs_user_parameters.f90. @ @ @@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@ @ No error detected during the data verification cs_user_parameters.f90 and others). =========================================================== CALCULATION PARAMETERS SUMMARY ============================== ----------------------------------------------------------- ** DIMENSIONS ---------- --- Physics NVAR = 4 (Nb variables ) NSCAL = 0 (Nb scalars ) NSCAUS = 0 (Nb user scalars ) NSCAPP = 0 (Nb specific physics scalars ) ----------------------------------------------------------- ** VOF METHOD ---------------------------------------- IVOFMT = -1 ( -1: inactive ) ( 0: active ) ** HOMOGENEOUS MIXTURE MODEL FOR CAVITATION ---------------------------------------- ICAVIT = -1 (-1: single phase flow ) ( 0: no vap./cond. model ) ( 1: Merkle's model ) ----------------------------------------------------------- ** TIME STEPPING ------------- --- Per-variable properties ------------------------------------ Variable ISTAT CDTVAR ------------------------------------ Velocity 1 0.1000E+01 Pressure 0 0.1000E+01 ---------------------------- ISTAT = 0 ou 1 (1 for unsteady ) CDTVAR > 0 (time step multiplier ) --- Order of base time stepping scheme ISCHTP = 2 (1: order 1; 2: order 2 ) ----------------------------------------------------------- ** STOKES ------ -- Phase continue : ISTMPF = 2 (time scheme for flow (0: explicit (THETFL = 0 ) (1: std scheme (Saturne 1.0 ) (2: 2nd-order (THETFL = 0.5 ) THETFL = 0.50000E+00 (theta for mass flow ) IROEXT = 0 (density extrapolation (0: explicit (1: n+thetro with thetro=1/2 (2: n+thetro with thetro=1 THETRO = 0.00000E+00 (theta for density ((1+theta).new-theta.old IVIEXT = 0 (total viscosity extrapolation (0: explicit (1: n+thetvi with thetro=1/2 (2: n+thetvi with thetro=1 THETVI = 0.00000E+00 (theta for total viscosity ((1+theta).new-theta.old ICPEXT = 0 (specific heat extrapolation (0: explicit (1: n+thetcp with thetro=1/2 (2: n+thetcp with thetro=1 THETCP = 0.00000E+00 (specific heat theta-scheme ((1+theta).new-theta.old THETSN = 0.50000E+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 ) ----------------------------------------------------------- ** BASE ITERATIVE SOLVERS ---------------------- ------------------------------------ Variable EPSILO IDIRCL ------------------------------------ Velocity 0.1000E-04 1 Pressure 0.1000E-04 1 ------------------------------------ EPSILO = (resolution precision) IDIRCL = 0 ou 1 (shift diagonal if ISTAT=0 and no Dirichlet) ----------------------------------------------------------- ** 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. INPDT0 = 0 (1: 0 time step calcuation ) NTMABS = 100000 (Final time step required ) --- CPU time margin TMARUS = -0.10000E+01 (CPU time margin before stop ) ----------------------------------------------------------- ** INPUT-OUTPUT ------------ --- Restart file NTSUIT = 5000 (Checkpoint frequency ) --- Probe history files NTHIST = 1 (Output frequency ) FRHIST = -.10000E+01 (Output frequency (s) ) -- -- -- --- Log files NTLIST = 1 (Output frequency ) Number Name IWARNI verbosity level (-999: not applicable) Velocity 0 Pressure 0 TurbVisc -999 CourantNb -999 FourierNb -999 total_pressure -999 Yplus -999 -- -- -- --- Additional post-processing variables (ipstdv) ipstfo = 1 (Force exerted by the fluid on the boundary) ipstyp = 1 (y+ at boundary) ipsttp = 0 (T+ at boundary) ipstft = 1 (Thermal flux at boundary) ipstnu = 0 (Dimensionless thermal flux at boundary) ----------------------------------------------------------- ** ALE METHOD (MOVING MESH) ----------- IALE = 0 (1: activated ) 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: time dependency: transient connectivity output: every 1000 time steps and at calculation end -5: name: directory: monitoring format: time_plot options: time dependency: fixed mesh output: every 1 time steps -6: name: directory: profiles format: plot options: time dependency: fixed mesh output: at calculation end -7: name: histograms directory: histograms format: histogram options: txt time dependency: fixed mesh output: at calculation end Reading file: mesh_input Finished reading: mesh_input No "partition_input/domain_number_192" file available; ---------------------------------------------------------- Partitioning by space-filling curve: Morton (in bounding box). Number of cells per domain (histogramm): [ 12587 ; 12588 ] = 192 Partitioning finished (10.7 s) ------------------------------------------------------- Joining number 1: Selection criteria: "not (I1 or I2)" Parameters for the joining operation: Shortest incident edge fraction: 0.10000 Maximum angle between joined face planes: 25.00000 Advanced joining parameters: Verbosity level: 1 Visualization level: 1 Deepest level reachable in tree building: 30 Max boxes by leaf: 25 Max ratio of linked boxes / init. boxes: 5.00000 Max ratio of boxes for distribution: 2.00000 Merge step tolerance multiplier: 1.00000 Pre-merge factor: 0.05000 Tolerance computation mode: 1 Intersection computation mode: 1 Max. number of equiv. breaks: 500 Max. number of subfaces by face: 200 Before joining Number of cells: 2416860 Number of interior faces: 7350183 Number of boundary faces: 42480 Number of vertices: 2558936 Global number of boundary faces selected for joining: 22320 Element selection successfully done. Global min/max. tolerance: Glob. Num. | Tolerance | Coordinates 2019679 | 0.000003 | 6.7439362251e-01 -5.3189766473e-01 2.7755575616e-17 | ORI 726769 | 0.000500 | 3.0000000000e+01 1.5000000000e+01 7.0000000000e-02 | ORI Determination of possible face intersections: bounding-box tree layout: 3D Global number of intersections detected: 0 Vertex-Vertex intersections: 0 Other intersections: 0 Joining operation did modify any vertices. Edge intersections and vertex creation done. Global number of faces after splitting: 22320 Global configuration after the joining operation: Global number of border faces to add: 22320 Joining operation is null. Mesh cleaning done for degenerate faces. Global number of cleaned interior faces: 0 Global number of cleaned border faces: 0 After joining Number of cells: 2416860 Number of interior faces: 7350183 Number of boundary faces: 42480 Number of vertices: 2558936 Joining 1 completed (0.115 s). ------------------------------------------------------- Joining number 2: Periodicity type: translation Transformation matrix: 1 0 0 0 0 1 0 0 0 0 1 0.1 Selection criteria: "p1 or p2" Parameters for the joining operation: Shortest incident edge fraction: 0.10000 Maximum angle between joined face planes: 25.00000 Advanced joining parameters: Verbosity level: 1 Visualization level: 1 Deepest level reachable in tree building: 30 Max boxes by leaf: 25 Max ratio of linked boxes / init. boxes: 5.00000 Max ratio of boxes for distribution: 2.00000 Merge step tolerance multiplier: 1.00000 Pre-merge factor: 0.05000 Tolerance computation mode: 1 Intersection computation mode: 1 Max. number of equiv. breaks: 500 Max. number of subfaces by face: 200 Before joining Number of cells: 2416860 Number of interior faces: 7350183 Number of boundary faces: 42480 Number of vertices: 2558936 Global number of boundary faces selected for joining: 0 Element selection successfully done. Stop joining algorithm: no face selected... After joining Number of cells: 2416860 Number of interior faces: 7350183 Number of boundary faces: 42480 Number of vertices: 2558936 Joining 2 completed (0.0134 s). All joining operations successfully finished: Wall clock time: 0.129 ---------------------------------------------------------- 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 Histogram of the number of cells per rank: minimum value = 12587 maximum value = 12588 1 : [ 12587 ; 12588 ] = 192 ---------------------------------------------------------- Histogram of the number of standard + halo cells per rank: minimum value = 16508 maximum value = 38650 1 : [ 16508 ; 20936 [ = 26 2 : [ 20936 ; 25364 [ = 22 3 : [ 25364 ; 29793 [ = 12 4 : [ 29793 ; 34221 [ = 10 5 : [ 34221 ; 38650 ] = 122 ---------------------------------------------------------- Histogram of the number of ghost cells per rank: minimum value = 3920 maximum value = 26063 1 : [ 3920 ; 8348 [ = 26 2 : [ 8348 ; 12777 [ = 22 3 : [ 12777 ; 17205 [ = 12 4 : [ 17205 ; 21634 [ = 10 5 : [ 21634 ; 26063 ] = 122 ---------------------------------------------------------- Histogram of the number of interior faces per rank: minimum value = 39241 maximum value = 50867 1 : [ 39241 ; 41566 [ = 14 2 : [ 41566 ; 43891 [ = 33 3 : [ 43891 ; 46216 [ = 12 4 : [ 46216 ; 48541 [ = 11 5 : [ 48541 ; 50867 ] = 122 ---------------------------------------------------------- Histogram of the number of boundary faces per rank: minimum value = 0 maximum value = 1250 1 : [ 0 ; 250 [ = 129 2 : [ 250 ; 500 [ = 50 3 : [ 500 ; 750 [ = 9 4 : [ 750 ; 1000 [ = 3 5 : [ 1000 ; 1250 ] = 1 ---------------------------------------------------------- Histogram of the number of interior faces per cell: minimum value = 5 maximum value = 6 1 : [ 5 ; 6 ] = 2416860 ---------------------------------------------------------- Histogram of the number of neighboring domains per rank: minimum value = 6 maximum value = 43 1 : [ 6 ; 13 [ = 41 2 : [ 13 ; 20 [ = 50 3 : [ 20 ; 28 [ = 65 4 : [ 28 ; 35 [ = 31 5 : [ 35 ; 43 ] = 5 ---------------------------------------------------------- Global definition of the number of elements (cells, vertices, faces...) Synchronizing cell families ---------------------------------------------------------- Ignoring periodicity for graph-based partitioning. Partitioning 2416860 cells to 192 domains on 192 ranks (ParMETIS_V3_PartKway). Total number of faces on parallel boundaries: 259246 wall-clock time: 0.097730 s Number of cells per domain (histogramm): [ 7947 ; 8883 [ = 3 [ 8883 ; 9819 [ = 5 [ 9819 ; 10755 [ = 9 [ 10755 ; 11691 [ = 37 [ 11691 ; 12627 [ = 50 [ 12627 ; 13563 [ = 44 [ 13563 ; 14499 [ = 25 [ 14499 ; 15435 [ = 12 [ 15435 ; 16371 [ = 4 [ 16371 ; 17307 ] = 3 Writing file: partition_output/domain_number_192 Finished writing: partition_output/domain_number_192 Partitioning finished (0.153 s) ---------------------------------------------------------- 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 Histogram of the number of cells per rank: minimum value = 7947 maximum value = 17307 1 : [ 7947 ; 9819 [ = 8 2 : [ 9819 ; 11691 [ = 46 3 : [ 11691 ; 13563 [ = 94 4 : [ 13563 ; 15435 [ = 37 5 : [ 15435 ; 17307 ] = 7 ---------------------------------------------------------- Histogram of the number of standard + halo cells per rank: minimum value = 10463 maximum value = 21371 1 : [ 10463 ; 12644 [ = 10 2 : [ 12644 ; 14826 [ = 47 3 : [ 14826 ; 17007 [ = 97 4 : [ 17007 ; 19189 [ = 30 5 : [ 19189 ; 21371 ] = 8 ---------------------------------------------------------- Histogram of the number of ghost cells per rank: minimum value = 2110 maximum value = 4064 1 : [ 2110 ; 2500 [ = 9 2 : [ 2500 ; 2891 [ = 48 3 : [ 2891 ; 3282 [ = 67 4 : [ 3282 ; 3673 [ = 54 5 : [ 3673 ; 4064 ] = 14 ---------------------------------------------------------- Histogram of the number of interior faces per rank: minimum value = 25415 maximum value = 54569 1 : [ 25415 ; 31245 [ = 9 2 : [ 31245 ; 37076 [ = 48 3 : [ 37076 ; 42907 [ = 94 4 : [ 42907 ; 48738 [ = 34 5 : [ 48738 ; 54569 ] = 7 ---------------------------------------------------------- Histogram of the number of boundary faces per rank: minimum value = 0 maximum value = 903 1 : [ 0 ; 180 [ = 107 2 : [ 180 ; 361 [ = 14 3 : [ 361 ; 541 [ = 39 4 : [ 541 ; 722 [ = 23 5 : [ 722 ; 903 ] = 9 ---------------------------------------------------------- Histogram of the number of interior faces per cell: minimum value = 5 maximum value = 6 1 : [ 5 ; 6 ] = 2416860 ---------------------------------------------------------- Histogram of the number of neighboring domains per rank: minimum value = 4 maximum value = 9 1 : [ 4 ; 5 [ = 8 2 : [ 5 ; 6 [ = 25 3 : [ 6 ; 7 [ = 44 4 : [ 7 ; 8 [ = 55 5 : [ 8 ; 9 ] = 60 ---------------------------------------------------------- Global definition of the number of elements (cells, vertices, faces...) 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 Numbering for cells: type: default Numbering for interior faces: type: default Numbering for boundary faces: type: default ---------------------------------------------------------- Histogram of volume mesh matrix bandwidth per rank: minimum value = 10265 maximum value = 20958 1 : [ 10265 ; 12403 [ = 11 2 : [ 12403 ; 14542 [ = 55 3 : [ 14542 ; 16680 [ = 88 4 : [ 16680 ; 18819 [ = 32 5 : [ 18819 ; 20958 ] = 6 Histogram of volume mesh matrix profile/lines per rank: minimum value = 1624 maximum value = 3139 1 : [ 1624 ; 1927 [ = 14 2 : [ 1927 ; 2230 [ = 58 3 : [ 2230 ; 2533 [ = 74 4 : [ 2533 ; 2836 [ = 38 5 : [ 2836 ; 3139 ] = 8 Mesh coordinates: minimum and maximum X : -1.2000000e+01 3.0000000e+01 Y : -1.5000000e+01 1.5000000e+01 Z : 0.0000000e+00 1.0000000e-01 Mesh Number of cells: 2416860 Number of interior faces: 7350183 Number of boundary faces: 42480 Number of vertices: 2558936 Periodic faces (which are also interior faces): Periodicity 1: 120843 face couples Groups: "1" cells: 352800 "2" cells: 493920 "I1" boundary faces: 10080 "I2" boundary faces: 10080 "blk-1" cells: 7220 "blk-10" cells: 14440 "blk-11" cells: 42560 "blk-12" cells: 57000 "blk-13" cells: 367200 "blk-14" cells: 49400 "blk-2" cells: 57000 "blk-3" cells: 42560 "blk-4" cells: 49400 "blk-5" cells: 367200 "blk-6" cells: 367200 "blk-7" cells: 49400 "blk-8" cells: 42560 "blk-9" cells: 57000 "inlet" boundary faces: 2480 "outlet" boundary faces: 2100 "p1" interior faces: 120843 "p2" interior faces: 120843 "symmetry" boundary faces: 5500 "wall1" boundary faces: 4080 "wall2" boundary faces: 4080 "wall3" boundary faces: 4080 Criterion 1: Orthogonality: Number of bad cells detected: 0 --> 0 % Criterion 2: Offset: Number of bad cells detected: 20 --> 0 % Criterion 3: Least-Squares Gradient Quality: Number of bad cells detected: 14140 --> 1 % Criterion 4: Cells Volume Ratio: Number of bad cells detected: 0 --> 0 % Criterion 5: Guilt by Association: Number of bad cells detected: 0 --> 0 % Warning: -------- Mesh quality issue has been detected The mesh should be re-considered using the listed criteria. The calculation will run but the solution quality may be degraded... Computing geometric quantities (0.0317 s) ALMAX = 0.50133E+01 (Characteristic length ) ALMAX is the cubic root of the domain volume. ----------------------------------------------------------- ** READING MAIN AND AUXILIARY RESTART FILES ---------------------------------------- READING THE MAIN RESTART FILE Start reading Code_Saturne: /work/e01/e01/yyan/code_saturne/code_saturne-5.2.0/src/base/cs_restart.c:1445: Warning The size of location "interior_faces" associated with the restart file "restart/main" is 7360263 and does not correspond to that of the current mesh (7350183). Code_Saturne: /work/e01/e01/yyan/code_saturne/code_saturne-5.2.0/src/base/cs_restart.c:1445: Warning The size of location "boundary_faces" associated with the restart file "restart/main" is 22320 and does not correspond to that of the current mesh (42480). Code_Saturne: /work/e01/e01/yyan/code_saturne/code_saturne-5.2.0/src/base/cs_restart.c:1445: Warning The size of location "vertices" associated with the restart file "restart/main" is 2549379 and does not correspond to that of the current mesh (2558936). Reading dimensions complete Reading the previous time step number (restarting computation) NTPABS = 54998 Reading the previous time step number (restarting computation) TTPABS = 0.8748E-01 restart/main: section "turbomachinery:rotor_time_and_angle" has 2 values and not 3. Reading options complete Read variables from restart: restart/main Reading complete READING THE AUXILIARY RESTART FILE Start reading Code_Saturne: /work/e01/e01/yyan/code_saturne/code_saturne-5.2.0/src/base/cs_restart.c:1445: Warning The size of location "interior_faces" associated with the restart file "restart/auxiliary" is 7360263 and does not correspond to that of the current mesh (7350183). Code_Saturne: /work/e01/e01/yyan/code_saturne/code_saturne-5.2.0/src/base/cs_restart.c:1445: Warning The size of location "boundary_faces" associated with the restart file "restart/auxiliary" is 22320 and does not correspond to that of the current mesh (42480). Code_Saturne: /work/e01/e01/yyan/code_saturne/code_saturne-5.2.0/src/base/cs_restart.c:1445: Warning The size of location "vertices" associated with the restart file "restart/auxiliary" is 2549379 and does not correspond to that of the current mesh (2558936). @ @@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@ @ @ @@ WARNING: WHEN READING THE AUXILIARY RESTART FILE @ ======= @ PREVIOUS and PRESENT INPUT DATA ARE DIFFERENT @ @ The number of the faces internes has been modified @ @ The run can continue but the data on the @ faces internes will not be reread @ in the suite file. @ They will be initialized by the default values. @ @ This situation can occur when the restart file @ originates from a run using different options @ to join the grids or when the periodicity boundary @ conditions have been modified. @ This situation can also be generated when the @ run is conducted on a different machine @ in which case the precision of the machine modifies @ the number of faces generated when joinning the grids. @ @ Finally, this situation can be due to the fact that @ the auxiliary restart file does not correspond to @ the present case. @ @ Verify that the auxiliary restart file being used @ corresponds to the present case. @ @ The run will continue... @ @@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@ @ @ @@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@ @ @ @@ WARNING: WHEN READING THE AUXILIARY RESTART FILE @ ======= @ PREVIOUS and PRESENT INPUT DATA ARE DIFFERENT @ @ The number of the faces de bord has been modified @ @ The run can continue but the data on the @ faces de bord will not be reread @ in the suite file. @ They will be initialized by the default values. @ @ This situation can occur when the restart file @ originates from a run using different options @ to join the grids or when the periodicity boundary @ conditions have been modified. @ This situation can also be generated when the @ run is conducted on a different machine @ in which case the precision of the machine modifies @ the number of faces generated when joinning the grids. @ @ Finally, this situation can be due to the fact that @ the auxiliary restart file does not correspond to @ the present case. @ @ Verify that the auxiliary restart file being used @ corresponds to the present case. @ @ The run will continue... @ @@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@ @ Fin de la lecture des options Fin de la lecture des proprietes physiques Fin de la lecture du pas de temps restart/auxiliary: section "time_moments:sizes" not present. End reading ----------------------------------------------------------- ----------------------------------------------------------- ** VARIABLES INITIALIZATION ------------------------ ----------------------------------------- Variable Min. value Max. value ----------------------------------------- Velocity -0.6042E+01 0.1308E+02 Velocity -0.1038E+02 0.1193E+02 Velocity -0.3136E+01 0.2969E+01 Pressure -0.8543E+02 0.3606E+02 --------------------------------- dt 0.1000E-06 0.1000E-06 --------------------------------- ------------------------------------------------------------- ------------------------------------------------------------- =============================================================== MAIN CALCULATION ================ =============================================================== =============================================================== INSTANT 0.874801000E-01 TIME STEP NUMBER 54999 ============================================================= ----------------------------------------- Property Min. value Max. value ----------------------------------------- density 0.1179E+01 0.1179E+01 molecular_viscos 0.1830E-04 0.1830E-04 turbulent_viscos 0.1160E-19 0.4963E-02 ----------------------------------------- ** INFORMATION ON BOUNDARY FACES TYPE ---------------------------------- ------------------------------------------------------------------------- Boundary type Code Nb faces ------------------------------------------------------------------------- Inlet 2 2480 Smooth wall 5 12240 Rough wall 6 0 Symmetry 4 5500 Free outlet 3 2100 Free inlet 14 0 Convective inlet 16 0 Sat/Sat coupling 13 20160 Free surface 15 0 Undefined 1 0 ------------------------------------------------------------------------- Boundary faces with free inlet/outlet detected Update of reference point for total pressure XYZP0 = 0.30000E+02 0.44113E-15 0.25000E-02 ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 0.000000000E+00 Smooth wall 5 12240 0.000000000E+00 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.000000000E+00 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 0.000000000E+00 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19766E-01 0.21048E+01 Friction velocity uk : 0.19766E-01 0.21048E+01 Dimensionless distance yplus : 0.19146E-01 0.20667E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 2.659533579e-03 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29435E+08 1 0.11573E-13 0.41900E+03 0.80842E+04 c Velocity[X] 0.20937E+03 c Velocity[Y] 0.20963E+03 c Velocity[Z] 0.41692E-03 c Pressure 0.12709E-03 74 0.61806E-04 0.17685E+00 0.10032E+08 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -6.0844 13.083 5.6084 8.0002 v Velocity[Y] -10.367 11.974 -0.14285 -0.00067431 v Velocity[Z] -3.1359 2.9695 3.6286e-06 -5.3857e-08 v ǁVelocityǁ 0.002979 14.455 6.3226 8.0016 v Pressure -19244 25144 -1040.9 23.49 v TurbVisc 1.1603e-20 0.0049634 2.1899e-05 9.3621e-07 v CourantNb 0 0 0 0 v FourierNb 1.2425e-07 0.046711 0.00013879 1.3407e-07 v total_pressure 82081 1.2647e+05 1.0028e+05 1.0135e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0667 0.11616 0.0033789 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.2425e-07 0.046711 0.00013879 1.3407e-07 INSTANT 0.874802000E-01 TIME STEP NUMBER 55000 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.377158400E+02 Smooth wall 5 12240 0.287417690E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.377158407E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.108570885E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.70257E-02 0.21224E+01 Friction velocity uk : 0.70257E-02 0.21224E+01 Dimensionless distance yplus : 0.67628E-02 0.20840E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.287492372e+01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29435E+08 1 0.74563E-09 0.26511E+03 0.64304E+04 c Velocity[X] 0.13259E+03 c Velocity[Y] 0.13252E+03 c Velocity[Z] 0.55482E-03 c Pressure 0.37464E-02 420 0.82055E-04 0.98172E+00 0.99917E+07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -6.0842 13.083 5.6084 8.0003 v Velocity[Y] -10.367 11.98 -0.14284 -0.00067429 v Velocity[Z] -3.1356 2.9697 3.6269e-06 -5.3857e-08 v ǁVelocityǁ 0.0035451 14.456 6.3227 8.0017 v Pressure -16369 61259 49620 26314 v TurbVisc 2.1663e-19 0.0049634 2.438e-05 9.986e-07 v CourantNb 6.4546e-08 0.015678 0.00022165 6.5065e-06 v FourierNb 1.2425e-07 0.046816 0.00014699 1.3465e-07 v total_pressure 84956 1.6258e+05 1.5095e+05 1.2764e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.084 0.11705 0.0034617 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.5444e-07 0.053727 0.00036865 6.6411e-06 INSTANT 0.874803000E-01 TIME STEP NUMBER 55001 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.314298667E+02 Smooth wall 5 12240 0.239514742E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.314304170E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.256904569E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13505E-01 0.21251E+01 Friction velocity uk : 0.13505E-01 0.21251E+01 Dimensionless distance yplus : 0.12999E-01 0.20866E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -6.637965789e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29436E+08 1 0.58306E-09 0.21640E+03 0.58096E+04 c Velocity[X] 0.10821E+03 c Velocity[Y] 0.10819E+03 c Velocity[Z] 0.87632E-03 c Pressure 0.27532E-02 65 0.86645E-04 0.44409E+00 0.16352E+07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -6.0814 13.084 5.6084 8.0004 v Velocity[Y] -10.369 11.989 -0.14284 -0.00067423 v Velocity[Z] -3.1354 2.9699 3.6255e-06 -5.3857e-08 v ǁVelocityǁ 0.0031703 14.458 6.3228 8.0018 v Pressure -34673 94932 62972 31417 v TurbVisc 3.6219e-19 0.0049634 2.6389e-05 1.0811e-06 v CourantNb 2.8769e-08 0.013067 0.00018471 5.4221e-06 v FourierNb 1.2425e-07 0.046811 0.00014604 1.3528e-07 v total_pressure 66652 1.9626e+05 1.643e+05 1.3274e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0866 0.11693 0.0034584 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.6608e-07 0.052573 0.00033075 5.5574e-06 INSTANT 0.874804000E-01 TIME STEP NUMBER 55002 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.293345422E+02 Smooth wall 5 12240 0.223547092E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.293356603E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.294687913E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.80774E-02 0.21280E+01 Friction velocity uk : 0.80774E-02 0.21280E+01 Dimensionless distance yplus : 0.78244E-02 0.20895E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.681201967e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29436E+08 1 0.52461E-09 0.19230E+03 0.54764E+04 c Velocity[X] 0.96124E+02 c Velocity[Y] 0.96170E+02 c Velocity[Z] 0.72820E-03 c Pressure 0.22490E-02 109 0.51146E-04 0.28230E+00 0.88006E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -6.0783 13.084 5.6084 8.0005 v Velocity[Y] -10.37 11.998 -0.14284 -0.00067415 v Velocity[Z] -3.1352 2.97 3.6243e-06 -5.3857e-08 v ǁVelocityǁ 0.0030263 14.46 6.3229 8.0019 v Pressure -48759 1.1393e+05 69438 34421 v TurbVisc 2.8754e-18 0.0049635 2.8017e-05 1.1488e-06 v CourantNb 9.4748e-08 0.012197 0.00017239 5.0607e-06 v FourierNb 1.2425e-07 0.046818 0.00014562 1.358e-07 v total_pressure 52566 2.1526e+05 1.7076e+05 1.3575e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0895 0.11678 0.0034549 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.3664e-07 0.052204 0.00031801 5.1965e-06 INSTANT 0.874805000E-01 TIME STEP NUMBER 55003 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.286361007E+02 Smooth wall 5 12240 0.218224543E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.286377928E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.322825423E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.87446E-02 0.21311E+01 Friction velocity uk : 0.87446E-02 0.21311E+01 Dimensionless distance yplus : 0.84174E-02 0.20925E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.636280051e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29437E+08 1 0.49899E-09 0.17188E+03 0.51774E+04 c Velocity[X] 0.85918E+02 c Velocity[Y] 0.85958E+02 c Velocity[Z] 0.53065E-03 c Pressure 0.17697E-02 42 0.85309E-04 0.18829E+00 0.76158E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -6.0764 13.084 5.6084 8.0006 v Velocity[Y] -10.371 12.004 -0.14284 -0.00067402 v Velocity[Z] -3.1349 2.9701 3.6231e-06 -5.3857e-08 v ǁVelocityǁ 0.0023901 14.462 6.323 8.0021 v Pressure -54009 1.2393e+05 72657 37262 v TurbVisc 7.0563e-19 0.0049635 2.9457e-05 1.209e-06 v CourantNb 9.3884e-08 0.011907 0.00016828 4.9403e-06 v FourierNb 1.2425e-07 0.046834 0.0001454 1.3626e-07 v total_pressure 47316 2.2525e+05 1.7398e+05 1.3859e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0925 0.11667 0.0034517 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2683e-07 0.052098 0.00031368 5.0765e-06 INSTANT 0.874806000E-01 TIME STEP NUMBER 55004 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.284032869E+02 Smooth wall 5 12240 0.216450359E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.284055906E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.344455765E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.46836E-02 0.21329E+01 Friction velocity uk : 0.46836E-02 0.21329E+01 Dimensionless distance yplus : 0.45083E-02 0.20944E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -7.065533819e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29437E+08 1 0.47951E-09 0.15242E+03 0.48755E+04 c Velocity[X] 0.76228E+02 c Velocity[Y] 0.76192E+02 c Velocity[Z] 0.36974E-03 c Pressure 0.14426E-02 41 0.79282E-04 0.13575E+00 0.71589E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -6.0766 13.084 5.6084 8.0007 v Velocity[Y] -10.371 12.005 -0.14284 -0.00067393 v Velocity[Z] -3.1346 2.9703 3.622e-06 -5.3857e-08 v ǁVelocityǁ 0.0023936 14.462 6.3232 8.0022 v Pressure -50427 1.2956e+05 74097 40120 v TurbVisc 2.7507e-19 0.0049635 3.0752e-05 1.2632e-06 v CourantNb 9.4035e-08 0.01181 0.00016691 4.9001e-06 v FourierNb 1.2425e-07 0.046846 0.00014527 1.3668e-07 v total_pressure 50898 2.3089e+05 1.7542e+05 1.4145e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0944 0.11658 0.003449 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2356e-07 0.05207 0.00031217 5.0368e-06 INSTANT 0.874807000E-01 TIME STEP NUMBER 55005 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.283256823E+02 Smooth wall 5 12240 0.215858965E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283286388E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.363867746E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15379E-01 0.21329E+01 Friction velocity uk : 0.15379E-01 0.21329E+01 Dimensionless distance yplus : 0.14804E-01 0.20944E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 6.213246044e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29438E+08 1 0.45967E-09 0.13701E+03 0.46223E+04 c Velocity[X] 0.68564E+02 c Velocity[Y] 0.68441E+02 c Velocity[Z] 0.27309E-03 c Pressure 0.13247E-02 41 0.76552E-04 0.11326E+00 0.58204E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -6.0787 13.084 5.6084 8.0008 v Velocity[Y] -10.37 12.001 -0.14284 -0.0006738 v Velocity[Z] -3.1344 2.9704 3.6208e-06 -5.3857e-08 v ǁVelocityǁ 0.003172 14.46 6.3235 8.0023 v Pressure -42337 1.3467e+05 74876 42579 v TurbVisc 6.9155e-19 0.0049635 3.1949e-05 1.3135e-06 v CourantNb 9.3772e-08 0.011778 0.00016645 4.8868e-06 v FourierNb 1.2425e-07 0.046847 0.00014518 1.3707e-07 v total_pressure 58988 2.3599e+05 1.762e+05 1.439e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0944 0.11653 0.0034469 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2248e-07 0.052056 0.00031164 5.0239e-06 INSTANT 0.874808000E-01 TIME STEP NUMBER 55006 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282998141E+02 Smooth wall 5 12240 0.215661833E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283034555E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.381084702E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.20780E-01 0.21312E+01 Friction velocity uk : 0.20780E-01 0.21312E+01 Dimensionless distance yplus : 0.20003E-01 0.20926E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.870932864e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29438E+08 1 0.44179E-09 0.12622E+03 0.44366E+04 c Velocity[X] 0.63203E+02 c Velocity[Y] 0.63021E+02 c Velocity[Z] 0.22639E-03 c Pressure 0.12318E-02 45 0.41725E-04 0.97513E-01 0.36482E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -6.0819 13.084 5.6084 8.001 v Velocity[Y] -10.37 11.994 -0.14284 -0.00067373 v Velocity[Z] -3.1341 2.9705 3.6197e-06 -5.3857e-08 v ǁVelocityǁ 0.0026571 14.458 6.3238 8.0025 v Pressure -34881 1.45e+05 75650 44178 v TurbVisc 1.3183e-18 0.0049635 3.3078e-05 1.3611e-06 v CourantNb 9.2801e-08 0.011768 0.00016631 4.8824e-06 v FourierNb 1.2425e-07 0.046836 0.00014513 1.3743e-07 v total_pressure 66444 2.4633e+05 1.7697e+05 1.455e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0926 0.11651 0.0034455 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2213e-07 0.052037 0.00031143 5.0198e-06 INSTANT 0.874809000E-01 TIME STEP NUMBER 55007 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282911914E+02 Smooth wall 5 12240 0.215596123E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282955378E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.395510188E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12138E-01 0.21284E+01 Friction velocity uk : 0.12138E-01 0.21284E+01 Dimensionless distance yplus : 0.11684E-01 0.20899E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 2.686695212e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29439E+08 1 0.42798E-09 0.11823E+03 0.42938E+04 c Velocity[X] 0.59223E+02 c Velocity[Y] 0.59007E+02 c Velocity[Z] 0.19066E-03 c Pressure 0.10690E-02 31 0.58603E-04 0.79403E-01 0.15582E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -6.0854 13.083 5.6084 8.0011 v Velocity[Y] -10.369 11.986 -0.14283 -0.00067363 v Velocity[Z] -3.1338 2.9705 3.6185e-06 -5.3857e-08 v ǁVelocityǁ 0.0031068 14.456 6.3242 8.0026 v Pressure -31480 1.5036e+05 76715 44871 v TurbVisc 2.4976e-19 0.0049636 3.4141e-05 1.4062e-06 v CourantNb 9.75e-08 0.011764 0.00016626 4.881e-06 v FourierNb 1.2425e-07 0.046819 0.00014509 1.3778e-07 v total_pressure 69845 2.5168e+05 1.7804e+05 1.462e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0899 0.11651 0.0034445 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2202e-07 0.052012 0.00031135 5.0187e-06 INSTANT 0.874810000E-01 TIME STEP NUMBER 55008 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282883171E+02 Smooth wall 5 12240 0.215574219E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282933757E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.406999102E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.88544E-02 0.21254E+01 Friction velocity uk : 0.88544E-02 0.21254E+01 Dimensionless distance yplus : 0.88534E-02 0.20870E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 2.988772589e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29440E+08 1 0.41754E-09 0.11189E+03 0.41770E+04 c Velocity[X] 0.56066E+02 c Velocity[Y] 0.55828E+02 c Velocity[Z] 0.16581E-03 c Pressure 0.92015E-03 21 0.49441E-04 0.64719E-01 0.44766E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -6.0884 13.083 5.6084 8.0013 v Velocity[Y] -10.368 11.979 -0.14283 -0.00067352 v Velocity[Z] -3.1336 2.9706 3.6174e-06 -5.3857e-08 v ǁVelocityǁ 0.0036157 14.454 6.3245 8.0028 v Pressure -32988 1.5313e+05 78031 44971 v TurbVisc 1.74e-18 0.0049636 3.5145e-05 1.4493e-06 v CourantNb 4.0567e-08 0.011763 0.00016625 4.8805e-06 v FourierNb 1.2425e-07 0.046801 0.00014507 1.3811e-07 v total_pressure 68337 2.5445e+05 1.7936e+05 1.463e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.087 0.1165 0.0034436 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2199e-07 0.051988 0.00031132 5.0186e-06 INSTANT 0.874811000E-01 TIME STEP NUMBER 55009 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282873590E+02 Smooth wall 5 12240 0.215566918E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282931195E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.416045212E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.77825E-02 0.21228E+01 Friction velocity uk : 0.77825E-02 0.21228E+01 Dimensionless distance yplus : 0.75388E-02 0.20845E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 2.955984386e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29440E+08 1 0.40924E-09 0.10724E+03 0.40891E+04 c Velocity[X] 0.53741E+02 c Velocity[Y] 0.53493E+02 c Velocity[Z] 0.15965E-03 c Pressure 0.86807E-03 24 0.50738E-04 0.58193E-01 0.67721E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -6.0907 13.083 5.6084 8.0014 v Velocity[Y] -10.368 11.974 -0.14283 -0.0006734 v Velocity[Z] -3.1333 2.9707 3.6162e-06 -5.3857e-08 v ǁVelocityǁ 0.0034211 14.452 6.3248 8.0029 v Pressure -38192 1.5712e+05 79340 44742 v TurbVisc 1.2768e-18 0.0049636 3.6101e-05 1.4909e-06 v CourantNb 2.8941e-08 0.011763 0.00016625 4.8804e-06 v FourierNb 1.2425e-07 0.046785 0.00014505 1.3843e-07 v total_pressure 63133 2.5844e+05 1.8067e+05 1.4607e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0845 0.11654 0.003443 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2199e-07 0.051969 0.0003113 5.0188e-06 INSTANT 0.874812000E-01 TIME STEP NUMBER 55010 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282870397E+02 Smooth wall 5 12240 0.215564484E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282934966E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.423547171E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.74950E-02 0.21209E+01 Friction velocity uk : 0.74950E-02 0.21209E+01 Dimensionless distance yplus : 0.72145E-02 0.20825E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 2.791010073e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29441E+08 1 0.40274E-09 0.10393E+03 0.40256E+04 c Velocity[X] 0.52091E+02 c Velocity[Y] 0.51842E+02 c Velocity[Z] 0.15658E-03 c Pressure 0.85704E-03 20 0.39276E-04 0.55040E-01 0.52308E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -6.0927 13.083 5.6084 8.0015 v Velocity[Y] -10.367 11.97 -0.14284 -0.00067326 v Velocity[Z] -3.133 2.9708 3.6151e-06 -5.3857e-08 v ǁVelocityǁ 0.0031739 14.451 6.3252 8.0031 v Pressure -44354 1.6113e+05 80365 44575 v TurbVisc 9.9467e-20 0.0049636 3.7014e-05 1.531e-06 v CourantNb 2.9349e-08 0.011763 0.00016625 4.8804e-06 v FourierNb 1.2425e-07 0.046774 0.00014504 1.3874e-07 v total_pressure 56971 2.6246e+05 1.8169e+05 1.459e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0825 0.11658 0.0034424 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.22e-07 0.051954 0.00031129 5.0192e-06 INSTANT 0.874813000E-01 TIME STEP NUMBER 55011 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282869332E+02 Smooth wall 5 12240 0.215563673E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282940865E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.430379446E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15701E-01 0.21192E+01 Friction velocity uk : 0.15701E-01 0.21192E+01 Dimensionless distance yplus : 0.15114E-01 0.20809E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 2.730646612e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29442E+08 1 0.39761E-09 0.10099E+03 0.39680E+04 c Velocity[X] 0.50620E+02 c Velocity[Y] 0.50369E+02 c Velocity[Z] 0.14283E-03 c Pressure 0.81270E-03 35 0.28187E-04 0.50207E-01 0.33062E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -6.0947 13.082 5.6084 8.0017 v Velocity[Y] -10.367 11.966 -0.14284 -0.00067311 v Velocity[Z] -3.1327 2.9709 3.6139e-06 -5.3857e-08 v ǁVelocityǁ 0.0029064 14.449 6.3255 8.0032 v Pressure -49014 1.6325e+05 80953 44693 v TurbVisc 1.8869e-18 0.0049637 3.7889e-05 1.5698e-06 v CourantNb 3.0692e-08 0.011763 0.00016625 4.8804e-06 v FourierNb 1.2425e-07 0.046764 0.00014503 1.3904e-07 v total_pressure 52311 2.6457e+05 1.8228e+05 1.4602e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0809 0.1166 0.0034418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2201e-07 0.051943 0.00031128 5.0195e-06 INSTANT 0.874814000E-01 TIME STEP NUMBER 55012 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868977E+02 Smooth wall 5 12240 0.215563403E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282947526E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.437102284E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.16722E-01 0.21176E+01 Friction velocity uk : 0.16722E-01 0.21176E+01 Dimensionless distance yplus : 0.16199E-01 0.20793E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 2.874451446e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29442E+08 1 0.39280E-09 0.97689E+02 0.39026E+04 c Velocity[X] 0.48977E+02 c Velocity[Y] 0.48713E+02 c Velocity[Z] 0.12377E-03 c Pressure 0.74331E-03 22 0.34492E-04 0.44327E-01 0.94474E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -6.097 13.082 5.6084 8.0018 v Velocity[Y] -10.366 11.961 -0.14284 -0.00067297 v Velocity[Z] -3.1324 2.971 3.6128e-06 -5.3857e-08 v ǁVelocityǁ 0.0026546 14.447 6.3259 8.0034 v Pressure -50951 1.6393e+05 81143 45112 v TurbVisc 1.9353e-18 0.0049637 3.8731e-05 1.6072e-06 v CourantNb 3.144e-08 0.011763 0.00016625 4.8805e-06 v FourierNb 1.2425e-07 0.046755 0.00014503 1.3933e-07 v total_pressure 50374 2.6525e+05 1.8247e+05 1.4644e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0793 0.11663 0.0034413 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2202e-07 0.051932 0.00031128 5.0198e-06 INSTANT 0.874815000E-01 TIME STEP NUMBER 55013 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868859E+02 Smooth wall 5 12240 0.215563313E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282954508E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.443852236E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.14242E-01 0.21157E+01 Friction velocity uk : 0.14242E-01 0.21157E+01 Dimensionless distance yplus : 0.13772E-01 0.20774E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 3.185340880e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29443E+08 1 0.38743E-09 0.94128E+02 0.38307E+04 c Velocity[X] 0.47207E+02 c Velocity[Y] 0.46921E+02 c Velocity[Z] 0.10899E-03 c Pressure 0.69268E-03 20 0.41768E-04 0.39996E-01 0.12137E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -6.0999 13.082 5.6085 8.002 v Velocity[Y] -10.366 11.954 -0.14285 -0.00067283 v Velocity[Z] -3.1321 2.971 3.6116e-06 -5.3857e-08 v ǁVelocityǁ 0.0024556 14.445 6.3263 8.0035 v Pressure -50372 1.653e+05 81056 45652 v TurbVisc 2.2798e-18 0.0049637 3.9542e-05 1.6432e-06 v CourantNb 7.0528e-08 0.011763 0.00016626 4.8805e-06 v FourierNb 1.2425e-07 0.046744 0.00014502 1.396e-07 v total_pressure 50953 2.6663e+05 1.8238e+05 1.4698e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0774 0.11666 0.003441 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2203e-07 0.051917 0.00031128 5.0202e-06 INSTANT 0.874816000E-01 TIME STEP NUMBER 55014 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868820E+02 Smooth wall 5 12240 0.215563283E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282961648E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.450436948E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.21075E-01 0.21133E+01 Friction velocity uk : 0.21075E-01 0.21133E+01 Dimensionless distance yplus : 0.20286E-01 0.20751E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 3.535643760e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29443E+08 1 0.38150E-09 0.90744E+02 0.37612E+04 c Velocity[X] 0.45526E+02 c Velocity[Y] 0.45218E+02 c Velocity[Z] 0.99329E-04 c Pressure 0.66813E-03 20 0.39255E-04 0.37453E-01 0.10383E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -6.1032 13.082 5.6085 8.0021 v Velocity[Y] -10.365 11.947 -0.14285 -0.00067271 v Velocity[Z] -3.1318 2.9711 3.6104e-06 -5.3857e-08 v ǁVelocityǁ 0.0023013 14.443 6.3267 8.0037 v Pressure -48405 1.6793e+05 80892 46114 v TurbVisc 2.4404e-18 0.0049637 4.0323e-05 1.678e-06 v CourantNb 9.7745e-08 0.011763 0.00016626 4.8806e-06 v FourierNb 1.2425e-07 0.046729 0.00014502 1.3987e-07 v total_pressure 52920 2.6925e+05 1.8222e+05 1.4744e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0751 0.1167 0.0034408 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2204e-07 0.051898 0.00031129 5.0205e-06 INSTANT 0.874817000E-01 TIME STEP NUMBER 55015 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868807E+02 Smooth wall 5 12240 0.215563273E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282968868E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.456543562E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.18638E-01 0.21105E+01 Friction velocity uk : 0.18638E-01 0.21105E+01 Dimensionless distance yplus : 0.18189E-01 0.20723E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 3.780325634e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29444E+08 1 0.37562E-09 0.87774E+02 0.36990E+04 c Velocity[X] 0.44050E+02 c Velocity[Y] 0.43724E+02 c Velocity[Z] 0.91800E-04 c Pressure 0.64442E-03 27 0.33175E-04 0.35155E-01 0.54006E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -6.1066 13.081 5.6085 8.0023 v Velocity[Y] -10.364 11.939 -0.14286 -0.0006726 v Velocity[Z] -3.1316 2.9712 3.6093e-06 -5.3857e-08 v ǁVelocityǁ 0.002186 14.44 6.3272 8.0039 v Pressure -46428 1.6952e+05 80778 46343 v TurbVisc 1.7063e-18 0.0049637 4.1076e-05 1.7117e-06 v CourantNb 8.9959e-08 0.011763 0.00016627 4.8807e-06 v FourierNb 1.2425e-07 0.046711 0.00014503 1.4013e-07 v total_pressure 54897 2.7084e+05 1.821e+05 1.4767e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0723 0.11675 0.0034406 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2205e-07 0.051875 0.0003113 5.0208e-06 INSTANT 0.874818000E-01 TIME STEP NUMBER 55016 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868802E+02 Smooth wall 5 12240 0.215563269E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282976107E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.461937806E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.23166E-01 0.21076E+01 Friction velocity uk : 0.23166E-01 0.21076E+01 Dimensionless distance yplus : 0.22440E-01 0.20695E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 3.844445426e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29445E+08 1 0.37027E-09 0.85222E+02 0.36448E+04 c Velocity[X] 0.42780E+02 c Velocity[Y] 0.42442E+02 c Velocity[Z] 0.86028E-04 c Pressure 0.61220E-03 16 0.31720E-04 0.32568E-01 0.16642E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -6.1099 13.081 5.6086 8.0024 v Velocity[Y] -10.363 11.932 -0.14286 -0.00067249 v Velocity[Z] -3.1313 2.9713 3.6081e-06 -5.3857e-08 v ǁVelocityǁ 0.0020916 14.438 6.3276 8.004 v Pressure -45421 1.7016e+05 80783 46323 v TurbVisc 6.421e-19 0.0049638 4.1805e-05 1.7445e-06 v CourantNb 9.889e-08 0.011763 0.00016628 4.8807e-06 v FourierNb 1.2425e-07 0.046692 0.00014503 1.4038e-07 v total_pressure 55904 2.7149e+05 1.8211e+05 1.4765e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0695 0.11678 0.0034403 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2206e-07 0.051852 0.0003113 5.0211e-06 INSTANT 0.874819000E-01 TIME STEP NUMBER 55017 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868801E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282983326E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.466572680E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.93000E-02 0.21049E+01 Friction velocity uk : 0.93000E-02 0.21049E+01 Dimensionless distance yplus : 0.90758E-02 0.20668E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 3.712612360e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29445E+08 1 0.36560E-09 0.83046E+02 0.35979E+04 c Velocity[X] 0.41695E+02 c Velocity[Y] 0.41351E+02 c Velocity[Z] 0.82733E-04 c Pressure 0.58398E-03 17 0.36587E-04 0.30347E-01 0.56051E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -6.1128 13.081 5.6086 8.0025 v Velocity[Y] -10.363 11.925 -0.14286 -0.00067239 v Velocity[Z] -3.131 2.9713 3.607e-06 -5.3857e-08 v ǁVelocityǁ 0.0019983 14.436 6.328 8.0042 v Pressure -45592 1.702e+05 80845 46073 v TurbVisc 2.3179e-18 0.0049638 4.2512e-05 1.7765e-06 v CourantNb 2.5414e-08 0.011763 0.00016628 4.8808e-06 v FourierNb 1.2425e-07 0.046674 0.00014503 1.4063e-07 v total_pressure 55733 2.7152e+05 1.8217e+05 1.474e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0668 0.11681 0.0034398 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2208e-07 0.051829 0.00031131 5.0214e-06 INSTANT 0.874820000E-01 TIME STEP NUMBER 55018 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282990487E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.470585951E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.82926E-02 0.21025E+01 Friction velocity uk : 0.82926E-02 0.21025E+01 Dimensionless distance yplus : 0.80845E-02 0.20644E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 3.435912021e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29446E+08 1 0.36155E-09 0.81204E+02 0.35577E+04 c Velocity[X] 0.40775E+02 c Velocity[Y] 0.40428E+02 c Velocity[Z] 0.80639E-04 c Pressure 0.56751E-03 19 0.38514E-04 0.28849E-01 0.75544E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -6.1153 13.081 5.6087 8.0027 v Velocity[Y] -10.362 11.919 -0.14286 -0.0006723 v Velocity[Z] -3.1307 2.9714 3.6058e-06 -5.3857e-08 v ǁVelocityǁ 0.0019077 14.434 6.3285 8.0043 v Pressure -46561 1.7005e+05 80893 45737 v TurbVisc 1.9453e-18 0.0049638 4.3201e-05 1.8081e-06 v CourantNb 6.8087e-08 0.011763 0.00016628 4.8808e-06 v FourierNb 1.2425e-07 0.046658 0.00014503 1.4087e-07 v total_pressure 54764 2.7138e+05 1.8222e+05 1.4706e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0644 0.11681 0.0034391 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2209e-07 0.05181 0.00031132 5.0217e-06 INSTANT 0.874821000E-01 TIME STEP NUMBER 55019 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282997601E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.474216820E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.22179E-01 0.21005E+01 Friction velocity uk : 0.22179E-01 0.21005E+01 Dimensionless distance yplus : 0.21392E-01 0.20625E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 3.091835612e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29447E+08 1 0.35799E-09 0.79591E+02 0.35221E+04 c Velocity[X] 0.39969E+02 c Velocity[Y] 0.39622E+02 c Velocity[Z] 0.77552E-04 c Pressure 0.55527E-03 19 0.35473E-04 0.27646E-01 0.72014E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -6.1174 13.08 5.6088 8.0028 v Velocity[Y] -10.361 11.915 -0.14286 -0.0006722 v Velocity[Z] -3.1304 2.9715 3.6047e-06 -5.3857e-08 v ǁVelocityǁ 0.0018199 14.432 6.3289 8.0045 v Pressure -47660 1.6995e+05 80843 45418 v TurbVisc 1.4877e-18 0.0049638 4.3872e-05 1.839e-06 v CourantNb 7.745e-08 0.011763 0.00016629 4.8809e-06 v FourierNb 1.2425e-07 0.046645 0.00014503 1.411e-07 v total_pressure 53665 2.7127e+05 1.8217e+05 1.4674e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0625 0.1168 0.003438 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.221e-07 0.051794 0.00031132 5.022e-06 INSTANT 0.874822000E-01 TIME STEP NUMBER 55020 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283004669E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.477696394E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15880E-01 0.20989E+01 Friction velocity uk : 0.15880E-01 0.20989E+01 Dimensionless distance yplus : 0.15317E-01 0.20609E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 2.739475460e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29447E+08 1 0.35475E-09 0.78065E+02 0.34881E+04 c Velocity[X] 0.39205E+02 c Velocity[Y] 0.38860E+02 c Velocity[Z] 0.72899E-04 c Pressure 0.53921E-03 17 0.29956E-04 0.26321E-01 0.57260E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -6.1191 13.08 5.6088 8.003 v Velocity[Y] -10.361 11.912 -0.14286 -0.00067211 v Velocity[Z] -3.1301 2.9715 3.6035e-06 -5.3857e-08 v ǁVelocityǁ 0.0017415 14.431 6.3294 8.0046 v Pressure -48814 1.6984e+05 80652 45170 v TurbVisc 1.4754e-18 0.0049638 4.4527e-05 1.8695e-06 v CourantNb 9.0301e-08 0.011762 0.00016629 4.881e-06 v FourierNb 1.2425e-07 0.046635 0.00014504 1.4134e-07 v total_pressure 52511 2.7117e+05 1.8198e+05 1.4649e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0609 0.11676 0.0034366 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2211e-07 0.051782 0.00031133 5.0223e-06 INSTANT 0.874823000E-01 TIME STEP NUMBER 55021 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283011700E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.481166978E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15184E-01 0.20976E+01 Friction velocity uk : 0.15184E-01 0.20976E+01 Dimensionless distance yplus : 0.14789E-01 0.20597E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 2.408726948e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29448E+08 1 0.35162E-09 0.76536E+02 0.34537E+04 c Velocity[X] 0.38440E+02 c Velocity[Y] 0.38097E+02 c Velocity[Z] 0.67770E-04 c Pressure 0.52065E-03 17 0.23599E-04 0.24943E-01 0.44380E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -6.1205 13.08 5.6089 8.0031 v Velocity[Y] -10.361 11.909 -0.14285 -0.00067203 v Velocity[Z] -3.1298 2.9716 3.6024e-06 -5.3857e-08 v ǁVelocityǁ 0.0016851 14.43 6.3298 8.0048 v Pressure -49078 1.7054e+05 80326 44986 v TurbVisc 1.7336e-18 0.0049639 4.5169e-05 1.8994e-06 v CourantNb 9.6343e-08 0.011762 0.00016629 4.881e-06 v FourierNb 1.2425e-07 0.046628 0.00014504 1.4156e-07 v total_pressure 52247 2.7186e+05 1.8165e+05 1.4631e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0597 0.11672 0.0034349 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2212e-07 0.051773 0.00031133 5.0226e-06 INSTANT 0.874824000E-01 TIME STEP NUMBER 55022 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283018703E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.484657812E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.14672E-01 0.20967E+01 Friction velocity uk : 0.14672E-01 0.20967E+01 Dimensionless distance yplus : 0.14334E-01 0.20587E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 2.098148811e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29449E+08 1 0.34844E-09 0.75023E+02 0.34193E+04 c Velocity[X] 0.37682E+02 c Velocity[Y] 0.37341E+02 c Velocity[Z] 0.63299E-04 c Pressure 0.50443E-03 10 0.95502E-04 0.23738E-01 0.38488E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -6.1215 13.08 5.609 8.0033 v Velocity[Y] -10.361 11.907 -0.14285 -0.00067195 v Velocity[Z] -3.1295 2.9717 3.6012e-06 -5.3857e-08 v ǁVelocityǁ 0.0016264 14.429 6.3303 8.005 v Pressure -48478 1.734e+05 79745 44837 v TurbVisc 1.6898e-18 0.0049639 4.5796e-05 1.9288e-06 v CourantNb 9.0883e-08 0.011762 0.00016629 4.8811e-06 v FourierNb 1.2425e-07 0.046623 0.00014504 1.4179e-07 v total_pressure 52847 2.7473e+05 1.8107e+05 1.4616e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0587 0.11666 0.0034329 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2213e-07 0.051767 0.00031134 5.0229e-06 INSTANT 0.874825000E-01 TIME STEP NUMBER 55023 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283025676E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.488111083E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13003E-01 0.20961E+01 Friction velocity uk : 0.13003E-01 0.20961E+01 Dimensionless distance yplus : 0.12677E-01 0.20582E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.750799789e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29449E+08 1 0.34523E-09 0.73549E+02 0.33855E+04 c Velocity[X] 0.36943E+02 c Velocity[Y] 0.36606E+02 c Velocity[Z] 0.59818E-04 c Pressure 0.49187E-03 10 0.92678E-04 0.22757E-01 0.51391E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -6.1222 13.08 5.6091 8.0034 v Velocity[Y] -10.361 11.906 -0.14284 -0.00067188 v Velocity[Z] -3.1292 2.9717 3.6e-06 -5.3857e-08 v ǁVelocityǁ 0.0015919 14.429 6.3307 8.0051 v Pressure -47377 1.7609e+05 79428 44618 v TurbVisc 5.9995e-19 0.0049639 4.6412e-05 1.9576e-06 v CourantNb 9.6809e-08 0.011762 0.0001663 4.8811e-06 v FourierNb 1.2425e-07 0.04662 0.00014504 1.4201e-07 v total_pressure 53948 2.7741e+05 1.8075e+05 1.4594e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0582 0.11658 0.0034306 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2214e-07 0.051764 0.00031134 5.0231e-06 INSTANT 0.874826000E-01 TIME STEP NUMBER 55024 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283032589E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.491463747E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.89970E-02 0.20957E+01 Friction velocity uk : 0.89970E-02 0.20957E+01 Dimensionless distance yplus : 0.86769E-02 0.20578E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.428928667e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29450E+08 1 0.34209E-09 0.72176E+02 0.33537E+04 c Velocity[X] 0.36254E+02 c Velocity[Y] 0.35923E+02 c Velocity[Z] 0.57178E-04 c Pressure 0.48002E-03 11 0.99502E-04 0.21851E-01 0.67927E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -6.1225 13.081 5.6092 8.0035 v Velocity[Y] -10.361 11.906 -0.14283 -0.00067184 v Velocity[Z] -3.1289 2.9718 3.5989e-06 -5.3857e-08 v ǁVelocityǁ 0.0015711 14.428 6.3312 8.0053 v Pressure -46211 1.7828e+05 78892 44324 v TurbVisc 9.027e-20 0.0049639 4.7015e-05 1.986e-06 v CourantNb 1.1103e-07 0.011762 0.0001663 4.8812e-06 v FourierNb 1.2425e-07 0.04662 0.00014504 1.4223e-07 v total_pressure 55114 2.7961e+05 1.8022e+05 1.4565e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0578 0.1165 0.003428 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2216e-07 0.051764 0.00031134 5.0234e-06 INSTANT 0.874827000E-01 TIME STEP NUMBER 55025 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283039463E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.494593469E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.18790E-01 0.20958E+01 Friction velocity uk : 0.18790E-01 0.20958E+01 Dimensionless distance yplus : 0.18074E-01 0.20579E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.011742634e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29450E+08 1 0.33911E-09 0.70916E+02 0.33242E+04 c Velocity[X] 0.35619E+02 c Velocity[Y] 0.35297E+02 c Velocity[Z] 0.55130E-04 c Pressure 0.46920E-03 24 0.35776E-04 0.21030E-01 0.98113E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -6.1223 13.081 5.6093 8.0037 v Velocity[Y] -10.361 11.907 -0.14282 -0.00067183 v Velocity[Z] -3.1286 2.9718 3.5977e-06 -5.3857e-08 v ǁVelocityǁ 0.0015294 14.428 6.3316 8.0054 v Pressure -45305 1.7992e+05 78605 43903 v TurbVisc 1.4878e-19 0.0049639 4.7608e-05 2.0139e-06 v CourantNb 1.0344e-07 0.011762 0.0001663 4.8813e-06 v FourierNb 1.2425e-07 0.046623 0.00014504 1.4244e-07 v total_pressure 56020 2.8125e+05 1.7993e+05 1.4523e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0579 0.1164 0.0034251 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2217e-07 0.051767 0.00031134 5.0237e-06 INSTANT 0.874828000E-01 TIME STEP NUMBER 55026 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283046296E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.497480772E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.51513E-02 0.20963E+01 Friction velocity uk : 0.51513E-02 0.20963E+01 Dimensionless distance yplus : 0.49549E-02 0.20584E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 6.520223989e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29451E+08 1 0.33635E-09 0.69779E+02 0.32974E+04 c Velocity[X] 0.35046E+02 c Velocity[Y] 0.34734E+02 c Velocity[Z] 0.53449E-04 c Pressure 0.45997E-03 22 0.25454E-04 0.20313E-01 0.10015E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -6.1215 13.081 5.6094 8.0038 v Velocity[Y] -10.361 11.91 -0.14281 -0.00067181 v Velocity[Z] -3.1283 2.9719 3.5966e-06 -5.3857e-08 v ǁVelocityǁ 0.0014786 14.429 6.332 8.0056 v Pressure -44787 1.8116e+05 77952 43466 v TurbVisc 1.782e-18 0.004964 4.8189e-05 2.0414e-06 v CourantNb 9.8697e-08 0.011761 0.0001663 4.8813e-06 v FourierNb 1.2425e-07 0.046629 0.00014504 1.4265e-07 v total_pressure 56538 2.8249e+05 1.7928e+05 1.4479e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0584 0.11628 0.0034219 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2218e-07 0.051774 0.00031134 5.024e-06 INSTANT 0.874829000E-01 TIME STEP NUMBER 55027 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283053028E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.500146338E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13847E-01 0.20973E+01 Friction velocity uk : 0.13847E-01 0.20973E+01 Dimensionless distance yplus : 0.13319E-01 0.20593E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.790071231e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29452E+08 1 0.33378E-09 0.68744E+02 0.32728E+04 c Velocity[X] 0.34522E+02 c Velocity[Y] 0.34222E+02 c Velocity[Z] 0.51813E-04 c Pressure 0.45276E-03 22 0.24696E-04 0.19711E-01 0.10933E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -6.1201 13.081 5.6095 8.0039 v Velocity[Y] -10.362 11.914 -0.14279 -0.00067179 v Velocity[Z] -3.128 2.972 3.5954e-06 -5.3857e-08 v ǁVelocityǁ 0.0013956 14.43 6.3325 8.0057 v Pressure -44639 1.8222e+05 77371 42995 v TurbVisc 1.5408e-18 0.004964 4.8761e-05 2.0686e-06 v CourantNb 1.2158e-07 0.011761 0.00016629 4.8814e-06 v FourierNb 1.2425e-07 0.046638 0.00014504 1.4286e-07 v total_pressure 56686 2.8355e+05 1.787e+05 1.4432e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0593 0.11617 0.0034189 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2219e-07 0.051786 0.00031134 5.0242e-06 INSTANT 0.874830000E-01 TIME STEP NUMBER 55028 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283059680E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.502689903E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15507E-01 0.20987E+01 Friction velocity uk : 0.15507E-01 0.20987E+01 Dimensionless distance yplus : 0.14928E-01 0.20608E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -2.378869698e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29452E+08 1 0.33139E-09 0.67781E+02 0.32497E+04 c Velocity[X] 0.34034E+02 c Velocity[Y] 0.33747E+02 c Velocity[Z] 0.49980E-04 c Pressure 0.44585E-03 22 0.25656E-04 0.19145E-01 0.11412E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -6.1183 13.082 5.6096 8.0041 v Velocity[Y] -10.363 11.919 -0.14278 -0.00067178 v Velocity[Z] -3.1278 2.972 3.5943e-06 -5.3857e-08 v ǁVelocityǁ 0.0012845 14.431 6.333 8.0059 v Pressure -44738 1.833e+05 76747 42509 v TurbVisc 1.5142e-18 0.004964 4.9324e-05 2.0954e-06 v CourantNb 1.0639e-07 0.011761 0.00016629 4.8815e-06 v FourierNb 1.2425e-07 0.046651 0.00014504 1.4306e-07 v total_pressure 56587 2.8463e+05 1.7807e+05 1.4383e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0608 0.11606 0.0034159 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.222e-07 0.051802 0.00031133 5.0245e-06 INSTANT 0.874831000E-01 TIME STEP NUMBER 55029 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283066252E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.505122814E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.14805E-01 0.21007E+01 Friction velocity uk : 0.14805E-01 0.21007E+01 Dimensionless distance yplus : 0.14252E-01 0.20627E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -5.992008391e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29453E+08 1 0.32912E-09 0.66866E+02 0.32276E+04 c Velocity[X] 0.33570E+02 c Velocity[Y] 0.33296E+02 c Velocity[Z] 0.47911E-04 c Pressure 0.43826E-03 11 0.97176E-04 0.18570E-01 0.10793E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -6.1162 13.082 5.6097 8.0042 v Velocity[Y] -10.363 11.925 -0.14277 -0.00067174 v Velocity[Z] -3.1275 2.9721 3.5931e-06 -5.3857e-08 v ǁVelocityǁ 0.0011702 14.432 6.3334 8.006 v Pressure -44932 1.8448e+05 75991 42049 v TurbVisc 1.5511e-18 0.004964 4.9878e-05 2.122e-06 v CourantNb 9.9691e-08 0.011761 0.00016629 4.8815e-06 v FourierNb 1.2425e-07 0.046668 0.00014504 1.4326e-07 v total_pressure 56393 2.858e+05 1.7732e+05 1.4337e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0627 0.11593 0.0034126 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2221e-07 0.051823 0.00031133 5.0248e-06 INSTANT 0.874832000E-01 TIME STEP NUMBER 55030 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283072729E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.507484994E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.20196E-01 0.21028E+01 Friction velocity uk : 0.20196E-01 0.21028E+01 Dimensionless distance yplus : 0.19442E-01 0.20648E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -9.283751597e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29453E+08 1 0.32692E-09 0.65973E+02 0.32059E+04 c Velocity[X] 0.33117E+02 c Velocity[Y] 0.32857E+02 c Velocity[Z] 0.45789E-04 c Pressure 0.43027E-03 11 0.98835E-04 0.17999E-01 0.10910E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -6.1136 13.082 5.6098 8.0043 v Velocity[Y] -10.364 11.932 -0.14276 -0.00067175 v Velocity[Z] -3.1272 2.9721 3.592e-06 -5.3857e-08 v ǁVelocityǁ 0.0010015 14.434 6.3339 8.0062 v Pressure -45276 1.8568e+05 75257 41596 v TurbVisc 1.6144e-18 0.004964 5.0424e-05 2.1483e-06 v CourantNb 1.0322e-07 0.011761 0.00016629 4.8816e-06 v FourierNb 1.2425e-07 0.046686 0.00014504 1.4346e-07 v total_pressure 56049 2.8701e+05 1.7658e+05 1.4292e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0648 0.11579 0.0034091 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2222e-07 0.051845 0.00031132 5.0251e-06 INSTANT 0.874833000E-01 TIME STEP NUMBER 55031 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283079103E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.509828704E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.98432E-02 0.21054E+01 Friction velocity uk : 0.98432E-02 0.21054E+01 Dimensionless distance yplus : 0.94931E-02 0.20673E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.188266655e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29454E+08 1 0.32476E-09 0.65105E+02 0.31847E+04 c Velocity[X] 0.32675E+02 c Velocity[Y] 0.32430E+02 c Velocity[Z] 0.43785E-04 c Pressure 0.42188E-03 25 0.36144E-04 0.17430E-01 0.14021E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -6.1106 13.083 5.61 8.0045 v Velocity[Y] -10.366 11.94 -0.14275 -0.00067181 v Velocity[Z] -3.1269 2.9722 3.5908e-06 -5.3857e-08 v ǁVelocityǁ 0.00078028 14.436 6.3344 8.0063 v Pressure -46038 1.8679e+05 74447 41035 v TurbVisc 1.6543e-18 0.0049641 5.0962e-05 2.1743e-06 v CourantNb 4.9042e-08 0.011761 0.00016629 4.8817e-06 v FourierNb 1.2425e-07 0.046706 0.00014503 1.4366e-07 v total_pressure 55287 2.8811e+05 1.7577e+05 1.4236e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0673 0.11565 0.0034056 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2223e-07 0.051871 0.00031132 5.0253e-06 INSTANT 0.874834000E-01 TIME STEP NUMBER 55032 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283085508E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.512041683E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.17235E-01 0.21083E+01 Friction velocity uk : 0.17235E-01 0.21083E+01 Dimensionless distance yplus : 0.16591E-01 0.20702E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.239433263e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29455E+08 1 0.32263E-09 0.64267E+02 0.31641E+04 c Velocity[X] 0.32250E+02 c Velocity[Y] 0.32018E+02 c Velocity[Z] 0.41964E-04 c Pressure 0.41454E-03 11 0.91034E-04 0.16923E-01 0.11889E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -6.1076 13.083 5.6101 8.0046 v Velocity[Y] -10.367 11.948 -0.14274 -0.00067181 v Velocity[Z] -3.1266 2.9723 3.5897e-06 -5.3857e-08 v ǁVelocityǁ 0.00059674 14.438 6.3348 8.0065 v Pressure -47034 1.8765e+05 73545 40543 v TurbVisc 1.4257e-18 0.0049641 5.1491e-05 2.1999e-06 v CourantNb 9.6972e-08 0.011761 0.00016628 4.8817e-06 v FourierNb 1.2425e-07 0.04673 0.00014503 1.4386e-07 v total_pressure 54291 2.8897e+05 1.7487e+05 1.4187e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0702 0.11551 0.0034022 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2224e-07 0.051899 0.00031132 5.0256e-06 INSTANT 0.874835000E-01 TIME STEP NUMBER 55033 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283091772E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.514233361E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.16033E-01 0.21112E+01 Friction velocity uk : 0.16033E-01 0.21112E+01 Dimensionless distance yplus : 0.15531E-01 0.20730E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.371563099e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29455E+08 1 0.32055E-09 0.63469E+02 0.31443E+04 c Velocity[X] 0.31844E+02 c Velocity[Y] 0.31625E+02 c Velocity[Z] 0.40409E-04 c Pressure 0.40796E-03 11 0.96024E-04 0.16463E-01 0.11307E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -6.1044 13.083 5.6103 8.0047 v Velocity[Y] -10.368 11.957 -0.14274 -0.00067183 v Velocity[Z] -3.1263 2.9723 3.5885e-06 -5.3857e-08 v ǁVelocityǁ 0.00039301 14.441 6.3353 8.0066 v Pressure -48477 1.8816e+05 72526 40091 v TurbVisc 2.3753e-18 0.0049641 5.2012e-05 2.2253e-06 v CourantNb 1.5155e-07 0.011761 0.00016628 4.8818e-06 v FourierNb 1.2425e-07 0.046752 0.00014503 1.4405e-07 v total_pressure 52848 2.8949e+05 1.7385e+05 1.4142e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.073 0.11535 0.0033987 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2225e-07 0.051927 0.00031131 5.0258e-06 INSTANT 0.874836000E-01 TIME STEP NUMBER 55034 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283097881E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.516395930E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15494E-01 0.21143E+01 Friction velocity uk : 0.15494E-01 0.21143E+01 Dimensionless distance yplus : 0.15121E-01 0.20760E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.538241961e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29456E+08 1 0.31853E-09 0.62715E+02 0.31255E+04 c Velocity[X] 0.31459E+02 c Velocity[Y] 0.31255E+02 c Velocity[Z] 0.39022E-04 c Pressure 0.40226E-03 28 0.57509E-04 0.16051E-01 0.17031E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -6.1009 13.084 5.6104 8.0048 v Velocity[Y] -10.369 11.966 -0.14274 -0.00067191 v Velocity[Z] -3.126 2.9724 3.5874e-06 -5.3857e-08 v ǁVelocityǁ 0.0003016 14.443 6.3359 8.0068 v Pressure -50281 1.8829e+05 71471 39429 v TurbVisc 2.2877e-18 0.0049641 5.2524e-05 2.2503e-06 v CourantNb 1.1834e-07 0.011761 0.00016628 4.8819e-06 v FourierNb 1.2425e-07 0.046776 0.00014503 1.4424e-07 v total_pressure 51044 2.8962e+05 1.728e+05 1.4075e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.076 0.11519 0.0033952 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2226e-07 0.051956 0.00031131 5.0261e-06 INSTANT 0.874837000E-01 TIME STEP NUMBER 55035 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283104017E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.518446917E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10351E-01 0.21175E+01 Friction velocity uk : 0.10351E-01 0.21175E+01 Dimensionless distance yplus : 0.10013E-01 0.20792E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.433696458e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29456E+08 1 0.31660E-09 0.61994E+02 0.31074E+04 c Velocity[X] 0.31092E+02 c Velocity[Y] 0.30901E+02 c Velocity[Z] 0.37756E-04 c Pressure 0.39856E-03 11 0.89437E-04 0.15731E-01 0.15439E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -6.0976 13.104 5.6105 8.005 v Velocity[Y] -10.37 11.975 -0.14274 -0.00067202 v Velocity[Z] -3.1257 2.9724 3.5862e-06 -5.3857e-08 v ǁVelocityǁ 0.00046779 14.446 6.3364 8.0069 v Pressure -52306 1.8806e+05 70495 38819 v TurbVisc 5.0436e-19 0.0049641 5.3029e-05 2.2751e-06 v CourantNb 5.5229e-08 0.011761 0.00016628 4.8819e-06 v FourierNb 1.2425e-07 0.0468 0.00014503 1.4443e-07 v total_pressure 49019 2.8939e+05 1.7182e+05 1.4014e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0792 0.11504 0.003392 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2227e-07 0.051986 0.0003113 5.0264e-06 INSTANT 0.874838000E-01 TIME STEP NUMBER 55036 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283110009E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.520544311E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15292E-01 0.21206E+01 Friction velocity uk : 0.15292E-01 0.21206E+01 Dimensionless distance yplus : 0.14721E-01 0.20822E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.309064933e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29457E+08 1 0.31475E-09 0.61312E+02 0.30903E+04 c Velocity[X] 0.30745E+02 c Velocity[Y] 0.30568E+02 c Velocity[Z] 0.36603E-04 c Pressure 0.39582E-03 22 0.83560E-04 0.15459E-01 0.16065E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -6.0944 13.167 5.6107 8.0051 v Velocity[Y] -10.372 11.983 -0.14275 -0.00067219 v Velocity[Z] -3.1254 2.9725 3.5851e-06 -5.3857e-08 v ǁVelocityǁ 0.0007747 14.448 6.3369 8.007 v Pressure -54919 1.875e+05 69259 38218 v TurbVisc 1.0945e-18 0.0049642 5.3526e-05 2.2995e-06 v CourantNb 8.6915e-09 0.011761 0.00016628 4.882e-06 v FourierNb 1.2425e-07 0.046824 0.00014503 1.4461e-07 v total_pressure 46406 2.8883e+05 1.7058e+05 1.3954e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0822 0.11487 0.0033888 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2228e-07 0.052015 0.0003113 5.0266e-06 INSTANT 0.874839000E-01 TIME STEP NUMBER 55037 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283115898E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.522618687E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.16153E-01 0.21236E+01 Friction velocity uk : 0.16153E-01 0.21236E+01 Dimensionless distance yplus : 0.15550E-01 0.20852E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.243010923e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29457E+08 1 0.31297E-09 0.60651E+02 0.30735E+04 c Velocity[X] 0.30407E+02 c Velocity[Y] 0.30243E+02 c Velocity[Z] 0.35472E-04 c Pressure 0.39476E-03 29 0.59801E-04 0.15261E-01 0.16214E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -6.0913 13.231 5.6108 8.0052 v Velocity[Y] -10.373 11.992 -0.14275 -0.00067227 v Velocity[Z] -3.1251 2.9725 3.5839e-06 -5.3857e-08 v ǁVelocityǁ 0.0011091 14.45 6.3375 8.0072 v Pressure -57798 1.8666e+05 68134 37603 v TurbVisc 1.4215e-18 0.0049642 5.4015e-05 2.3237e-06 v CourantNb 5.0224e-08 0.011761 0.00016628 4.8821e-06 v FourierNb 1.2425e-07 0.046846 0.00014502 1.448e-07 v total_pressure 43527 2.8798e+05 1.6946e+05 1.3893e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0852 0.11471 0.0033856 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2229e-07 0.052043 0.0003113 5.0269e-06 INSTANT 0.874840000E-01 TIME STEP NUMBER 55038 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283121679E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.524730725E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13445E-01 0.21265E+01 Friction velocity uk : 0.13445E-01 0.21265E+01 Dimensionless distance yplus : 0.12943E-01 0.20880E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -9.684673814e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29458E+08 1 0.31125E-09 0.60002E+02 0.30569E+04 c Velocity[X] 0.30077E+02 c Velocity[Y] 0.29925E+02 c Velocity[Z] 0.34409E-04 c Pressure 0.39439E-03 11 0.76173E-04 0.15095E-01 0.16347E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -6.0884 13.294 5.611 8.0053 v Velocity[Y] -10.374 11.999 -0.14276 -0.00067223 v Velocity[Z] -3.1248 2.9726 3.5828e-06 -5.3857e-08 v ǁVelocityǁ 0.0014575 14.452 6.338 8.0073 v Pressure -60880 1.8554e+05 67010 36986 v TurbVisc 2.0165e-18 0.0049642 5.4498e-05 2.3476e-06 v CourantNb 9.523e-08 0.011761 0.00016628 4.8821e-06 v FourierNb 1.2425e-07 0.046867 0.00014502 1.4498e-07 v total_pressure 40445 2.8686e+05 1.6833e+05 1.3831e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.088 0.11459 0.0033828 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.223e-07 0.052069 0.0003113 5.0271e-06 INSTANT 0.874841000E-01 TIME STEP NUMBER 55039 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283127313E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.526873016E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.91006E-02 0.21291E+01 Friction velocity uk : 0.91006E-02 0.21291E+01 Dimensionless distance yplus : 0.87609E-02 0.20906E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -6.338342943e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29458E+08 1 0.30958E-09 0.59374E+02 0.30408E+04 c Velocity[X] 0.29756E+02 c Velocity[Y] 0.29618E+02 c Velocity[Z] 0.33419E-04 c Pressure 0.39420E-03 35 0.58511E-04 0.14942E-01 0.19705E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -6.086 13.356 5.6112 8.0054 v Velocity[Y] -10.375 12.006 -0.14278 -0.00067238 v Velocity[Z] -3.1245 2.9726 3.5816e-06 -5.3857e-08 v ǁVelocityǁ 0.0018181 14.454 6.3386 8.0075 v Pressure -64073 1.8416e+05 65518 36287 v TurbVisc 1.6848e-18 0.0049642 5.4975e-05 2.3714e-06 v CourantNb 1.2828e-07 0.011761 0.00016628 4.8822e-06 v FourierNb 1.2425e-07 0.046886 0.00014502 1.4516e-07 v total_pressure 37252 2.8548e+05 1.6684e+05 1.3761e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0906 0.11449 0.0033802 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2231e-07 0.052093 0.0003113 5.0274e-06 INSTANT 0.874842000E-01 TIME STEP NUMBER 55040 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283132908E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.529020552E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.72582E-02 0.21314E+01 Friction velocity uk : 0.72582E-02 0.21314E+01 Dimensionless distance yplus : 0.69872E-02 0.20928E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -3.490771063e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29459E+08 1 0.30793E-09 0.58753E+02 0.30248E+04 c Velocity[X] 0.29439E+02 c Velocity[Y] 0.29313E+02 c Velocity[Z] 0.32524E-04 c Pressure 0.39510E-03 31 0.49869E-04 0.14835E-01 0.19686E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -6.084 13.417 5.6113 8.0056 v Velocity[Y] -10.376 12.012 -0.1428 -0.00067251 v Velocity[Z] -3.1241 2.9727 3.5805e-06 -5.3857e-08 v ǁVelocityǁ 0.0021722 14.455 6.3392 8.0076 v Pressure -67349 1.825e+05 64213 35579 v TurbVisc 1.3698e-18 0.0049642 5.5445e-05 2.3948e-06 v CourantNb 1.3765e-07 0.011762 0.00016628 4.8823e-06 v FourierNb 1.2425e-07 0.046902 0.00014502 1.4534e-07 v total_pressure 33976 2.8383e+05 1.6554e+05 1.369e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0928 0.11439 0.0033776 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2232e-07 0.052113 0.0003113 5.0276e-06 INSTANT 0.874843000E-01 TIME STEP NUMBER 55041 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283138377E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.531272788E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.89617E-02 0.21333E+01 Friction velocity uk : 0.89617E-02 0.21333E+01 Dimensionless distance yplus : 0.86186E-02 0.20947E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.042521884e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29459E+08 1 0.30632E-09 0.58144E+02 0.30091E+04 c Velocity[X] 0.29129E+02 c Velocity[Y] 0.29015E+02 c Velocity[Z] 0.31792E-04 c Pressure 0.39507E-03 11 0.85063E-04 0.14698E-01 0.19005E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -6.0822 13.476 5.6115 8.0057 v Velocity[Y] -10.377 12.017 -0.14282 -0.00067268 v Velocity[Z] -3.1238 2.9727 3.5793e-06 -5.3857e-08 v ǁVelocityǁ 0.00162 14.457 6.3398 8.0077 v Pressure -70663 1.8055e+05 62933 34904 v TurbVisc 1.6182e-18 0.0049643 5.591e-05 2.4181e-06 v CourantNb 1.2798e-07 0.011762 0.00016628 4.8823e-06 v FourierNb 1.2425e-07 0.046916 0.00014502 1.4551e-07 v total_pressure 30662 2.8188e+05 1.6426e+05 1.3623e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0947 0.11429 0.0033753 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2233e-07 0.05213 0.0003113 5.0278e-06 INSTANT 0.874844000E-01 TIME STEP NUMBER 55042 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283143710E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.533479436E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.74032E-02 0.21350E+01 Friction velocity uk : 0.74032E-02 0.21350E+01 Dimensionless distance yplus : 0.71268E-02 0.20963E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 5.867149003e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29460E+08 1 0.30476E-09 0.57562E+02 0.29939E+04 c Velocity[X] 0.28832E+02 c Velocity[Y] 0.28729E+02 c Velocity[Z] 0.31193E-04 c Pressure 0.39371E-03 22 0.65697E-04 0.14517E-01 0.22011E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -6.0812 13.534 5.6116 8.0058 v Velocity[Y] -10.377 12.02 -0.14284 -0.0006729 v Velocity[Z] -3.1235 2.9728 3.5782e-06 -5.3857e-08 v ǁVelocityǁ 0.0017595 14.457 6.3405 8.0078 v Pressure -73984 1.7836e+05 61291 34173 v TurbVisc 8.2641e-19 0.0049643 5.6369e-05 2.4411e-06 v CourantNb 1.3192e-07 0.011762 0.00016628 4.8824e-06 v FourierNb 1.2425e-07 0.046928 0.00014502 1.4569e-07 v total_pressure 27341 2.7968e+05 1.6262e+05 1.355e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0963 0.11421 0.0033737 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2234e-07 0.052144 0.0003113 5.0281e-06 INSTANT 0.874845000E-01 TIME STEP NUMBER 55043 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283148969E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.535620527E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12916E-01 0.21360E+01 Friction velocity uk : 0.12916E-01 0.21360E+01 Dimensionless distance yplus : 0.12434E-01 0.20974E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 9.918048655e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29460E+08 1 0.30322E-09 0.56996E+02 0.29791E+04 c Velocity[X] 0.28545E+02 c Velocity[Y] 0.28452E+02 c Velocity[Z] 0.30700E-04 c Pressure 0.39251E-03 32 0.49231E-04 0.14347E-01 0.21967E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -6.0806 13.591 5.6118 8.0059 v Velocity[Y] -10.377 12.022 -0.14286 -0.00067304 v Velocity[Z] -3.1232 2.9729 3.5771e-06 -5.3857e-08 v ǁVelocityǁ 0.0021231 14.458 6.3411 8.008 v Pressure -77322 1.7597e+05 59886 33435 v TurbVisc 7.4073e-19 0.0049643 5.6824e-05 2.464e-06 v CourantNb 1.2569e-07 0.011762 0.00016629 4.8824e-06 v FourierNb 1.2425e-07 0.046935 0.00014502 1.4586e-07 v total_pressure 24003 2.7729e+05 1.6121e+05 1.3476e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0974 0.11414 0.0033723 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2234e-07 0.052153 0.00031131 5.0283e-06 INSTANT 0.874846000E-01 TIME STEP NUMBER 55044 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283154094E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.537831718E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13381E-01 0.21366E+01 Friction velocity uk : 0.13381E-01 0.21366E+01 Dimensionless distance yplus : 0.12881E-01 0.20980E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.490230384e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29461E+08 1 0.30174E-09 0.56452E+02 0.29648E+04 c Velocity[X] 0.28268E+02 c Velocity[Y] 0.28184E+02 c Velocity[Z] 0.30347E-04 c Pressure 0.38910E-03 12 0.85529E-04 0.14103E-01 0.22621E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -6.0802 13.647 5.612 8.006 v Velocity[Y] -10.378 12.024 -0.14289 -0.00067308 v Velocity[Z] -3.1229 2.9729 3.5759e-06 -5.3857e-08 v ǁVelocityǁ 0.0022872 14.458 6.3418 8.0081 v Pressure -80624 1.7344e+05 58489 32681 v TurbVisc 9.5628e-19 0.0049643 5.7273e-05 2.4866e-06 v CourantNb 8.7432e-08 0.011762 0.00016629 4.8825e-06 v FourierNb 1.2425e-07 0.04694 0.00014502 1.4603e-07 v total_pressure 20701 2.7476e+05 1.5981e+05 1.3401e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.098 0.11408 0.0033712 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2235e-07 0.052159 0.00031131 5.0285e-06 INSTANT 0.874847000E-01 TIME STEP NUMBER 55045 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283159044E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.539907619E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.16057E-01 0.21370E+01 Friction velocity uk : 0.16057E-01 0.21370E+01 Dimensionless distance yplus : 0.15532E-01 0.20983E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.997445485e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29461E+08 1 0.30030E-09 0.55937E+02 0.29512E+04 c Velocity[X] 0.28006E+02 c Velocity[Y] 0.27931E+02 c Velocity[Z] 0.30059E-04 c Pressure 0.38388E-03 29 0.53286E-04 0.13799E-01 0.26363E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -6.0807 13.702 5.6121 8.0061 v Velocity[Y] -10.378 12.023 -0.14291 -0.00067328 v Velocity[Z] -3.1226 2.973 3.5748e-06 -5.3857e-08 v ǁVelocityǁ 0.0019431 14.457 6.3424 8.0082 v Pressure -83897 1.7087e+05 56760 31862 v TurbVisc 5.8945e-19 0.0049643 5.7716e-05 2.5092e-06 v CourantNb 3.9512e-08 0.011762 0.0001663 4.8826e-06 v FourierNb 1.2425e-07 0.046943 0.00014502 1.4621e-07 v total_pressure 17428 2.7219e+05 1.5809e+05 1.3319e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0983 0.11402 0.0033703 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2236e-07 0.052162 0.00031132 5.0288e-06 INSTANT 0.874848000E-01 TIME STEP NUMBER 55046 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283163948E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.541863812E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.81626E-02 0.21367E+01 Friction velocity uk : 0.81626E-02 0.21367E+01 Dimensionless distance yplus : 0.78722E-02 0.20980E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 2.433299614e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29461E+08 1 0.29890E-09 0.55436E+02 0.29379E+04 c Velocity[X] 0.27751E+02 c Velocity[Y] 0.27684E+02 c Velocity[Z] 0.29796E-04 c Pressure 0.37891E-03 11 0.97810E-04 0.13510E-01 0.26177E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -6.0814 13.756 5.6123 8.0062 v Velocity[Y] -10.378 12.022 -0.14294 -0.00067352 v Velocity[Z] -3.1223 2.973 3.5736e-06 -5.3857e-08 v ǁVelocityǁ 0.0016173 14.485 6.3431 8.0083 v Pressure -87110 1.6836e+05 55330 31027 v TurbVisc 4.8315e-19 0.0049644 5.8155e-05 2.5315e-06 v CourantNb 3.8839e-08 0.011762 0.0001663 4.8826e-06 v FourierNb 1.2425e-07 0.046941 0.00014503 1.4637e-07 v total_pressure 14215 2.6969e+05 1.5665e+05 1.3235e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.098 0.11398 0.0033695 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2237e-07 0.052159 0.00031133 5.029e-06 INSTANT 0.874849000E-01 TIME STEP NUMBER 55047 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283168673E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.543833219E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13378E-01 0.21361E+01 Friction velocity uk : 0.13378E-01 0.21361E+01 Dimensionless distance yplus : 0.12878E-01 0.20975E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 2.872790304e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29462E+08 1 0.29754E-09 0.54958E+02 0.29252E+04 c Velocity[X] 0.27509E+02 c Velocity[Y] 0.27449E+02 c Velocity[Z] 0.29622E-04 c Pressure 0.37185E-03 22 0.85001E-04 0.13154E-01 0.28392E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -6.0828 13.809 5.6124 8.0063 v Velocity[Y] -10.377 12.019 -0.14297 -0.0006738 v Velocity[Z] -3.122 2.9731 3.5725e-06 -5.3857e-08 v ǁVelocityǁ 0.0019601 14.549 6.3438 8.0085 v Pressure -90172 1.6598e+05 53589 30196 v TurbVisc 6.4018e-19 0.0049644 5.8589e-05 2.5536e-06 v CourantNb 1.1746e-07 0.011762 0.00016631 4.8827e-06 v FourierNb 1.2425e-07 0.046937 0.00014503 1.4654e-07 v total_pressure 11153 2.6731e+05 1.5491e+05 1.3152e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0975 0.11395 0.003369 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2238e-07 0.052155 0.00031133 5.0292e-06 INSTANT 0.874850000E-01 TIME STEP NUMBER 55048 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283173309E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.545595252E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15515E-01 0.21350E+01 Friction velocity uk : 0.15515E-01 0.21350E+01 Dimensionless distance yplus : 0.14936E-01 0.20964E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 3.291724787e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29462E+08 1 0.29621E-09 0.54492E+02 0.29127E+04 c Velocity[X] 0.27273E+02 c Velocity[Y] 0.27219E+02 c Velocity[Z] 0.29425E-04 c Pressure 0.36568E-03 31 0.60301E-04 0.12837E-01 0.28693E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -6.0845 13.861 5.6126 8.0064 v Velocity[Y] -10.377 12.016 -0.143 -0.00067395 v Velocity[Z] -3.1217 2.9731 3.5714e-06 -5.3857e-08 v ǁVelocityǁ 0.0033609 14.611 6.3445 8.0086 v Pressure -93048 1.6377e+05 52025 29348 v TurbVisc 6.6502e-19 0.0049644 5.9018e-05 2.5756e-06 v CourantNb 1.32e-07 0.011762 0.00016631 4.8827e-06 v FourierNb 1.2425e-07 0.04693 0.00014503 1.4671e-07 v total_pressure 8277.5 2.651e+05 1.5335e+05 1.3067e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0964 0.11392 0.0033686 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2238e-07 0.052145 0.00031134 5.0294e-06 INSTANT 0.874851000E-01 TIME STEP NUMBER 55049 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283177796E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.547342324E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.16393E-01 0.21337E+01 Friction velocity uk : 0.16393E-01 0.21337E+01 Dimensionless distance yplus : 0.15782E-01 0.20951E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 3.630428240e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29463E+08 1 0.29491E-09 0.54041E+02 0.29006E+04 c Velocity[X] 0.27045E+02 c Velocity[Y] 0.26995E+02 c Velocity[Z] 0.29285E-04 c Pressure 0.35912E-03 11 0.78544E-04 0.12512E-01 0.29142E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -6.0863 13.912 5.6127 8.0065 v Velocity[Y] -10.376 12.012 -0.14302 -0.000674 v Velocity[Z] -3.1214 2.9732 3.5702e-06 -5.3857e-08 v ǁVelocityǁ 0.0033193 14.672 6.3452 8.0087 v Pressure -95650 1.6174e+05 50455 28498 v TurbVisc 5.617e-19 0.0049644 5.9443e-05 2.5973e-06 v CourantNb 1.3987e-07 0.011762 0.00016632 4.8828e-06 v FourierNb 1.2425e-07 0.04692 0.00014503 1.4687e-07 v total_pressure 5674.9 2.6307e+05 1.5178e+05 1.2982e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0951 0.1139 0.0033683 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2239e-07 0.052133 0.00031135 5.0297e-06 INSTANT 0.874852000E-01 TIME STEP NUMBER 55050 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283182089E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.548916682E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.75886E-02 0.21321E+01 Friction velocity uk : 0.75886E-02 0.21321E+01 Dimensionless distance yplus : 0.73052E-02 0.20936E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 3.939366003e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29463E+08 1 0.29365E-09 0.53603E+02 0.28887E+04 c Velocity[X] 0.26824E+02 c Velocity[Y] 0.26778E+02 c Velocity[Z] 0.29145E-04 c Pressure 0.35324E-03 29 0.60731E-04 0.12217E-01 0.34161E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -6.0887 13.962 5.6129 8.0065 v Velocity[Y] -10.376 12.007 -0.14305 -0.00067422 v Velocity[Z] -3.1211 2.9732 3.5691e-06 -5.3857e-08 v ǁVelocityǁ 0.0023623 14.732 6.3459 8.0088 v Pressure -97945 1.6e+05 48687 27579 v TurbVisc 4.8448e-19 0.0049644 5.9862e-05 2.6189e-06 v CourantNb 1.0422e-07 0.011762 0.00016632 4.8828e-06 v FourierNb 1.2425e-07 0.046909 0.00014503 1.4704e-07 v total_pressure 3379.6 2.6133e+05 1.5001e+05 1.289e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0936 0.11386 0.0033679 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.224e-07 0.05212 0.00031136 5.0299e-06 INSTANT 0.874853000E-01 TIME STEP NUMBER 55051 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283186327E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.550361813E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19584E-01 0.21302E+01 Friction velocity uk : 0.19584E-01 0.21302E+01 Dimensionless distance yplus : 0.18854E-01 0.20917E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 4.161102130e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29463E+08 1 0.29241E-09 0.53174E+02 0.28771E+04 c Velocity[X] 0.26608E+02 c Velocity[Y] 0.26565E+02 c Velocity[Z] 0.28962E-04 c Pressure 0.34956E-03 12 0.98541E-04 0.12002E-01 0.34418E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -6.091 14.012 5.613 8.0066 v Velocity[Y] -10.375 12.002 -0.14307 -0.00067453 v Velocity[Z] -3.1208 2.9733 3.5679e-06 -5.3857e-08 v ǁVelocityǁ 0.0030728 14.792 6.3466 8.0089 v Pressure -99873 1.5856e+05 47082 26635 v TurbVisc 4.0993e-19 0.0049645 6.0277e-05 2.6404e-06 v CourantNb 1.2797e-07 0.011762 0.00016633 4.8829e-06 v FourierNb 1.2425e-07 0.046896 0.00014503 1.472e-07 v total_pressure 1451.6 2.5988e+05 1.4841e+05 1.2796e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0917 0.11383 0.0033676 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2241e-07 0.052103 0.00031136 5.0301e-06 INSTANT 0.874854000E-01 TIME STEP NUMBER 55052 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283190361E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.551745963E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.92424E-02 0.21282E+01 Friction velocity uk : 0.92424E-02 0.21282E+01 Dimensionless distance yplus : 0.91358E-02 0.20897E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 4.291522475e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29464E+08 1 0.29121E-09 0.52753E+02 0.28657E+04 c Velocity[X] 0.26396E+02 c Velocity[Y] 0.26356E+02 c Velocity[Z] 0.28789E-04 c Pressure 0.34684E-03 39 0.73010E-04 0.11825E-01 0.38294E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -6.0936 14.061 5.6131 8.0067 v Velocity[Y] -10.374 11.996 -0.14309 -0.00067458 v Velocity[Z] -3.1205 2.9733 3.5668e-06 -5.3857e-08 v ǁVelocityǁ 0.0030119 14.85 6.3473 8.009 v Pressure -1.0144e+05 1.5709e+05 45334 25693 v TurbVisc 2.5171e-19 0.0049645 6.0688e-05 2.6616e-06 v CourantNb 1.1511e-07 0.011761 0.00016634 4.8829e-06 v FourierNb 1.2425e-07 0.046882 0.00014504 1.4736e-07 v total_pressure -113.91 2.5841e+05 1.4666e+05 1.2702e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0897 0.11379 0.0033672 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2241e-07 0.052086 0.00031137 5.0303e-06 INSTANT 0.874855000E-01 TIME STEP NUMBER 55053 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283194338E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.552996819E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.16981E-01 0.21261E+01 Friction velocity uk : 0.16981E-01 0.21261E+01 Dimensionless distance yplus : 0.16348E-01 0.20876E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 4.378724907e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29464E+08 1 0.29003E-09 0.52339E+02 0.28543E+04 c Velocity[X] 0.26188E+02 c Velocity[Y] 0.26150E+02 c Velocity[Z] 0.28529E-04 c Pressure 0.34622E-03 139 0.82615E-04 0.11723E-01 0.40078E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -6.0961 14.109 5.6132 8.0068 v Velocity[Y] -10.374 11.99 -0.14311 -0.00067502 v Velocity[Z] -3.1202 2.9734 3.5657e-06 -5.3857e-08 v ǁVelocityǁ 0.0030457 14.909 6.348 8.0091 v Pressure -1.0262e+05 1.5557e+05 43666 24688 v TurbVisc 9.3161e-20 0.0049645 6.1094e-05 2.6827e-06 v CourantNb 1.1395e-07 0.011761 0.00016634 4.883e-06 v FourierNb 1.2425e-07 0.046867 0.00014504 1.4752e-07 v total_pressure -1296.6 2.569e+05 1.4499e+05 1.2601e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0876 0.11384 0.0033673 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2242e-07 0.052068 0.00031138 5.0305e-06 INSTANT 0.874856000E-01 TIME STEP NUMBER 55054 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283198130E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.554195241E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.70231E-02 0.21239E+01 Friction velocity uk : 0.70231E-02 0.21239E+01 Dimensionless distance yplus : 0.67613E-02 0.20855E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 4.369107989e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29465E+08 1 0.28888E-09 0.51931E+02 0.28432E+04 c Velocity[X] 0.25985E+02 c Velocity[Y] 0.25947E+02 c Velocity[Z] 0.28217E-04 c Pressure 0.34672E-03 102 0.89010E-04 0.11661E-01 0.37092E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -6.0986 14.157 5.6134 8.0069 v Velocity[Y] -10.373 11.984 -0.14312 -0.000675 v Velocity[Z] -3.1198 2.9734 3.5645e-06 -5.3857e-08 v ǁVelocityǁ 0.0032878 14.966 6.3487 8.0092 v Pressure -1.0345e+05 1.5403e+05 41994 23809 v TurbVisc 9.0693e-21 0.0049645 6.1497e-05 2.7037e-06 v CourantNb 1.5825e-07 0.011761 0.00016635 4.883e-06 v FourierNb 1.2425e-07 0.046852 0.00014504 1.4768e-07 v total_pressure -2120.7 2.5535e+05 1.4332e+05 1.2513e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0855 0.11384 0.0033672 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2242e-07 0.052049 0.00031139 5.0307e-06 INSTANT 0.874857000E-01 TIME STEP NUMBER 55055 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283201712E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.555318172E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.82728E-02 0.21219E+01 Friction velocity uk : 0.82728E-02 0.21219E+01 Dimensionless distance yplus : 0.80651E-02 0.20835E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 4.279859422e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29465E+08 1 0.28776E-09 0.51531E+02 0.28321E+04 c Velocity[X] 0.25784E+02 c Velocity[Y] 0.25747E+02 c Velocity[Z] 0.27817E-04 c Pressure 0.34815E-03 251 0.74498E-04 0.11631E-01 0.47188E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -6.1009 14.207 5.6135 8.0069 v Velocity[Y] -10.372 11.979 -0.14314 -0.00067521 v Velocity[Z] -3.1195 2.9734 3.5634e-06 -5.3857e-08 v ǁVelocityǁ 0.0037475 15.024 6.3494 8.0093 v Pressure -1.0395e+05 1.5246e+05 40262 22726 v TurbVisc 4.3824e-19 0.0049645 6.1895e-05 2.7245e-06 v CourantNb 9.5032e-08 0.011761 0.00016636 4.8831e-06 v FourierNb 1.2425e-07 0.046837 0.00014504 1.4784e-07 v total_pressure -2623.1 2.5379e+05 1.4159e+05 1.2405e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0835 0.11387 0.003367 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2243e-07 0.052031 0.0003114 5.0309e-06 INSTANT 0.874858000E-01 TIME STEP NUMBER 55056 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283205168E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.556396895E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.93040E-02 0.21199E+01 Friction velocity uk : 0.93040E-02 0.21199E+01 Dimensionless distance yplus : 0.90126E-02 0.20815E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 4.104503016e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29465E+08 1 0.28667E-09 0.51142E+02 0.28214E+04 c Velocity[X] 0.25590E+02 c Velocity[Y] 0.25552E+02 c Velocity[Z] 0.27332E-04 c Pressure 0.34991E-03 11 0.98837E-04 0.11614E-01 0.41217E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -6.1032 14.265 5.6136 8.007 v Velocity[Y] -10.372 11.974 -0.14315 -0.00067552 v Velocity[Z] -3.1192 2.9735 3.5623e-06 -5.3857e-08 v ǁVelocityǁ 0.0039878 15.08 6.3501 8.0094 v Pressure -1.0469e+05 1.5096e+05 38512 21805 v TurbVisc 3.3155e-19 0.0049646 6.229e-05 2.7452e-06 v CourantNb 6.6996e-08 0.011761 0.00016636 4.8831e-06 v FourierNb 1.2425e-07 0.046823 0.00014505 1.4799e-07 v total_pressure -3364.4 2.5229e+05 1.3984e+05 1.2313e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0815 0.11396 0.0033671 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2244e-07 0.052014 0.00031141 5.0311e-06 INSTANT 0.874859000E-01 TIME STEP NUMBER 55057 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283208394E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.557452904E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.51041E-02 0.21181E+01 Friction velocity uk : 0.51041E-02 0.21181E+01 Dimensionless distance yplus : 0.49138E-02 0.20797E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 3.815316128e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29465E+08 1 0.28562E-09 0.50754E+02 0.28106E+04 c Velocity[X] 0.25396E+02 c Velocity[Y] 0.25358E+02 c Velocity[Z] 0.26790E-04 c Pressure 0.35169E-03 22 0.97726E-04 0.11599E-01 0.54013E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -6.105 14.323 5.6136 8.0071 v Velocity[Y] -10.371 11.97 -0.14315 -0.00067583 v Velocity[Z] -3.1189 2.9735 3.5611e-06 -5.3857e-08 v ǁVelocityǁ 0.0039226 15.137 6.3508 8.0095 v Pressure -1.0525e+05 1.4994e+05 36846 20710 v TurbVisc 4.0355e-19 0.0049646 6.2681e-05 2.7658e-06 v CourantNb 1.0269e-07 0.011761 0.00016637 4.8831e-06 v FourierNb 1.2425e-07 0.04681 0.00014505 1.4815e-07 v total_pressure -3928.9 2.5127e+05 1.3817e+05 1.2203e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0797 0.11403 0.003367 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2244e-07 0.051998 0.00031142 5.0313e-06 INSTANT 0.874860000E-01 TIME STEP NUMBER 55058 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283211555E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.558514006E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13809E-01 0.21165E+01 Friction velocity uk : 0.13809E-01 0.21165E+01 Dimensionless distance yplus : 0.13377E-01 0.20782E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 3.532049042e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29466E+08 1 0.28458E-09 0.50379E+02 0.28002E+04 c Velocity[X] 0.25208E+02 c Velocity[Y] 0.25171E+02 c Velocity[Z] 0.26169E-04 c Pressure 0.35232E-03 29 0.76542E-04 0.11547E-01 0.53043E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -6.1066 14.38 5.6137 8.0071 v Velocity[Y] -10.371 11.966 -0.14316 -0.00067596 v Velocity[Z] -3.1186 2.9736 3.56e-06 -5.3857e-08 v ǁVelocityǁ 0.0037815 15.193 6.3515 8.0096 v Pressure -1.0576e+05 1.4915e+05 35061 19657 v TurbVisc 6.9909e-20 0.0049646 6.3069e-05 2.7862e-06 v CourantNb 8.5154e-08 0.01176 0.00016637 4.8832e-06 v FourierNb 1.2425e-07 0.046799 0.00014506 1.483e-07 v total_pressure -4430.5 2.5047e+05 1.3639e+05 1.2098e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0782 0.11408 0.0033668 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2245e-07 0.051984 0.00031143 5.0315e-06 INSTANT 0.874861000E-01 TIME STEP NUMBER 55059 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283214543E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.559563847E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11370E-01 0.21152E+01 Friction velocity uk : 0.11370E-01 0.21152E+01 Dimensionless distance yplus : 0.11085E-01 0.20770E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 3.152649625e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29466E+08 1 0.28357E-09 0.50015E+02 0.27900E+04 c Velocity[X] 0.25026E+02 c Velocity[Y] 0.24988E+02 c Velocity[Z] 0.25494E-04 c Pressure 0.35238E-03 26 0.36665E-04 0.11478E-01 0.56712E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -6.1079 14.436 5.6138 8.0072 v Velocity[Y] -10.371 11.964 -0.14316 -0.00067603 v Velocity[Z] -3.1183 2.9736 3.5588e-06 -5.3857e-08 v ǁVelocityǁ 0.0041913 15.248 6.3522 8.0097 v Pressure -1.0623e+05 1.4851e+05 33294 18590 v TurbVisc 1.8337e-20 0.0049646 6.3454e-05 2.8065e-06 v CourantNb 1.0197e-07 0.01176 0.00016637 4.8832e-06 v FourierNb 1.2425e-07 0.04679 0.00014506 1.4846e-07 v total_pressure -4909.7 2.4984e+05 1.3462e+05 1.1992e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.077 0.1141 0.0033662 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2245e-07 0.051973 0.00031143 5.0317e-06 INSTANT 0.874862000E-01 TIME STEP NUMBER 55060 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283217352E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.560663251E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.25026E-01 0.21142E+01 Friction velocity uk : 0.25026E-01 0.21142E+01 Dimensionless distance yplus : 0.24375E-01 0.20760E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 2.706651080e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29466E+08 1 0.28257E-09 0.49669E+02 0.27803E+04 c Velocity[X] 0.24854E+02 c Velocity[Y] 0.24815E+02 c Velocity[Z] 0.24788E-04 c Pressure 0.35126E-03 12 0.98673E-04 0.11373E-01 0.59198E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -6.109 14.492 5.6138 8.0073 v Velocity[Y] -10.371 11.962 -0.14317 -0.00067609 v Velocity[Z] -3.118 2.9737 3.5577e-06 -5.3857e-08 v ǁVelocityǁ 0.004097 15.303 6.3528 8.0097 v Pressure -1.0683e+05 1.4799e+05 31412 17521 v TurbVisc 2.9371e-21 0.0049647 6.3835e-05 2.8267e-06 v CourantNb 9.4633e-08 0.01176 0.00016638 4.8832e-06 v FourierNb 1.2425e-07 0.046782 0.00014506 1.4861e-07 v total_pressure -5504.8 2.4932e+05 1.3274e+05 1.1885e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.076 0.1141 0.0033653 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2246e-07 0.051965 0.00031144 5.0318e-06 INSTANT 0.874863000E-01 TIME STEP NUMBER 55061 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283219936E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.561793199E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.22436E-01 0.21135E+01 Friction velocity uk : 0.22436E-01 0.21135E+01 Dimensionless distance yplus : 0.21695E-01 0.20753E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 2.178282298e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29466E+08 1 0.28161E-09 0.49330E+02 0.27708E+04 c Velocity[X] 0.24685E+02 c Velocity[Y] 0.24645E+02 c Velocity[Z] 0.24074E-04 c Pressure 0.34958E-03 12 0.98629E-04 0.11252E-01 0.61472E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -6.1096 14.546 5.6139 8.0073 v Velocity[Y] -10.371 11.961 -0.14317 -0.00067621 v Velocity[Z] -3.1177 2.9737 3.5566e-06 -5.3857e-08 v ǁVelocityǁ 0.0039232 15.358 6.3535 8.0098 v Pressure -1.0757e+05 1.4754e+05 29710 16496 v TurbVisc 1.4923e-20 0.0049647 6.4213e-05 2.8468e-06 v CourantNb 7.715e-08 0.01176 0.00016638 4.8833e-06 v FourierNb 1.2425e-07 0.046777 0.00014507 1.4876e-07 v total_pressure -6242.1 2.4887e+05 1.3104e+05 1.1782e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0753 0.11408 0.0033641 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2246e-07 0.051959 0.00031145 5.032e-06 INSTANT 0.874864000E-01 TIME STEP NUMBER 55062 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283222305E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.562994453E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15702E-01 0.21131E+01 Friction velocity uk : 0.15702E-01 0.21131E+01 Dimensionless distance yplus : 0.15341E-01 0.20749E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.640121261e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29467E+08 1 0.28066E-09 0.48998E+02 0.27614E+04 c Velocity[X] 0.24519E+02 c Velocity[Y] 0.24479E+02 c Velocity[Z] 0.23363E-04 c Pressure 0.34628E-03 27 0.32340E-04 0.11081E-01 0.85236E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -6.1098 14.6 5.6139 8.0074 v Velocity[Y] -10.371 11.961 -0.14316 -0.00067636 v Velocity[Z] -3.1174 2.9738 3.5554e-06 -5.3857e-08 v ǁVelocityǁ 0.003928 15.412 6.3541 8.0099 v Pressure -1.0842e+05 1.4752e+05 28027 15216 v TurbVisc 9.5631e-20 0.0049647 6.4588e-05 2.8668e-06 v CourantNb 7.6136e-08 0.01176 0.00016638 4.8833e-06 v FourierNb 1.2425e-07 0.046775 0.00014507 1.4891e-07 v total_pressure -7096.8 2.4884e+05 1.2935e+05 1.1654e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0749 0.11405 0.0033627 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2246e-07 0.051956 0.00031145 5.0322e-06 INSTANT 0.874865000E-01 TIME STEP NUMBER 55063 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283224751E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.564195547E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12628E-01 0.21132E+01 Friction velocity uk : 0.12628E-01 0.21132E+01 Dimensionless distance yplus : 0.12338E-01 0.20750E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.266870510e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29467E+08 1 0.27973E-09 0.48681E+02 0.27524E+04 c Velocity[X] 0.24361E+02 c Velocity[Y] 0.24320E+02 c Velocity[Z] 0.22631E-04 c Pressure 0.34256E-03 26 0.25202E-04 0.10899E-01 0.75800E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -6.1096 14.653 5.6139 8.0074 v Velocity[Y] -10.371 11.962 -0.14316 -0.00067644 v Velocity[Z] -3.1171 2.9738 3.5543e-06 -5.3857e-08 v ǁVelocityǁ 0.0040591 15.466 6.3548 8.01 v Pressure -1.0941e+05 1.474e+05 26091 14117 v TurbVisc 8.3148e-20 0.0049647 6.4959e-05 2.8866e-06 v CourantNb 7.6237e-08 0.01176 0.00016638 4.8833e-06 v FourierNb 1.2425e-07 0.046775 0.00014507 1.4906e-07 v total_pressure -8080.5 2.4872e+05 1.2742e+05 1.1544e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.075 0.114 0.003361 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2247e-07 0.051957 0.00031145 5.0324e-06 INSTANT 0.874866000E-01 TIME STEP NUMBER 55064 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283226912E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.565445595E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15097E-01 0.21135E+01 Friction velocity uk : 0.15097E-01 0.21135E+01 Dimensionless distance yplus : 0.14749E-01 0.20753E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 6.616931846e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29467E+08 1 0.27882E-09 0.48381E+02 0.27439E+04 c Velocity[X] 0.24211E+02 c Velocity[Y] 0.24169E+02 c Velocity[Z] 0.21906E-04 c Pressure 0.33916E-03 15 0.98978E-04 0.10730E-01 0.79033E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -6.1093 14.704 5.6139 8.0074 v Velocity[Y] -10.372 11.963 -0.14316 -0.00067647 v Velocity[Z] -3.1167 2.9739 3.5531e-06 -5.3857e-08 v ǁVelocityǁ 0.0040612 15.52 6.3554 8.01 v Pressure -1.1045e+05 1.4715e+05 24108 13037 v TurbVisc 3.3059e-20 0.0049647 6.5328e-05 2.9063e-06 v CourantNb 7.7218e-08 0.01176 0.00016638 4.8833e-06 v FourierNb 1.2425e-07 0.046777 0.00014507 1.4921e-07 v total_pressure -9127.5 2.4847e+05 1.2543e+05 1.1436e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0753 0.11393 0.003359 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2247e-07 0.051961 0.00031146 5.0326e-06 INSTANT 0.874867000E-01 TIME STEP NUMBER 55065 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283228817E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.566754465E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.18987E-01 0.21141E+01 Friction velocity uk : 0.18987E-01 0.21141E+01 Dimensionless distance yplus : 0.18360E-01 0.20758E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 3.705085811e-03 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29467E+08 1 0.27792E-09 0.48082E+02 0.27354E+04 c Velocity[X] 0.24062E+02 c Velocity[Y] 0.24020E+02 c Velocity[Z] 0.21226E-04 c Pressure 0.33641E-03 12 0.99001E-04 0.10584E-01 0.83274E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -6.1086 14.755 5.6139 8.0075 v Velocity[Y] -10.372 11.966 -0.14315 -0.00067648 v Velocity[Z] -3.1164 2.9739 3.552e-06 -5.3857e-08 v ǁVelocityǁ 0.0038374 15.573 6.356 8.0101 v Pressure -1.1157e+05 1.4671e+05 22375 12009 v TurbVisc 2.6978e-20 0.0049648 6.5693e-05 2.9259e-06 v CourantNb 7.9172e-08 0.01176 0.00016638 4.8834e-06 v FourierNb 1.2425e-07 0.046782 0.00014508 1.4936e-07 v total_pressure -10247 2.4804e+05 1.237e+05 1.1333e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0758 0.11385 0.0033566 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2247e-07 0.051966 0.00031146 5.0327e-06 INSTANT 0.874868000E-01 TIME STEP NUMBER 55066 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283230474E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.568120401E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.16384E-01 0.21150E+01 Friction velocity uk : 0.16384E-01 0.21150E+01 Dimensionless distance yplus : 0.15871E-01 0.20767E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -5.065195945e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29467E+08 1 0.27705E-09 0.47784E+02 0.27269E+04 c Velocity[X] 0.23913E+02 c Velocity[Y] 0.23871E+02 c Velocity[Z] 0.20588E-04 c Pressure 0.33316E-03 63 0.46255E-04 0.10425E-01 0.12119E+07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -6.1076 14.805 5.6139 8.0075 v Velocity[Y] -10.373 11.969 -0.14315 -0.00067655 v Velocity[Z] -3.1161 2.9739 3.5509e-06 -5.3857e-08 v ǁVelocityǁ 0.0037384 15.627 6.3567 8.0102 v Pressure -1.1277e+05 1.4604e+05 20602 10696 v TurbVisc 9.8588e-21 0.0049648 6.6056e-05 2.9454e-06 v CourantNb 1.2353e-07 0.01176 0.00016638 4.8834e-06 v FourierNb 1.2425e-07 0.046788 0.00014508 1.495e-07 v total_pressure -11440 2.4737e+05 1.2193e+05 1.1202e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0767 0.11374 0.0033538 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2248e-07 0.051975 0.00031146 5.0329e-06 INSTANT 0.874869000E-01 TIME STEP NUMBER 55067 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283232216E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.569445527E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.21252E-01 0.21160E+01 Friction velocity uk : 0.21252E-01 0.21160E+01 Dimensionless distance yplus : 0.20494E-01 0.20778E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -8.404391847e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29467E+08 1 0.27618E-09 0.47496E+02 0.27186E+04 c Velocity[X] 0.23769E+02 c Velocity[Y] 0.23727E+02 c Velocity[Z] 0.19943E-04 c Pressure 0.33053E-03 28 0.35538E-04 0.10287E-01 0.11360E+07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -6.1064 14.853 5.6139 8.0075 v Velocity[Y] -10.374 11.973 -0.14314 -0.00067655 v Velocity[Z] -3.1158 2.974 3.5497e-06 -5.3857e-08 v ǁVelocityǁ 0.0033858 15.68 6.3573 8.0102 v Pressure -1.1427e+05 1.4514e+05 18572 9547.6 v TurbVisc 9.8294e-21 0.0049648 6.6415e-05 2.9648e-06 v CourantNb 1.0645e-07 0.01176 0.00016637 4.8834e-06 v FourierNb 1.2425e-07 0.046796 0.00014508 1.4965e-07 v total_pressure -12944 2.4646e+05 1.199e+05 1.1087e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0778 0.1136 0.0033508 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2248e-07 0.051985 0.00031146 5.0331e-06 INSTANT 0.874870000E-01 TIME STEP NUMBER 55068 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283233671E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.570777478E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10191E-01 0.21174E+01 Friction velocity uk : 0.10191E-01 0.21174E+01 Dimensionless distance yplus : 0.98716E-02 0.20791E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.372925283e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29468E+08 1 0.27532E-09 0.47220E+02 0.27107E+04 c Velocity[X] 0.23631E+02 c Velocity[Y] 0.23588E+02 c Velocity[Z] 0.19332E-04 c Pressure 0.32931E-03 12 0.93872E-04 0.10195E-01 0.11849E+07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -6.1051 14.901 5.6138 8.0076 v Velocity[Y] -10.374 11.977 -0.14313 -0.00067651 v Velocity[Z] -3.1155 2.974 3.5486e-06 -5.3857e-08 v ǁVelocityǁ 0.0031077 15.734 6.3579 8.0103 v Pressure -1.1612e+05 1.4398e+05 16517 8453.4 v TurbVisc 4.5409e-20 0.0049648 6.6771e-05 2.984e-06 v CourantNb 8.5055e-08 0.01176 0.00016637 4.8834e-06 v FourierNb 1.2425e-07 0.046806 0.00014509 1.4979e-07 v total_pressure -14795 2.453e+05 1.1784e+05 1.0978e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0791 0.11344 0.0033474 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2248e-07 0.051998 0.00031145 5.0332e-06 INSTANT 0.874871000E-01 TIME STEP NUMBER 55069 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283234873E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.572136334E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.17712E-01 0.21188E+01 Friction velocity uk : 0.17712E-01 0.21188E+01 Dimensionless distance yplus : 0.17546E-01 0.20805E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.877801063e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29468E+08 1 0.27448E-09 0.46940E+02 0.27026E+04 c Velocity[X] 0.23492E+02 c Velocity[Y] 0.23448E+02 c Velocity[Z] 0.18787E-04 c Pressure 0.32911E-03 12 0.98652E-04 0.10135E-01 0.12819E+07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -6.1037 14.949 5.6138 8.0076 v Velocity[Y] -10.375 11.981 -0.14312 -0.0006764 v Velocity[Z] -3.1152 2.9741 3.5475e-06 -5.3857e-08 v ǁVelocityǁ 0.0030339 15.788 6.3584 8.0103 v Pressure -1.1822e+05 1.4257e+05 14734 7419.1 v TurbVisc 5.0482e-20 0.0049648 6.7125e-05 3.0031e-06 v CourantNb 8.8666e-08 0.01176 0.00016636 4.8834e-06 v FourierNb 1.2425e-07 0.046817 0.00014509 1.4994e-07 v total_pressure -16899 2.439e+05 1.1606e+05 1.0874e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0805 0.11326 0.0033437 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2248e-07 0.052011 0.00031145 5.0334e-06 INSTANT 0.874872000E-01 TIME STEP NUMBER 55070 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283235815E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.573496158E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19486E-01 0.21204E+01 Friction velocity uk : 0.19486E-01 0.21204E+01 Dimensionless distance yplus : 0.18980E-01 0.20820E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -2.232705551e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29468E+08 1 0.27365E-09 0.46660E+02 0.26945E+04 c Velocity[X] 0.23351E+02 c Velocity[Y] 0.23309E+02 c Velocity[Z] 0.18297E-04 c Pressure 0.32857E-03 71 0.61941E-04 0.10067E-01 0.19861E+07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -6.1415 14.995 5.6137 8.0076 v Velocity[Y] -10.376 11.986 -0.14312 -0.00067638 v Velocity[Z] -3.1149 2.9741 3.5463e-06 -5.3857e-08 v ǁVelocityǁ 0.0029068 15.842 6.359 8.0104 v Pressure -1.2065e+05 1.4092e+05 12794 6083.2 v TurbVisc 1.0326e-19 0.0049648 6.7475e-05 3.0222e-06 v CourantNb 3.9177e-08 0.01176 0.00016636 4.8835e-06 v FourierNb 1.2425e-07 0.046828 0.00014509 1.5008e-07 v total_pressure -19326 2.4224e+05 1.1412e+05 1.0741e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.082 0.11315 0.0033402 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2249e-07 0.052026 0.00031145 5.0335e-06 INSTANT 0.874873000E-01 TIME STEP NUMBER 55071 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283236849E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.574768444E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.25099E-01 0.21219E+01 Friction velocity uk : 0.25099E-01 0.21219E+01 Dimensionless distance yplus : 0.24494E-01 0.20835E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -2.450402104e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29468E+08 1 0.27284E-09 0.46386E+02 0.26866E+04 c Velocity[X] 0.23214E+02 c Velocity[Y] 0.23172E+02 c Velocity[Z] 0.17825E-04 c Pressure 0.32852E-03 31 0.45228E-04 0.10014E-01 0.19245E+07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -6.1876 15.041 5.6137 8.0076 v Velocity[Y] -10.377 11.99 -0.14311 -0.00067629 v Velocity[Z] -3.1146 2.9742 3.5452e-06 -5.3857e-08 v ǁVelocityǁ 0.0025747 15.896 6.3596 8.0104 v Pressure -1.2341e+05 1.3905e+05 10708 4930.8 v TurbVisc 2.8577e-19 0.0049649 6.7823e-05 3.041e-06 v CourantNb 6.7068e-08 0.01176 0.00016636 4.8835e-06 v FourierNb 1.2425e-07 0.046839 0.00014509 1.5022e-07 v total_pressure -22081 2.4038e+05 1.1203e+05 1.0626e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0835 0.11299 0.0033363 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2249e-07 0.052039 0.00031145 5.0337e-06 INSTANT 0.874874000E-01 TIME STEP NUMBER 55072 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283237597E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.575990504E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.71599E-02 0.21234E+01 Friction velocity uk : 0.71599E-02 0.21234E+01 Dimensionless distance yplus : 0.70774E-02 0.20850E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -2.755009227e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29468E+08 1 0.27203E-09 0.46120E+02 0.26788E+04 c Velocity[X] 0.23080E+02 c Velocity[Y] 0.23040E+02 c Velocity[Z] 0.17402E-04 c Pressure 0.32909E-03 12 0.87804E-04 0.99810E-02 0.20966E+07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -6.2336 15.086 5.6136 8.0076 v Velocity[Y] -10.377 11.995 -0.1431 -0.00067619 v Velocity[Z] -3.1142 2.9742 3.5441e-06 -5.3857e-08 v ǁVelocityǁ 0.0022509 15.951 6.3602 8.0105 v Pressure -1.2644e+05 1.3697e+05 8659.1 3835.6 v TurbVisc 4.528e-19 0.0049649 6.8168e-05 3.0598e-06 v CourantNb 8.7182e-08 0.01176 0.00016635 4.8835e-06 v FourierNb 1.2425e-07 0.04685 0.0001451 1.5037e-07 v total_pressure -25112 2.383e+05 1.0998e+05 1.0516e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.085 0.11281 0.0033321 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2249e-07 0.052053 0.00031145 5.0339e-06 INSTANT 0.874875000E-01 TIME STEP NUMBER 55073 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283238091E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.577188749E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.48551E-02 0.21250E+01 Friction velocity uk : 0.48551E-02 0.21250E+01 Dimensionless distance yplus : 0.48308E-02 0.20866E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -3.000009145e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29468E+08 1 0.27123E-09 0.45853E+02 0.26711E+04 c Velocity[X] 0.22946E+02 c Velocity[Y] 0.22907E+02 c Velocity[Z] 0.17052E-04 c Pressure 0.32971E-03 12 0.99759E-04 0.99503E-02 0.23042E+07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -6.2796 15.131 5.6135 8.0076 v Velocity[Y] -10.378 11.999 -0.14309 -0.00067596 v Velocity[Z] -3.1139 2.9742 3.5429e-06 -5.3857e-08 v ǁVelocityǁ 0.0019516 16.006 6.3608 8.0105 v Pressure -1.2967e+05 1.3474e+05 6785.5 2820.3 v TurbVisc 7.4702e-19 0.0049649 6.851e-05 3.0785e-06 v CourantNb 1.0036e-07 0.01176 0.00016634 4.8835e-06 v FourierNb 1.2425e-07 0.046861 0.0001451 1.5051e-07 v total_pressure -28340 2.3607e+05 1.0811e+05 1.0415e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0866 0.11269 0.003328 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2249e-07 0.052068 0.00031145 5.034e-06 INSTANT 0.874876000E-01 TIME STEP NUMBER 55074 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283238317E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.578322722E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19647E-01 0.21264E+01 Friction velocity uk : 0.19647E-01 0.21264E+01 Dimensionless distance yplus : 0.19154E-01 0.20880E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -3.085522777e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29468E+08 1 0.27045E-09 0.45589E+02 0.26634E+04 c Velocity[X] 0.22813E+02 c Velocity[Y] 0.22776E+02 c Velocity[Z] 0.16763E-04 c Pressure 0.33002E-03 38 0.77134E-04 0.99111E-02 0.36288E+07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -6.3258 15.176 5.6134 8.0076 v Velocity[Y] -10.378 12.002 -0.14308 -0.00067585 v Velocity[Z] -3.1136 2.9743 3.5418e-06 -5.3857e-08 v ǁVelocityǁ 0.0016561 16.061 6.3614 8.0105 v Pressure -1.3301e+05 1.3238e+05 4663.3 1493.8 v TurbVisc 1.2636e-18 0.0049649 6.8849e-05 3.0971e-06 v CourantNb 1.0412e-07 0.01176 0.00016634 4.8835e-06 v FourierNb 1.2425e-07 0.046871 0.00014511 1.5065e-07 v total_pressure -31684 2.3371e+05 1.0599e+05 1.0282e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.088 0.11257 0.003324 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2249e-07 0.05208 0.00031145 5.0342e-06 INSTANT 0.874877000E-01 TIME STEP NUMBER 55075 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283238643E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.579369317E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.16495E-01 0.21276E+01 Friction velocity uk : 0.16495E-01 0.21276E+01 Dimensionless distance yplus : 0.16098E-01 0.20891E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -3.149886092e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29468E+08 1 0.26968E-09 0.45329E+02 0.26557E+04 c Velocity[X] 0.22682E+02 c Velocity[Y] 0.22647E+02 c Velocity[Z] 0.16513E-04 c Pressure 0.33082E-03 26 0.54702E-04 0.98872E-02 0.32432E+07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -6.3717 15.22 5.6133 8.0076 v Velocity[Y] -10.379 12.006 -0.14308 -0.00067569 v Velocity[Z] -3.1133 2.9743 3.5407e-06 -5.3857e-08 v ǁVelocityǁ 0.0014106 16.117 6.3619 8.0106 v Pressure -1.3641e+05 1.2991e+05 2592.9 351.59 v TurbVisc 1.0876e-18 0.0049649 6.9185e-05 3.1156e-06 v CourantNb 1.1242e-07 0.01176 0.00016633 4.8835e-06 v FourierNb 1.2425e-07 0.04688 0.00014511 1.5079e-07 v total_pressure -35080 2.3123e+05 1.0392e+05 1.0168e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0891 0.11246 0.0033198 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2249e-07 0.05209 0.00031144 5.0343e-06 INSTANT 0.874878000E-01 TIME STEP NUMBER 55076 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283238681E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.580347188E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.18957E-01 0.21287E+01 Friction velocity uk : 0.18957E-01 0.21287E+01 Dimensionless distance yplus : 0.18500E-01 0.20902E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -3.157723172e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29468E+08 1 0.26891E-09 0.45072E+02 0.26482E+04 c Velocity[X] 0.22552E+02 c Velocity[Y] 0.22520E+02 c Velocity[Z] 0.16312E-04 c Pressure 0.33128E-03 11 0.79994E-04 0.98541E-02 0.29514E+07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -6.4173 15.264 5.6132 8.0076 v Velocity[Y] -10.379 12.009 -0.14307 -0.00067555 v Velocity[Z] -3.113 2.9744 3.5395e-06 -5.3857e-08 v ǁVelocityǁ 0.0011926 16.172 6.3625 8.0106 v Pressure -1.3981e+05 1.2734e+05 588.51 -725.37 v TurbVisc 1.0301e-18 0.004965 6.9518e-05 3.1339e-06 v CourantNb 9.9246e-08 0.01176 0.00016633 4.8835e-06 v FourierNb 1.2425e-07 0.046887 0.00014512 1.5092e-07 v total_pressure -38480 2.2866e+05 1.0191e+05 1.006e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0902 0.11235 0.0033158 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2249e-07 0.0521 0.00031144 5.0344e-06 INSTANT 0.874879000E-01 TIME STEP NUMBER 55077 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283238472E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.581266886E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.22662E-01 0.21297E+01 Friction velocity uk : 0.22662E-01 0.21297E+01 Dimensionless distance yplus : 0.22116E-01 0.20911E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -3.109110202e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29468E+08 1 0.26816E-09 0.44821E+02 0.26408E+04 c Velocity[X] 0.22426E+02 c Velocity[Y] 0.22395E+02 c Velocity[Z] 0.16175E-04 c Pressure 0.33129E-03 22 0.63386E-04 0.98082E-02 0.28984E+07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -6.4627 15.309 5.6131 8.0076 v Velocity[Y] -10.38 12.011 -0.14306 -0.00067548 v Velocity[Z] -3.1127 2.9744 3.5384e-06 -5.3857e-08 v ǁVelocityǁ 0.00099155 16.227 6.3631 8.0106 v Pressure -1.4316e+05 1.2472e+05 -1516.2 -1853.9 v TurbVisc 1.0468e-18 0.004965 6.9849e-05 3.1521e-06 v CourantNb 9.49e-08 0.01176 0.00016632 4.8835e-06 v FourierNb 1.2425e-07 0.046894 0.00014512 1.5106e-07 v total_pressure -41838 2.2604e+05 99809 99471 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0911 0.11223 0.0033118 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2249e-07 0.052109 0.00031144 5.0346e-06 INSTANT 0.874880000E-01 TIME STEP NUMBER 55078 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283238163E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.582097782E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.22876E-01 0.21302E+01 Friction velocity uk : 0.22876E-01 0.21302E+01 Dimensionless distance yplus : 0.22722E-01 0.20917E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -2.980075210e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29468E+08 1 0.26742E-09 0.44569E+02 0.26333E+04 c Velocity[X] 0.22298E+02 c Velocity[Y] 0.22271E+02 c Velocity[Z] 0.16060E-04 c Pressure 0.33224E-03 12 0.95558E-04 0.97908E-02 0.22155E+07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -6.5076 15.353 5.613 8.0076 v Velocity[Y] -10.38 12.012 -0.14304 -0.000675 v Velocity[Z] -3.1123 2.9745 3.5373e-06 -5.3857e-08 v ǁVelocityǁ 0.00084356 16.282 6.3637 8.0106 v Pressure -1.4645e+05 1.2204e+05 -3462.2 -2888.6 v TurbVisc 9.2582e-19 0.004965 7.0177e-05 3.1703e-06 v CourantNb 9.1877e-08 0.011761 0.00016632 4.8835e-06 v FourierNb 1.2425e-07 0.046898 0.00014513 1.512e-07 v total_pressure -45127 2.2336e+05 97863 98436 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0917 0.11211 0.0033079 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2249e-07 0.052114 0.00031145 5.0347e-06 INSTANT 0.874881000E-01 TIME STEP NUMBER 55079 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283237584E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.582916016E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.22696E-01 0.21307E+01 Friction velocity uk : 0.22696E-01 0.21307E+01 Dimensionless distance yplus : 0.22127E-01 0.20922E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -2.834386644e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29468E+08 1 0.26669E-09 0.44325E+02 0.26261E+04 c Velocity[X] 0.22175E+02 c Velocity[Y] 0.22150E+02 c Velocity[Z] 0.16008E-04 c Pressure 0.33175E-03 58 0.91879E-04 0.97317E-02 0.22248E+07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -6.5522 15.397 5.6129 8.0076 v Velocity[Y] -10.38 12.013 -0.14303 -0.00067483 v Velocity[Z] -3.112 2.9745 3.5362e-06 -5.3857e-08 v ǁVelocityǁ 0.00071599 16.336 6.3644 8.0106 v Pressure -1.4964e+05 1.1932e+05 -5663.6 -4066.9 v TurbVisc 9.2096e-19 0.004965 7.0502e-05 3.1883e-06 v CourantNb 9.9031e-08 0.011761 0.00016632 4.8835e-06 v FourierNb 1.2425e-07 0.046901 0.00014513 1.5133e-07 v total_pressure -48314 2.2065e+05 95661 97258 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0922 0.112 0.0033041 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2249e-07 0.052118 0.00031145 5.0349e-06 INSTANT 0.874882000E-01 TIME STEP NUMBER 55080 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283236932E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.583618809E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.23468E-01 0.21309E+01 Friction velocity uk : 0.23468E-01 0.21309E+01 Dimensionless distance yplus : 0.22700E-01 0.20923E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -2.609622336e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29468E+08 1 0.26597E-09 0.44081E+02 0.26189E+04 c Velocity[X] 0.22051E+02 c Velocity[Y] 0.22030E+02 c Velocity[Z] 0.15953E-04 c Pressure 0.33248E-03 70 0.71658E-04 0.97091E-02 0.18064E+07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -6.5961 15.442 5.6128 8.0076 v Velocity[Y] -10.38 12.013 -0.14302 -0.00067463 v Velocity[Z] -3.1117 2.9745 3.535e-06 -5.3857e-08 v ǁVelocityǁ 0.00062363 16.39 6.365 8.0107 v Pressure -1.5271e+05 1.1659e+05 -7692.1 -5226.1 v TurbVisc 7.4406e-19 0.004965 7.0825e-05 3.2063e-06 v CourantNb 8.7715e-08 0.011761 0.00016631 4.8835e-06 v FourierNb 1.2425e-07 0.046902 0.00014513 1.5147e-07 v total_pressure -51390 2.1792e+05 93633 96099 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0923 0.1119 0.0033006 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2249e-07 0.052119 0.00031145 5.035e-06 INSTANT 0.874883000E-01 TIME STEP NUMBER 55081 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283236087E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.584361795E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.16545E-01 0.21308E+01 Friction velocity uk : 0.16545E-01 0.21308E+01 Dimensionless distance yplus : 0.16027E-01 0.20923E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -2.360319610e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29468E+08 1 0.26526E-09 0.43839E+02 0.26116E+04 c Velocity[X] 0.21928E+02 c Velocity[Y] 0.21911E+02 c Velocity[Z] 0.15941E-04 c Pressure 0.33184E-03 11 0.81122E-04 0.96477E-02 0.14320E+07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -6.6394 15.486 5.6127 8.0076 v Velocity[Y] -10.38 12.013 -0.14301 -0.0006745 v Velocity[Z] -3.1114 2.9746 3.5339e-06 -5.3857e-08 v ǁVelocityǁ 0.0005682 16.443 6.3656 8.0107 v Pressure -1.5569e+05 1.1386e+05 -9598.7 -6281.2 v TurbVisc 6.9779e-19 0.0049651 7.1145e-05 3.2241e-06 v CourantNb 7.4257e-08 0.011761 0.00016631 4.8835e-06 v FourierNb 1.2425e-07 0.046901 0.00014514 1.516e-07 v total_pressure -54368 2.1519e+05 91726 95044 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0923 0.1118 0.0032973 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2249e-07 0.052118 0.00031145 5.0351e-06 INSTANT 0.874884000E-01 TIME STEP NUMBER 55082 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283235030E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.585021531E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.16319E-01 0.21305E+01 Friction velocity uk : 0.16319E-01 0.21305E+01 Dimensionless distance yplus : 0.15786E-01 0.20920E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -2.060581254e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29468E+08 1 0.26456E-09 0.43608E+02 0.26048E+04 c Velocity[X] 0.21812E+02 c Velocity[Y] 0.21797E+02 c Velocity[Z] 0.15933E-04 c Pressure 0.33003E-03 28 0.87663E-04 0.95529E-02 0.13760E+07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -6.6822 15.531 5.6126 8.0076 v Velocity[Y] -10.379 12.011 -0.143 -0.00067442 v Velocity[Z] -3.1111 2.9746 3.5328e-06 -5.3857e-08 v ǁVelocityǁ 0.00052275 16.496 6.3663 8.0107 v Pressure -1.5855e+05 1.1117e+05 -11872 -7383.6 v TurbVisc 8.3776e-19 0.0049651 7.1462e-05 3.2418e-06 v CourantNb 7.0315e-08 0.011761 0.00016631 4.8835e-06 v FourierNb 1.2425e-07 0.046899 0.00014514 1.5173e-07 v total_pressure -57222 2.1249e+05 89453 93941 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.092 0.11171 0.0032942 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2248e-07 0.052115 0.00031145 5.0352e-06 INSTANT 0.874885000E-01 TIME STEP NUMBER 55083 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283233858E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.585613309E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.17831E-01 0.21300E+01 Friction velocity uk : 0.17831E-01 0.21300E+01 Dimensionless distance yplus : 0.17248E-01 0.20914E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.786328827e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29467E+08 1 0.26386E-09 0.43378E+02 0.25979E+04 c Velocity[X] 0.21695E+02 c Velocity[Y] 0.21683E+02 c Velocity[Z] 0.15910E-04 c Pressure 0.32933E-03 42 0.68959E-04 0.94915E-02 0.11506E+07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -6.7243 15.576 5.6125 8.0075 v Velocity[Y] -10.379 12.01 -0.14298 -0.00067416 v Velocity[Z] -3.1108 2.9747 3.5317e-06 -5.3857e-08 v ǁVelocityǁ 0.00050028 16.547 6.3669 8.0107 v Pressure -1.6131e+05 1.0853e+05 -13813 -8451.7 v TurbVisc 4.9069e-19 0.0049651 7.1777e-05 3.2595e-06 v CourantNb 7.4393e-08 0.011761 0.00016631 4.8835e-06 v FourierNb 1.2425e-07 0.046895 0.00014515 1.5187e-07 v total_pressure -59984 2.0985e+05 87512 92873 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0914 0.11164 0.0032915 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2248e-07 0.05211 0.00031145 5.0354e-06 INSTANT 0.874886000E-01 TIME STEP NUMBER 55084 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283232490E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.586294795E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.16267E-01 0.21292E+01 Friction velocity uk : 0.16267E-01 0.21292E+01 Dimensionless distance yplus : 0.15875E-01 0.20907E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.445029834e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29467E+08 1 0.26318E-09 0.43150E+02 0.25910E+04 c Velocity[X] 0.21580E+02 c Velocity[Y] 0.21570E+02 c Velocity[Z] 0.15917E-04 c Pressure 0.32652E-03 11 0.80912E-04 0.93708E-02 0.99128E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -6.7657 15.622 5.6124 8.0075 v Velocity[Y] -10.379 12.007 -0.14297 -0.00067371 v Velocity[Z] -3.1104 2.9747 3.5305e-06 -5.3857e-08 v ǁVelocityǁ 0.00049348 16.598 6.3676 8.0107 v Pressure -1.6396e+05 1.0597e+05 -15655 -9477 v TurbVisc 4.5808e-19 0.0049651 7.209e-05 3.277e-06 v CourantNb 8.7095e-08 0.011761 0.00016631 4.8835e-06 v FourierNb 1.2425e-07 0.046889 0.00014515 1.52e-07 v total_pressure -62639 2.0729e+05 85670 91848 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0907 0.11157 0.0032891 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2248e-07 0.052103 0.00031146 5.0355e-06 INSTANT 0.874887000E-01 TIME STEP NUMBER 55085 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283230883E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.586905292E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.94877E-02 0.21282E+01 Friction velocity uk : 0.94877E-02 0.21282E+01 Dimensionless distance yplus : 0.92495E-02 0.20897E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.090670057e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29467E+08 1 0.26252E-09 0.42935E+02 0.25846E+04 c Velocity[X] 0.21472E+02 c Velocity[Y] 0.21464E+02 c Velocity[Z] 0.15903E-04 c Pressure 0.32229E-03 47 0.76316E-04 0.92107E-02 0.10283E+07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -6.8065 15.667 5.6123 8.0075 v Velocity[Y] -10.378 12.004 -0.14296 -0.00067353 v Velocity[Z] -3.1101 2.9747 3.5294e-06 -5.3857e-08 v ǁVelocityǁ 0.00048757 16.647 6.3683 8.0107 v Pressure -1.6651e+05 1.0351e+05 -17947 -10607 v TurbVisc 5.9233e-19 0.0049651 7.2399e-05 3.2945e-06 v CourantNb 1.1121e-07 0.011761 0.00016631 4.8835e-06 v FourierNb 1.2425e-07 0.046882 0.00014515 1.5213e-07 v total_pressure -65185 2.0484e+05 83378 90718 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0897 0.11152 0.003287 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2248e-07 0.052094 0.00031146 5.0356e-06 INSTANT 0.874888000E-01 TIME STEP NUMBER 55086 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283229213E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.587473665E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.14919E-01 0.21271E+01 Friction velocity uk : 0.14919E-01 0.21271E+01 Dimensionless distance yplus : 0.14575E-01 0.20886E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -7.946210207e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29467E+08 1 0.26185E-09 0.42722E+02 0.25781E+04 c Velocity[X] 0.21364E+02 c Velocity[Y] 0.21358E+02 c Velocity[Z] 0.15858E-04 c Pressure 0.31905E-03 31 0.64273E-04 0.90805E-02 0.89548E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -6.8467 15.713 5.6122 8.0074 v Velocity[Y] -10.378 12.001 -0.14294 -0.00067334 v Velocity[Z] -3.1098 2.9748 3.5283e-06 -5.3857e-08 v ǁVelocityǁ 0.00048662 16.696 6.369 8.0107 v Pressure -1.6896e+05 1.0117e+05 -19843 -11721 v TurbVisc 4.6027e-19 0.0049652 7.2707e-05 3.3119e-06 v CourantNb 5.8026e-08 0.011762 0.00016631 4.8835e-06 v FourierNb 1.2425e-07 0.046874 0.00014516 1.5226e-07 v total_pressure -67635 2.0249e+05 81482 89604 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0886 0.11147 0.0032853 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2248e-07 0.052084 0.00031147 5.0357e-06 INSTANT 0.874889000E-01 TIME STEP NUMBER 55087 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283227344E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.588148645E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.16775E-01 0.21258E+01 Friction velocity uk : 0.16775E-01 0.21258E+01 Dimensionless distance yplus : 0.16133E-01 0.20873E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -4.483302905e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29467E+08 1 0.26120E-09 0.42512E+02 0.25718E+04 c Velocity[X] 0.21259E+02 c Velocity[Y] 0.21253E+02 c Velocity[Z] 0.15834E-04 c Pressure 0.31386E-03 11 0.81813E-04 0.88965E-02 0.76496E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -6.8863 15.758 5.6121 8.0074 v Velocity[Y] -10.377 11.997 -0.14293 -0.00067326 v Velocity[Z] -3.1095 2.9748 3.5271e-06 -5.3857e-08 v ǁVelocityǁ 0.00050414 16.743 6.3697 8.0107 v Pressure -1.7129e+05 98935 -21668 -12754 v TurbVisc 1.2556e-20 0.0049652 7.3012e-05 3.3291e-06 v CourantNb 1.0498e-07 0.011762 0.00016631 4.8835e-06 v FourierNb 1.2425e-07 0.046864 0.00014516 1.5239e-07 v total_pressure -69964 2.0026e+05 79657 88571 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0873 0.11144 0.0032838 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2247e-07 0.052072 0.00031147 5.0359e-06 INSTANT 0.874890000E-01 TIME STEP NUMBER 55088 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283225266E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.588769819E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.14825E-01 0.21243E+01 Friction velocity uk : 0.14825E-01 0.21243E+01 Dimensionless distance yplus : 0.14258E-01 0.20859E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -9.056523929e-03 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29467E+08 1 0.26056E-09 0.42312E+02 0.25657E+04 c Velocity[X] 0.21159E+02 c Velocity[Y] 0.21153E+02 c Velocity[Z] 0.15782E-04 c Pressure 0.30775E-03 22 0.83101E-04 0.86885E-02 0.77699E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -6.9254 15.804 5.612 8.0073 v Velocity[Y] -10.377 11.993 -0.14292 -0.00067323 v Velocity[Z] -3.1092 2.9748 3.526e-06 -5.3857e-08 v ǁVelocityǁ 0.00051124 16.789 6.3704 8.0106 v Pressure -1.7351e+05 96803 -23861 -13838 v TurbVisc 1.0516e-19 0.0049652 7.3315e-05 3.3463e-06 v CourantNb 6.316e-08 0.011762 0.00016631 4.8835e-06 v FourierNb 1.2425e-07 0.046854 0.00014516 1.5252e-07 v total_pressure -72183 1.9813e+05 77464 87487 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0859 0.1114 0.0032826 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2247e-07 0.052059 0.00031148 5.036e-06 INSTANT 0.874891000E-01 TIME STEP NUMBER 55089 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283223080E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.589372366E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13069E-01 0.21228E+01 Friction velocity uk : 0.13069E-01 0.21228E+01 Dimensionless distance yplus : 0.12569E-01 0.20844E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.574584099e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29466E+08 1 0.25992E-09 0.42113E+02 0.25597E+04 c Velocity[X] 0.21060E+02 c Velocity[Y] 0.21054E+02 c Velocity[Z] 0.15698E-04 c Pressure 0.30279E-03 34 0.63635E-04 0.85149E-02 0.67054E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -6.964 15.849 5.612 8.0073 v Velocity[Y] -10.376 11.989 -0.1429 -0.00067304 v Velocity[Z] -3.1088 2.9749 3.5249e-06 -5.3857e-08 v ǁVelocityǁ 0.00052145 16.834 6.3711 8.0106 v Pressure -1.7559e+05 94779 -25694 -14873 v TurbVisc 1.4431e-20 0.0049652 7.3615e-05 3.3634e-06 v CourantNb 1.2768e-07 0.011762 0.00016632 4.8834e-06 v FourierNb 1.2425e-07 0.046843 0.00014517 1.5265e-07 v total_pressure -74269 1.961e+05 75631 86452 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0844 0.11139 0.0032817 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2247e-07 0.052046 0.00031148 5.0361e-06 INSTANT 0.874892000E-01 TIME STEP NUMBER 55090 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283220707E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.590056991E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11645E-01 0.21212E+01 Friction velocity uk : 0.11645E-01 0.21212E+01 Dimensionless distance yplus : 0.11199E-01 0.20829E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 4.578434540e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29466E+08 1 0.25929E-09 0.41917E+02 0.25537E+04 c Velocity[X] 0.20962E+02 c Velocity[Y] 0.20955E+02 c Velocity[Z] 0.15625E-04 c Pressure 0.29688E-03 11 0.76301E-04 0.83161E-02 0.60498E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -7.0022 15.894 5.6119 8.0072 v Velocity[Y] -10.375 11.985 -0.14289 -0.00067263 v Velocity[Z] -3.1085 2.9749 3.5238e-06 -5.3857e-08 v ǁVelocityǁ 0.00053706 16.879 6.3719 8.0106 v Pressure -1.7755e+05 92852 -27498 -15879 v TurbVisc 2.216e-20 0.0049652 7.3913e-05 3.3805e-06 v CourantNb 9.3075e-08 0.011762 0.00016632 4.8834e-06 v FourierNb 1.2425e-07 0.046831 0.00014517 1.5277e-07 v total_pressure -76229 1.9418e+05 73827 85446 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0829 0.1114 0.003281 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2246e-07 0.052031 0.00031149 5.0362e-06 INSTANT 0.874893000E-01 TIME STEP NUMBER 55091 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283218098E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.590707916E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.94854E-02 0.21196E+01 Friction velocity uk : 0.94854E-02 0.21196E+01 Dimensionless distance yplus : 0.91224E-02 0.20812E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 7.311755626e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29466E+08 1 0.25867E-09 0.41724E+02 0.25478E+04 c Velocity[X] 0.20867E+02 c Velocity[Y] 0.20858E+02 c Velocity[Z] 0.15524E-04 c Pressure 0.29118E-03 38 0.70048E-04 0.81254E-02 0.65600E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -7.04 15.939 5.6118 8.0072 v Velocity[Y] -10.375 11.98 -0.14288 -0.00067254 v Velocity[Z] -3.1082 2.975 3.5226e-06 -5.3857e-08 v ǁVelocityǁ 0.00053689 16.922 6.3726 8.0106 v Pressure -1.7939e+05 91011 -29541 -16998 v TurbVisc 2.497e-20 0.0049653 7.4209e-05 3.3975e-06 v CourantNb 8.0127e-08 0.011763 0.00016632 4.8834e-06 v FourierNb 1.2425e-07 0.046819 0.00014517 1.529e-07 v total_pressure -78062 1.9234e+05 71784 84327 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0812 0.11142 0.0032806 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2246e-07 0.052016 0.0003115 5.0363e-06 INSTANT 0.874894000E-01 TIME STEP NUMBER 55092 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283215417E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.591357052E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.70992E-02 0.21179E+01 Friction velocity uk : 0.70992E-02 0.21179E+01 Dimensionless distance yplus : 0.68275E-02 0.20796E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 9.077786439e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29466E+08 1 0.25806E-09 0.41531E+02 0.25419E+04 c Velocity[X] 0.20771E+02 c Velocity[Y] 0.20760E+02 c Velocity[Z] 0.15385E-04 c Pressure 0.28681E-03 25 0.59190E-04 0.79733E-02 0.56727E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -7.0776 15.984 5.6118 8.0071 v Velocity[Y] -10.374 11.976 -0.14287 -0.00067248 v Velocity[Z] -3.1079 2.975 3.5215e-06 -5.3857e-08 v ǁVelocityǁ 0.0005335 16.965 6.3734 8.0106 v Pressure -1.8111e+05 89250 -31347 -18057 v TurbVisc 2.3191e-19 0.0049653 7.4503e-05 3.4144e-06 v CourantNb 1.0035e-07 0.011763 0.00016633 4.8834e-06 v FourierNb 1.2425e-07 0.046807 0.00014518 1.5303e-07 v total_pressure -79782 1.9058e+05 69978 83268 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0796 0.11144 0.0032803 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2245e-07 0.052001 0.0003115 5.0364e-06 INSTANT 0.874895000E-01 TIME STEP NUMBER 55093 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283212553E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.592038673E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.38813E-02 0.21163E+01 Friction velocity uk : 0.38813E-02 0.21163E+01 Dimensionless distance yplus : 0.37328E-02 0.20780E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.097259473e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29466E+08 1 0.25745E-09 0.41340E+02 0.25361E+04 c Velocity[X] 0.20677E+02 c Velocity[Y] 0.20663E+02 c Velocity[Z] 0.15237E-04 c Pressure 0.28270E-03 11 0.78275E-04 0.78301E-02 0.52681E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -7.1148 16.028 5.6117 8.0071 v Velocity[Y] -10.374 11.972 -0.14286 -0.00067253 v Velocity[Z] -3.1076 2.975 3.5204e-06 -5.3857e-08 v ǁVelocityǁ 0.00052586 17.007 6.3742 8.0105 v Pressure -1.8272e+05 87562 -33183 -19101 v TurbVisc 3.7899e-19 0.0049653 7.4795e-05 3.4312e-06 v CourantNb 1.1904e-07 0.011763 0.00016633 4.8834e-06 v FourierNb 1.2425e-07 0.046795 0.00014518 1.5315e-07 v total_pressure -81398 1.8889e+05 68142 82224 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.078 0.11148 0.0032802 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2245e-07 0.051987 0.00031151 5.0366e-06 INSTANT 0.874896000E-01 TIME STEP NUMBER 55094 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283209468E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.592709105E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.68652E-02 0.21148E+01 Friction velocity uk : 0.68652E-02 0.21148E+01 Dimensionless distance yplus : 0.66025E-02 0.20765E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.256046603e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29465E+08 1 0.25686E-09 0.41144E+02 0.25301E+04 c Velocity[X] 0.20582E+02 c Velocity[Y] 0.20562E+02 c Velocity[Z] 0.15068E-04 c Pressure 0.27965E-03 57 0.77344E-04 0.77172E-02 0.52536E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -7.1519 16.071 5.6117 8.007 v Velocity[Y] -10.373 11.968 -0.14285 -0.00067263 v Velocity[Z] -3.1072 2.9751 3.5193e-06 -5.3857e-08 v ǁVelocityǁ 0.00049817 17.049 6.375 8.0105 v Pressure -1.8448e+05 85954 -34985 -20149 v TurbVisc 3.6079e-19 0.0049653 7.5084e-05 3.4479e-06 v CourantNb 5.8012e-08 0.011763 0.00016633 4.8834e-06 v FourierNb 1.2425e-07 0.046783 0.00014518 1.5328e-07 v total_pressure -83158 1.8728e+05 66340 81176 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0765 0.11152 0.0032801 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2244e-07 0.051973 0.00031152 5.0367e-06 INSTANT 0.874897000E-01 TIME STEP NUMBER 55095 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283206288E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.593387992E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.95736E-02 0.21133E+01 Friction velocity uk : 0.95736E-02 0.21133E+01 Dimensionless distance yplus : 0.92073E-02 0.20750E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.332411445e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29465E+08 1 0.25626E-09 0.40949E+02 0.25241E+04 c Velocity[X] 0.20487E+02 c Velocity[Y] 0.20462E+02 c Velocity[Z] 0.14869E-04 c Pressure 0.27716E-03 31 0.59230E-04 0.76210E-02 0.46898E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -7.1888 16.114 5.6116 8.0069 v Velocity[Y] -10.373 11.964 -0.14285 -0.00067257 v Velocity[Z] -3.1069 2.9751 3.5181e-06 -5.3857e-08 v ǁVelocityǁ 0.00046939 17.09 6.3757 8.0105 v Pressure -1.8617e+05 84422 -36770 -21164 v TurbVisc 3.7662e-19 0.0049653 7.5372e-05 3.4646e-06 v CourantNb 7.0807e-08 0.011763 0.00016634 4.8834e-06 v FourierNb 1.2425e-07 0.046772 0.00014519 1.5341e-07 v total_pressure -84840 1.8575e+05 64555 80161 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.075 0.11156 0.00328 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2244e-07 0.051959 0.00031153 5.0368e-06 INSTANT 0.874898000E-01 TIME STEP NUMBER 55096 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283202924E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.594039475E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.44550E-02 0.21119E+01 Friction velocity uk : 0.44550E-02 0.21119E+01 Dimensionless distance yplus : 0.44037E-02 0.20737E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.398452938e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29465E+08 1 0.25568E-09 0.40758E+02 0.25182E+04 c Velocity[X] 0.20393E+02 c Velocity[Y] 0.20364E+02 c Velocity[Z] 0.14637E-04 c Pressure 0.27539E-03 11 0.78074E-04 0.75454E-02 0.42598E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -7.2255 16.157 5.6116 8.0069 v Velocity[Y] -10.372 11.961 -0.14285 -0.00067227 v Velocity[Z] -3.1066 2.9752 3.517e-06 -5.3857e-08 v ǁVelocityǁ 0.00044492 17.131 6.3765 8.0104 v Pressure -1.8777e+05 82960 -38599 -22139 v TurbVisc 3.9182e-19 0.0049654 7.5657e-05 3.4812e-06 v CourantNb 1.1227e-07 0.011763 0.00016634 4.8834e-06 v FourierNb 1.2425e-07 0.046762 0.00014519 1.5353e-07 v total_pressure -86442 1.8428e+05 62726 79186 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0737 0.11158 0.0032798 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2243e-07 0.051947 0.00031153 5.0369e-06 INSTANT 0.874899000E-01 TIME STEP NUMBER 55097 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283199332E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.594695851E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.26179E-02 0.21107E+01 Friction velocity uk : 0.26179E-02 0.21107E+01 Dimensionless distance yplus : 0.25177E-02 0.20725E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.410401718e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29464E+08 1 0.25510E-09 0.40557E+02 0.25120E+04 c Velocity[X] 0.20297E+02 c Velocity[Y] 0.20260E+02 c Velocity[Z] 0.14401E-04 c Pressure 0.27448E-03 28 0.66219E-04 0.74938E-02 0.46994E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -7.262 16.199 5.6116 8.0068 v Velocity[Y] -10.372 11.958 -0.14284 -0.0006723 v Velocity[Z] -3.1063 2.9752 3.5159e-06 -5.3857e-08 v ǁVelocityǁ 0.00043733 17.172 6.3773 8.0104 v Pressure -1.8927e+05 81571 -40179 -23221 v TurbVisc 1.8796e-19 0.0049654 7.594e-05 3.4978e-06 v CourantNb 1.1176e-07 0.011763 0.00016635 4.8833e-06 v FourierNb 1.2425e-07 0.046753 0.00014519 1.5365e-07 v total_pressure -87944 1.829e+05 61146 78104 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0725 0.11163 0.0032796 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2243e-07 0.051936 0.00031154 5.037e-06 INSTANT 0.874900000E-01 TIME STEP NUMBER 55098 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283195670E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.595359627E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.75678E-02 0.21095E+01 Friction velocity uk : 0.75678E-02 0.21095E+01 Dimensionless distance yplus : 0.72782E-02 0.20714E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.386739367e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29464E+08 1 0.25454E-09 0.40362E+02 0.25059E+04 c Velocity[X] 0.20203E+02 c Velocity[Y] 0.20159E+02 c Velocity[Z] 0.14141E-04 c Pressure 0.27259E-03 28 0.56063E-04 0.74165E-02 0.42047E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -7.2985 16.24 5.6116 8.0067 v Velocity[Y] -10.372 11.955 -0.14284 -0.00067238 v Velocity[Z] -3.106 2.9752 3.5148e-06 -5.3857e-08 v ǁVelocityǁ 0.0004627 17.212 6.3781 8.0103 v Pressure -1.9068e+05 80254 -41957 -24265 v TurbVisc 3.6165e-19 0.0049654 7.6221e-05 3.5143e-06 v CourantNb 1.2697e-07 0.011763 0.00016635 4.8833e-06 v FourierNb 1.2425e-07 0.046745 0.0001452 1.5378e-07 v total_pressure -89353 1.8158e+05 59368 77060 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0714 0.11165 0.0032792 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2242e-07 0.051926 0.00031155 5.0371e-06 INSTANT 0.874901000E-01 TIME STEP NUMBER 55099 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283191822E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.595945628E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.45432E-02 0.21086E+01 Friction velocity uk : 0.45432E-02 0.21086E+01 Dimensionless distance yplus : 0.43694E-02 0.20705E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.324994600e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29464E+08 1 0.25397E-09 0.40174E+02 0.25001E+04 c Velocity[X] 0.20113E+02 c Velocity[Y] 0.20061E+02 c Velocity[Z] 0.13838E-04 c Pressure 0.27122E-03 11 0.83461E-04 0.73540E-02 0.37395E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -7.3347 16.281 5.6115 8.0066 v Velocity[Y] -10.371 11.954 -0.14284 -0.00067258 v Velocity[Z] -3.1056 2.9753 3.5136e-06 -5.3857e-08 v ǁVelocityǁ 0.00055466 17.253 6.3789 8.0103 v Pressure -1.9201e+05 79003 -43767 -25234 v TurbVisc 1.2214e-20 0.0049654 7.6501e-05 3.5307e-06 v CourantNb 1.4929e-07 0.011763 0.00016635 4.8833e-06 v FourierNb 1.2425e-07 0.046738 0.0001452 1.539e-07 v total_pressure -90687 1.8033e+05 57558 76091 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0705 0.11166 0.0032786 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2241e-07 0.051918 0.00031155 5.0372e-06 INSTANT 0.874902000E-01 TIME STEP NUMBER 55100 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283187776E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.596545501E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11795E-01 0.21080E+01 Friction velocity uk : 0.11795E-01 0.21080E+01 Dimensionless distance yplus : 0.11344E-01 0.20698E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.213742269e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29463E+08 1 0.25342E-09 0.39977E+02 0.24940E+04 c Velocity[X] 0.20019E+02 c Velocity[Y] 0.19958E+02 c Velocity[Z] 0.13550E-04 c Pressure 0.27005E-03 59 0.72944E-04 0.72972E-02 0.38874E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -7.3709 16.321 5.6115 8.0066 v Velocity[Y] -10.371 11.952 -0.14284 -0.00067283 v Velocity[Z] -3.1053 2.9753 3.5125e-06 -5.3857e-08 v ǁVelocityǁ 0.00072338 17.294 6.3797 8.0103 v Pressure -1.9329e+05 77828 -45136 -26235 v TurbVisc 3.4572e-19 0.0049654 7.6778e-05 3.547e-06 v CourantNb 1.3597e-07 0.011764 0.00016635 4.8833e-06 v FourierNb 1.2425e-07 0.046733 0.0001452 1.5402e-07 v total_pressure -91967 1.7915e+05 56189 75090 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0698 0.11166 0.0032779 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2241e-07 0.051913 0.00031156 5.0373e-06 INSTANT 0.874903000E-01 TIME STEP NUMBER 55101 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283183639E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.597144351E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.14875E-01 0.21074E+01 Friction velocity uk : 0.14875E-01 0.21074E+01 Dimensionless distance yplus : 0.14323E-01 0.20692E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.098217694e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29463E+08 1 0.25288E-09 0.39789E+02 0.24881E+04 c Velocity[X] 0.19929E+02 c Velocity[Y] 0.19860E+02 c Velocity[Z] 0.13250E-04 c Pressure 0.26660E-03 30 0.56490E-04 0.71800E-02 0.35285E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -7.4069 16.361 5.6115 8.0065 v Velocity[Y] -10.371 11.951 -0.14285 -0.00067288 v Velocity[Z] -3.105 2.9753 3.5114e-06 -5.3857e-08 v ǁVelocityǁ 0.00093607 17.335 6.3805 8.0102 v Pressure -1.945e+05 76735 -46863 -27211 v TurbVisc 3.9832e-19 0.0049655 7.7053e-05 3.5633e-06 v CourantNb 1.3636e-07 0.011763 0.00016636 4.8833e-06 v FourierNb 1.2425e-07 0.046729 0.00014521 1.5414e-07 v total_pressure -93171 1.7806e+05 54462 74114 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0692 0.11164 0.0032769 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.224e-07 0.051908 0.00031156 5.0374e-06 INSTANT 0.874904000E-01 TIME STEP NUMBER 55102 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283179319E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.597636449E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11358E-01 0.21070E+01 Friction velocity uk : 0.11358E-01 0.21070E+01 Dimensionless distance yplus : 0.10936E-01 0.20689E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 9.428361164e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29462E+08 1 0.25233E-09 0.39613E+02 0.24826E+04 c Velocity[X] 0.19845E+02 c Velocity[Y] 0.19767E+02 c Velocity[Z] 0.12909E-04 c Pressure 0.26357E-03 11 0.81125E-04 0.70747E-02 0.31759E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -7.4427 16.401 5.6115 8.0064 v Velocity[Y] -10.371 11.951 -0.14286 -0.00067269 v Velocity[Z] -3.1047 2.9754 3.5103e-06 -5.3857e-08 v ǁVelocityǁ 0.0011947 17.376 6.3813 8.0102 v Pressure -1.9563e+05 75695 -48630 -28127 v TurbVisc 3.0346e-20 0.0049655 7.7326e-05 3.5795e-06 v CourantNb 1.3873e-07 0.011763 0.00016636 4.8833e-06 v FourierNb 1.2425e-07 0.046727 0.00014521 1.5427e-07 v total_pressure -94301 1.7702e+05 52695 73198 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0689 0.11161 0.0032756 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2239e-07 0.051905 0.00031156 5.0375e-06 INSTANT 0.874905000E-01 TIME STEP NUMBER 55103 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283174791E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.598140356E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13329E-01 0.21070E+01 Friction velocity uk : 0.13329E-01 0.21070E+01 Dimensionless distance yplus : 0.12834E-01 0.20689E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 7.439126812e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29462E+08 1 0.25180E-09 0.39428E+02 0.24768E+04 c Velocity[X] 0.19759E+02 c Velocity[Y] 0.19669E+02 c Velocity[Z] 0.12604E-04 c Pressure 0.26058E-03 30 0.62722E-04 0.69714E-02 0.34612E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -7.4783 16.44 5.6115 8.0063 v Velocity[Y] -10.372 11.951 -0.14286 -0.00067284 v Velocity[Z] -3.1044 2.9754 3.5092e-06 -5.3857e-08 v ǁVelocityǁ 0.0015029 17.417 6.3821 8.0101 v Pressure -1.9669e+05 74704 -49863 -29119 v TurbVisc 3.2931e-19 0.0049655 7.7598e-05 3.5957e-06 v CourantNb 1.3489e-07 0.011763 0.00016636 4.8832e-06 v FourierNb 1.2425e-07 0.046727 0.00014521 1.5439e-07 v total_pressure -95365 1.7603e+05 51462 72206 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0689 0.11157 0.0032741 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2239e-07 0.051906 0.00031157 5.0376e-06 INSTANT 0.874906000E-01 TIME STEP NUMBER 55104 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283170204E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.598634213E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.96426E-02 0.21071E+01 Friction velocity uk : 0.96426E-02 0.21071E+01 Dimensionless distance yplus : 0.92846E-02 0.20689E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 5.784935505e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29462E+08 1 0.25128E-09 0.39260E+02 0.24715E+04 c Velocity[X] 0.19680E+02 c Velocity[Y] 0.19581E+02 c Velocity[Z] 0.12296E-04 c Pressure 0.25517E-03 11 0.99701E-04 0.68046E-02 0.31053E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -7.5138 16.479 5.6115 8.0062 v Velocity[Y] -10.372 11.952 -0.14287 -0.00067327 v Velocity[Z] -3.104 2.9754 3.508e-06 -5.3857e-08 v ǁVelocityǁ 0.001833 17.458 6.3828 8.01 v Pressure -1.9771e+05 73755 -51695 -30079 v TurbVisc 6.1904e-20 0.0049655 7.7867e-05 3.6118e-06 v CourantNb 1.3597e-07 0.011763 0.00016636 4.8832e-06 v FourierNb 1.2425e-07 0.046728 0.00014521 1.5451e-07 v total_pressure -96381 1.7508e+05 49630 71246 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0689 0.11151 0.0032723 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2238e-07 0.051907 0.00031157 5.0377e-06 INSTANT 0.874907000E-01 TIME STEP NUMBER 55105 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283165419E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.599017509E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.16233E-01 0.21074E+01 Friction velocity uk : 0.16233E-01 0.21074E+01 Dimensionless distance yplus : 0.15630E-01 0.20693E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 3.437774292e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29461E+08 1 0.25076E-09 0.39087E+02 0.24661E+04 c Velocity[X] 0.19598E+02 c Velocity[Y] 0.19488E+02 c Velocity[Z] 0.11977E-04 c Pressure 0.25151E-03 76 0.77537E-04 0.66854E-02 0.30140E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -7.549 16.518 5.6115 8.0061 v Velocity[Y] -10.372 11.953 -0.14289 -0.00067316 v Velocity[Z] -3.1037 2.9755 3.5069e-06 -5.3857e-08 v ǁVelocityǁ 0.002213 17.5 6.3836 8.01 v Pressure -1.9869e+05 72843 -52887 -30973 v TurbVisc 2.9987e-19 0.0049655 7.8134e-05 3.6279e-06 v CourantNb 1.3406e-07 0.011763 0.00016636 4.8832e-06 v FourierNb 1.2425e-07 0.046731 0.00014521 1.5463e-07 v total_pressure -97365 1.7417e+05 48438 70352 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0693 0.11144 0.0032703 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2237e-07 0.051912 0.00031157 5.0378e-06 INSTANT 0.874908000E-01 TIME STEP NUMBER 55106 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283160566E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.599439923E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.16725E-01 0.21079E+01 Friction velocity uk : 0.16725E-01 0.21079E+01 Dimensionless distance yplus : 0.16104E-01 0.20698E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.543712039e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29461E+08 1 0.25025E-09 0.38921E+02 0.24609E+04 c Velocity[X] 0.19521E+02 c Velocity[Y] 0.19400E+02 c Velocity[Z] 0.11688E-04 c Pressure 0.24583E-03 136 0.86790E-04 0.65136E-02 0.29438E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -7.5842 16.556 5.6115 8.006 v Velocity[Y] -10.373 11.955 -0.1429 -0.00067373 v Velocity[Z] -3.1034 2.9755 3.5058e-06 -5.3857e-08 v ǁVelocityǁ 0.0026033 17.541 6.3844 8.0099 v Pressure -1.9965e+05 71947 -54516 -31925 v TurbVisc 2.5416e-19 0.0049656 7.84e-05 3.6439e-06 v CourantNb 1.3381e-07 0.011762 0.00016636 4.8832e-06 v FourierNb 1.2425e-07 0.046735 0.00014521 1.5475e-07 v total_pressure -98324 1.7327e+05 46809 69400 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0698 0.11135 0.003268 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2236e-07 0.051916 0.00031157 5.0379e-06 INSTANT 0.874909000E-01 TIME STEP NUMBER 55107 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283155546E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.599758951E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.18945E-01 0.21086E+01 Friction velocity uk : 0.18945E-01 0.21086E+01 Dimensionless distance yplus : 0.18242E-01 0.20705E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -4.632706220e-03 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29460E+08 1 0.24973E-09 0.38759E+02 0.24557E+04 c Velocity[X] 0.19444E+02 c Velocity[Y] 0.19314E+02 c Velocity[Z] 0.11388E-04 c Pressure 0.24138E-03 49 0.95603E-04 0.63754E-02 0.23313E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -7.6191 16.594 5.6115 8.0059 v Velocity[Y] -10.373 11.958 -0.14291 -0.0006735 v Velocity[Z] -3.1031 2.9756 3.5047e-06 -5.3857e-08 v ǁVelocityǁ 0.0030145 17.583 6.3852 8.0098 v Pressure -2.006e+05 71070 -55925 -32674 v TurbVisc 6.9017e-20 0.0049656 7.8663e-05 3.6598e-06 v CourantNb 1.3264e-07 0.011762 0.00016635 4.8832e-06 v FourierNb 1.2425e-07 0.046741 0.00014522 1.5487e-07 v total_pressure -99276 1.7239e+05 45400 68651 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0705 0.11125 0.0032655 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2236e-07 0.051924 0.00031157 5.038e-06 INSTANT 0.874910000E-01 TIME STEP NUMBER 55108 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283150323E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.600079108E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.23256E-01 0.21095E+01 Friction velocity uk : 0.23256E-01 0.21095E+01 Dimensionless distance yplus : 0.22393E-01 0.20713E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -2.460129953e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29460E+08 1 0.24923E-09 0.38599E+02 0.24507E+04 c Velocity[X] 0.19370E+02 c Velocity[Y] 0.19228E+02 c Velocity[Z] 0.11118E-04 c Pressure 0.23708E-03 514 0.80021E-04 0.62421E-02 0.27436E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -7.6538 16.632 5.6115 8.0058 v Velocity[Y] -10.374 11.961 -0.14293 -0.00067373 v Velocity[Z] -3.1028 2.9756 3.5035e-06 -5.3857e-08 v ǁVelocityǁ 0.0034421 17.625 6.386 8.0098 v Pressure -2.0156e+05 70209 -57348 -33602 v TurbVisc 3.3721e-20 0.0049656 7.8925e-05 3.6757e-06 v CourantNb 1.3156e-07 0.011762 0.00016635 4.8831e-06 v FourierNb 1.2425e-07 0.046748 0.00014522 1.5498e-07 v total_pressure -1.0023e+05 1.7153e+05 43977 67723 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0713 0.11114 0.0032627 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2235e-07 0.051933 0.00031157 5.0381e-06 INSTANT 0.874911000E-01 TIME STEP NUMBER 55109 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283145013E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.600360647E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.60414E-02 0.21105E+01 Friction velocity uk : 0.60414E-02 0.21105E+01 Dimensionless distance yplus : 0.59717E-02 0.20724E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -4.294727255e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29459E+08 1 0.24873E-09 0.38444E+02 0.24458E+04 c Velocity[X] 0.19297E+02 c Velocity[Y] 0.19146E+02 c Velocity[Z] 0.10866E-04 c Pressure 0.23316E-03 11 0.74471E-04 0.61198E-02 0.20681E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -7.6884 16.67 5.6115 8.0057 v Velocity[Y] -10.374 11.964 -0.14295 -0.00067417 v Velocity[Z] -3.1024 2.9756 3.5024e-06 -5.3857e-08 v ǁVelocityǁ 0.0038704 17.667 6.3867 8.0097 v Pressure -2.0253e+05 69329 -58780 -34326 v TurbVisc 2.8339e-20 0.0049656 7.9185e-05 3.6915e-06 v CourantNb 1.441e-07 0.011762 0.00016635 4.8831e-06 v FourierNb 1.2425e-07 0.046757 0.00014522 1.551e-07 v total_pressure -1.0121e+05 1.7065e+05 42545 66999 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0724 0.111 0.0032596 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2234e-07 0.051943 0.00031157 5.0382e-06 INSTANT 0.874912000E-01 TIME STEP NUMBER 55110 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283139527E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.600616082E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.14442E-01 0.21118E+01 Friction velocity uk : 0.14442E-01 0.21118E+01 Dimensionless distance yplus : 0.13986E-01 0.20736E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -5.972802719e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29459E+08 1 0.24823E-09 0.38285E+02 0.24407E+04 c Velocity[X] 0.19224E+02 c Velocity[Y] 0.19061E+02 c Velocity[Z] 0.10638E-04 c Pressure 0.23041E-03 133 0.73746E-04 0.60289E-02 0.24831E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -7.7228 16.708 5.6115 8.0056 v Velocity[Y] -10.375 11.968 -0.14296 -0.00067415 v Velocity[Z] -3.1021 2.9757 3.5013e-06 -5.3857e-08 v ǁVelocityǁ 0.0039337 17.709 6.3875 8.0096 v Pressure -2.0355e+05 68411 -60000 -35162 v TurbVisc 9.5924e-20 0.0049656 7.9443e-05 3.7073e-06 v CourantNb 1.3579e-07 0.011762 0.00016635 4.8831e-06 v FourierNb 1.2425e-07 0.046766 0.00014522 1.5522e-07 v total_pressure -1.0222e+05 1.6974e+05 41325 66163 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0736 0.11089 0.0032565 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2233e-07 0.051955 0.00031156 5.0383e-06 INSTANT 0.874913000E-01 TIME STEP NUMBER 55111 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283134009E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.600860382E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.17835E-01 0.21130E+01 Friction velocity uk : 0.17835E-01 0.21130E+01 Dimensionless distance yplus : 0.17272E-01 0.20748E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -7.378203981e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29458E+08 1 0.24774E-09 0.38129E+02 0.24358E+04 c Velocity[X] 0.19151E+02 c Velocity[Y] 0.18978E+02 c Velocity[Z] 0.10423E-04 c Pressure 0.22779E-03 128 0.78542E-04 0.59420E-02 0.23321E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -7.757 16.745 5.6115 8.0055 v Velocity[Y] -10.376 11.972 -0.14298 -0.0006747 v Velocity[Z] -3.1018 2.9757 3.5002e-06 -5.3857e-08 v ǁVelocityǁ 0.0038718 17.752 6.3883 8.0095 v Pressure -2.0462e+05 67453 -61405 -36007 v TurbVisc 2.6793e-20 0.0049657 7.9699e-05 3.723e-06 v CourantNb 1.3394e-07 0.011762 0.00016634 4.8831e-06 v FourierNb 1.2425e-07 0.046776 0.00014522 1.5534e-07 v total_pressure -1.033e+05 1.6878e+05 39920 65318 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0748 0.11076 0.0032532 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2232e-07 0.051968 0.00031156 5.0384e-06 INSTANT 0.874914000E-01 TIME STEP NUMBER 55112 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283128359E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.601075598E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.21443E-01 0.21144E+01 Friction velocity uk : 0.21443E-01 0.21144E+01 Dimensionless distance yplus : 0.20735E-01 0.20761E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -8.486119122e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29458E+08 1 0.24726E-09 0.37972E+02 0.24308E+04 c Velocity[X] 0.19077E+02 c Velocity[Y] 0.18895E+02 c Velocity[Z] 0.10221E-04 c Pressure 0.22623E-03 120 0.88069E-04 0.58836E-02 0.18064E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -7.7911 16.782 5.6115 8.0054 v Velocity[Y] -10.376 11.975 -0.143 -0.00067453 v Velocity[Z] -3.1015 2.9757 3.4991e-06 -5.3857e-08 v ǁVelocityǁ 0.004171 17.794 6.3891 8.0095 v Pressure -2.0592e+05 66444 -62674 -36653 v TurbVisc 4.2127e-20 0.0049657 7.9953e-05 3.7386e-06 v CourantNb 1.2444e-07 0.011761 0.00016634 4.8831e-06 v FourierNb 1.2425e-07 0.046786 0.00014522 1.5545e-07 v total_pressure -1.046e+05 1.6777e+05 38651 64672 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0761 0.11061 0.0032498 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2231e-07 0.051981 0.00031156 5.0385e-06 INSTANT 0.874915000E-01 TIME STEP NUMBER 55113 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283122530E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.601297387E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19214E-01 0.21158E+01 Friction velocity uk : 0.19214E-01 0.21158E+01 Dimensionless distance yplus : 0.18580E-01 0.20775E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -9.344763635e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29457E+08 1 0.24677E-09 0.37816E+02 0.24258E+04 c Velocity[X] 0.19004E+02 c Velocity[Y] 0.18812E+02 c Velocity[Z] 0.10045E-04 c Pressure 0.22504E-03 151 0.98857E-04 0.58351E-02 0.21475E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -7.825 16.819 5.6115 8.0052 v Velocity[Y] -10.377 11.979 -0.14302 -0.00067518 v Velocity[Z] -3.1011 2.9758 3.4979e-06 -5.3857e-08 v ǁVelocityǁ 0.0043067 17.836 6.3899 8.0094 v Pressure -2.0731e+05 65377 -63952 -37447 v TurbVisc 6.7352e-20 0.0049657 8.0205e-05 3.7542e-06 v CourantNb 1.0258e-07 0.011761 0.00016634 4.883e-06 v FourierNb 1.2425e-07 0.046797 0.00014522 1.5557e-07 v total_pressure -1.0598e+05 1.667e+05 37373 63878 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0775 0.11047 0.0032463 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.223e-07 0.051994 0.00031156 5.0386e-06 INSTANT 0.874916000E-01 TIME STEP NUMBER 55114 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283116661E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.601513564E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.18265E-01 0.21172E+01 Friction velocity uk : 0.18265E-01 0.21172E+01 Dimensionless distance yplus : 0.17807E-01 0.20789E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -9.863183704e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29457E+08 1 0.24630E-09 0.37658E+02 0.24207E+04 c Velocity[X] 0.18930E+02 c Velocity[Y] 0.18728E+02 c Velocity[Z] 0.98893E-05 c Pressure 0.22419E-03 411 0.81322E-04 0.57958E-02 0.17326E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -7.8589 16.855 5.6115 8.0051 v Velocity[Y] -10.378 11.983 -0.14304 -0.00067532 v Velocity[Z] -3.1008 2.9758 3.4968e-06 -5.3857e-08 v ǁVelocityǁ 0.0043908 17.878 6.3907 8.0093 v Pressure -2.0878e+05 64316 -65178 -38094 v TurbVisc 3.5959e-21 0.0049657 8.0456e-05 3.7697e-06 v CourantNb 4.3318e-08 0.011761 0.00016634 4.883e-06 v FourierNb 1.2425e-07 0.046808 0.00014522 1.5568e-07 v total_pressure -1.0745e+05 1.6564e+05 36147 63231 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0789 0.11033 0.003243 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2229e-07 0.052007 0.00031156 5.0387e-06 INSTANT 0.874917000E-01 TIME STEP NUMBER 55115 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283110651E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.601732658E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.14008E-01 0.21186E+01 Friction velocity uk : 0.14008E-01 0.21186E+01 Dimensionless distance yplus : 0.13685E-01 0.20802E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.006869617e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29456E+08 1 0.24582E-09 0.37501E+02 0.24157E+04 c Velocity[X] 0.18855E+02 c Velocity[Y] 0.18646E+02 c Velocity[Z] 0.97547E-05 c Pressure 0.22316E-03 11 0.66750E-04 0.57521E-02 0.14412E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -7.8926 16.892 5.6115 8.005 v Velocity[Y] -10.379 11.987 -0.14306 -0.0006751 v Velocity[Z] -3.1005 2.9758 3.4957e-06 -5.3857e-08 v ǁVelocityǁ 0.0040395 17.92 6.3914 8.0092 v Pressure -2.1035e+05 63210 -66282 -38663 v TurbVisc 1.335e-19 0.0049657 8.0705e-05 3.7852e-06 v CourantNb 6.941e-08 0.011761 0.00016633 4.883e-06 v FourierNb 1.2425e-07 0.046818 0.00014522 1.558e-07 v total_pressure -1.0902e+05 1.6453e+05 35043 62662 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0802 0.11021 0.0032398 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2228e-07 0.05202 0.00031156 5.0388e-06 INSTANT 0.874918000E-01 TIME STEP NUMBER 55116 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283104463E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.601959188E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11499E-01 0.21198E+01 Friction velocity uk : 0.11499E-01 0.21198E+01 Dimensionless distance yplus : 0.11230E-01 0.20815E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.009594839e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29456E+08 1 0.24536E-09 0.37347E+02 0.24108E+04 c Velocity[X] 0.18783E+02 c Velocity[Y] 0.18565E+02 c Velocity[Z] 0.96438E-05 c Pressure 0.22200E-03 24 0.98902E-04 0.57056E-02 0.18536E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -7.9262 16.927 5.6115 8.0049 v Velocity[Y] -10.379 11.991 -0.14308 -0.00067524 v Velocity[Z] -3.1002 2.9759 3.4946e-06 -5.3857e-08 v ǁVelocityǁ 0.0028167 17.962 6.3922 8.0091 v Pressure -2.1199e+05 62032 -67580 -39376 v TurbVisc 3.2964e-19 0.0049658 8.0951e-05 3.8006e-06 v CourantNb 5.7626e-08 0.011761 0.00016633 4.8829e-06 v FourierNb 1.2425e-07 0.046827 0.00014523 1.5591e-07 v total_pressure -1.1067e+05 1.6336e+05 33745 61949 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0815 0.11009 0.0032366 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2227e-07 0.052032 0.00031156 5.0389e-06 INSTANT 0.874919000E-01 TIME STEP NUMBER 55117 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283098280E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.602178803E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.20599E-01 0.21211E+01 Friction velocity uk : 0.20599E-01 0.21211E+01 Dimensionless distance yplus : 0.19937E-01 0.20827E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -9.666333102e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29455E+08 1 0.24489E-09 0.37193E+02 0.24058E+04 c Velocity[X] 0.18710E+02 c Velocity[Y] 0.18484E+02 c Velocity[Z] 0.95433E-05 c Pressure 0.22114E-03 27 0.82581E-04 0.56670E-02 0.16342E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -7.9597 16.963 5.6115 8.0047 v Velocity[Y] -10.38 11.994 -0.1431 -0.00067547 v Velocity[Z] -3.0998 2.9759 3.4935e-06 -5.3857e-08 v ǁVelocityǁ 0.0023418 18.004 6.3931 8.009 v Pressure -2.1371e+05 60781 -68692 -40034 v TurbVisc 1.9741e-19 0.0049658 8.1196e-05 3.816e-06 v CourantNb 5.913e-08 0.011761 0.00016633 4.8829e-06 v FourierNb 1.2425e-07 0.046837 0.00014523 1.5603e-07 v total_pressure -1.1239e+05 1.6211e+05 32633 61291 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0827 0.10997 0.0032336 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2226e-07 0.052043 0.00031156 5.0389e-06 INSTANT 0.874920000E-01 TIME STEP NUMBER 55118 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283091998E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.602448540E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.14919E-01 0.21222E+01 Friction velocity uk : 0.14919E-01 0.21222E+01 Dimensionless distance yplus : 0.14570E-01 0.20838E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -8.839848913e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29455E+08 1 0.24443E-09 0.37039E+02 0.24008E+04 c Velocity[X] 0.18635E+02 c Velocity[Y] 0.18403E+02 c Velocity[Z] 0.94885E-05 c Pressure 0.21949E-03 10 0.63399E-04 0.56088E-02 0.13595E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -7.993 16.998 5.6114 8.0046 v Velocity[Y] -10.38 11.997 -0.14312 -0.00067597 v Velocity[Z] -3.0995 2.9759 3.4924e-06 -5.3857e-08 v ǁVelocityǁ 0.002638 18.045 6.3939 8.009 v Pressure -2.1551e+05 59459 -69678 -40590 v TurbVisc 2.2028e-19 0.0049658 8.1439e-05 3.8313e-06 v CourantNb 7.7858e-08 0.011761 0.00016633 4.8829e-06 v FourierNb 1.2425e-07 0.046844 0.00014523 1.5614e-07 v total_pressure -1.1418e+05 1.6078e+05 31647 60735 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0838 0.10986 0.0032308 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2225e-07 0.052053 0.00031156 5.039e-06 INSTANT 0.874921000E-01 TIME STEP NUMBER 55119 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283085619E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.602717975E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.16828E-01 0.21230E+01 Friction velocity uk : 0.16828E-01 0.21230E+01 Dimensionless distance yplus : 0.16205E-01 0.20846E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -7.985193199e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29454E+08 1 0.24398E-09 0.36891E+02 0.23960E+04 c Velocity[X] 0.18565E+02 c Velocity[Y] 0.18326E+02 c Velocity[Z] 0.94322E-05 c Pressure 0.21718E-03 225 0.73626E-04 0.55341E-02 0.14266E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.0263 17.032 5.6114 8.0045 v Velocity[Y] -10.381 11.999 -0.14314 -0.00067587 v Velocity[Z] -3.0992 2.976 3.4913e-06 -5.3857e-08 v ǁVelocityǁ 0.0033592 18.086 6.3947 8.0089 v Pressure -2.1734e+05 58085 -70953 -41133 v TurbVisc 2.0459e-19 0.0049658 8.1681e-05 3.8465e-06 v CourantNb 8.7878e-08 0.011761 0.00016633 4.8829e-06 v FourierNb 1.2425e-07 0.046851 0.00014523 1.5625e-07 v total_pressure -1.1601e+05 1.5941e+05 30372 60192 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0846 0.10976 0.0032281 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2224e-07 0.052062 0.00031156 5.0391e-06 INSTANT 0.874922000E-01 TIME STEP NUMBER 55120 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283079179E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.602977772E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.14416E-01 0.21238E+01 Friction velocity uk : 0.14416E-01 0.21238E+01 Dimensionless distance yplus : 0.13883E-01 0.20854E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -6.705965984e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29453E+08 1 0.24352E-09 0.36742E+02 0.23912E+04 c Velocity[X] 0.18493E+02 c Velocity[Y] 0.18249E+02 c Velocity[Z] 0.93895E-05 c Pressure 0.21523E-03 81 0.77241E-04 0.54688E-02 0.14057E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.0595 17.066 5.6114 8.0044 v Velocity[Y] -10.381 12.001 -0.14315 -0.00067638 v Velocity[Z] -3.0988 2.976 3.4901e-06 -5.3857e-08 v ǁVelocityǁ 0.0040421 18.127 6.3955 8.0088 v Pressure -2.192e+05 56656 -71888 -41711 v TurbVisc 2.6081e-19 0.0049658 8.192e-05 3.8617e-06 v CourantNb 6.0659e-08 0.011761 0.00016633 4.8828e-06 v FourierNb 1.2425e-07 0.046857 0.00014523 1.5637e-07 v total_pressure -1.1787e+05 1.5798e+05 29437 59614 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0854 0.10967 0.0032257 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2223e-07 0.052068 0.00031156 5.0392e-06 INSTANT 0.874923000E-01 TIME STEP NUMBER 55121 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283072672E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.603300279E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11634E-01 0.21243E+01 Friction velocity uk : 0.11634E-01 0.21243E+01 Dimensionless distance yplus : 0.11203E-01 0.20859E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -5.535838401e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29453E+08 1 0.24307E-09 0.36595E+02 0.23865E+04 c Velocity[X] 0.18422E+02 c Velocity[Y] 0.18173E+02 c Velocity[Z] 0.93837E-05 c Pressure 0.21205E-03 151 0.87447E-04 0.53732E-02 0.10851E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.0925 17.1 5.6113 8.0042 v Velocity[Y] -10.381 12.002 -0.14317 -0.00067613 v Velocity[Z] -3.0985 2.976 3.489e-06 -5.3857e-08 v ǁVelocityǁ 0.0040483 18.167 6.3963 8.0087 v Pressure -2.2107e+05 55184 -72860 -42139 v TurbVisc 2.5589e-19 0.0049659 8.2158e-05 3.8768e-06 v CourantNb 4.3681e-08 0.011761 0.00016633 4.8828e-06 v FourierNb 1.2425e-07 0.04686 0.00014524 1.5648e-07 v total_pressure -1.1974e+05 1.5651e+05 28465 59186 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0859 0.1096 0.0032235 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2222e-07 0.052073 0.00031156 5.0393e-06 INSTANT 0.874924000E-01 TIME STEP NUMBER 55122 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283066016E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.603602515E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.72072E-02 0.21246E+01 Friction velocity uk : 0.72072E-02 0.21246E+01 Dimensionless distance yplus : 0.69406E-02 0.20862E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -4.161515893e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29452E+08 1 0.24263E-09 0.36450E+02 0.23818E+04 c Velocity[X] 0.18352E+02 c Velocity[Y] 0.18098E+02 c Velocity[Z] 0.93810E-05 c Pressure 0.20841E-03 194 0.97666E-04 0.52665E-02 0.13277E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.1253 17.134 5.6113 8.0041 v Velocity[Y] -10.382 12.002 -0.14318 -0.00067671 v Velocity[Z] -3.0982 2.9761 3.4879e-06 -5.3857e-08 v ǁVelocityǁ 0.003752 18.206 6.3971 8.0086 v Pressure -2.2307e+05 53690 -73817 -42680 v TurbVisc 2.5474e-19 0.0049659 8.2394e-05 3.8919e-06 v CourantNb 3.3113e-08 0.011761 0.00016633 4.8828e-06 v FourierNb 1.2425e-07 0.046862 0.00014524 1.5659e-07 v total_pressure -1.2174e+05 1.5502e+05 27508 58645 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0862 0.10954 0.0032216 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2221e-07 0.052075 0.00031157 5.0394e-06 INSTANT 0.874925000E-01 TIME STEP NUMBER 55123 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283059367E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.603911163E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10942E-01 0.21246E+01 Friction velocity uk : 0.10942E-01 0.21246E+01 Dimensionless distance yplus : 0.10538E-01 0.20862E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -2.725834348e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29452E+08 1 0.24219E-09 0.36306E+02 0.23771E+04 c Velocity[X] 0.18282E+02 c Velocity[Y] 0.18024E+02 c Velocity[Z] 0.93874E-05 c Pressure 0.20434E-03 891 0.80782E-04 0.51499E-02 0.10318E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.1579 17.167 5.6112 8.004 v Velocity[Y] -10.382 12.002 -0.14319 -0.00067677 v Velocity[Z] -3.0979 2.9761 3.4868e-06 -5.3857e-08 v ǁVelocityǁ 0.0037269 18.245 6.398 8.0085 v Pressure -2.2512e+05 52189 -74730 -43102 v TurbVisc 7.9567e-21 0.0049659 8.2628e-05 3.9069e-06 v CourantNb 3.3043e-08 0.011761 0.00016633 4.8827e-06 v FourierNb 1.2425e-07 0.046862 0.00014524 1.567e-07 v total_pressure -1.238e+05 1.5351e+05 26595 58223 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0862 0.10949 0.0032199 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.222e-07 0.052075 0.00031157 5.0394e-06 INSTANT 0.874926000E-01 TIME STEP NUMBER 55124 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283052607E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.604221985E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.36360E-02 0.21244E+01 Friction velocity uk : 0.36360E-02 0.21244E+01 Dimensionless distance yplus : 0.35015E-02 0.20860E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.315515617e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29451E+08 1 0.24175E-09 0.36163E+02 0.23724E+04 c Velocity[X] 0.18211E+02 c Velocity[Y] 0.17952E+02 c Velocity[Z] 0.94052E-05 c Pressure 0.19958E-03 10 0.60438E-04 0.50165E-02 0.82718E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.1901 17.2 5.6112 8.0038 v Velocity[Y] -10.381 12.001 -0.1432 -0.00067644 v Velocity[Z] -3.0975 2.9761 3.4857e-06 -5.3857e-08 v ǁVelocityǁ 0.0039918 18.284 6.3988 8.0084 v Pressure -2.2714e+05 50705 -75453 -43463 v TurbVisc 3.0072e-19 0.0049659 8.2861e-05 3.9219e-06 v CourantNb 3.2034e-08 0.011761 0.00016633 4.8827e-06 v FourierNb 1.2425e-07 0.046861 0.00014524 1.5681e-07 v total_pressure -1.2582e+05 1.5203e+05 25872 57862 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.086 0.10945 0.0032185 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2219e-07 0.052073 0.00031157 5.0395e-06 INSTANT 0.874927000E-01 TIME STEP NUMBER 55125 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283045733E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.604530753E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.92573E-02 0.21239E+01 Friction velocity uk : 0.92573E-02 0.21239E+01 Dimensionless distance yplus : 0.89149E-02 0.20855E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -2.244607425e-03 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29450E+08 1 0.24131E-09 0.36024E+02 0.23679E+04 c Velocity[X] 0.18144E+02 c Velocity[Y] 0.17880E+02 c Velocity[Z] 0.94190E-05 c Pressure 0.19438E-03 71 0.98369E-04 0.48728E-02 0.11328E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.2223 17.234 5.6111 8.0037 v Velocity[Y] -10.381 11.999 -0.1432 -0.00067644 v Velocity[Z] -3.0972 2.9762 3.4846e-06 -5.3857e-08 v ǁVelocityǁ 0.0041337 18.321 6.3996 8.0083 v Pressure -2.2908e+05 49261 -76477 -43946 v TurbVisc 2.2838e-19 0.0049659 8.3092e-05 3.9368e-06 v CourantNb 4.2337e-08 0.011761 0.00016633 4.8827e-06 v FourierNb 1.2425e-07 0.046857 0.00014524 1.5693e-07 v total_pressure -1.2776e+05 1.5059e+05 24848 57379 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0855 0.10942 0.0032174 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2218e-07 0.052069 0.00031158 5.0396e-06 INSTANT 0.874928000E-01 TIME STEP NUMBER 55126 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283038864E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.604802961E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10774E-01 0.21231E+01 Friction velocity uk : 0.10774E-01 0.21231E+01 Dimensionless distance yplus : 0.10376E-01 0.20847E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.199824224e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29450E+08 1 0.24087E-09 0.35884E+02 0.23633E+04 c Velocity[X] 0.18075E+02 c Velocity[Y] 0.17809E+02 c Velocity[Z] 0.94300E-05 c Pressure 0.18976E-03 23 0.81213E-04 0.47446E-02 0.92332E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.2541 17.267 5.611 8.0035 v Velocity[Y] -10.381 11.996 -0.14321 -0.00067658 v Velocity[Z] -3.0969 2.9762 3.4835e-06 -5.3857e-08 v ǁVelocityǁ 0.0034861 18.358 6.4005 8.0082 v Pressure -2.3092e+05 47881 -77182 -44353 v TurbVisc 2.8173e-19 0.004966 8.3321e-05 3.9517e-06 v CourantNb 5.8593e-08 0.011762 0.00016633 4.8826e-06 v FourierNb 1.2425e-07 0.046852 0.00014525 1.5704e-07 v total_pressure -1.296e+05 1.4921e+05 24143 56972 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0847 0.10941 0.0032165 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2217e-07 0.052062 0.00031158 5.0397e-06 INSTANT 0.874929000E-01 TIME STEP NUMBER 55127 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283031946E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.605119661E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10916E-01 0.21221E+01 Friction velocity uk : 0.10916E-01 0.21221E+01 Dimensionless distance yplus : 0.10665E-01 0.20837E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 2.102212872e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29449E+08 1 0.24044E-09 0.35745E+02 0.23587E+04 c Velocity[X] 0.18006E+02 c Velocity[Y] 0.17739E+02 c Velocity[Z] 0.94616E-05 c Pressure 0.18446E-03 10 0.55363E-04 0.46003E-02 0.78821E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.2856 17.3 5.6109 8.0034 v Velocity[Y] -10.381 11.994 -0.14321 -0.00067697 v Velocity[Z] -3.0966 2.9762 3.4824e-06 -5.3857e-08 v ǁVelocityǁ 0.0027781 18.395 6.4013 8.0081 v Pressure -2.3264e+05 46686 -77850 -44703 v TurbVisc 2.5537e-19 0.004966 8.3549e-05 3.9666e-06 v CourantNb 8.6298e-08 0.011762 0.00016634 4.8826e-06 v FourierNb 1.2425e-07 0.046844 0.00014525 1.5715e-07 v total_pressure -1.3132e+05 1.4801e+05 23475 56622 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0837 0.10941 0.0032158 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2216e-07 0.052053 0.00031159 5.0397e-06 INSTANT 0.874930000E-01 TIME STEP NUMBER 55128 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283024970E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.605379689E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11321E-01 0.21209E+01 Friction velocity uk : 0.11321E-01 0.21209E+01 Dimensionless distance yplus : 0.10902E-01 0.20826E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 2.552186242e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29449E+08 1 0.24001E-09 0.35607E+02 0.23542E+04 c Velocity[X] 0.17938E+02 c Velocity[Y] 0.17669E+02 c Velocity[Z] 0.94723E-05 c Pressure 0.17927E-03 83 0.96425E-04 0.44593E-02 0.79303E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.3168 17.333 5.6108 8.0033 v Velocity[Y] -10.38 11.99 -0.14321 -0.00067716 v Velocity[Z] -3.0962 2.9763 3.4813e-06 -5.3857e-08 v ǁVelocityǁ 0.0023492 18.43 6.4022 8.008 v Pressure -2.3421e+05 45658 -78607 -45036 v TurbVisc 2.0782e-19 0.004966 8.3774e-05 3.9813e-06 v CourantNb 8.572e-08 0.011762 0.00016634 4.8825e-06 v FourierNb 1.2425e-07 0.046836 0.00014525 1.5726e-07 v total_pressure -1.3288e+05 1.4698e+05 22718 56289 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0826 0.10942 0.0032153 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2214e-07 0.052042 0.00031159 5.0398e-06 INSTANT 0.874931000E-01 TIME STEP NUMBER 55129 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283017953E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.605598209E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10072E-01 0.21195E+01 Friction velocity uk : 0.10072E-01 0.21195E+01 Dimensionless distance yplus : 0.96998E-02 0.20812E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 3.307640637e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29448E+08 1 0.23958E-09 0.35469E+02 0.23496E+04 c Velocity[X] 0.17869E+02 c Velocity[Y] 0.17600E+02 c Velocity[Z] 0.94734E-05 c Pressure 0.17464E-03 23 0.79328E-04 0.43333E-02 0.68387E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.3476 17.367 5.6107 8.0031 v Velocity[Y] -10.379 11.986 -0.1432 -0.00067709 v Velocity[Z] -3.0959 2.9763 3.4801e-06 -5.3857e-08 v ǁVelocityǁ 0.0027478 18.465 6.403 8.0079 v Pressure -2.356e+05 44762 -79186 -45342 v TurbVisc 2.5234e-19 0.004966 8.3999e-05 3.9961e-06 v CourantNb 3.4114e-08 0.011762 0.00016634 4.8825e-06 v FourierNb 1.2425e-07 0.046825 0.00014526 1.5737e-07 v total_pressure -1.3427e+05 1.4609e+05 22139 55983 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0812 0.10944 0.0032149 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2213e-07 0.052029 0.0003116 5.0399e-06 INSTANT 0.874932000E-01 TIME STEP NUMBER 55130 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283010874E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.605832541E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12359E-01 0.21179E+01 Friction velocity uk : 0.12359E-01 0.21179E+01 Dimensionless distance yplus : 0.11902E-01 0.20796E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 3.206651624e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29447E+08 1 0.23916E-09 0.35332E+02 0.23451E+04 c Velocity[X] 0.17800E+02 c Velocity[Y] 0.17532E+02 c Velocity[Z] 0.94829E-05 c Pressure 0.17012E-03 9 0.52184E-04 0.42106E-02 0.59566E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.3781 17.4 5.6106 8.003 v Velocity[Y] -10.379 11.981 -0.1432 -0.00067667 v Velocity[Z] -3.0956 2.9763 3.479e-06 -5.3857e-08 v ǁVelocityǁ 0.0038723 18.499 6.4038 8.0078 v Pressure -2.368e+05 44009 -79735 -45609 v TurbVisc 1.7698e-19 0.004966 8.4222e-05 4.0108e-06 v CourantNb 1.226e-07 0.011762 0.00016634 4.8824e-06 v FourierNb 1.2425e-07 0.046813 0.00014526 1.5747e-07 v total_pressure -1.3547e+05 1.4533e+05 21590 55716 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0796 0.10946 0.0032146 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2212e-07 0.052014 0.0003116 5.0399e-06 INSTANT 0.874933000E-01 TIME STEP NUMBER 55131 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283003728E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.606008481E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.49768E-02 0.21162E+01 Friction velocity uk : 0.49768E-02 0.21162E+01 Dimensionless distance yplus : 0.49763E-02 0.20779E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 2.624723422e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29447E+08 1 0.23874E-09 0.35194E+02 0.23406E+04 c Velocity[X] 0.17732E+02 c Velocity[Y] 0.17462E+02 c Velocity[Z] 0.94615E-05 c Pressure 0.16645E-03 22 0.91143E-04 0.41097E-02 0.73148E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.4081 17.434 5.6105 8.0028 v Velocity[Y] -10.378 11.976 -0.14319 -0.00067666 v Velocity[Z] -3.0952 2.9763 3.4779e-06 -5.3857e-08 v ǁVelocityǁ 0.0044661 18.533 6.4047 8.0077 v Pressure -2.3779e+05 43421 -80249 -45932 v TurbVisc 2.3777e-19 0.0049661 8.4443e-05 4.0255e-06 v CourantNb 1.2171e-07 0.011763 0.00016635 4.8824e-06 v FourierNb 1.2425e-07 0.046801 0.00014526 1.5758e-07 v total_pressure -1.3646e+05 1.4475e+05 21076 55393 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0779 0.10948 0.0032143 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2211e-07 0.051999 0.00031161 5.04e-06 INSTANT 0.874934000E-01 TIME STEP NUMBER 55132 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282996579E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.606147254E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11452E-01 0.21143E+01 Friction velocity uk : 0.11452E-01 0.21143E+01 Dimensionless distance yplus : 0.11029E-01 0.20761E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 2.265578212e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29446E+08 1 0.23833E-09 0.35057E+02 0.23360E+04 c Velocity[X] 0.17663E+02 c Velocity[Y] 0.17394E+02 c Velocity[Z] 0.94322E-05 c Pressure 0.16354E-03 86 0.76361E-04 0.40279E-02 0.58810E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.4378 17.469 5.6103 8.0027 v Velocity[Y] -10.377 11.971 -0.14319 -0.00067667 v Velocity[Z] -3.0949 2.9764 3.4768e-06 -5.3857e-08 v ǁVelocityǁ 0.0043019 18.566 6.4055 8.0076 v Pressure -2.3854e+05 43006 -80714 -46203 v TurbVisc 7.4354e-20 0.0049661 8.4663e-05 4.0402e-06 v CourantNb 1.1391e-07 0.011763 0.00016635 4.8824e-06 v FourierNb 1.2425e-07 0.046787 0.00014527 1.5769e-07 v total_pressure -1.3722e+05 1.4433e+05 20611 55122 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0761 0.10952 0.0032142 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.221e-07 0.051982 0.00031162 5.0401e-06 INSTANT 0.874935000E-01 TIME STEP NUMBER 55133 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282989390E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.606275514E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.79664E-02 0.21124E+01 Friction velocity uk : 0.79664E-02 0.21124E+01 Dimensionless distance yplus : 0.76718E-02 0.20742E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.033905821e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29445E+08 1 0.23791E-09 0.34921E+02 0.23315E+04 c Velocity[X] 0.17595E+02 c Velocity[Y] 0.17326E+02 c Velocity[Z] 0.93939E-05 c Pressure 0.16151E-03 9 0.50161E-04 0.39683E-02 0.46655E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.4672 17.503 5.6102 8.0025 v Velocity[Y] -10.376 11.966 -0.14318 -0.00067688 v Velocity[Z] -3.0946 2.9764 3.4757e-06 -5.3857e-08 v ǁVelocityǁ 0.0041292 18.599 6.4063 8.0074 v Pressure -2.3907e+05 42771 -81150 -46411 v TurbVisc 1.3864e-19 0.0049661 8.4881e-05 4.0548e-06 v CourantNb 1.0131e-07 0.011763 0.00016635 4.8823e-06 v FourierNb 1.2425e-07 0.046773 0.00014527 1.578e-07 v total_pressure -1.3774e+05 1.441e+05 20175 54914 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0742 0.10957 0.0032141 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2209e-07 0.051964 0.00031162 5.0401e-06 INSTANT 0.874936000E-01 TIME STEP NUMBER 55134 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282982181E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.606361070E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.89000E-02 0.21105E+01 Friction velocity uk : 0.89000E-02 0.21105E+01 Dimensionless distance yplus : 0.85708E-02 0.20723E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -5.757182614e-03 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29445E+08 1 0.23751E-09 0.34782E+02 0.23269E+04 c Velocity[X] 0.17525E+02 c Velocity[Y] 0.17257E+02 c Velocity[Z] 0.93313E-05 c Pressure 0.16074E-03 37 0.89816E-04 0.39399E-02 0.45319E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.4961 17.538 5.61 8.0024 v Velocity[Y] -10.376 11.961 -0.14317 -0.00067694 v Velocity[Z] -3.0942 2.9764 3.4746e-06 -5.3857e-08 v ǁVelocityǁ 0.0038769 18.632 6.4072 8.0073 v Pressure -2.3935e+05 42717 -81401 -46605 v TurbVisc 1.1421e-19 0.0049661 8.5098e-05 4.0694e-06 v CourantNb 9.1028e-08 0.011763 0.00016635 4.8823e-06 v FourierNb 1.2425e-07 0.046759 0.00014528 1.5791e-07 v total_pressure -1.3802e+05 1.4404e+05 19924 54720 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0723 0.10962 0.0032139 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2207e-07 0.051947 0.00031163 5.0402e-06 INSTANT 0.874937000E-01 TIME STEP NUMBER 55135 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282974933E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.606422611E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12376E-01 0.21085E+01 Friction velocity uk : 0.12376E-01 0.21085E+01 Dimensionless distance yplus : 0.12086E-01 0.20704E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -2.116503549e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29444E+08 1 0.23710E-09 0.34643E+02 0.23223E+04 c Velocity[X] 0.17455E+02 c Velocity[Y] 0.17188E+02 c Velocity[Z] 0.92585E-05 c Pressure 0.16055E-03 45 0.73892E-04 0.39260E-02 0.39973E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.5248 17.573 5.6099 8.0022 v Velocity[Y] -10.375 11.956 -0.14316 -0.00067679 v Velocity[Z] -3.0939 2.9765 3.4735e-06 -5.3857e-08 v ǁVelocityǁ 0.0037663 18.664 6.408 8.0072 v Pressure -2.3939e+05 42842 -81720 -46783 v TurbVisc 9.7451e-20 0.0049661 8.5314e-05 4.084e-06 v CourantNb 8.1075e-08 0.011763 0.00016636 4.8822e-06 v FourierNb 1.2425e-07 0.046744 0.00014528 1.5802e-07 v total_pressure -1.3806e+05 1.4417e+05 19605 54542 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0704 0.10966 0.0032136 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2206e-07 0.051929 0.00031164 5.0402e-06 INSTANT 0.874938000E-01 TIME STEP NUMBER 55136 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282967653E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.606450005E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15963E-01 0.21066E+01 Friction velocity uk : 0.15963E-01 0.21066E+01 Dimensionless distance yplus : 0.15372E-01 0.20685E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -4.335348278e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29443E+08 1 0.23670E-09 0.34508E+02 0.23177E+04 c Velocity[X] 0.17387E+02 c Velocity[Y] 0.17121E+02 c Velocity[Z] 0.91629E-05 c Pressure 0.16120E-03 9 0.48063E-04 0.39327E-02 0.32047E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.5532 17.608 5.6097 8.0021 v Velocity[Y] -10.374 11.951 -0.14314 -0.0006763 v Velocity[Z] -3.0936 2.9765 3.4724e-06 -5.3857e-08 v ǁVelocityǁ 0.0035819 18.696 6.4088 8.0071 v Pressure -2.3921e+05 43141 -82027 -46921 v TurbVisc 1.2112e-19 0.0049662 8.5528e-05 4.0985e-06 v CourantNb 7.4356e-08 0.011763 0.00016636 4.8822e-06 v FourierNb 1.2425e-07 0.04673 0.00014529 1.5812e-07 v total_pressure -1.3788e+05 1.4447e+05 19298 54404 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0685 0.10969 0.0032131 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2205e-07 0.051912 0.00031164 5.0403e-06 INSTANT 0.874939000E-01 TIME STEP NUMBER 55137 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282960332E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.606459111E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.17716E-01 0.21048E+01 Friction velocity uk : 0.17716E-01 0.21048E+01 Dimensionless distance yplus : 0.17136E-01 0.20667E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -6.871099087e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29443E+08 1 0.23631E-09 0.34368E+02 0.23131E+04 c Velocity[X] 0.17317E+02 c Velocity[Y] 0.17051E+02 c Velocity[Z] 0.90486E-05 c Pressure 0.16258E-03 46 0.85610E-04 0.39571E-02 0.41459E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.5812 17.643 5.6095 8.002 v Velocity[Y] -10.374 11.946 -0.14313 -0.0006761 v Velocity[Z] -3.0933 2.9765 3.4713e-06 -5.3857e-08 v ǁVelocityǁ 0.0034167 18.727 6.4096 8.007 v Pressure -2.3882e+05 43600 -82072 -47104 v TurbVisc 9.6303e-20 0.0049662 8.5741e-05 4.113e-06 v CourantNb 7.125e-08 0.011764 0.00016636 4.8821e-06 v FourierNb 1.2425e-07 0.046716 0.00014529 1.5823e-07 v total_pressure -1.3749e+05 1.4493e+05 19253 54221 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0667 0.10971 0.0032124 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2204e-07 0.051895 0.00031165 5.0404e-06 INSTANT 0.874940000E-01 TIME STEP NUMBER 55138 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282953020E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.606465018E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.83080E-02 0.21031E+01 Friction velocity uk : 0.83080E-02 0.21031E+01 Dimensionless distance yplus : 0.82122E-02 0.20651E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -9.294191921e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29442E+08 1 0.23592E-09 0.34235E+02 0.23086E+04 c Velocity[X] 0.17250E+02 c Velocity[Y] 0.16985E+02 c Velocity[Z] 0.89242E-05 c Pressure 0.16390E-03 9 0.97932E-04 0.39799E-02 0.34649E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.6091 17.678 5.6094 8.0018 v Velocity[Y] -10.373 11.942 -0.14312 -0.00067656 v Velocity[Z] -3.0929 2.9766 3.4702e-06 -5.3857e-08 v ǁVelocityǁ 0.0032547 18.759 6.4104 8.0069 v Pressure -2.3824e+05 44213 -82321 -47219 v TurbVisc 1.8874e-19 0.0049662 8.5952e-05 4.1275e-06 v CourantNb 7.1581e-08 0.011764 0.00016636 4.8821e-06 v FourierNb 1.2425e-07 0.046704 0.0001453 1.5834e-07 v total_pressure -1.3691e+05 1.4554e+05 19004 54106 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0651 0.10971 0.0032115 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2203e-07 0.05188 0.00031165 5.0404e-06 INSTANT 0.874941000E-01 TIME STEP NUMBER 55139 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282945722E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.606424107E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15946E-01 0.21016E+01 Friction velocity uk : 0.15946E-01 0.21016E+01 Dimensionless distance yplus : 0.15504E-01 0.20636E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.217881207e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29441E+08 1 0.23553E-09 0.34097E+02 0.23040E+04 c Velocity[X] 0.17181E+02 c Velocity[Y] 0.16916E+02 c Velocity[Z] 0.87659E-05 c Pressure 0.16555E-03 748 0.80713E-04 0.40109E-02 0.30853E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.6367 17.713 5.6092 8.0017 v Velocity[Y] -10.372 11.938 -0.1431 -0.00067635 v Velocity[Z] -3.0926 2.9766 3.469e-06 -5.3857e-08 v ǁVelocityǁ 0.0031224 18.79 6.4112 8.0068 v Pressure -2.375e+05 44959 -82226 -47296 v TurbVisc 1.642e-19 0.0049662 8.6162e-05 4.142e-06 v CourantNb 7.5784e-08 0.011764 0.00016636 4.882e-06 v FourierNb 1.2425e-07 0.046692 0.0001453 1.5844e-07 v total_pressure -1.3617e+05 1.4628e+05 19099 54029 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0636 0.10972 0.0032104 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2202e-07 0.051866 0.00031166 5.0405e-06 INSTANT 0.874942000E-01 TIME STEP NUMBER 55140 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282938377E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.606418415E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.16860E-01 0.21003E+01 Friction velocity uk : 0.16860E-01 0.21003E+01 Dimensionless distance yplus : 0.16491E-01 0.20623E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.489335145e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29441E+08 1 0.23516E-09 0.33966E+02 0.22996E+04 c Velocity[X] 0.17114E+02 c Velocity[Y] 0.16852E+02 c Velocity[Z] 0.86081E-05 c Pressure 0.16625E-03 8 0.58126E-04 0.40187E-02 0.15746E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.6642 17.748 5.609 8.0015 v Velocity[Y] -10.372 11.935 -0.14309 -0.00067577 v Velocity[Z] -3.0923 2.9766 3.4679e-06 -5.3857e-08 v ǁVelocityǁ 0.0030144 18.822 6.412 8.0067 v Pressure -2.3662e+05 45827 -82394 -47308 v TurbVisc 5.3329e-20 0.0049662 8.637e-05 4.1564e-06 v CourantNb 8.5074e-08 0.011764 0.00016636 4.882e-06 v FourierNb 1.2425e-07 0.046682 0.00014531 1.5855e-07 v total_pressure -1.3529e+05 1.4715e+05 18931 54017 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0623 0.10972 0.0032089 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.22e-07 0.051854 0.00031166 5.0405e-06 INSTANT 0.874943000E-01 TIME STEP NUMBER 55141 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282931010E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.606359623E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19759E-01 0.20991E+01 Friction velocity uk : 0.19759E-01 0.20991E+01 Dimensionless distance yplus : 0.19531E-01 0.20611E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.794498847e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29440E+08 1 0.23478E-09 0.33832E+02 0.22951E+04 c Velocity[X] 0.17048E+02 c Velocity[Y] 0.16785E+02 c Velocity[Z] 0.84184E-05 c Pressure 0.16667E-03 57 0.99462E-04 0.40198E-02 0.21390E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.6916 17.783 5.6088 8.0014 v Velocity[Y] -10.372 11.933 -0.14308 -0.00067548 v Velocity[Z] -3.0919 2.9767 3.4668e-06 -5.3857e-08 v ǁVelocityǁ 0.0028016 18.854 6.4128 8.0066 v Pressure -2.3564e+05 46790 -82242 -47390 v TurbVisc 1.3408e-20 0.0049663 8.6578e-05 4.1708e-06 v CourantNb 9.7574e-08 0.011764 0.00016636 4.8819e-06 v FourierNb 1.2425e-07 0.046674 0.00014531 1.5866e-07 v total_pressure -1.3431e+05 1.4811e+05 19083 53935 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0611 0.10969 0.0032072 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2199e-07 0.051844 0.00031167 5.0406e-06 INSTANT 0.874944000E-01 TIME STEP NUMBER 55142 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282923652E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.606356679E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.76934E-02 0.20982E+01 Friction velocity uk : 0.76934E-02 0.20982E+01 Dimensionless distance yplus : 0.76046E-02 0.20602E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -2.076680343e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29439E+08 1 0.23441E-09 0.33704E+02 0.22907E+04 c Velocity[X] 0.16983E+02 c Velocity[Y] 0.16721E+02 c Velocity[Z] 0.82321E-05 c Pressure 0.16632E-03 21 0.82002E-04 0.40024E-02 0.11130E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.719 17.817 5.6086 8.0012 v Velocity[Y] -10.371 11.931 -0.14307 -0.0006754 v Velocity[Z] -3.0916 2.9767 3.4657e-06 -5.3857e-08 v ǁVelocityǁ 0.0024928 18.886 6.4136 8.0065 v Pressure -2.3458e+05 47825 -82207 -47398 v TurbVisc 1.4118e-20 0.0049663 8.6784e-05 4.1853e-06 v CourantNb 1.0702e-07 0.011764 0.00016636 4.8819e-06 v FourierNb 1.2425e-07 0.046667 0.00014531 1.5876e-07 v total_pressure -1.3325e+05 1.4915e+05 19118 53927 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0602 0.10965 0.0032052 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2198e-07 0.051836 0.00031167 5.0406e-06 INSTANT 0.874945000E-01 TIME STEP NUMBER 55143 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282916313E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.606300755E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19080E-01 0.20975E+01 Friction velocity uk : 0.19080E-01 0.20975E+01 Dimensionless distance yplus : 0.18633E-01 0.20596E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -2.340430009e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29439E+08 1 0.23404E-09 0.33581E+02 0.22866E+04 c Velocity[X] 0.16921E+02 c Velocity[Y] 0.16660E+02 c Velocity[Z] 0.80256E-05 c Pressure 0.16520E-03 8 0.54152E-04 0.39664E-02 0.14625E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.7464 17.851 5.6084 8.0011 v Velocity[Y] -10.371 11.93 -0.14305 -0.00067565 v Velocity[Z] -3.0913 2.9767 3.4646e-06 -5.3857e-08 v ǁVelocityǁ 0.0022076 18.918 6.4143 8.0064 v Pressure -2.3348e+05 48912 -82158 -47395 v TurbVisc 5.4772e-21 0.0049663 8.6989e-05 4.1996e-06 v CourantNb 1.1516e-07 0.011764 0.00016635 4.8818e-06 v FourierNb 1.2425e-07 0.046663 0.00014532 1.5887e-07 v total_pressure -1.3216e+05 1.5024e+05 19167 53930 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0596 0.10962 0.003203 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2197e-07 0.05183 0.00031167 5.0407e-06 INSTANT 0.874946000E-01 TIME STEP NUMBER 55144 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282908989E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.606292467E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12837E-01 0.20970E+01 Friction velocity uk : 0.12837E-01 0.20970E+01 Dimensionless distance yplus : 0.12536E-01 0.20591E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -2.588678717e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29438E+08 1 0.23368E-09 0.33456E+02 0.22824E+04 c Velocity[X] 0.16859E+02 c Velocity[Y] 0.16598E+02 c Velocity[Z] 0.78246E-05 c Pressure 0.16350E-03 70 0.95969E-04 0.39170E-02 0.21190E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.7738 17.885 5.6082 8.0009 v Velocity[Y] -10.371 11.929 -0.14304 -0.0006756 v Velocity[Z] -3.0909 2.9767 3.4635e-06 -5.3857e-08 v ǁVelocityǁ 0.0019762 18.95 6.4151 8.0062 v Pressure -2.3238e+05 50021 -81806 -47312 v TurbVisc 1.188e-20 0.0049663 8.7192e-05 4.2139e-06 v CourantNb 1.0442e-07 0.011764 0.00016635 4.8818e-06 v FourierNb 1.2425e-07 0.046659 0.00014532 1.5898e-07 v total_pressure -1.3106e+05 1.5135e+05 19519 54013 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0591 0.10957 0.0032005 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2196e-07 0.051826 0.00031167 5.0408e-06 INSTANT 0.874947000E-01 TIME STEP NUMBER 55145 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282901660E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.606321288E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.17204E-01 0.20968E+01 Friction velocity uk : 0.17204E-01 0.20968E+01 Dimensionless distance yplus : 0.16802E-01 0.20589E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -2.825401479e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29438E+08 1 0.23332E-09 0.33337E+02 0.22783E+04 c Velocity[X] 0.16799E+02 c Velocity[Y] 0.16538E+02 c Velocity[Z] 0.76328E-05 c Pressure 0.16150E-03 22 0.79843E-04 0.38608E-02 0.20376E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.8013 17.917 5.608 8.0008 v Velocity[Y] -10.371 11.929 -0.14303 -0.00067535 v Velocity[Z] -3.0906 2.9768 3.4624e-06 -5.3857e-08 v ǁVelocityǁ 0.0017103 18.983 6.4159 8.0061 v Pressure -2.313e+05 51129 -81657 -47228 v TurbVisc 3.6623e-21 0.0049663 8.7395e-05 4.2283e-06 v CourantNb 8.7255e-08 0.011764 0.00016635 4.8817e-06 v FourierNb 1.2425e-07 0.046658 0.00014533 1.5908e-07 v total_pressure -1.2998e+05 1.5245e+05 19668 54097 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0589 0.10951 0.0031977 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2194e-07 0.051825 0.00031167 5.0408e-06 INSTANT 0.874948000E-01 TIME STEP NUMBER 55146 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282894337E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.606304030E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.16526E-01 0.20968E+01 Friction velocity uk : 0.16526E-01 0.20968E+01 Dimensionless distance yplus : 0.15986E-01 0.20589E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -3.006221130e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29437E+08 1 0.23296E-09 0.33221E+02 0.22744E+04 c Velocity[X] 0.16740E+02 c Velocity[Y] 0.16481E+02 c Velocity[Z] 0.74325E-05 c Pressure 0.15897E-03 8 0.52908E-04 0.37919E-02 0.24847E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.8289 17.95 5.6078 8.0006 v Velocity[Y] -10.371 11.93 -0.14302 -0.00067475 v Velocity[Z] -3.0903 2.9768 3.4613e-06 -5.3857e-08 v ǁVelocityǁ 0.0014767 19.016 6.4167 8.006 v Pressure -2.3027e+05 52220 -81450 -47129 v TurbVisc 2.2341e-21 0.0049663 8.7596e-05 4.2426e-06 v CourantNb 4.7652e-08 0.011764 0.00016634 4.8817e-06 v FourierNb 1.2425e-07 0.046658 0.00014533 1.5919e-07 v total_pressure -1.2894e+05 1.5354e+05 19875 54196 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0589 0.10942 0.0031947 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2193e-07 0.051826 0.00031167 5.0409e-06 INSTANT 0.874949000E-01 TIME STEP NUMBER 55147 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282887025E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.606346317E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.98185E-02 0.20969E+01 Friction velocity uk : 0.98185E-02 0.20969E+01 Dimensionless distance yplus : 0.97693E-02 0.20590E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -3.163217972e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29436E+08 1 0.23261E-09 0.33103E+02 0.22704E+04 c Velocity[X] 0.16681E+02 c Velocity[Y] 0.16422E+02 c Velocity[Z] 0.72437E-05 c Pressure 0.15661E-03 47 0.94476E-04 0.37275E-02 0.33986E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.8565 17.982 5.6076 8.0005 v Velocity[Y] -10.372 11.93 -0.14301 -0.00067444 v Velocity[Z] -3.09 2.9768 3.4602e-06 -5.3857e-08 v ǁVelocityǁ 0.0012824 19.049 6.4175 8.0059 v Pressure -2.2931e+05 53266 -81027 -46987 v TurbVisc 1.9816e-21 0.0049664 8.7796e-05 4.2569e-06 v CourantNb 3.7325e-08 0.011764 0.00016634 4.8816e-06 v FourierNb 1.2425e-07 0.04666 0.00014534 1.5929e-07 v total_pressure -1.2799e+05 1.5459e+05 20298 54338 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.059 0.10932 0.0031913 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2192e-07 0.051828 0.00031167 5.0409e-06 INSTANT 0.874950000E-01 TIME STEP NUMBER 55148 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282879749E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.606426158E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.14766E-01 0.20973E+01 Friction velocity uk : 0.14766E-01 0.20973E+01 Dimensionless distance yplus : 0.14764E-01 0.20593E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -3.269536639e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29436E+08 1 0.23226E-09 0.32989E+02 0.22664E+04 c Velocity[X] 0.16624E+02 c Velocity[Y] 0.16365E+02 c Velocity[Z] 0.70710E-05 c Pressure 0.15484E-03 22 0.78156E-04 0.36775E-02 0.34594E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.8843 18.013 5.6074 8.0003 v Velocity[Y] -10.372 11.932 -0.14301 -0.00067435 v Velocity[Z] -3.0896 2.9769 3.4591e-06 -5.3857e-08 v ǁVelocityǁ 0.0010841 19.083 6.4182 8.0058 v Pressure -2.2844e+05 54250 -80720 -46832 v TurbVisc 1.4969e-21 0.0049664 8.7995e-05 4.2713e-06 v CourantNb 5.4615e-08 0.011764 0.00016633 4.8816e-06 v FourierNb 1.2425e-07 0.046663 0.00014534 1.594e-07 v total_pressure -1.2712e+05 1.5557e+05 20605 54493 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0593 0.10923 0.003188 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2191e-07 0.051832 0.00031167 5.041e-06 INSTANT 0.874951000E-01 TIME STEP NUMBER 55149 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282872504E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.606476980E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.20886E-01 0.20978E+01 Friction velocity uk : 0.20886E-01 0.20978E+01 Dimensionless distance yplus : 0.20350E-01 0.20598E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -3.328656518e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29435E+08 1 0.23191E-09 0.32875E+02 0.22626E+04 c Velocity[X] 0.16567E+02 c Velocity[Y] 0.16309E+02 c Velocity[Z] 0.69012E-05 c Pressure 0.15344E-03 9 0.49302E-04 0.36364E-02 0.38365E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.9123 18.044 5.6073 8.0002 v Velocity[Y] -10.372 11.933 -0.143 -0.00067464 v Velocity[Z] -3.0893 2.9769 3.458e-06 -5.3857e-08 v ǁVelocityǁ 0.00090604 19.117 6.419 8.0057 v Pressure -2.2768e+05 55160 -80368 -46661 v TurbVisc 1.1285e-21 0.0049664 8.8192e-05 4.2855e-06 v CourantNb 3.2501e-08 0.011765 0.00016633 4.8816e-06 v FourierNb 1.2425e-07 0.046667 0.00014534 1.595e-07 v total_pressure -1.2636e+05 1.5649e+05 20957 54664 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0598 0.10916 0.0031846 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.219e-07 0.051837 0.00031167 5.0411e-06 INSTANT 0.874952000E-01 TIME STEP NUMBER 55150 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282865317E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.606579424E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.22047E-01 0.20983E+01 Friction velocity uk : 0.22047E-01 0.20983E+01 Dimensionless distance yplus : 0.21481E-01 0.20604E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -3.348161773e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29434E+08 1 0.23156E-09 0.32760E+02 0.22586E+04 c Velocity[X] 0.16508E+02 c Velocity[Y] 0.16252E+02 c Velocity[Z] 0.67514E-05 c Pressure 0.15312E-03 48 0.90956E-04 0.36209E-02 0.62059E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.9404 18.074 5.6071 8 v Velocity[Y] -10.373 11.935 -0.14299 -0.00067449 v Velocity[Z] -3.089 2.9769 3.4568e-06 -5.3857e-08 v ǁVelocityǁ 0.0007576 19.151 6.4198 8.0056 v Pressure -2.2704e+05 55980 -79875 -46383 v TurbVisc 1.5033e-21 0.0049664 8.8389e-05 4.2997e-06 v CourantNb 8.458e-08 0.011765 0.00016632 4.8815e-06 v FourierNb 1.2425e-07 0.046672 0.00014535 1.5961e-07 v total_pressure -1.2571e+05 1.573e+05 21450 54942 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0604 0.10907 0.003181 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2188e-07 0.051843 0.00031167 5.0411e-06 INSTANT 0.874953000E-01 TIME STEP NUMBER 55151 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282858133E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.606709165E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.14301E-01 0.20990E+01 Friction velocity uk : 0.14301E-01 0.20990E+01 Dimensionless distance yplus : 0.13938E-01 0.20610E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -3.305276797e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29434E+08 1 0.23122E-09 0.32646E+02 0.22547E+04 c Velocity[X] 0.16451E+02 c Velocity[Y] 0.16195E+02 c Velocity[Z] 0.66187E-05 c Pressure 0.15387E-03 192 0.75910E-04 0.36311E-02 0.56413E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.9686 18.104 5.6069 7.9999 v Velocity[Y] -10.373 11.937 -0.14298 -0.00067426 v Velocity[Z] -3.0886 2.977 3.4557e-06 -5.3857e-08 v ǁVelocityǁ 0.00061027 19.185 6.4206 8.0055 v Pressure -2.2651e+05 56701 -79425 -46122 v TurbVisc 3.2608e-21 0.0049664 8.8584e-05 4.314e-06 v CourantNb 6.7887e-08 0.011765 0.00016632 4.8815e-06 v FourierNb 1.2425e-07 0.046678 0.00014535 1.5971e-07 v total_pressure -1.2518e+05 1.5803e+05 21900 55203 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.061 0.10897 0.0031772 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2187e-07 0.051851 0.00031167 5.0412e-06 INSTANT 0.874954000E-01 TIME STEP NUMBER 55152 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282850990E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.606828306E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19874E-01 0.20997E+01 Friction velocity uk : 0.19874E-01 0.20997E+01 Dimensionless distance yplus : 0.19199E-01 0.20617E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -3.223581269e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29433E+08 1 0.23088E-09 0.32530E+02 0.22507E+04 c Velocity[X] 0.16392E+02 c Velocity[Y] 0.16138E+02 c Velocity[Z] 0.64995E-05 c Pressure 0.15541E-03 9 0.49139E-04 0.36596E-02 0.60284E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -8.9975 18.133 5.6067 7.9997 v Velocity[Y] -10.373 11.939 -0.14297 -0.00067382 v Velocity[Z] -3.0883 2.977 3.4546e-06 -5.3857e-08 v ǁVelocityǁ 0.00048925 19.22 6.4214 8.0054 v Pressure -2.2609e+05 57323 -78921 -45849 v TurbVisc 3.952e-21 0.0049665 8.8778e-05 4.3282e-06 v CourantNb 3.4189e-08 0.011765 0.00016631 4.8814e-06 v FourierNb 1.2425e-07 0.046684 0.00014535 1.5982e-07 v total_pressure -1.2476e+05 1.5865e+05 22404 55476 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0617 0.10887 0.0031735 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2186e-07 0.051858 0.00031167 5.0412e-06 INSTANT 0.874955000E-01 TIME STEP NUMBER 55153 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282843892E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.606977623E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.21774E-01 0.21004E+01 Friction velocity uk : 0.21774E-01 0.21004E+01 Dimensionless distance yplus : 0.21063E-01 0.20624E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -3.087548130e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29432E+08 1 0.23054E-09 0.32414E+02 0.22467E+04 c Velocity[X] 0.16333E+02 c Velocity[Y] 0.16080E+02 c Velocity[Z] 0.64016E-05 c Pressure 0.15806E-03 123 0.89253E-04 0.37143E-02 0.73531E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.0295 18.163 5.6066 7.9996 v Velocity[Y] -10.374 11.941 -0.14297 -0.00067352 v Velocity[Z] -3.088 2.977 3.4535e-06 -5.3857e-08 v ǁVelocityǁ 0.00037084 19.254 6.4222 8.0053 v Pressure -2.2577e+05 57842 -78384 -45529 v TurbVisc 7.2567e-21 0.0049665 8.8971e-05 4.3425e-06 v CourantNb 7.5538e-08 0.011765 0.00016631 4.8814e-06 v FourierNb 1.2425e-07 0.04669 0.00014535 1.5992e-07 v total_pressure -1.2445e+05 1.5917e+05 22941 55796 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0624 0.10876 0.0031697 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2185e-07 0.051865 0.00031166 5.0413e-06 INSTANT 0.874956000E-01 TIME STEP NUMBER 55154 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282836847E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.607134714E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19315E-01 0.21011E+01 Friction velocity uk : 0.19315E-01 0.21011E+01 Dimensionless distance yplus : 0.18574E-01 0.20631E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -2.903174882e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29432E+08 1 0.23020E-09 0.32297E+02 0.22427E+04 c Velocity[X] 0.16274E+02 c Velocity[Y] 0.16023E+02 c Velocity[Z] 0.63166E-05 c Pressure 0.16111E-03 23 0.73812E-04 0.37781E-02 0.74381E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.0617 18.191 5.6064 7.9994 v Velocity[Y] -10.374 11.943 -0.14296 -0.00067346 v Velocity[Z] -3.0876 2.977 3.4524e-06 -5.3857e-08 v ǁVelocityǁ 0.00027454 19.289 6.423 8.0052 v Pressure -2.2555e+05 58263 -77797 -45196 v TurbVisc 1.1054e-20 0.0049665 8.9163e-05 4.3567e-06 v CourantNb 3.7775e-08 0.011765 0.00016631 4.8813e-06 v FourierNb 1.2425e-07 0.046696 0.00014535 1.6003e-07 v total_pressure -1.2422e+05 1.5959e+05 23528 56129 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0631 0.10865 0.003166 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2184e-07 0.051872 0.00031166 5.0414e-06 INSTANT 0.874957000E-01 TIME STEP NUMBER 55155 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282829860E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.607300077E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.16540E-01 0.21017E+01 Friction velocity uk : 0.16540E-01 0.21017E+01 Dimensionless distance yplus : 0.15905E-01 0.20637E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -2.688699193e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29431E+08 1 0.22986E-09 0.32179E+02 0.22386E+04 c Velocity[X] 0.16215E+02 c Velocity[Y] 0.15964E+02 c Velocity[Z] 0.62501E-05 c Pressure 0.16453E-03 10 0.51436E-04 0.38502E-02 0.78035E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.094 18.22 5.6063 7.9993 v Velocity[Y] -10.375 11.945 -0.14295 -0.00067378 v Velocity[Z] -3.0873 2.9771 3.4513e-06 -5.3857e-08 v ǁVelocityǁ 0.00020478 19.324 6.4238 8.0051 v Pressure -2.254e+05 58594 -77140 -44846 v TurbVisc 6.6455e-22 0.0049665 8.9354e-05 4.3709e-06 v CourantNb 6.8261e-08 0.011765 0.0001663 4.8813e-06 v FourierNb 1.2425e-07 0.046701 0.00014536 1.6013e-07 v total_pressure -1.2407e+05 1.5992e+05 24185 56479 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0637 0.10854 0.0031624 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2183e-07 0.051879 0.00031166 5.0414e-06 INSTANT 0.874958000E-01 TIME STEP NUMBER 55156 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282822966E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.607466481E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10262E-01 0.21023E+01 Friction velocity uk : 0.10262E-01 0.21023E+01 Dimensionless distance yplus : 0.99775E-02 0.20642E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -2.424076413e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29430E+08 1 0.22953E-09 0.32062E+02 0.22345E+04 c Velocity[X] 0.16155E+02 c Velocity[Y] 0.15907E+02 c Velocity[Z] 0.62042E-05 c Pressure 0.16836E-03 23 0.86144E-04 0.39319E-02 0.10507E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.1263 18.249 5.6061 7.9992 v Velocity[Y] -10.375 11.946 -0.14294 -0.00067375 v Velocity[Z] -3.087 2.9771 3.4502e-06 -5.3857e-08 v ǁVelocityǁ 0.00012846 19.358 6.4246 8.005 v Pressure -2.2529e+05 58848 -76532 -44391 v TurbVisc 1.0294e-20 0.0049665 8.9544e-05 4.3851e-06 v CourantNb 2.9589e-08 0.011765 0.0001663 4.8813e-06 v FourierNb 1.2425e-07 0.046706 0.00014536 1.6023e-07 v total_pressure -1.2397e+05 1.6017e+05 24793 56934 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0642 0.10844 0.003159 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2182e-07 0.051884 0.00031165 5.0415e-06 INSTANT 0.874959000E-01 TIME STEP NUMBER 55157 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282816091E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.607619257E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10741E-01 0.21027E+01 Friction velocity uk : 0.10741E-01 0.21027E+01 Dimensionless distance yplus : 0.10443E-01 0.20646E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -2.135734073e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29430E+08 1 0.22920E-09 0.31945E+02 0.22305E+04 c Velocity[X] 0.16095E+02 c Velocity[Y] 0.15850E+02 c Velocity[Z] 0.61689E-05 c Pressure 0.17152E-03 23 0.72069E-04 0.39974E-02 0.10242E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.1588 18.277 5.606 7.999 v Velocity[Y] -10.375 11.947 -0.14294 -0.00067358 v Velocity[Z] -3.0866 2.9771 3.4491e-06 -5.3857e-08 v ǁVelocityǁ 8.5082e-05 19.393 6.4255 8.0049 v Pressure -2.2522e+05 59039 -75808 -43939 v TurbVisc 3.6824e-21 0.0049666 8.9732e-05 4.3993e-06 v CourantNb 1.9894e-08 0.011765 0.00016629 4.8812e-06 v FourierNb 1.2425e-07 0.046709 0.00014536 1.6034e-07 v total_pressure -1.2389e+05 1.6036e+05 25517 57386 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0646 0.10836 0.0031559 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.218e-07 0.051888 0.00031165 5.0416e-06 INSTANT 0.874960000E-01 TIME STEP NUMBER 55158 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282809290E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.607794824E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.74421E-02 0.21029E+01 Friction velocity uk : 0.74421E-02 0.21029E+01 Dimensionless distance yplus : 0.71566E-02 0.20649E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.824086323e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29429E+08 1 0.22888E-09 0.31827E+02 0.22264E+04 c Velocity[X] 0.16035E+02 c Velocity[Y] 0.15792E+02 c Velocity[Z] 0.61567E-05 c Pressure 0.17458E-03 10 0.55091E-04 0.40604E-02 0.10214E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.1914 18.306 5.6059 7.9989 v Velocity[Y] -10.375 11.947 -0.14293 -0.00067312 v Velocity[Z] -3.0863 2.9772 3.448e-06 -5.3857e-08 v ǁVelocityǁ 8.5965e-05 19.427 6.4263 8.0048 v Pressure -2.2514e+05 59181 -75007 -43492 v TurbVisc 3.5215e-21 0.0049666 8.992e-05 4.4134e-06 v CourantNb 3.42e-08 0.011765 0.00016629 4.8812e-06 v FourierNb 1.2425e-07 0.046712 0.00014536 1.6044e-07 v total_pressure -1.2381e+05 1.6051e+05 26318 57833 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0649 0.10828 0.0031529 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2179e-07 0.051891 0.00031165 5.0416e-06 INSTANT 0.874961000E-01 TIME STEP NUMBER 55159 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282802575E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.607943211E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.79854E-02 0.21031E+01 Friction velocity uk : 0.79854E-02 0.21031E+01 Dimensionless distance yplus : 0.76790E-02 0.20650E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.474203662e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29429E+08 1 0.22855E-09 0.31713E+02 0.22224E+04 c Velocity[X] 0.15977E+02 c Velocity[Y] 0.15737E+02 c Velocity[Z] 0.61592E-05 c Pressure 0.17759E-03 139 0.86578E-04 0.41222E-02 0.11776E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.2241 18.335 5.6057 7.9988 v Velocity[Y] -10.376 11.947 -0.14292 -0.00067288 v Velocity[Z] -3.086 2.9772 3.4469e-06 -5.3857e-08 v ǁVelocityǁ 0.00013947 19.461 6.4272 8.0047 v Pressure -2.2503e+05 59298 -74346 -43008 v TurbVisc 1.9074e-22 0.0049666 9.0106e-05 4.4276e-06 v CourantNb 2.5045e-08 0.011765 0.00016629 4.8812e-06 v FourierNb 1.2425e-07 0.046713 0.00014536 1.6055e-07 v total_pressure -1.237e+05 1.6062e+05 26979 58317 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.065 0.1082 0.0031503 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2178e-07 0.051893 0.00031165 5.0417e-06 INSTANT 0.874962000E-01 TIME STEP NUMBER 55160 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282795910E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.608060784E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.49563E-02 0.21030E+01 Friction velocity uk : 0.49563E-02 0.21030E+01 Dimensionless distance yplus : 0.47662E-02 0.20650E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.148867023e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29428E+08 1 0.22823E-09 0.31600E+02 0.22185E+04 c Velocity[X] 0.15919E+02 c Velocity[Y] 0.15682E+02 c Velocity[Z] 0.61703E-05 c Pressure 0.17928E-03 26 0.70713E-04 0.41529E-02 0.12003E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.2568 18.364 5.6056 7.9986 v Velocity[Y] -10.376 11.947 -0.14292 -0.0006729 v Velocity[Z] -3.0856 2.9772 3.4458e-06 -5.3857e-08 v ǁVelocityǁ 0.00018452 19.494 6.4281 8.0046 v Pressure -2.2486e+05 59409 -73470 -42498 v TurbVisc 5.9321e-23 0.0049666 9.0291e-05 4.4418e-06 v CourantNb 3.7355e-08 0.011765 0.00016629 4.8811e-06 v FourierNb 1.2425e-07 0.046713 0.00014536 1.6065e-07 v total_pressure -1.2354e+05 1.6073e+05 27855 58827 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.065 0.10815 0.003148 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2177e-07 0.051893 0.00031165 5.0418e-06 INSTANT 0.874963000E-01 TIME STEP NUMBER 55161 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282789345E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.608213438E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.69859E-02 0.21027E+01 Friction velocity uk : 0.69859E-02 0.21027E+01 Dimensionless distance yplus : 0.67179E-02 0.20647E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -8.048532451e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29427E+08 1 0.22791E-09 0.31488E+02 0.22146E+04 c Velocity[X] 0.15861E+02 c Velocity[Y] 0.15627E+02 c Velocity[Z] 0.62042E-05 c Pressure 0.18099E-03 10 0.56747E-04 0.41843E-02 0.12178E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.2896 18.393 5.6055 7.9985 v Velocity[Y] -10.376 11.946 -0.14291 -0.0006733 v Velocity[Z] -3.0853 2.9772 3.4447e-06 -5.3857e-08 v ǁVelocityǁ 0.00021413 19.528 6.429 8.0045 v Pressure -2.2462e+05 59534 -72513 -41981 v TurbVisc 7.3016e-22 0.0049666 9.0475e-05 4.4559e-06 v CourantNb 4.9214e-08 0.011765 0.00016629 4.8811e-06 v FourierNb 1.2425e-07 0.046712 0.00014537 1.6075e-07 v total_pressure -1.2329e+05 1.6086e+05 28812 59344 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0647 0.1081 0.003146 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2176e-07 0.051891 0.00031165 5.0418e-06 INSTANT 0.874964000E-01 TIME STEP NUMBER 55162 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282782904E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.608317862E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10184E-01 0.21023E+01 Friction velocity uk : 0.10184E-01 0.21023E+01 Dimensionless distance yplus : 0.97935E-02 0.20643E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -4.297360339e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29427E+08 1 0.22759E-09 0.31380E+02 0.22108E+04 c Velocity[X] 0.15804E+02 c Velocity[Y] 0.15576E+02 c Velocity[Z] 0.62456E-05 c Pressure 0.18281E-03 57 0.82056E-04 0.42181E-02 0.15089E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.3224 18.422 5.6054 7.9984 v Velocity[Y] -10.375 11.945 -0.1429 -0.00067336 v Velocity[Z] -3.0849 2.9773 3.4436e-06 -5.3857e-08 v ǁVelocityǁ 0.00028372 19.561 6.4299 8.0044 v Pressure -2.2426e+05 59699 -71762 -41373 v TurbVisc 2.1489e-22 0.0049667 9.0658e-05 4.47e-06 v CourantNb 5.1854e-08 0.011765 0.00016629 4.8811e-06 v FourierNb 1.2425e-07 0.046709 0.00014537 1.6086e-07 v total_pressure -1.2294e+05 1.6102e+05 29563 59952 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0643 0.10807 0.0031444 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2175e-07 0.051888 0.00031165 5.0419e-06 INSTANT 0.874965000E-01 TIME STEP NUMBER 55163 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282776492E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.608382447E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13568E-01 0.21018E+01 Friction velocity uk : 0.13568E-01 0.21018E+01 Dimensionless distance yplus : 0.13047E-01 0.20637E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.390301638e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29426E+08 1 0.22728E-09 0.31273E+02 0.22070E+04 c Velocity[X] 0.15749E+02 c Velocity[Y] 0.15525E+02 c Velocity[Z] 0.62867E-05 c Pressure 0.18329E-03 27 0.69408E-04 0.42208E-02 0.15092E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.3552 18.452 5.6053 7.9982 v Velocity[Y] -10.375 11.943 -0.1429 -0.00067326 v Velocity[Z] -3.0846 2.9773 3.4425e-06 -5.3857e-08 v ǁVelocityǁ 0.00030636 19.593 6.4308 8.0044 v Pressure -2.2378e+05 59924 -70728 -40753 v TurbVisc 1.1123e-23 0.0049667 9.084e-05 4.4842e-06 v CourantNb 3.9728e-08 0.011765 0.00016629 4.881e-06 v FourierNb 1.2425e-07 0.046705 0.00014537 1.6096e-07 v total_pressure -1.2246e+05 1.6125e+05 30597 60572 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0637 0.10804 0.003143 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2174e-07 0.051883 0.00031166 5.042e-06 INSTANT 0.874966000E-01 TIME STEP NUMBER 55164 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282770185E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.608488672E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.16236E-01 0.21010E+01 Friction velocity uk : 0.16236E-01 0.21010E+01 Dimensionless distance yplus : 0.15613E-01 0.20630E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.780613580e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29426E+08 1 0.22697E-09 0.31167E+02 0.22033E+04 c Velocity[X] 0.15693E+02 c Velocity[Y] 0.15474E+02 c Velocity[Z] 0.63467E-05 c Pressure 0.18438E-03 10 0.59116E-04 0.42374E-02 0.14501E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.388 18.482 5.6053 7.9981 v Velocity[Y] -10.375 11.94 -0.14289 -0.00067288 v Velocity[Z] -3.0843 2.9773 3.4414e-06 -5.3857e-08 v ǁVelocityǁ 0.00033384 19.625 6.4317 8.0043 v Pressure -2.2316e+05 60226 -69648 -40164 v TurbVisc 1.2627e-22 0.0049667 9.1021e-05 4.4983e-06 v CourantNb 1.9752e-08 0.011765 0.00016629 4.881e-06 v FourierNb 1.2425e-07 0.046699 0.00014538 1.6106e-07 v total_pressure -1.2183e+05 1.6155e+05 31677 61161 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.063 0.10803 0.003142 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2173e-07 0.051876 0.00031166 5.0421e-06 INSTANT 0.874967000E-01 TIME STEP NUMBER 55165 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282763990E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.608539283E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15823E-01 0.21001E+01 Friction velocity uk : 0.15823E-01 0.21001E+01 Dimensionless distance yplus : 0.15261E-01 0.20621E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 5.100920806e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29425E+08 1 0.22666E-09 0.31066E+02 0.21997E+04 c Velocity[X] 0.15640E+02 c Velocity[Y] 0.15426E+02 c Velocity[Z] 0.64029E-05 c Pressure 0.18598E-03 28 0.85433E-04 0.42660E-02 0.16692E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.4206 18.512 5.6052 7.998 v Velocity[Y] -10.375 11.938 -0.14289 -0.0006727 v Velocity[Z] -3.0839 2.9773 3.4403e-06 -5.3857e-08 v ǁVelocityǁ 0.00038313 19.657 6.4327 8.0042 v Pressure -2.2237e+05 60628 -68775 -39528 v TurbVisc 8.7885e-24 0.0049667 9.1201e-05 4.5124e-06 v CourantNb 1.725e-08 0.011765 0.00016629 4.881e-06 v FourierNb 1.2425e-07 0.046693 0.00014538 1.6117e-07 v total_pressure -1.2105e+05 1.6195e+05 32550 61797 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0621 0.10803 0.0031412 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2172e-07 0.051868 0.00031167 5.0422e-06 INSTANT 0.874968000E-01 TIME STEP NUMBER 55166 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282757861E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.608555780E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.16044E-01 0.20991E+01 Friction velocity uk : 0.16044E-01 0.20991E+01 Dimensionless distance yplus : 0.15707E-01 0.20611E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 7.071345463e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29425E+08 1 0.22635E-09 0.30965E+02 0.21962E+04 c Velocity[X] 0.15586E+02 c Velocity[Y] 0.15378E+02 c Velocity[Z] 0.64499E-05 c Pressure 0.18662E-03 27 0.70019E-04 0.42725E-02 0.16843E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.4531 18.542 5.6051 7.9979 v Velocity[Y] -10.374 11.935 -0.14289 -0.0006728 v Velocity[Z] -3.0836 2.9774 3.4392e-06 -5.3857e-08 v ǁVelocityǁ 0.00040133 19.688 6.4336 8.0041 v Pressure -2.2142e+05 61143 -67610 -38870 v TurbVisc 2.8587e-23 0.0049667 9.138e-05 4.5266e-06 v CourantNb 2.1524e-08 0.011765 0.00016629 4.881e-06 v FourierNb 1.2425e-07 0.046686 0.00014538 1.6127e-07 v total_pressure -1.201e+05 1.6247e+05 33715 62455 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0611 0.10805 0.0031408 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2171e-07 0.051858 0.00031167 5.0422e-06 INSTANT 0.874969000E-01 TIME STEP NUMBER 55167 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282751856E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.608613779E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11892E-01 0.20979E+01 Friction velocity uk : 0.11892E-01 0.20979E+01 Dimensionless distance yplus : 0.11482E-01 0.20600E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 9.467538151e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29424E+08 1 0.22605E-09 0.30864E+02 0.21926E+04 c Velocity[X] 0.15533E+02 c Velocity[Y] 0.15331E+02 c Velocity[Z] 0.65065E-05 c Pressure 0.18834E-03 10 0.58636E-04 0.43037E-02 0.16503E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.4854 18.573 5.6051 7.9977 v Velocity[Y] -10.374 11.962 -0.14288 -0.00067328 v Velocity[Z] -3.0833 2.9774 3.4381e-06 -5.3857e-08 v ǁVelocityǁ 0.00040909 19.718 6.4346 8.004 v Pressure -2.203e+05 61784 -66395 -38228 v TurbVisc 1.5852e-21 0.0049667 9.1558e-05 4.5407e-06 v CourantNb 3.8822e-08 0.011765 0.00016629 4.8809e-06 v FourierNb 1.2425e-07 0.046677 0.00014539 1.6137e-07 v total_pressure -1.1897e+05 1.6311e+05 34930 63097 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.06 0.10807 0.0031406 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.217e-07 0.051848 0.00031168 5.0423e-06 INSTANT 0.874970000E-01 TIME STEP NUMBER 55168 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282746003E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.608624809E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15173E-01 0.20967E+01 Friction velocity uk : 0.15173E-01 0.20967E+01 Dimensionless distance yplus : 0.15094E-01 0.20588E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.174576861e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29424E+08 1 0.22575E-09 0.30766E+02 0.21891E+04 c Velocity[X] 0.15481E+02 c Velocity[Y] 0.15285E+02 c Velocity[Z] 0.65492E-05 c Pressure 0.19087E-03 24 0.81550E-04 0.43532E-02 0.20164E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.5175 18.603 5.605 7.9976 v Velocity[Y] -10.374 11.991 -0.14288 -0.0006734 v Velocity[Z] -3.0829 2.9774 3.437e-06 -5.3857e-08 v ǁVelocityǁ 0.00042575 19.748 6.4355 8.004 v Pressure -2.1905e+05 62564 -65355 -37489 v TurbVisc 2.5975e-21 0.0049668 9.1735e-05 4.5548e-06 v CourantNb 4.9983e-08 0.011765 0.00016629 4.8809e-06 v FourierNb 1.2425e-07 0.046668 0.00014539 1.6148e-07 v total_pressure -1.1773e+05 1.6389e+05 35970 63836 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0588 0.10809 0.0031406 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2169e-07 0.051837 0.00031168 5.0424e-06 INSTANT 0.874971000E-01 TIME STEP NUMBER 55169 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282740187E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.608615660E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.80295E-02 0.20955E+01 Friction velocity uk : 0.80295E-02 0.20955E+01 Dimensionless distance yplus : 0.77566E-02 0.20576E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.248358677e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29423E+08 1 0.22545E-09 0.30668E+02 0.21857E+04 c Velocity[X] 0.15428E+02 c Velocity[Y] 0.15240E+02 c Velocity[Z] 0.65755E-05 c Pressure 0.19291E-03 19 0.69126E-04 0.43915E-02 0.20342E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.5494 18.634 5.605 7.9975 v Velocity[Y] -10.404 12.02 -0.14288 -0.00067337 v Velocity[Z] -3.0826 2.9775 3.4359e-06 -5.3857e-08 v ǁVelocityǁ 0.00042523 19.777 6.4365 8.0039 v Pressure -2.1773e+05 63488 -64062 -36734 v TurbVisc 1.0297e-20 0.0049668 9.1911e-05 4.569e-06 v CourantNb 7.1888e-08 0.011765 0.0001663 4.8809e-06 v FourierNb 1.2425e-07 0.046659 0.00014539 1.6158e-07 v total_pressure -1.1641e+05 1.6481e+05 37263 64591 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0576 0.10813 0.0031408 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2168e-07 0.051826 0.00031169 5.0425e-06 INSTANT 0.874972000E-01 TIME STEP NUMBER 55170 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282734503E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.608640740E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.21041E-01 0.20942E+01 Friction velocity uk : 0.21041E-01 0.20942E+01 Dimensionless distance yplus : 0.20298E-01 0.20563E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.371930851e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29423E+08 1 0.22516E-09 0.30571E+02 0.21822E+04 c Velocity[X] 0.15376E+02 c Velocity[Y] 0.15195E+02 c Velocity[Z] 0.66003E-05 c Pressure 0.19597E-03 10 0.59141E-04 0.44528E-02 0.19282E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.581 18.665 5.6049 7.9974 v Velocity[Y] -10.439 12.049 -0.14289 -0.00067307 v Velocity[Z] -3.0823 2.9775 3.4348e-06 -5.3857e-08 v ǁVelocityǁ 0.00042408 19.806 6.4375 8.0038 v Pressure -2.1656e+05 64562 -62755 -36027 v TurbVisc 7.5721e-21 0.0049668 9.2086e-05 4.5832e-06 v CourantNb 1.0247e-08 0.011765 0.0001663 4.8809e-06 v FourierNb 1.2425e-07 0.046649 0.0001454 1.6168e-07 v total_pressure -1.1523e+05 1.6589e+05 38570 65298 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0563 0.10817 0.0031411 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2167e-07 0.051814 0.0003117 5.0426e-06 INSTANT 0.874973000E-01 TIME STEP NUMBER 55171 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282728954E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.608639308E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15467E-01 0.20929E+01 Friction velocity uk : 0.15467E-01 0.20929E+01 Dimensionless distance yplus : 0.14945E-01 0.20550E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.465043914e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29422E+08 1 0.22487E-09 0.30475E+02 0.21788E+04 c Velocity[X] 0.15324E+02 c Velocity[Y] 0.15151E+02 c Velocity[Z] 0.66040E-05 c Pressure 0.19964E-03 36 0.85537E-04 0.45276E-02 0.22151E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.6123 18.695 5.6049 7.9973 v Velocity[Y] -10.473 12.077 -0.14289 -0.00067294 v Velocity[Z] -3.0819 2.9775 3.4337e-06 -5.3857e-08 v ǁVelocityǁ 0.00042033 19.835 6.4385 8.0038 v Pressure -2.1521e+05 66028 -61531 -35268 v TurbVisc 2.0212e-21 0.0049668 9.2261e-05 4.5973e-06 v CourantNb 7.0034e-08 0.011765 0.0001663 4.8809e-06 v FourierNb 1.2425e-07 0.04664 0.0001454 1.6179e-07 v total_pressure -1.1388e+05 1.6735e+05 39794 66057 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.055 0.1082 0.0031415 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2166e-07 0.051802 0.0003117 5.0427e-06 INSTANT 0.874974000E-01 TIME STEP NUMBER 55172 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282723484E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.608639390E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.79603E-02 0.20917E+01 Friction velocity uk : 0.79603E-02 0.20917E+01 Dimensionless distance yplus : 0.76851E-02 0.20539E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.418821743e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29422E+08 1 0.22458E-09 0.30379E+02 0.21754E+04 c Velocity[X] 0.15273E+02 c Velocity[Y] 0.15106E+02 c Velocity[Z] 0.65923E-05 c Pressure 0.20320E-03 27 0.70026E-04 0.45999E-02 0.21680E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.6433 18.726 5.6049 7.9972 v Velocity[Y] -10.506 12.105 -0.14289 -0.0006731 v Velocity[Z] -3.0816 2.9775 3.4326e-06 -5.3857e-08 v ǁVelocityǁ 0.00040002 19.863 6.4395 8.0037 v Pressure -2.1369e+05 67746 -60136 -34513 v TurbVisc 2.1638e-21 0.0049668 9.2435e-05 4.6116e-06 v CourantNb 7.5597e-08 0.011765 0.00016631 4.8809e-06 v FourierNb 1.2425e-07 0.046631 0.0001454 1.6189e-07 v total_pressure -1.1236e+05 1.6907e+05 41189 66812 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0539 0.10824 0.0031419 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2165e-07 0.051792 0.00031171 5.0427e-06 INSTANT 0.874975000E-01 TIME STEP NUMBER 55173 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282718151E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.608659850E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10137E-01 0.20905E+01 Friction velocity uk : 0.10137E-01 0.20905E+01 Dimensionless distance yplus : 0.97925E-02 0.20527E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.410775107e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29421E+08 1 0.22430E-09 0.30284E+02 0.21719E+04 c Velocity[X] 0.15221E+02 c Velocity[Y] 0.15062E+02 c Velocity[Z] 0.65722E-05 c Pressure 0.20721E-03 11 0.58164E-04 0.46820E-02 0.21679E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.674 18.757 5.6049 7.9971 v Velocity[Y] -10.539 12.134 -0.1429 -0.00067368 v Velocity[Z] -3.0812 2.9776 3.4315e-06 -5.3857e-08 v ǁVelocityǁ 0.000368 19.891 6.4405 8.0036 v Pressure -2.12e+05 69591 -58731 -33764 v TurbVisc 1.8924e-21 0.0049669 9.2608e-05 4.6258e-06 v CourantNb 2.2711e-08 0.011765 0.00016631 4.8808e-06 v FourierNb 1.2425e-07 0.046622 0.00014541 1.6199e-07 v total_pressure -1.1068e+05 1.7092e+05 42594 67561 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0527 0.10827 0.0031424 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2165e-07 0.051781 0.00031172 5.0428e-06 INSTANT 0.874976000E-01 TIME STEP NUMBER 55174 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282712997E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.608679114E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.74182E-02 0.20894E+01 Friction velocity uk : 0.74182E-02 0.20894E+01 Dimensionless distance yplus : 0.71445E-02 0.20516E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.368137507e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29421E+08 1 0.22402E-09 0.30189E+02 0.21685E+04 c Velocity[X] 0.15170E+02 c Velocity[Y] 0.15019E+02 c Velocity[Z] 0.65239E-05 c Pressure 0.21136E-03 24 0.81969E-04 0.47671E-02 0.26016E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.7044 18.787 5.6049 7.997 v Velocity[Y] -10.571 12.162 -0.14291 -0.00067384 v Velocity[Z] -3.0809 2.9776 3.4304e-06 -5.3857e-08 v ǁVelocityǁ 0.00034384 19.918 6.4415 8.0036 v Pressure -2.1018e+05 71548 -57314 -32922 v TurbVisc 2.6513e-21 0.0049669 9.278e-05 4.6399e-06 v CourantNb 3.8358e-08 0.011765 0.00016632 4.8808e-06 v FourierNb 1.2425e-07 0.046614 0.00014541 1.621e-07 v total_pressure -1.0885e+05 1.7287e+05 44011 68403 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0516 0.1083 0.0031428 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2164e-07 0.051771 0.00031173 5.0429e-06 INSTANT 0.874977000E-01 TIME STEP NUMBER 55175 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282707887E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.608718488E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.67748E-02 0.20885E+01 Friction velocity uk : 0.67748E-02 0.20885E+01 Dimensionless distance yplus : 0.65248E-02 0.20508E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.226904585e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29420E+08 1 0.22374E-09 0.30094E+02 0.21652E+04 c Velocity[X] 0.15118E+02 c Velocity[Y] 0.14976E+02 c Velocity[Z] 0.64702E-05 c Pressure 0.21570E-03 66 0.69400E-04 0.48561E-02 0.26267E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.7344 18.817 5.6049 7.9969 v Velocity[Y] -10.604 12.19 -0.14292 -0.00067381 v Velocity[Z] -3.0806 2.9776 3.4293e-06 -5.3857e-08 v ǁVelocityǁ 0.0002927 19.945 6.4426 8.0035 v Pressure -2.0823e+05 73600 -55812 -32066 v TurbVisc 5.0267e-21 0.0049669 9.2952e-05 4.6542e-06 v CourantNb 7.6053e-08 0.011765 0.00016632 4.8808e-06 v FourierNb 1.2425e-07 0.046608 0.00014541 1.622e-07 v total_pressure -1.069e+05 1.7493e+05 45513 69259 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0508 0.10832 0.0031431 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2163e-07 0.051763 0.00031173 5.043e-06 INSTANT 0.874978000E-01 TIME STEP NUMBER 55176 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282702928E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.608760582E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.97210E-02 0.20878E+01 Friction velocity uk : 0.97210E-02 0.20878E+01 Dimensionless distance yplus : 0.93623E-02 0.20500E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.100840662e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29420E+08 1 0.22346E-09 0.30001E+02 0.21618E+04 c Velocity[X] 0.15068E+02 c Velocity[Y] 0.14934E+02 c Velocity[Z] 0.64023E-05 c Pressure 0.21974E-03 11 0.59668E-04 0.49382E-02 0.25426E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.7641 18.847 5.6049 7.9968 v Velocity[Y] -10.635 12.218 -0.14293 -0.00067362 v Velocity[Z] -3.0802 2.9776 3.4282e-06 -5.3857e-08 v ǁVelocityǁ 0.00024964 19.972 6.4436 8.0035 v Pressure -2.0616e+05 75738 -54337 -31254 v TurbVisc 4.4703e-21 0.0049669 9.3123e-05 4.6684e-06 v CourantNb 8.9523e-08 0.011765 0.00016632 4.8808e-06 v FourierNb 1.2425e-07 0.046602 0.00014541 1.623e-07 v total_pressure -1.0484e+05 1.7706e+05 46988 70071 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.05 0.10833 0.0031433 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2162e-07 0.051757 0.00031174 5.0431e-06 INSTANT 0.874979000E-01 TIME STEP NUMBER 55177 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282698126E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.608823119E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.53798E-02 0.20871E+01 Friction velocity uk : 0.53798E-02 0.20871E+01 Dimensionless distance yplus : 0.51813E-02 0.20493E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 9.514377335e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29419E+08 1 0.22319E-09 0.29908E+02 0.21585E+04 c Velocity[X] 0.15017E+02 c Velocity[Y] 0.14891E+02 c Velocity[Z] 0.63136E-05 c Pressure 0.22340E-03 54 0.86742E-04 0.50114E-02 0.28473E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.7935 18.877 5.6049 7.9967 v Velocity[Y] -10.667 12.246 -0.14294 -0.00067351 v Velocity[Z] -3.0799 2.9777 3.4271e-06 -5.3857e-08 v ǁVelocityǁ 0.00020343 19.999 6.4446 8.0034 v Pressure -2.0401e+05 77941 -52735 -30406 v TurbVisc 2.5859e-21 0.0049669 9.3293e-05 4.6827e-06 v CourantNb 7.9316e-08 0.011765 0.00016633 4.8808e-06 v FourierNb 1.2425e-07 0.046597 0.00014542 1.6241e-07 v total_pressure -1.0268e+05 1.7927e+05 48590 70919 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0493 0.10834 0.0031434 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2161e-07 0.051751 0.00031174 5.0432e-06 INSTANT 0.874980000E-01 TIME STEP NUMBER 55178 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282693411E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.608919791E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.69978E-02 0.20867E+01 Friction velocity uk : 0.69978E-02 0.20867E+01 Dimensionless distance yplus : 0.67396E-02 0.20489E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 7.572580434e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29419E+08 1 0.22292E-09 0.29817E+02 0.21552E+04 c Velocity[X] 0.14967E+02 c Velocity[Y] 0.14850E+02 c Velocity[Z] 0.62265E-05 c Pressure 0.22749E-03 27 0.70815E-04 0.50941E-02 0.28278E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.8227 18.907 5.6049 7.9966 v Velocity[Y] -10.698 12.275 -0.14295 -0.00067371 v Velocity[Z] -3.0796 2.9777 3.426e-06 -5.3857e-08 v ǁVelocityǁ 0.00015588 20.025 6.4456 8.0034 v Pressure -2.0177e+05 80189 -51177 -29558 v TurbVisc 4.2075e-21 0.004967 9.3463e-05 4.697e-06 v CourantNb 8.3108e-08 0.011765 0.00016633 4.8808e-06 v FourierNb 1.2425e-07 0.046594 0.00014542 1.6251e-07 v total_pressure -1.0045e+05 1.8151e+05 50148 71767 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0489 0.10833 0.0031433 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2161e-07 0.051747 0.00031175 5.0433e-06 INSTANT 0.874981000E-01 TIME STEP NUMBER 55179 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282688850E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.608997553E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.71658E-02 0.20864E+01 Friction velocity uk : 0.71658E-02 0.20864E+01 Dimensionless distance yplus : 0.69014E-02 0.20487E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 5.620927700e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29419E+08 1 0.22266E-09 0.29728E+02 0.21520E+04 c Velocity[X] 0.14919E+02 c Velocity[Y] 0.14809E+02 c Velocity[Z] 0.61232E-05 c Pressure 0.23058E-03 11 0.60239E-04 0.51542E-02 0.28437E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.8515 18.936 5.6049 7.9965 v Velocity[Y] -10.729 12.304 -0.14296 -0.00067435 v Velocity[Z] -3.0792 2.9777 3.4249e-06 -5.3857e-08 v ǁVelocityǁ 0.00010412 20.052 6.4466 8.0033 v Pressure -1.9948e+05 82476 -49639 -28717 v TurbVisc 9.3641e-21 0.004967 9.3632e-05 4.7113e-06 v CourantNb 3.2518e-08 0.011765 0.00016633 4.8808e-06 v FourierNb 1.2425e-07 0.046593 0.00014542 1.6262e-07 v total_pressure -98154 1.838e+05 51686 72608 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0487 0.10831 0.003143 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.216e-07 0.051746 0.00031175 5.0434e-06 INSTANT 0.874982000E-01 TIME STEP NUMBER 55180 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282684491E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.609112310E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.77531E-02 0.20863E+01 Friction velocity uk : 0.77531E-02 0.20863E+01 Dimensionless distance yplus : 0.74670E-02 0.20485E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 3.365662983e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29418E+08 1 0.22239E-09 0.29638E+02 0.21487E+04 c Velocity[X] 0.14869E+02 c Velocity[Y] 0.14769E+02 c Velocity[Z] 0.60091E-05 c Pressure 0.23295E-03 76 0.83072E-04 0.51979E-02 0.33961E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.8801 18.965 5.6049 7.9964 v Velocity[Y] -10.76 12.333 -0.14298 -0.00067455 v Velocity[Z] -3.0789 2.9777 3.4238e-06 -5.3857e-08 v ǁVelocityǁ 7.6524e-05 20.078 6.4477 8.0033 v Pressure -1.9715e+05 84780 -47869 -27784 v TurbVisc 2.2352e-21 0.004967 9.38e-05 4.7256e-06 v CourantNb 2.505e-08 0.011765 0.00016634 4.8808e-06 v FourierNb 1.2425e-07 0.046593 0.00014542 1.6272e-07 v total_pressure -95822 1.8611e+05 53456 73541 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0485 0.10828 0.0031424 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2159e-07 0.051745 0.00031176 5.0435e-06 INSTANT 0.874983000E-01 TIME STEP NUMBER 55181 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282680182E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.609265438E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.61074E-02 0.20864E+01 Friction velocity uk : 0.61074E-02 0.20864E+01 Dimensionless distance yplus : 0.58821E-02 0.20487E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.462519906e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29418E+08 1 0.22213E-09 0.29552E+02 0.21456E+04 c Velocity[X] 0.14822E+02 c Velocity[Y] 0.14730E+02 c Velocity[Z] 0.59013E-05 c Pressure 0.23597E-03 24 0.70400E-04 0.52560E-02 0.34216E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.9085 18.994 5.6049 7.9963 v Velocity[Y] -10.79 12.363 -0.14299 -0.00067457 v Velocity[Z] -3.0785 2.9778 3.4227e-06 -5.3857e-08 v ǁVelocityǁ 8.2243e-05 20.105 6.4487 8.0032 v Pressure -1.9479e+05 87085 -46241 -26844 v TurbVisc 3.3315e-21 0.004967 9.3968e-05 4.74e-06 v CourantNb 2.6135e-08 0.011765 0.00016634 4.8808e-06 v FourierNb 1.2425e-07 0.046594 0.00014542 1.6283e-07 v total_pressure -93463 1.8841e+05 55084 74481 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0487 0.10824 0.0031416 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2158e-07 0.051747 0.00031176 5.0436e-06 INSTANT 0.874984000E-01 TIME STEP NUMBER 55182 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282676037E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.609380856E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.57020E-02 0.20867E+01 Friction velocity uk : 0.57020E-02 0.20867E+01 Dimensionless distance yplus : 0.54917E-02 0.20490E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -7.815381860e-03 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29417E+08 1 0.22188E-09 0.29469E+02 0.21426E+04 c Velocity[X] 0.14776E+02 c Velocity[Y] 0.14693E+02 c Velocity[Z] 0.57818E-05 c Pressure 0.23761E-03 11 0.62952E-04 0.52832E-02 0.33436E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.9367 19.023 5.6049 7.9962 v Velocity[Y] -10.821 12.393 -0.14301 -0.00067434 v Velocity[Z] -3.0782 2.9778 3.4216e-06 -5.3857e-08 v ǁVelocityǁ 0.00014022 20.132 6.4497 8.0032 v Pressure -1.9242e+05 89388 -44621 -25948 v TurbVisc 9.4521e-21 0.004967 9.4135e-05 4.7543e-06 v CourantNb 4.128e-08 0.011765 0.00016634 4.8808e-06 v FourierNb 1.2425e-07 0.046597 0.00014542 1.6293e-07 v total_pressure -91100 1.9071e+05 56704 75377 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.049 0.10819 0.0031405 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2158e-07 0.051751 0.00031176 5.0438e-06 INSTANT 0.874985000E-01 TIME STEP NUMBER 55183 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282672073E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.609538750E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.73111E-02 0.20871E+01 Friction velocity uk : 0.73111E-02 0.20871E+01 Dimensionless distance yplus : 0.70414E-02 0.20494E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -3.179151179e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29417E+08 1 0.22162E-09 0.29386E+02 0.21395E+04 c Velocity[X] 0.14730E+02 c Velocity[Y] 0.14655E+02 c Velocity[Z] 0.56612E-05 c Pressure 0.23851E-03 67 0.88271E-04 0.52937E-02 0.38257E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.9646 19.051 5.6049 7.9962 v Velocity[Y] -10.851 12.423 -0.14302 -0.00067423 v Velocity[Z] -3.0779 2.9778 3.4205e-06 -5.3857e-08 v ǁVelocityǁ 0.0001892 20.159 6.4507 8.0032 v Pressure -1.9007e+05 91671 -42759 -25003 v TurbVisc 1.5657e-20 0.0049671 9.4302e-05 4.7687e-06 v CourantNb 5.4068e-08 0.011766 0.00016634 4.8808e-06 v FourierNb 1.2425e-07 0.046601 0.00014541 1.6303e-07 v total_pressure -88747 1.93e+05 58566 76322 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0494 0.10813 0.0031392 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2157e-07 0.051756 0.00031176 5.0439e-06 INSTANT 0.874986000E-01 TIME STEP NUMBER 55184 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282668205E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.609729018E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.88534E-02 0.20878E+01 Friction velocity uk : 0.88534E-02 0.20878E+01 Dimensionless distance yplus : 0.85268E-02 0.20500E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -4.681559294e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29417E+08 1 0.22137E-09 0.29306E+02 0.21366E+04 c Velocity[X] 0.14687E+02 c Velocity[Y] 0.14619E+02 c Velocity[Z] 0.55539E-05 c Pressure 0.24014E-03 27 0.71895E-04 0.53206E-02 0.38025E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -9.9924 19.079 5.6049 7.9961 v Velocity[Y] -10.881 12.454 -0.14304 -0.00067445 v Velocity[Z] -3.0775 2.9778 3.4194e-06 -5.3857e-08 v ǁVelocityǁ 0.00023894 20.186 6.4517 8.0031 v Pressure -1.8773e+05 93922 -41073 -24065 v TurbVisc 1.4726e-21 0.0049671 9.4468e-05 4.7831e-06 v CourantNb 1.5272e-08 0.011765 0.00016634 4.8808e-06 v FourierNb 1.2425e-07 0.046607 0.00014541 1.6314e-07 v total_pressure -86407 1.9525e+05 60252 77260 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.05 0.10805 0.0031377 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2156e-07 0.051763 0.00031176 5.044e-06 INSTANT 0.874987000E-01 TIME STEP NUMBER 55185 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282664508E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.609872645E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.99329E-02 0.20885E+01 Friction velocity uk : 0.99329E-02 0.20885E+01 Dimensionless distance yplus : 0.95664E-02 0.20508E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -6.678834479e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29416E+08 1 0.22112E-09 0.29230E+02 0.21339E+04 c Velocity[X] 0.14645E+02 c Velocity[Y] 0.14585E+02 c Velocity[Z] 0.54382E-05 c Pressure 0.24044E-03 11 0.63876E-04 0.53180E-02 0.38439E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -10.02 19.107 5.6049 7.996 v Velocity[Y] -10.912 12.485 -0.14305 -0.00067512 v Velocity[Z] -3.0772 2.9779 3.4183e-06 -5.3857e-08 v ǁVelocityǁ 0.00030654 20.214 6.4527 8.0031 v Pressure -1.8541e+05 96149 -39395 -23140 v TurbVisc 6.0344e-21 0.0049671 9.4634e-05 4.7975e-06 v CourantNb 4.521e-08 0.011765 0.00016635 4.8808e-06 v FourierNb 1.2425e-07 0.046614 0.00014541 1.6324e-07 v total_pressure -84088 1.9747e+05 61930 78185 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0508 0.10797 0.0031359 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2156e-07 0.051771 0.00031176 5.0441e-06 INSTANT 0.874988000E-01 TIME STEP NUMBER 55186 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282661030E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.610054720E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11195E-01 0.20894E+01 Friction velocity uk : 0.11195E-01 0.20894E+01 Dimensionless distance yplus : 0.10782E-01 0.20516E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -8.637480662e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29416E+08 1 0.22087E-09 0.29153E+02 0.21311E+04 c Velocity[X] 0.14603E+02 c Velocity[Y] 0.14551E+02 c Velocity[Z] 0.53294E-05 c Pressure 0.24024E-03 77 0.84265E-04 0.53043E-02 0.46490E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -10.048 19.134 5.605 7.9959 v Velocity[Y] -10.942 12.516 -0.14307 -0.00067532 v Velocity[Z] -3.0768 2.9779 3.4172e-06 -5.3857e-08 v ǁVelocityǁ 0.00034798 20.241 6.4537 8.0031 v Pressure -1.8314e+05 98350 -37466 -22111 v TurbVisc 1.2238e-20 0.0049671 9.4799e-05 4.8119e-06 v CourantNb 3.9644e-08 0.011766 0.00016635 4.8809e-06 v FourierNb 1.2425e-07 0.046621 0.00014541 1.6335e-07 v total_pressure -81819 1.9967e+05 63859 79214 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0516 0.10789 0.0031339 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2155e-07 0.051781 0.00031176 5.0442e-06 INSTANT 0.874989000E-01 TIME STEP NUMBER 55187 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282657614E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.610260501E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10529E-01 0.20904E+01 Friction velocity uk : 0.10529E-01 0.20904E+01 Dimensionless distance yplus : 0.10140E-01 0.20526E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -9.479016860e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29416E+08 1 0.22062E-09 0.29080E+02 0.21284E+04 c Velocity[X] 0.14562E+02 c Velocity[Y] 0.14517E+02 c Velocity[Z] 0.52360E-05 c Pressure 0.24090E-03 19 0.71418E-04 0.53096E-02 0.46885E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -10.075 19.161 5.605 7.9959 v Velocity[Y] -10.972 12.547 -0.14308 -0.00067533 v Velocity[Z] -3.0765 2.9779 3.4161e-06 -5.3857e-08 v ǁVelocityǁ 0.00038891 20.269 6.4548 8.0031 v Pressure -1.8091e+05 1.005e+05 -35711 -21086 v TurbVisc 7.0236e-21 0.0049671 9.4964e-05 4.8264e-06 v CourantNb 2.1248e-08 0.011765 0.00016635 4.8809e-06 v FourierNb 1.2425e-07 0.04663 0.00014541 1.6345e-07 v total_pressure -79585 2.0182e+05 65614 80239 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0526 0.10779 0.0031317 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2155e-07 0.051791 0.00031175 5.0443e-06 INSTANT 0.874990000E-01 TIME STEP NUMBER 55188 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282654377E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.610420927E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.76537E-02 0.20915E+01 Friction velocity uk : 0.76537E-02 0.20915E+01 Dimensionless distance yplus : 0.73713E-02 0.20537E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.086414146e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29416E+08 1 0.22038E-09 0.29009E+02 0.21258E+04 c Velocity[X] 0.14523E+02 c Velocity[Y] 0.14485E+02 c Velocity[Z] 0.51452E-05 c Pressure 0.24065E-03 11 0.66559E-04 0.52947E-02 0.46915E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -10.103 19.189 5.605 7.9958 v Velocity[Y] -11.003 12.578 -0.14309 -0.0006751 v Velocity[Z] -3.0762 2.9779 3.415e-06 -5.3857e-08 v ǁVelocityǁ 0.00045726 20.298 6.4558 8.0031 v Pressure -1.7871e+05 1.026e+05 -33934 -20097 v TurbVisc 6.3903e-21 0.0049672 9.5128e-05 4.8409e-06 v CourantNb 2.0528e-08 0.011765 0.00016635 4.8809e-06 v FourierNb 1.2425e-07 0.046639 0.00014541 1.6356e-07 v total_pressure -77388 2.0393e+05 67391 81228 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0537 0.10769 0.0031293 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2154e-07 0.051802 0.00031175 5.0444e-06 INSTANT 0.874991000E-01 TIME STEP NUMBER 55189 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282651342E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.610610192E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.48351E-02 0.20926E+01 Friction velocity uk : 0.48351E-02 0.20926E+01 Dimensionless distance yplus : 0.46567E-02 0.20548E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.198363718e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29415E+08 1 0.22013E-09 0.28937E+02 0.21232E+04 c Velocity[X] 0.14485E+02 c Velocity[Y] 0.14453E+02 c Velocity[Z] 0.50627E-05 c Pressure 0.24042E-03 72 0.89519E-04 0.52805E-02 0.54384E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -10.13 19.216 5.605 7.9958 v Velocity[Y] -11.033 12.609 -0.1431 -0.00067496 v Velocity[Z] -3.0758 2.978 3.4139e-06 -5.3857e-08 v ǁVelocityǁ 0.0004853 20.326 6.4568 8.003 v Pressure -1.7657e+05 1.0467e+05 -32023 -19055 v TurbVisc 1.0632e-20 0.0049672 9.5291e-05 4.8554e-06 v CourantNb 3.2267e-08 0.011765 0.00016635 4.8809e-06 v FourierNb 1.2425e-07 0.046648 0.0001454 1.6366e-07 v total_pressure -75246 2.0599e+05 69302 82270 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0548 0.10758 0.0031268 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2154e-07 0.051814 0.00031175 5.0445e-06 INSTANT 0.874992000E-01 TIME STEP NUMBER 55190 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282648414E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.610809933E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.79149E-02 0.20938E+01 Friction velocity uk : 0.79149E-02 0.20938E+01 Dimensionless distance yplus : 0.76229E-02 0.20559E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.212082908e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29415E+08 1 0.21989E-09 0.28869E+02 0.21206E+04 c Velocity[X] 0.14447E+02 c Velocity[Y] 0.14421E+02 c Velocity[Z] 0.49969E-05 c Pressure 0.24085E-03 30 0.72781E-04 0.52806E-02 0.53999E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -10.157 19.242 5.605 7.9957 v Velocity[Y] -11.064 12.64 -0.14311 -0.00067517 v Velocity[Z] -3.0755 2.978 3.4129e-06 -5.3857e-08 v ǁVelocityǁ 0.00052489 20.355 6.4578 8.003 v Pressure -1.7447e+05 1.0667e+05 -30203 -18037 v TurbVisc 7.7604e-21 0.0049672 9.5454e-05 4.87e-06 v CourantNb 9.6131e-09 0.011765 0.00016634 4.8809e-06 v FourierNb 1.2425e-07 0.046658 0.0001454 1.6377e-07 v total_pressure -73143 2.08e+05 71122 83288 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0559 0.10747 0.0031242 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2153e-07 0.051825 0.00031175 5.0447e-06 INSTANT 0.874993000E-01 TIME STEP NUMBER 55191 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282645667E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.610981695E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.98228E-02 0.20950E+01 Friction velocity uk : 0.98228E-02 0.20950E+01 Dimensionless distance yplus : 0.94604E-02 0.20571E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.263055851e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29415E+08 1 0.21965E-09 0.28801E+02 0.21181E+04 c Velocity[X] 0.14411E+02 c Velocity[Y] 0.14390E+02 c Velocity[Z] 0.49404E-05 c Pressure 0.24094E-03 11 0.67974E-04 0.52735E-02 0.55508E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -10.184 19.269 5.605 7.9956 v Velocity[Y] -11.094 12.672 -0.14312 -0.00067586 v Velocity[Z] -3.0751 2.978 3.4118e-06 -5.3857e-08 v ǁVelocityǁ 0.00057595 20.385 6.4588 8.003 v Pressure -1.724e+05 1.0863e+05 -28358 -17031 v TurbVisc 9.5934e-21 0.0049672 9.5617e-05 4.8845e-06 v CourantNb 2.1861e-08 0.011765 0.00016634 4.8809e-06 v FourierNb 1.2425e-07 0.046667 0.0001454 1.6387e-07 v total_pressure -71077 2.0995e+05 72967 84294 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0571 0.10736 0.0031215 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2153e-07 0.051837 0.00031174 5.0448e-06 INSTANT 0.874994000E-01 TIME STEP NUMBER 55192 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282643160E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.611169711E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12353E-01 0.20961E+01 Friction velocity uk : 0.12353E-01 0.20961E+01 Dimensionless distance yplus : 0.11897E-01 0.20582E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.265434090e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29415E+08 1 0.21941E-09 0.28733E+02 0.21156E+04 c Velocity[X] 0.14374E+02 c Velocity[Y] 0.14359E+02 c Velocity[Z] 0.48903E-05 c Pressure 0.24146E-03 104 0.85336E-04 0.52756E-02 0.68976E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -10.211 19.296 5.605 7.9956 v Velocity[Y] -11.125 12.703 -0.14313 -0.00067603 v Velocity[Z] -3.0748 2.978 3.4107e-06 -5.3857e-08 v ǁVelocityǁ 0.00059485 20.414 6.4598 8.003 v Pressure -1.7038e+05 1.1054e+05 -26467 -15902 v TurbVisc 9.1487e-21 0.0049672 9.5779e-05 4.899e-06 v CourantNb 3.1793e-08 0.011765 0.00016634 4.8809e-06 v FourierNb 1.2425e-07 0.046676 0.0001454 1.6398e-07 v total_pressure -69055 2.1186e+05 74858 85423 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0582 0.10726 0.0031189 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2152e-07 0.051848 0.00031174 5.0449e-06 INSTANT 0.874995000E-01 TIME STEP NUMBER 55193 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282640723E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.611360765E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.65802E-02 0.20972E+01 Friction velocity uk : 0.65802E-02 0.20972E+01 Dimensionless distance yplus : 0.63565E-02 0.20593E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.219557171e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29414E+08 1 0.21918E-09 0.28667E+02 0.21132E+04 c Velocity[X] 0.14339E+02 c Velocity[Y] 0.14328E+02 c Velocity[Z] 0.48539E-05 c Pressure 0.24213E-03 19 0.72340E-04 0.52811E-02 0.69670E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -10.239 19.322 5.605 7.9955 v Velocity[Y] -11.156 12.734 -0.14314 -0.00067601 v Velocity[Z] -3.0745 2.9781 3.4096e-06 -5.3857e-08 v ǁVelocityǁ 0.00063411 20.444 6.4608 8.003 v Pressure -1.6853e+05 1.124e+05 -24567 -14798 v TurbVisc 7.4241e-21 0.0049672 9.5941e-05 4.9137e-06 v CourantNb 3.2649e-08 0.011765 0.00016634 4.8809e-06 v FourierNb 1.2425e-07 0.046685 0.0001454 1.6409e-07 v total_pressure -67209 2.1373e+05 76758 86527 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0593 0.10715 0.0031162 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2152e-07 0.051859 0.00031174 5.045e-06 INSTANT 0.874996000E-01 TIME STEP NUMBER 55194 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282638483E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.611549335E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12292E-01 0.20982E+01 Friction velocity uk : 0.12292E-01 0.20982E+01 Dimensionless distance yplus : 0.11855E-01 0.20602E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.172390778e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29414E+08 1 0.21894E-09 0.28600E+02 0.21107E+04 c Velocity[X] 0.14304E+02 c Velocity[Y] 0.14296E+02 c Velocity[Z] 0.48318E-05 c Pressure 0.24295E-03 11 0.72073E-04 0.52897E-02 0.71793E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -10.266 19.349 5.605 7.9955 v Velocity[Y] -11.186 12.765 -0.14315 -0.00067574 v Velocity[Z] -3.0741 2.9781 3.4085e-06 -5.3857e-08 v ǁVelocityǁ 0.0006699 20.474 6.4618 8.003 v Pressure -1.669e+05 1.1426e+05 -22642 -13725 v TurbVisc 7.4942e-21 0.0049673 9.6102e-05 4.9283e-06 v CourantNb 7.5298e-08 0.011765 0.00016634 4.881e-06 v FourierNb 1.2425e-07 0.046694 0.00014539 1.6419e-07 v total_pressure -65576 2.1558e+05 78683 87600 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0602 0.10706 0.0031137 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2152e-07 0.051869 0.00031173 5.0451e-06 INSTANT 0.874997000E-01 TIME STEP NUMBER 55195 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282636462E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.611741892E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.16143E-01 0.20991E+01 Friction velocity uk : 0.16143E-01 0.20991E+01 Dimensionless distance yplus : 0.16032E-01 0.20611E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.075542816e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29414E+08 1 0.21871E-09 0.28536E+02 0.21083E+04 c Velocity[X] 0.14270E+02 c Velocity[Y] 0.14266E+02 c Velocity[Z] 0.48123E-05 c Pressure 0.24429E-03 121 0.91145E-04 0.53099E-02 0.84073E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -10.293 19.376 5.605 7.9955 v Velocity[Y] -11.217 12.796 -0.14315 -0.00067554 v Velocity[Z] -3.0738 2.9781 3.4074e-06 -5.3857e-08 v ǁVelocityǁ 0.00068739 20.503 6.4628 8.003 v Pressure -1.6529e+05 1.1624e+05 -20810 -12607 v TurbVisc 7.9034e-21 0.0049673 9.6263e-05 4.9429e-06 v CourantNb 8.8355e-08 0.011765 0.00016634 4.881e-06 v FourierNb 1.2425e-07 0.046701 0.00014539 1.643e-07 v total_pressure -63969 2.1756e+05 80515 88718 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0611 0.10697 0.0031112 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2151e-07 0.051878 0.00031173 5.0453e-06 INSTANT 0.874998000E-01 TIME STEP NUMBER 55196 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282634551E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.611933635E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10419E-01 0.20999E+01 Friction velocity uk : 0.10419E-01 0.20999E+01 Dimensionless distance yplus : 0.10200E-01 0.20619E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -9.857959693e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29414E+08 1 0.21848E-09 0.28473E+02 0.21060E+04 c Velocity[X] 0.14237E+02 c Velocity[Y] 0.14235E+02 c Velocity[Z] 0.48041E-05 c Pressure 0.24493E-03 91 0.73980E-04 0.53145E-02 0.86738E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -10.32 19.402 5.6049 7.9954 v Velocity[Y] -11.248 12.827 -0.14315 -0.00067571 v Velocity[Z] -3.0734 2.9781 3.4063e-06 -5.3857e-08 v ǁVelocityǁ 0.00071095 20.533 6.4638 8.003 v Pressure -1.637e+05 1.1829e+05 -18860 -11503 v TurbVisc 6.2568e-21 0.0049673 9.6423e-05 4.9577e-06 v CourantNb 1.1299e-07 0.011765 0.00016634 4.881e-06 v FourierNb 1.2425e-07 0.046708 0.00014539 1.644e-07 v total_pressure -62380 2.1962e+05 82465 89822 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0619 0.10688 0.0031088 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2151e-07 0.051886 0.00031173 5.0454e-06 INSTANT 0.874999000E-01 TIME STEP NUMBER 55197 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282632841E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.612153020E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15578E-01 0.21006E+01 Friction velocity uk : 0.15578E-01 0.21006E+01 Dimensionless distance yplus : 0.15149E-01 0.20626E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -8.569128054e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29414E+08 1 0.21825E-09 0.28409E+02 0.21036E+04 c Velocity[X] 0.14204E+02 c Velocity[Y] 0.14205E+02 c Velocity[Z] 0.48124E-05 c Pressure 0.24594E-03 11 0.73756E-04 0.53272E-02 0.88206E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -10.347 19.429 5.6049 7.9954 v Velocity[Y] -11.279 12.858 -0.14316 -0.00067637 v Velocity[Z] -3.0731 2.9781 3.4052e-06 -5.3857e-08 v ǁVelocityǁ 0.0007505 20.563 6.4649 8.0031 v Pressure -1.6213e+05 1.2032e+05 -16861 -10449 v TurbVisc 7.8597e-21 0.0049673 9.6583e-05 4.9723e-06 v CourantNb 1.1215e-07 0.011765 0.00016634 4.881e-06 v FourierNb 1.2425e-07 0.046713 0.00014539 1.6451e-07 v total_pressure -60801 2.2165e+05 84464 90876 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0626 0.10681 0.0031066 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2151e-07 0.051893 0.00031173 5.0455e-06 INSTANT 0.875000000E-01 TIME STEP NUMBER 55198 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282631376E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.612368400E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15376E-01 0.21010E+01 Friction velocity uk : 0.15376E-01 0.21010E+01 Dimensionless distance yplus : 0.14857E-01 0.20630E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -6.858855671e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29414E+08 1 0.21802E-09 0.28350E+02 0.21014E+04 c Velocity[X] 0.14174E+02 c Velocity[Y] 0.14176E+02 c Velocity[Z] 0.48195E-05 c Pressure 0.24742E-03 39 0.87133E-04 0.53501E-02 0.11509E+07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -10.374 19.456 5.6049 7.9954 v Velocity[Y] -11.309 12.888 -0.14316 -0.00067649 v Velocity[Z] -3.0727 2.9782 3.4041e-06 -5.3857e-08 v ǁVelocityǁ 0.00075878 20.593 6.4659 8.0031 v Pressure -1.6061e+05 1.2233e+05 -15072 -9246.7 v TurbVisc 7.9152e-21 0.0049673 9.6742e-05 4.987e-06 v CourantNb 1.116e-07 0.011765 0.00016634 4.881e-06 v FourierNb 1.2425e-07 0.046717 0.00014539 1.6462e-07 v total_pressure -59286 2.2365e+05 86253 92078 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.063 0.10675 0.0031046 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.215e-07 0.051897 0.00031173 5.0457e-06 INSTANT 0.875001000E-01 TIME STEP NUMBER 55199 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282629994E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.612582283E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15221E-01 0.21014E+01 Friction velocity uk : 0.15221E-01 0.21014E+01 Dimensionless distance yplus : 0.14707E-01 0.20634E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -5.730620878e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29414E+08 1 0.21779E-09 0.28291E+02 0.20992E+04 c Velocity[X] 0.14144E+02 c Velocity[Y] 0.14147E+02 c Velocity[Z] 0.48344E-05 c Pressure 0.24742E-03 27 0.73851E-04 0.53408E-02 0.12008E+07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -10.401 19.483 5.6049 7.9953 v Velocity[Y] -11.34 12.919 -0.14316 -0.00067643 v Velocity[Z] -3.0724 2.9782 3.403e-06 -5.3857e-08 v ǁVelocityǁ 0.00079767 20.623 6.4669 8.0031 v Pressure -1.5916e+05 1.2431e+05 -13051 -8071.4 v TurbVisc 8.0101e-21 0.0049674 9.6901e-05 5.0018e-06 v CourantNb 1.3028e-07 0.011765 0.00016634 4.8811e-06 v FourierNb 1.2425e-07 0.04672 0.00014539 1.6472e-07 v total_pressure -57834 2.2564e+05 88274 93254 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0634 0.10669 0.0031027 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.215e-07 0.051901 0.00031173 5.0458e-06 INSTANT 0.875002000E-01 TIME STEP NUMBER 55200 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282628817E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.612849926E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12477E-01 0.21015E+01 Friction velocity uk : 0.12477E-01 0.21015E+01 Dimensionless distance yplus : 0.12171E-01 0.20635E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -4.008973292e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29413E+08 1 0.21757E-09 0.28234E+02 0.20971E+04 c Velocity[X] 0.14115E+02 c Velocity[Y] 0.14119E+02 c Velocity[Z] 0.48677E-05 c Pressure 0.24801E-03 11 0.77127E-04 0.53444E-02 0.12430E+07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -10.428 19.51 5.6048 7.9953 v Velocity[Y] -11.371 12.949 -0.14316 -0.00067607 v Velocity[Z] -3.072 2.9782 3.402e-06 -5.3857e-08 v ǁVelocityǁ 0.00082215 20.653 6.468 8.0031 v Pressure -1.5772e+05 1.2628e+05 -11017 -6958.6 v TurbVisc 8.1482e-21 0.0049674 9.706e-05 5.0165e-06 v CourantNb 1.1961e-07 0.011765 0.00016634 4.8811e-06 v FourierNb 1.2425e-07 0.046721 0.00014539 1.6483e-07 v total_pressure -56391 2.2761e+05 90308 94366 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0635 0.10665 0.003101 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.215e-07 0.051903 0.00031173 5.0459e-06 INSTANT 0.875003000E-01 TIME STEP NUMBER 55201 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282627866E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.613106569E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15881E-01 0.21015E+01 Friction velocity uk : 0.15881E-01 0.21015E+01 Dimensionless distance yplus : 0.15491E-01 0.20635E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.934022252e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29413E+08 1 0.21735E-09 0.28181E+02 0.20951E+04 c Velocity[X] 0.14088E+02 c Velocity[Y] 0.14093E+02 c Velocity[Z] 0.48941E-05 c Pressure 0.24898E-03 21 0.93210E-04 0.53562E-02 0.15169E+07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -10.455 19.537 5.6048 7.9953 v Velocity[Y] -11.402 12.979 -0.14315 -0.00067582 v Velocity[Z] -3.0717 2.9782 3.4009e-06 -5.3857e-08 v ǁVelocityǁ 0.00082604 20.682 6.469 8.0032 v Pressure -1.5627e+05 1.2824e+05 -9250 -5789.4 v TurbVisc 8.0566e-21 0.0049674 9.7218e-05 5.0313e-06 v CourantNb 1.1338e-07 0.011765 0.00016634 4.8811e-06 v FourierNb 1.2425e-07 0.046721 0.0001454 1.6494e-07 v total_pressure -54943 2.2956e+05 92075 95536 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0635 0.10661 0.0030996 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.215e-07 0.051902 0.00031173 5.046e-06 INSTANT 0.875004000E-01 TIME STEP NUMBER 55202 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282627031E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.613365950E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.16622E-01 0.21013E+01 Friction velocity uk : 0.16622E-01 0.21013E+01 Dimensionless distance yplus : 0.16508E-01 0.20633E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -8.001401247e-03 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29413E+08 1 0.21713E-09 0.28130E+02 0.20932E+04 c Velocity[X] 0.14063E+02 c Velocity[Y] 0.14067E+02 c Velocity[Z] 0.49247E-05 c Pressure 0.24813E-03 31 0.74910E-04 0.53288E-02 0.15852E+07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -10.481 19.564 5.6048 7.9953 v Velocity[Y] -11.432 13.009 -0.14315 -0.00067591 v Velocity[Z] -3.0714 2.9783 3.3998e-06 -5.3857e-08 v ǁVelocityǁ 0.00085343 20.711 6.47 8.0032 v Pressure -1.548e+05 1.3018e+05 -7211.1 -4650.2 v TurbVisc 8.5273e-21 0.0049674 9.7375e-05 5.0462e-06 v CourantNb 1.1049e-07 0.011765 0.00016634 4.8811e-06 v FourierNb 1.2425e-07 0.04672 0.0001454 1.6504e-07 v total_pressure -53478 2.315e+05 94114 96675 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0633 0.10658 0.0030983 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.215e-07 0.051901 0.00031173 5.0462e-06 INSTANT 0.875005000E-01 TIME STEP NUMBER 55203 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282626402E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.613691835E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13665E-01 0.21009E+01 Friction velocity uk : 0.13665E-01 0.21009E+01 Dimensionless distance yplus : 0.13201E-01 0.20629E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 9.831075674e-03 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29413E+08 1 0.21692E-09 0.28080E+02 0.20913E+04 c Velocity[X] 0.14038E+02 c Velocity[Y] 0.14042E+02 c Velocity[Z] 0.49781E-05 c Pressure 0.24807E-03 11 0.75399E-04 0.53183E-02 0.16548E+07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -10.508 19.592 5.6047 7.9953 v Velocity[Y] -11.463 13.039 -0.14315 -0.00067651 v Velocity[Z] -3.071 2.9783 3.3987e-06 -5.3857e-08 v ǁVelocityǁ 0.00088471 20.74 6.4711 8.0032 v Pressure -1.5331e+05 1.3211e+05 -5142.7 -3554.6 v TurbVisc 2.4316e-21 0.0049674 9.7533e-05 5.061e-06 v CourantNb 1.1182e-07 0.011765 0.00016634 4.8812e-06 v FourierNb 1.2425e-07 0.046718 0.0001454 1.6515e-07 v total_pressure -51985 2.3343e+05 96182 97770 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0629 0.10656 0.0030972 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.215e-07 0.051898 0.00031174 5.0463e-06 INSTANT 0.875006000E-01 TIME STEP NUMBER 55204 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282626028E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.614005837E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13219E-01 0.21003E+01 Friction velocity uk : 0.13219E-01 0.21003E+01 Dimensionless distance yplus : 0.12894E-01 0.20623E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 2.874676962e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29413E+08 1 0.21670E-09 0.28034E+02 0.20896E+04 c Velocity[X] 0.14016E+02 c Velocity[Y] 0.14018E+02 c Velocity[Z] 0.50166E-05 c Pressure 0.24849E-03 36 0.88340E-04 0.53183E-02 0.21051E+07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -10.535 19.619 5.6047 7.9953 v Velocity[Y] -11.494 13.068 -0.14314 -0.00067657 v Velocity[Z] -3.0707 2.9783 3.3976e-06 -5.3857e-08 v ǁVelocityǁ 0.00088492 20.769 6.4721 8.0033 v Pressure -1.5178e+05 1.3404e+05 -3357.7 -2334.9 v TurbVisc 8.1031e-21 0.0049674 9.769e-05 5.0757e-06 v CourantNb 1.178e-07 0.011765 0.00016634 4.8812e-06 v FourierNb 1.2425e-07 0.046713 0.0001454 1.6526e-07 v total_pressure -50456 2.3536e+05 97967 98990 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0623 0.10655 0.0030963 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.215e-07 0.051892 0.00031174 5.0464e-06 INSTANT 0.875007000E-01 TIME STEP NUMBER 55205 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282625733E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.614324735E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12308E-01 0.20996E+01 Friction velocity uk : 0.12308E-01 0.20996E+01 Dimensionless distance yplus : 0.11890E-01 0.20617E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 3.814510129e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29413E+08 1 0.21649E-09 0.27989E+02 0.20879E+04 c Velocity[X] 0.13994E+02 c Velocity[Y] 0.13995E+02 c Velocity[Z] 0.50594E-05 c Pressure 0.24731E-03 27 0.74932E-04 0.52842E-02 0.21170E+07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -10.562 19.647 5.6046 7.9953 v Velocity[Y] -11.524 13.097 -0.14314 -0.00067643 v Velocity[Z] -3.0703 2.9783 3.3965e-06 -5.3857e-08 v ǁVelocityǁ 0.00091314 20.797 6.4732 8.0033 v Pressure -1.5021e+05 1.3597e+05 -1289.5 -1140.8 v TurbVisc 6.3358e-21 0.0049675 9.7847e-05 5.0907e-06 v CourantNb 7.4413e-08 0.011766 0.00016634 4.8812e-06 v FourierNb 1.2425e-07 0.046708 0.00014541 1.6537e-07 v total_pressure -48885 2.3729e+05 1.0004e+05 1.0018e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0617 0.10655 0.0030956 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.215e-07 0.051886 0.00031174 5.0466e-06 INSTANT 0.875008000E-01 TIME STEP NUMBER 55206 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282625647E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.614707766E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.62472E-02 0.20988E+01 Friction velocity uk : 0.62472E-02 0.20988E+01 Dimensionless distance yplus : 0.60349E-02 0.20608E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 5.165524369e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29413E+08 1 0.21628E-09 0.27946E+02 0.20862E+04 c Velocity[X] 0.13973E+02 c Velocity[Y] 0.13973E+02 c Velocity[Z] 0.51158E-05 c Pressure 0.24710E-03 11 0.75924E-04 0.52707E-02 0.20212E+07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -10.589 19.675 5.6046 7.9953 v Velocity[Y] -11.554 13.126 -0.14313 -0.00067596 v Velocity[Z] -3.07 2.9784 3.3954e-06 -5.3857e-08 v ǁVelocityǁ 0.00092437 20.825 6.4743 8.0034 v Pressure -1.4858e+05 1.3792e+05 754.77 -15.703 v TurbVisc 8.1642e-21 0.0049675 9.8003e-05 5.1056e-06 v CourantNb 1.0377e-07 0.011766 0.00016634 4.8812e-06 v FourierNb 1.2425e-07 0.046702 0.00014541 1.6547e-07 v total_pressure -47252 2.3925e+05 1.0208e+05 1.0131e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0608 0.10656 0.0030951 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.215e-07 0.051878 0.00031175 5.0467e-06 INSTANT 0.875009000E-01 TIME STEP NUMBER 55207 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282625788E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.615078794E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.60631E-02 0.20977E+01 Friction velocity uk : 0.60631E-02 0.20977E+01 Dimensionless distance yplus : 0.58571E-02 0.20598E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 6.479456809e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29413E+08 1 0.21607E-09 0.27905E+02 0.20847E+04 c Velocity[X] 0.13954E+02 c Velocity[Y] 0.13951E+02 c Velocity[Z] 0.51540E-05 c Pressure 0.24737E-03 26 0.94558E-04 0.52678E-02 0.21366E+07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -10.615 19.703 5.6045 7.9953 v Velocity[Y] -11.585 13.155 -0.14313 -0.00067561 v Velocity[Z] -3.0696 2.9784 3.3944e-06 -5.3857e-08 v ǁVelocityǁ 0.00091271 20.853 6.4753 8.0034 v Pressure -1.4688e+05 1.3989e+05 2592.9 1151 v TurbVisc 7.9373e-21 0.0049675 9.8159e-05 5.1205e-06 v CourantNb 4.5564e-08 0.011766 0.00016634 4.8813e-06 v FourierNb 1.2425e-07 0.046694 0.00014541 1.6558e-07 v total_pressure -45550 2.4121e+05 1.0392e+05 1.0248e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0598 0.10657 0.0030948 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.215e-07 0.051869 0.00031175 5.0468e-06 INSTANT 0.875010000E-01 TIME STEP NUMBER 55208 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282626043E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.615459867E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.65278E-02 0.20967E+01 Friction velocity uk : 0.65278E-02 0.20967E+01 Dimensionless distance yplus : 0.65046E-02 0.20587E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 7.046526117e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29413E+08 1 0.21586E-09 0.27865E+02 0.20832E+04 c Velocity[X] 0.13936E+02 c Velocity[Y] 0.13930E+02 c Velocity[Z] 0.51927E-05 c Pressure 0.24664E-03 31 0.76346E-04 0.52434E-02 0.19053E+07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -10.642 19.731 5.6044 7.9953 v Velocity[Y] -11.615 13.183 -0.14312 -0.00067563 v Velocity[Z] -3.0693 2.9784 3.3933e-06 -5.3857e-08 v ǁVelocityǁ 0.00091758 20.88 6.4764 8.0035 v Pressure -1.4509e+05 1.4187e+05 4639.7 2293 v TurbVisc 5.1498e-21 0.0049675 9.8315e-05 5.1355e-06 v CourantNb 1.0687e-07 0.011766 0.00016634 4.8813e-06 v FourierNb 1.2425e-07 0.046686 0.00014542 1.6569e-07 v total_pressure -43770 2.4319e+05 1.0596e+05 1.0362e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0587 0.10659 0.0030946 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.215e-07 0.051859 0.00031176 5.047e-06 INSTANT 0.875011000E-01 TIME STEP NUMBER 55209 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282626506E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.615886920E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.89765E-02 0.20955E+01 Friction velocity uk : 0.89765E-02 0.20955E+01 Dimensionless distance yplus : 0.89446E-02 0.20576E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 7.686973597e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29413E+08 1 0.21565E-09 0.27826E+02 0.20817E+04 c Velocity[X] 0.13917E+02 c Velocity[Y] 0.13909E+02 c Velocity[Z] 0.52416E-05 c Pressure 0.24672E-03 11 0.71939E-04 0.52362E-02 0.16451E+07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -10.668 19.76 5.6044 7.9953 v Velocity[Y] -11.645 13.211 -0.14311 -0.00067617 v Velocity[Z] -3.0689 2.9784 3.3922e-06 -5.3857e-08 v ǁVelocityǁ 0.00092655 20.908 6.4775 8.0035 v Pressure -1.4323e+05 1.4387e+05 6665.5 3372.4 v TurbVisc 2.2326e-21 0.0049675 9.847e-05 5.1505e-06 v CourantNb 1.2488e-07 0.011766 0.00016635 4.8813e-06 v FourierNb 1.2425e-07 0.046677 0.00014542 1.658e-07 v total_pressure -41902 2.4519e+05 1.0799e+05 1.047e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0576 0.10662 0.0030946 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.215e-07 0.051848 0.00031177 5.0471e-06 INSTANT 0.875012000E-01 TIME STEP NUMBER 55210 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282627215E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.616306405E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10090E-01 0.20941E+01 Friction velocity uk : 0.10090E-01 0.20941E+01 Dimensionless distance yplus : 0.97475E-02 0.20563E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 8.065335848e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29413E+08 1 0.21545E-09 0.27787E+02 0.20802E+04 c Velocity[X] 0.13899E+02 c Velocity[Y] 0.13888E+02 c Velocity[Z] 0.52675E-05 c Pressure 0.24720E-03 37 0.89992E-04 0.52379E-02 0.17194E+07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -10.695 19.788 5.6043 7.9953 v Velocity[Y] -11.675 13.239 -0.1431 -0.00067616 v Velocity[Z] -3.0686 2.9784 3.3911e-06 -5.3857e-08 v ǁVelocityǁ 0.00090097 20.935 6.4786 8.0036 v Pressure -1.4127e+05 1.4589e+05 8579.2 4576.8 v TurbVisc 6.9129e-21 0.0049676 9.8626e-05 5.1654e-06 v CourantNb 6.9265e-08 0.011766 0.00016635 4.8814e-06 v FourierNb 1.2425e-07 0.046668 0.00014543 1.6591e-07 v total_pressure -39945 2.4722e+05 1.099e+05 1.059e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0563 0.10666 0.0030947 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.215e-07 0.051836 0.00031177 5.0473e-06 INSTANT 0.875013000E-01 TIME STEP NUMBER 55211 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282628002E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.616736681E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.16454E-01 0.20928E+01 Friction velocity uk : 0.16454E-01 0.20928E+01 Dimensionless distance yplus : 0.16050E-01 0.20550E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 8.105050364e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29413E+08 1 0.21525E-09 0.27750E+02 0.20788E+04 c Velocity[X] 0.13882E+02 c Velocity[Y] 0.13868E+02 c Velocity[Z] 0.52920E-05 c Pressure 0.24728E-03 24 0.76326E-04 0.52309E-02 0.14452E+07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -10.721 19.817 5.6043 7.9953 v Velocity[Y] -11.704 13.267 -0.14309 -0.00067588 v Velocity[Z] -3.0682 2.9785 3.39e-06 -5.3857e-08 v ǁVelocityǁ 0.00089147 20.961 6.4796 8.0037 v Pressure -1.3921e+05 1.4795e+05 10614 5738.4 v TurbVisc 4.4075e-21 0.0049676 9.8781e-05 5.1806e-06 v CourantNb 2.9611e-08 0.011766 0.00016635 4.8814e-06 v FourierNb 1.2425e-07 0.046658 0.00014543 1.6601e-07 v total_pressure -37890 2.4927e+05 1.1194e+05 1.0706e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.055 0.1067 0.0030949 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.215e-07 0.051824 0.00031178 5.0474e-06 INSTANT 0.875014000E-01 TIME STEP NUMBER 55212 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282628991E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.617186678E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.18506E-01 0.20915E+01 Friction velocity uk : 0.18506E-01 0.20915E+01 Dimensionless distance yplus : 0.18118E-01 0.20537E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 7.828942579e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29414E+08 1 0.21505E-09 0.27713E+02 0.20774E+04 c Velocity[X] 0.13865E+02 c Velocity[Y] 0.13848E+02 c Velocity[Z] 0.53145E-05 c Pressure 0.24772E-03 11 0.71981E-04 0.52315E-02 0.12557E+07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -10.748 19.846 5.6042 7.9953 v Velocity[Y] -11.734 13.294 -0.14308 -0.00067537 v Velocity[Z] -3.0679 2.9785 3.3889e-06 -5.3857e-08 v ǁVelocityǁ 0.0008752 20.988 6.4807 8.0037 v Pressure -1.3706e+05 1.5003e+05 12587 6858.5 v TurbVisc 8.2931e-21 0.0049676 9.8936e-05 5.1956e-06 v CourantNb 3.5589e-08 0.011766 0.00016635 4.8814e-06 v FourierNb 1.2425e-07 0.046648 0.00014543 1.6612e-07 v total_pressure -35734 2.5136e+05 1.1391e+05 1.0818e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0537 0.10674 0.0030951 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.215e-07 0.051812 0.00031179 5.0476e-06 INSTANT 0.875015000E-01 TIME STEP NUMBER 55213 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282630206E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.617633881E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12279E-01 0.20902E+01 Friction velocity uk : 0.12279E-01 0.20902E+01 Dimensionless distance yplus : 0.12022E-01 0.20524E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 7.234422202e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29414E+08 1 0.21485E-09 0.27676E+02 0.20760E+04 c Velocity[X] 0.13848E+02 c Velocity[Y] 0.13827E+02 c Velocity[Z] 0.53151E-05 c Pressure 0.24820E-03 123 0.95807E-04 0.52328E-02 0.11897E+07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -10.774 19.875 5.6041 7.9954 v Velocity[Y] -11.763 13.322 -0.14308 -0.00067494 v Velocity[Z] -3.0675 2.9785 3.3879e-06 -5.3857e-08 v ǁVelocityǁ 0.00083226 21.014 6.4818 8.0038 v Pressure -1.3482e+05 1.5215e+05 14575 7981 v TurbVisc 4.8557e-21 0.0049676 9.909e-05 5.2108e-06 v CourantNb 5.1444e-08 0.011766 0.00016635 4.8815e-06 v FourierNb 1.2425e-07 0.046638 0.00014544 1.6623e-07 v total_pressure -33492 2.5348e+05 1.159e+05 1.0931e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0524 0.10678 0.0030953 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.215e-07 0.0518 0.00031179 5.0477e-06 INSTANT 0.875016000E-01 TIME STEP NUMBER 55214 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282631526E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.618095575E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11414E-01 0.20889E+01 Friction velocity uk : 0.11414E-01 0.20889E+01 Dimensionless distance yplus : 0.11097E-01 0.20511E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 6.706951129e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29414E+08 1 0.21465E-09 0.27640E+02 0.20746E+04 c Velocity[X] 0.13832E+02 c Velocity[Y] 0.13808E+02 c Velocity[Z] 0.53147E-05 c Pressure 0.24871E-03 78 0.78122E-04 0.52350E-02 0.10222E+07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -10.8 19.904 5.6041 7.9954 v Velocity[Y] -11.792 13.348 -0.14307 -0.00067488 v Velocity[Z] -3.0672 2.9785 3.3868e-06 -5.3857e-08 v ǁVelocityǁ 0.00079948 21.04 6.4829 8.0039 v Pressure -1.3248e+05 1.5431e+05 16556 9072.4 v TurbVisc 4.0175e-21 0.0049676 9.9245e-05 5.226e-06 v CourantNb 2.5205e-08 0.011766 0.00016636 4.8815e-06 v FourierNb 1.2425e-07 0.046629 0.00014544 1.6634e-07 v total_pressure -31155 2.5563e+05 1.1788e+05 1.104e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0511 0.10682 0.0030954 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.215e-07 0.051788 0.0003118 5.0479e-06 INSTANT 0.875017000E-01 TIME STEP NUMBER 55215 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282633040E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.618547753E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.18123E-01 0.20877E+01 Friction velocity uk : 0.18123E-01 0.20877E+01 Dimensionless distance yplus : 0.18029E-01 0.20500E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 5.531523091e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29414E+08 1 0.21446E-09 0.27606E+02 0.20733E+04 c Velocity[X] 0.13816E+02 c Velocity[Y] 0.13790E+02 c Velocity[Z] 0.53044E-05 c Pressure 0.24887E-03 11 0.69326E-04 0.52298E-02 0.89901E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -10.826 19.933 5.604 7.9954 v Velocity[Y] -11.821 13.375 -0.14306 -0.00067539 v Velocity[Z] -3.0669 2.9785 3.3857e-06 -5.3858e-08 v ǁVelocityǁ 0.00077308 21.067 6.484 8.004 v Pressure -1.3005e+05 1.565e+05 18486 10126 v TurbVisc 4.0699e-21 0.0049677 9.9399e-05 5.2412e-06 v CourantNb 2.3994e-08 0.011766 0.00016636 4.8816e-06 v FourierNb 1.2425e-07 0.04662 0.00014545 1.6645e-07 v total_pressure -28726 2.5782e+05 1.1981e+05 1.1145e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.05 0.10686 0.0030955 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2151e-07 0.051778 0.0003118 5.048e-06 INSTANT 0.875018000E-01 TIME STEP NUMBER 55216 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282634802E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.619006649E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.65042E-02 0.20866E+01 Friction velocity uk : 0.65042E-02 0.20866E+01 Dimensionless distance yplus : 0.62745E-02 0.20489E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 4.127070321e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29414E+08 1 0.21426E-09 0.27571E+02 0.20720E+04 c Velocity[X] 0.13801E+02 c Velocity[Y] 0.13770E+02 c Velocity[Z] 0.52761E-05 c Pressure 0.24870E-03 96 0.92479E-04 0.52177E-02 0.94268E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -10.852 19.963 5.604 7.9955 v Velocity[Y] -11.85 13.402 -0.14305 -0.00067532 v Velocity[Z] -3.0665 2.9786 3.3846e-06 -5.3858e-08 v ǁVelocityǁ 0.00071725 21.093 6.4851 8.004 v Pressure -1.2754e+05 1.5872e+05 20531 11282 v TurbVisc 4.8048e-21 0.0049677 9.9554e-05 5.2564e-06 v CourantNb 3.1397e-08 0.011766 0.00016636 4.8816e-06 v FourierNb 1.2425e-07 0.046611 0.00014545 1.6656e-07 v total_pressure -26219 2.6004e+05 1.2186e+05 1.1261e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0489 0.10689 0.0030955 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2151e-07 0.051767 0.00031181 5.0482e-06 INSTANT 0.875019000E-01 TIME STEP NUMBER 55217 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282636628E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.619481035E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10744E-01 0.20856E+01 Friction velocity uk : 0.10744E-01 0.20856E+01 Dimensionless distance yplus : 0.10505E-01 0.20479E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 3.033952835e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29414E+08 1 0.21408E-09 0.27539E+02 0.20707E+04 c Velocity[X] 0.13787E+02 c Velocity[Y] 0.13752E+02 c Velocity[Z] 0.52476E-05 c Pressure 0.24887E-03 24 0.78377E-04 0.52126E-02 0.81796E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -10.878 19.992 5.6039 7.9955 v Velocity[Y] -11.878 13.429 -0.14304 -0.00067502 v Velocity[Z] -3.0662 2.9786 3.3835e-06 -5.3858e-08 v ǁVelocityǁ 0.00066149 21.119 6.4862 8.0041 v Pressure -1.2496e+05 1.6098e+05 22472 12403 v TurbVisc 2.8768e-21 0.0049677 9.9708e-05 5.2717e-06 v CourantNb 2.0418e-08 0.011766 0.00016636 4.8817e-06 v FourierNb 1.2425e-07 0.046604 0.00014545 1.6667e-07 v total_pressure -23637 2.623e+05 1.238e+05 1.1373e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0479 0.10691 0.0030953 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2151e-07 0.051759 0.00031182 5.0483e-06 INSTANT 0.875020000E-01 TIME STEP NUMBER 55218 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282638653E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.619924181E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15760E-01 0.20848E+01 Friction velocity uk : 0.15760E-01 0.20848E+01 Dimensionless distance yplus : 0.15410E-01 0.20471E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.306686911e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29414E+08 1 0.21389E-09 0.27509E+02 0.20696E+04 c Velocity[X] 0.13773E+02 c Velocity[Y] 0.13736E+02 c Velocity[Z] 0.52065E-05 c Pressure 0.24810E-03 11 0.69766E-04 0.51880E-02 0.72008E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -10.904 20.021 5.6039 7.9955 v Velocity[Y] -11.906 13.455 -0.14302 -0.00067439 v Velocity[Z] -3.0658 2.9786 3.3824e-06 -5.3858e-08 v ǁVelocityǁ 0.00063254 21.145 6.4873 8.0042 v Pressure -1.2232e+05 1.6327e+05 24371 13464 v TurbVisc 1.7432e-21 0.0049677 9.9862e-05 5.287e-06 v CourantNb 1.6746e-08 0.011766 0.00016636 4.8817e-06 v FourierNb 1.2425e-07 0.046598 0.00014546 1.6678e-07 v total_pressure -20992 2.646e+05 1.257e+05 1.1479e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0471 0.10692 0.0030949 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2152e-07 0.051751 0.00031182 5.0485e-06 INSTANT 0.875021000E-01 TIME STEP NUMBER 55219 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282640887E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.620383151E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.18260E-01 0.20841E+01 Friction velocity uk : 0.18260E-01 0.20841E+01 Dimensionless distance yplus : 0.17629E-01 0.20464E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -6.065228745e-03 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29415E+08 1 0.21370E-09 0.27479E+02 0.20684E+04 c Velocity[X] 0.13760E+02 c Velocity[Y] 0.13719E+02 c Velocity[Z] 0.51522E-05 c Pressure 0.24677E-03 26 0.97916E-04 0.51516E-02 0.70855E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -10.93 20.051 5.6039 7.9956 v Velocity[Y] -11.934 13.482 -0.14301 -0.00067393 v Velocity[Z] -3.0657 2.9786 3.3813e-06 -5.3858e-08 v ǁVelocityǁ 0.00057522 21.172 6.4884 8.0043 v Pressure -1.1963e+05 1.6559e+05 26412 14531 v TurbVisc 6.252e-21 0.0049677 0.00010002 5.3024e-06 v CourantNb 2.7524e-08 0.011766 0.00016636 4.8818e-06 v FourierNb 1.2425e-07 0.046593 0.00014546 1.6689e-07 v total_pressure -18306 2.6691e+05 1.2774e+05 1.1586e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0464 0.10692 0.0030943 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2152e-07 0.051745 0.00031182 5.0487e-06 INSTANT 0.875022000E-01 TIME STEP NUMBER 55220 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282643219E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.620859069E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.76081E-02 0.20836E+01 Friction velocity uk : 0.76081E-02 0.20836E+01 Dimensionless distance yplus : 0.73450E-02 0.20459E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -2.065739706e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29415E+08 1 0.21352E-09 0.27452E+02 0.20673E+04 c Velocity[X] 0.13748E+02 c Velocity[Y] 0.13703E+02 c Velocity[Z] 0.51001E-05 c Pressure 0.24591E-03 68 0.80410E-04 0.51251E-02 0.63633E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -10.955 20.08 5.6038 7.9956 v Velocity[Y] -11.962 13.508 -0.143 -0.00067385 v Velocity[Z] -3.0657 2.9787 3.3803e-06 -5.3858e-08 v ǁVelocityǁ 0.00052337 21.198 6.4895 8.0044 v Pressure -1.1692e+05 1.6791e+05 28304 15588 v TurbVisc 5.0654e-21 0.0049678 0.00010017 5.3179e-06 v CourantNb 2.6112e-08 0.011766 0.00016636 4.8818e-06 v FourierNb 1.2425e-07 0.04659 0.00014546 1.67e-07 v total_pressure -15594 2.6923e+05 1.2963e+05 1.1691e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0459 0.10691 0.0030934 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2152e-07 0.051741 0.00031183 5.0488e-06 INSTANT 0.875023000E-01 TIME STEP NUMBER 55221 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282645745E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.621293599E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12078E-01 0.20833E+01 Friction velocity uk : 0.12078E-01 0.20833E+01 Dimensionless distance yplus : 0.11660E-01 0.20456E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -3.981455004e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29415E+08 1 0.21334E-09 0.27428E+02 0.20664E+04 c Velocity[X] 0.13737E+02 c Velocity[Y] 0.13691E+02 c Velocity[Z] 0.50373E-05 c Pressure 0.24381E-03 11 0.67871E-04 0.50731E-02 0.55761E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -10.981 20.109 5.6038 7.9957 v Velocity[Y] -11.99 13.535 -0.14299 -0.00067434 v Velocity[Z] -3.0656 2.9787 3.3792e-06 -5.3858e-08 v ǁVelocityǁ 0.00048735 21.225 6.4906 8.0045 v Pressure -1.1419e+05 1.7024e+05 30132 16576 v TurbVisc 4.5049e-21 0.0049678 0.00010032 5.3333e-06 v CourantNb 1.7927e-08 0.011766 0.00016636 4.8819e-06 v FourierNb 1.2425e-07 0.046588 0.00014546 1.6712e-07 v total_pressure -12868 2.7156e+05 1.3146e+05 1.179e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0456 0.10688 0.0030924 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2153e-07 0.051739 0.00031183 5.049e-06 INSTANT 0.875024000E-01 TIME STEP NUMBER 55222 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282648499E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.621752232E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15481E-01 0.20831E+01 Friction velocity uk : 0.15481E-01 0.20831E+01 Dimensionless distance yplus : 0.15136E-01 0.20454E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -5.825758882e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29415E+08 1 0.21316E-09 0.27403E+02 0.20654E+04 c Velocity[X] 0.13727E+02 c Velocity[Y] 0.13676E+02 c Velocity[Z] 0.49668E-05 c Pressure 0.24109E-03 100 0.95459E-04 0.50083E-02 0.60904E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -11.006 20.138 5.6038 7.9957 v Velocity[Y] -12.017 13.562 -0.14298 -0.00067428 v Velocity[Z] -3.0656 2.9787 3.3781e-06 -5.3858e-08 v ǁVelocityǁ 0.00043611 21.252 6.4917 8.0046 v Pressure -1.1148e+05 1.7255e+05 32157 17675 v TurbVisc 5.7022e-21 0.0049678 0.00010048 5.3487e-06 v CourantNb 2.6081e-08 0.011767 0.00016637 4.8819e-06 v FourierNb 1.2425e-07 0.046587 0.00014547 1.6723e-07 v total_pressure -10154 2.7388e+05 1.3348e+05 1.19e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0454 0.10685 0.0030911 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2153e-07 0.051738 0.00031183 5.0492e-06 INSTANT 0.875025000E-01 TIME STEP NUMBER 55223 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282651310E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.622232313E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11611E-01 0.20832E+01 Friction velocity uk : 0.11611E-01 0.20832E+01 Dimensionless distance yplus : 0.11353E-01 0.20455E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -7.307093665e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29416E+08 1 0.21299E-09 0.27382E+02 0.20646E+04 c Velocity[X] 0.13719E+02 c Velocity[Y] 0.13664E+02 c Velocity[Z] 0.49041E-05 c Pressure 0.23902E-03 24 0.80717E-04 0.49571E-02 0.54417E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -11.031 20.167 5.6038 7.9958 v Velocity[Y] -12.044 13.589 -0.14297 -0.00067398 v Velocity[Z] -3.0656 2.9787 3.377e-06 -5.3858e-08 v ǁVelocityǁ 0.00038735 21.28 6.4928 8.0047 v Pressure -1.0883e+05 1.7485e+05 33998 18747 v TurbVisc 8.7043e-21 0.0049678 0.00010063 5.3643e-06 v CourantNb 4.6346e-08 0.011766 0.00016637 4.882e-06 v FourierNb 1.2425e-07 0.046589 0.00014547 1.6734e-07 v total_pressure -7507.6 2.7618e+05 1.3532e+05 1.2007e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0455 0.1068 0.0030895 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2154e-07 0.05174 0.00031183 5.0493e-06 INSTANT 0.875026000E-01 TIME STEP NUMBER 55224 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282654314E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.622671802E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.42056E-02 0.20835E+01 Friction velocity uk : 0.42056E-02 0.20835E+01 Dimensionless distance yplus : 0.40602E-02 0.20458E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -8.902991865e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29416E+08 1 0.21281E-09 0.27364E+02 0.20639E+04 c Velocity[X] 0.13711E+02 c Velocity[Y] 0.13653E+02 c Velocity[Z] 0.48336E-05 c Pressure 0.23574E-03 11 0.68923E-04 0.48810E-02 0.48431E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -11.056 20.196 5.6038 7.9959 v Velocity[Y] -12.071 13.617 -0.14296 -0.00067335 v Velocity[Z] -3.0656 2.9787 3.3759e-06 -5.3858e-08 v ǁVelocityǁ 0.00037754 21.307 6.4939 8.0049 v Pressure -1.0663e+05 1.7712e+05 35810 19751 v TurbVisc 1.2933e-21 0.0049678 0.00010078 5.3799e-06 v CourantNb 2.6457e-08 0.011767 0.00016637 4.8821e-06 v FourierNb 1.2425e-07 0.046592 0.00014547 1.6745e-07 v total_pressure -5300.8 2.7845e+05 1.3714e+05 1.2108e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0458 0.10674 0.0030878 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2154e-07 0.051744 0.00031183 5.0495e-06 INSTANT 0.875027000E-01 TIME STEP NUMBER 55225 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282657510E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.623141242E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15110E-01 0.20839E+01 Friction velocity uk : 0.15110E-01 0.20839E+01 Dimensionless distance yplus : 0.14587E-01 0.20462E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.024384734e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29416E+08 1 0.21264E-09 0.27346E+02 0.20632E+04 c Velocity[X] 0.13704E+02 c Velocity[Y] 0.13642E+02 c Velocity[Z] 0.47616E-05 c Pressure 0.23215E-03 179 0.74048E-04 0.47987E-02 0.49179E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -11.081 20.225 5.6038 7.9959 v Velocity[Y] -12.098 13.645 -0.14295 -0.0006736 v Velocity[Z] -3.0656 2.9788 3.3748e-06 -5.3858e-08 v ǁVelocityǁ 0.00034829 21.335 6.495 8.005 v Pressure -1.0449e+05 1.7951e+05 37753 20752 v TurbVisc 6.1316e-21 0.0049678 0.00010094 5.3955e-06 v CourantNb 4.5706e-08 0.011767 0.00016637 4.8821e-06 v FourierNb 1.2425e-07 0.046596 0.00014546 1.6756e-07 v total_pressure -3167 2.8084e+05 1.3908e+05 1.2208e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0462 0.10668 0.0030858 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2155e-07 0.051749 0.00031183 5.0497e-06 INSTANT 0.875028000E-01 TIME STEP NUMBER 55226 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282660773E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.623631768E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12599E-01 0.20846E+01 Friction velocity uk : 0.12599E-01 0.20846E+01 Dimensionless distance yplus : 0.12170E-01 0.20469E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.134685459e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29416E+08 1 0.21247E-09 0.27331E+02 0.20626E+04 c Velocity[X] 0.13698E+02 c Velocity[Y] 0.13633E+02 c Velocity[Z] 0.46997E-05 c Pressure 0.22930E-03 52 0.78804E-04 0.47319E-02 0.47676E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -11.106 20.253 5.6038 7.996 v Velocity[Y] -12.125 13.673 -0.14294 -0.00067288 v Velocity[Z] -3.0656 2.9788 3.3738e-06 -5.3858e-08 v ǁVelocityǁ 0.00033557 21.363 6.4962 8.0051 v Pressure -1.0243e+05 1.8195e+05 39523 21821 v TurbVisc 4.5217e-21 0.0049679 0.00010109 5.4111e-06 v CourantNb 2.7807e-08 0.011767 0.00016637 4.8822e-06 v FourierNb 1.2425e-07 0.046601 0.00014546 1.6768e-07 v total_pressure -1108.8 2.8327e+05 1.4085e+05 1.2315e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0469 0.1066 0.0030836 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2155e-07 0.051756 0.00031183 5.0499e-06 INSTANT 0.875029000E-01 TIME STEP NUMBER 55227 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282664208E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.624093659E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.84452E-02 0.20854E+01 Friction velocity uk : 0.84452E-02 0.20854E+01 Dimensionless distance yplus : 0.82680E-02 0.20477E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.219172601e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29417E+08 1 0.21230E-09 0.27317E+02 0.20620E+04 c Velocity[X] 0.13692E+02 c Velocity[Y] 0.13625E+02 c Velocity[Z] 0.46342E-05 c Pressure 0.22557E-03 141 0.89959E-04 0.46472E-02 0.38723E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -11.131 20.282 5.6038 7.9961 v Velocity[Y] -12.151 13.702 -0.14293 -0.00067339 v Velocity[Z] -3.0656 2.9788 3.3727e-06 -5.3858e-08 v ǁVelocityǁ 0.00033798 21.391 6.4973 8.0052 v Pressure -1.0046e+05 1.8446e+05 41285 22703 v TurbVisc 5.5434e-21 0.0049679 0.00010125 5.4269e-06 v CourantNb 3.7027e-08 0.011767 0.00016637 4.8823e-06 v FourierNb 1.2425e-07 0.046609 0.00014546 1.6779e-07 v total_pressure 862.45 2.8579e+05 1.4261e+05 1.2403e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0477 0.10651 0.0030813 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2156e-07 0.051765 0.00031183 5.05e-06 INSTANT 0.875030000E-01 TIME STEP NUMBER 55228 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282667889E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.624587047E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13569E-01 0.20863E+01 Friction velocity uk : 0.13569E-01 0.20863E+01 Dimensionless distance yplus : 0.13236E-01 0.20486E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.274128499e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29417E+08 1 0.21213E-09 0.27302E+02 0.20614E+04 c Velocity[X] 0.13688E+02 c Velocity[Y] 0.13614E+02 c Velocity[Z] 0.45773E-05 c Pressure 0.22190E-03 729 0.75869E-04 0.45641E-02 0.43637E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -11.156 20.31 5.6039 7.9961 v Velocity[Y] -12.178 13.731 -0.14292 -0.00067333 v Velocity[Z] -3.0655 2.9788 3.3716e-06 -5.3858e-08 v ǁVelocityǁ 0.00035055 21.42 6.4984 8.0053 v Pressure -98589 1.869e+05 43063 23761 v TurbVisc 1.3829e-20 0.0049679 0.0001014 5.4426e-06 v CourantNb 7.8424e-08 0.011767 0.00016637 4.8823e-06 v FourierNb 1.2425e-07 0.046617 0.00014546 1.679e-07 v total_pressure 2735.8 2.8823e+05 1.4439e+05 1.2509e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0486 0.10641 0.0030789 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2156e-07 0.051775 0.00031182 5.0502e-06 INSTANT 0.875031000E-01 TIME STEP NUMBER 55229 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282671658E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.625091784E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.16339E-01 0.20874E+01 Friction velocity uk : 0.16339E-01 0.20874E+01 Dimensionless distance yplus : 0.15889E-01 0.20497E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.289606833e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29417E+08 1 0.21196E-09 0.27291E+02 0.20609E+04 c Velocity[X] 0.13683E+02 c Velocity[Y] 0.13607E+02 c Velocity[Z] 0.45291E-05 c Pressure 0.21799E-03 11 0.67048E-04 0.44763E-02 0.34587E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -11.18 20.338 5.6039 7.9962 v Velocity[Y] -12.205 13.76 -0.14291 -0.00067269 v Velocity[Z] -3.0655 2.9788 3.3705e-06 -5.3858e-08 v ǁVelocityǁ 0.00039159 21.449 6.4996 8.0055 v Pressure -96825 1.8925e+05 44753 24645 v TurbVisc 5.9992e-21 0.0049679 0.00010155 5.4583e-06 v CourantNb 8.5131e-08 0.011767 0.00016637 4.8824e-06 v FourierNb 1.2425e-07 0.046626 0.00014546 1.6801e-07 v total_pressure 4499.8 2.9057e+05 1.4608e+05 1.2597e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0497 0.10631 0.0030763 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2157e-07 0.051786 0.00031182 5.0504e-06 INSTANT 0.875032000E-01 TIME STEP NUMBER 55230 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282675644E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.625609903E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.84241E-02 0.20886E+01 Friction velocity uk : 0.84241E-02 0.20886E+01 Dimensionless distance yplus : 0.82474E-02 0.20508E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.247739865e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29418E+08 1 0.21179E-09 0.27278E+02 0.20604E+04 c Velocity[X] 0.13680E+02 c Velocity[Y] 0.13598E+02 c Velocity[Z] 0.44813E-05 c Pressure 0.21449E-03 108 0.97416E-04 0.43971E-02 0.39704E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -11.205 20.365 5.604 7.9963 v Velocity[Y] -12.232 13.79 -0.14291 -0.0006723 v Velocity[Z] -3.0655 2.9789 3.3695e-06 -5.3858e-08 v ǁVelocityǁ 0.00042391 21.478 6.5007 8.0056 v Pressure -95184 1.9149e+05 46484 25656 v TurbVisc 5.3468e-21 0.0049679 0.00010171 5.4741e-06 v CourantNb 9.5266e-08 0.011767 0.00016637 4.8825e-06 v FourierNb 1.2425e-07 0.046635 0.00014545 1.6813e-07 v total_pressure 6141.2 2.9282e+05 1.4781e+05 1.2698e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0508 0.10621 0.0030737 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2158e-07 0.051798 0.00031182 5.0506e-06 INSTANT 0.875033000E-01 TIME STEP NUMBER 55231 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282679700E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.626147277E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11872E-01 0.20899E+01 Friction velocity uk : 0.11872E-01 0.20899E+01 Dimensionless distance yplus : 0.11811E-01 0.20521E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.219112676e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29418E+08 1 0.21163E-09 0.27268E+02 0.20600E+04 c Velocity[X] 0.13677E+02 c Velocity[Y] 0.13591E+02 c Velocity[Z] 0.44489E-05 c Pressure 0.21129E-03 37 0.79743E-04 0.43244E-02 0.34673E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -11.23 20.393 5.604 7.9964 v Velocity[Y] -12.259 13.82 -0.1429 -0.00067233 v Velocity[Z] -3.0655 2.9789 3.3684e-06 -5.3858e-08 v ǁVelocityǁ 0.00048374 21.507 6.5019 8.0057 v Pressure -93664 1.9362e+05 48162 26596 v TurbVisc 6.7524e-21 0.004968 0.00010186 5.4901e-06 v CourantNb 9.3055e-08 0.011767 0.00016637 4.8826e-06 v FourierNb 1.2425e-07 0.046646 0.00014545 1.6824e-07 v total_pressure 7661 2.9495e+05 1.4949e+05 1.2792e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0521 0.1061 0.0030711 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2158e-07 0.051811 0.00031182 5.0508e-06 INSTANT 0.875034000E-01 TIME STEP NUMBER 55232 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282683904E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.626688909E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.76209E-02 0.20912E+01 Friction velocity uk : 0.76209E-02 0.20912E+01 Dimensionless distance yplus : 0.75938E-02 0.20534E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.112596252e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29419E+08 1 0.21146E-09 0.27258E+02 0.20596E+04 c Velocity[X] 0.13674E+02 c Velocity[Y] 0.13584E+02 c Velocity[Z] 0.44244E-05 c Pressure 0.20806E-03 11 0.64992E-04 0.42511E-02 0.31594E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -11.254 20.42 5.6041 7.9965 v Velocity[Y] -12.286 13.85 -0.14289 -0.00067293 v Velocity[Z] -3.0655 2.9789 3.3673e-06 -5.3858e-08 v ǁVelocityǁ 0.00057746 21.537 6.5031 8.0059 v Pressure -92267 1.9565e+05 49822 27493 v TurbVisc 7.9551e-21 0.004968 0.00010201 5.506e-06 v CourantNb 9.1635e-08 0.011767 0.00016637 4.8826e-06 v FourierNb 1.2425e-07 0.046657 0.00014545 1.6836e-07 v total_pressure 9057.9 2.9697e+05 1.5115e+05 1.2882e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0534 0.106 0.0030686 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2159e-07 0.051824 0.00031181 5.051e-06 INSTANT 0.875035000E-01 TIME STEP NUMBER 55233 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282688326E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.627249476E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10832E-01 0.20925E+01 Friction velocity uk : 0.10832E-01 0.20925E+01 Dimensionless distance yplus : 0.10465E-01 0.20547E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -9.420074096e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29419E+08 1 0.21130E-09 0.27248E+02 0.20591E+04 c Velocity[X] 0.13672E+02 c Velocity[Y] 0.13575E+02 c Velocity[Z] 0.44034E-05 c Pressure 0.20541E-03 40 0.94449E-04 0.41899E-02 0.34142E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -11.279 20.447 5.6042 7.9966 v Velocity[Y] -12.313 13.881 -0.14289 -0.000673 v Velocity[Z] -3.0655 2.9789 3.3662e-06 -5.3858e-08 v ǁVelocityǁ 0.00065669 21.566 6.5042 8.006 v Pressure -90991 1.9756e+05 51381 28455 v TurbVisc 5.5164e-21 0.004968 0.00010217 5.5218e-06 v CourantNb 7.6715e-08 0.011767 0.00016637 4.8827e-06 v FourierNb 1.2425e-07 0.046668 0.00014545 1.6847e-07 v total_pressure 10334 2.9888e+05 1.5271e+05 1.2978e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0547 0.10591 0.0030662 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.216e-07 0.051837 0.00031181 5.0512e-06 INSTANT 0.875036000E-01 TIME STEP NUMBER 55234 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282692785E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.627822978E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.16975E-01 0.20939E+01 Friction velocity uk : 0.16975E-01 0.20939E+01 Dimensionless distance yplus : 0.16558E-01 0.20560E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -8.223195513e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29419E+08 1 0.21114E-09 0.27238E+02 0.20587E+04 c Velocity[X] 0.13670E+02 c Velocity[Y] 0.13568E+02 c Velocity[Z] 0.43956E-05 c Pressure 0.20245E-03 24 0.80448E-04 0.41227E-02 0.32082E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -11.304 20.474 5.6043 7.9966 v Velocity[Y] -12.341 13.911 -0.14288 -0.00067286 v Velocity[Z] -3.0655 2.9789 3.3651e-06 -5.3858e-08 v ǁVelocityǁ 0.00078212 21.596 6.5054 8.0062 v Pressure -89824 1.9935e+05 52999 29421 v TurbVisc 4.6852e-21 0.004968 0.00010232 5.5378e-06 v CourantNb 5.0488e-08 0.011767 0.00016637 4.8828e-06 v FourierNb 1.2425e-07 0.046679 0.00014544 1.6859e-07 v total_pressure 11501 3.0068e+05 1.5432e+05 1.3075e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.056 0.10581 0.003064 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.216e-07 0.051851 0.00031181 5.0514e-06 INSTANT 0.875037000E-01 TIME STEP NUMBER 55235 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282697415E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.628419063E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.85523E-02 0.20952E+01 Friction velocity uk : 0.85523E-02 0.20952E+01 Dimensionless distance yplus : 0.82256E-02 0.20573E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -5.998764446e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29420E+08 1 0.21098E-09 0.27229E+02 0.20583E+04 c Velocity[X] 0.13668E+02 c Velocity[Y] 0.13561E+02 c Velocity[Z] 0.44010E-05 c Pressure 0.19981E-03 11 0.66707E-04 0.40622E-02 0.27690E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -11.329 20.501 5.6043 7.9967 v Velocity[Y] -12.368 13.942 -0.14288 -0.00067236 v Velocity[Z] -3.0654 2.9789 3.3641e-06 -5.3858e-08 v ǁVelocityǁ 0.00092301 21.625 6.5066 8.0063 v Pressure -88760 2.0104e+05 54569 30282 v TurbVisc 9.8153e-21 0.004968 0.00010247 5.5538e-06 v CourantNb 2.7567e-08 0.011767 0.00016637 4.8829e-06 v FourierNb 1.2425e-07 0.046689 0.00014544 1.687e-07 v total_pressure 12565 3.0236e+05 1.5589e+05 1.3161e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0573 0.10573 0.0030618 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2161e-07 0.051864 0.00031181 5.0516e-06 INSTANT 0.875038000E-01 TIME STEP NUMBER 55236 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282702205E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.629021925E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.59247E-02 0.20965E+01 Friction velocity uk : 0.59247E-02 0.20965E+01 Dimensionless distance yplus : 0.56983E-02 0.20585E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -3.202052399e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29420E+08 1 0.21082E-09 0.27221E+02 0.20580E+04 c Velocity[X] 0.13667E+02 c Velocity[Y] 0.13554E+02 c Velocity[Z] 0.44077E-05 c Pressure 0.19773E-03 166 0.73828E-04 0.40132E-02 0.28990E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -11.353 20.528 5.6045 7.9968 v Velocity[Y] -12.396 13.973 -0.14288 -0.00067278 v Velocity[Z] -3.0654 2.979 3.363e-06 -5.3858e-08 v ǁVelocityǁ 0.0010526 21.655 6.5078 8.0065 v Pressure -87791 2.0262e+05 55975 31147 v TurbVisc 2.0257e-21 0.004968 0.00010262 5.5698e-06 v CourantNb 1.8419e-08 0.011767 0.00016637 4.883e-06 v FourierNb 1.2425e-07 0.046699 0.00014544 1.6882e-07 v total_pressure 13534 3.0394e+05 1.573e+05 1.3247e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0585 0.10565 0.0030599 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2162e-07 0.051876 0.00031181 5.0518e-06 INSTANT 0.875039000E-01 TIME STEP NUMBER 55237 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282707071E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.629631235E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.95693E-02 0.20977E+01 Friction velocity uk : 0.95693E-02 0.20977E+01 Dimensionless distance yplus : 0.92037E-02 0.20597E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.148317290e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29421E+08 1 0.21066E-09 0.27213E+02 0.20576E+04 c Velocity[X] 0.13666E+02 c Velocity[Y] 0.13547E+02 c Velocity[Z] 0.44243E-05 c Pressure 0.19485E-03 66 0.78899E-04 0.39483E-02 0.28618E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -11.378 20.554 5.6046 7.9969 v Velocity[Y] -12.424 14.004 -0.14288 -0.00067223 v Velocity[Z] -3.0654 2.979 3.3619e-06 -5.3858e-08 v ǁVelocityǁ 0.0012189 21.685 6.5091 8.0066 v Pressure -86904 2.0409e+05 57499 32067 v TurbVisc 1.9957e-21 0.0049681 0.00010278 5.5858e-06 v CourantNb 3.486e-08 0.011767 0.00016637 4.8831e-06 v FourierNb 1.2425e-07 0.046709 0.00014543 1.6893e-07 v total_pressure 14421 3.0541e+05 1.5882e+05 1.3339e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0597 0.10558 0.0030584 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2163e-07 0.051888 0.0003118 5.052e-06 INSTANT 0.875040000E-01 TIME STEP NUMBER 55238 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282712067E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.630273127E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11120E-01 0.20988E+01 Friction velocity uk : 0.11120E-01 0.20988E+01 Dimensionless distance yplus : 0.10695E-01 0.20608E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 2.003155695e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29421E+08 1 0.21050E-09 0.27206E+02 0.20573E+04 c Velocity[X] 0.13665E+02 c Velocity[Y] 0.13541E+02 c Velocity[Z] 0.44529E-05 c Pressure 0.19243E-03 150 0.90170E-04 0.38928E-02 0.23264E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -11.403 20.581 5.6047 7.997 v Velocity[Y] -12.452 14.035 -0.14289 -0.00067292 v Velocity[Z] -3.0654 2.979 3.3608e-06 -5.3858e-08 v ǁVelocityǁ 0.0014046 21.714 6.5103 8.0068 v Pressure -86089 2.0546e+05 58912 32812 v TurbVisc 1.8006e-21 0.0049681 0.00010293 5.602e-06 v CourantNb 4.8234e-08 0.011767 0.00016637 4.8832e-06 v FourierNb 1.2425e-07 0.046718 0.00014543 1.6905e-07 v total_pressure 15236 3.0678e+05 1.6024e+05 1.3414e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0608 0.10551 0.0030572 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2163e-07 0.051899 0.0003118 5.0522e-06 INSTANT 0.875041000E-01 TIME STEP NUMBER 55239 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282717288E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.630911724E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12470E-01 0.20998E+01 Friction velocity uk : 0.12470E-01 0.20998E+01 Dimensionless distance yplus : 0.12164E-01 0.20618E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 5.129119517e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29422E+08 1 0.21034E-09 0.27198E+02 0.20570E+04 c Velocity[X] 0.13666E+02 c Velocity[Y] 0.13533E+02 c Velocity[Z] 0.44864E-05 c Pressure 0.18978E-03 674 0.76083E-04 0.38327E-02 0.26396E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -11.428 20.608 5.6048 7.9972 v Velocity[Y] -12.48 14.066 -0.14289 -0.00067303 v Velocity[Z] -3.0654 2.979 3.3598e-06 -5.3858e-08 v ǁVelocityǁ 0.001607 21.743 6.5115 8.0069 v Pressure -85328 2.0675e+05 60317 33705 v TurbVisc 1.5736e-21 0.0049681 0.00010308 5.6181e-06 v CourantNb 5.7248e-08 0.011767 0.00016638 4.8832e-06 v FourierNb 1.2425e-07 0.046726 0.00014543 1.6916e-07 v total_pressure 15997 3.0807e+05 1.6164e+05 1.3503e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0618 0.10546 0.0030563 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2164e-07 0.051908 0.0003118 5.0524e-06 INSTANT 0.875042000E-01 TIME STEP NUMBER 55240 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282722569E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.631564220E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.17569E-01 0.21006E+01 Friction velocity uk : 0.17569E-01 0.21006E+01 Dimensionless distance yplus : 0.17138E-01 0.20626E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 8.279654365e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29422E+08 1 0.21019E-09 0.27192E+02 0.20567E+04 c Velocity[X] 0.13665E+02 c Velocity[Y] 0.13527E+02 c Velocity[Z] 0.45271E-05 c Pressure 0.18652E-03 10 0.64919E-04 0.37606E-02 0.20869E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -11.453 20.635 5.6049 7.9973 v Velocity[Y] -12.509 14.096 -0.1429 -0.00067257 v Velocity[Z] -3.0654 2.979 3.3587e-06 -5.3858e-08 v ǁVelocityǁ 0.001851 21.772 6.5128 8.0071 v Pressure -84606 2.0796e+05 61737 34441 v TurbVisc 1.9135e-21 0.0049681 0.00010324 5.6342e-06 v CourantNb 6.1762e-08 0.011767 0.00016638 4.8833e-06 v FourierNb 1.2425e-07 0.046733 0.00014543 1.6928e-07 v total_pressure 16719 3.0929e+05 1.6306e+05 1.3577e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0626 0.10541 0.0030556 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2165e-07 0.051917 0.00031181 5.0526e-06 INSTANT 0.875043000E-01 TIME STEP NUMBER 55241 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282728030E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.632224991E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13735E-01 0.21013E+01 Friction velocity uk : 0.13735E-01 0.21013E+01 Dimensionless distance yplus : 0.13252E-01 0.20633E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.195028079e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29423E+08 1 0.21003E-09 0.27189E+02 0.20565E+04 c Velocity[X] 0.13668E+02 c Velocity[Y] 0.13521E+02 c Velocity[Z] 0.45738E-05 c Pressure 0.18390E-03 55 0.97127E-04 0.37016E-02 0.23996E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -11.478 20.662 5.6051 7.9974 v Velocity[Y] -12.537 14.127 -0.1429 -0.00067238 v Velocity[Z] -3.0653 2.9791 3.3576e-06 -5.3858e-08 v ǁVelocityǁ 0.0020637 21.801 6.5141 8.0073 v Pressure -83905 2.0912e+05 62933 35270 v TurbVisc 1.4843e-21 0.0049681 0.00010339 5.6504e-06 v CourantNb 6.1482e-08 0.011767 0.00016638 4.8834e-06 v FourierNb 1.2425e-07 0.046738 0.00014543 1.6939e-07 v total_pressure 17420 3.1044e+05 1.6426e+05 1.3659e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0633 0.10537 0.0030551 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2166e-07 0.051923 0.00031181 5.0528e-06 INSTANT 0.875044000E-01 TIME STEP NUMBER 55242 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282733546E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.632878535E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11437E-01 0.21019E+01 Friction velocity uk : 0.11437E-01 0.21019E+01 Dimensionless distance yplus : 0.11064E-01 0.20639E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.461697988e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29423E+08 1 0.20988E-09 0.27186E+02 0.20563E+04 c Velocity[X] 0.13670E+02 c Velocity[Y] 0.13516E+02 c Velocity[Z] 0.46215E-05 c Pressure 0.17996E-03 38 0.79815E-04 0.36164E-02 0.21312E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -11.503 20.689 5.6052 7.9975 v Velocity[Y] -12.566 14.157 -0.14291 -0.00067258 v Velocity[Z] -3.0653 2.9791 3.3566e-06 -5.3858e-08 v ǁVelocityǁ 0.0023152 21.83 6.5153 8.0074 v Pressure -83209 2.1021e+05 64284 36046 v TurbVisc 1.4298e-21 0.0049682 0.00010354 5.6667e-06 v CourantNb 5.6658e-08 0.011767 0.00016639 4.8835e-06 v FourierNb 1.2425e-07 0.046743 0.00014542 1.6951e-07 v total_pressure 18116 3.1154e+05 1.6561e+05 1.3737e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0639 0.10534 0.0030548 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2167e-07 0.051929 0.00031181 5.053e-06 INSTANT 0.875045000E-01 TIME STEP NUMBER 55243 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282739193E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.633568790E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.95736E-02 0.21024E+01 Friction velocity uk : 0.95736E-02 0.21024E+01 Dimensionless distance yplus : 0.92495E-02 0.20643E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.785454816e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29424E+08 1 0.20973E-09 0.27183E+02 0.20562E+04 c Velocity[X] 0.13671E+02 c Velocity[Y] 0.13512E+02 c Velocity[Z] 0.46813E-05 c Pressure 0.17647E-03 10 0.61291E-04 0.35402E-02 0.18319E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -11.528 20.717 5.6054 7.9976 v Velocity[Y] -12.595 14.186 -0.14292 -0.00067335 v Velocity[Z] -3.0653 2.9791 3.3555e-06 -5.3858e-08 v ǁVelocityǁ 0.0026063 21.858 6.5166 8.0076 v Pressure -82502 2.1128e+05 65607 36734 v TurbVisc 2.3134e-21 0.0049682 0.00010369 5.6829e-06 v CourantNb 4.7485e-08 0.011767 0.00016639 4.8836e-06 v FourierNb 1.2425e-07 0.046747 0.00014542 1.6963e-07 v total_pressure 18823 3.126e+05 1.6693e+05 1.3806e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0643 0.10531 0.0030547 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2168e-07 0.051934 0.00031181 5.0533e-06 INSTANT 0.875046000E-01 TIME STEP NUMBER 55244 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282745009E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.634237368E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11153E-01 0.21027E+01 Friction velocity uk : 0.11153E-01 0.21027E+01 Dimensionless distance yplus : 0.10879E-01 0.20646E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 2.117128130e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29424E+08 1 0.20958E-09 0.27183E+02 0.20561E+04 c Velocity[X] 0.13676E+02 c Velocity[Y] 0.13507E+02 c Velocity[Z] 0.47377E-05 c Pressure 0.17336E-03 24 0.94408E-04 0.34722E-02 0.21300E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -11.554 20.744 5.6055 7.9977 v Velocity[Y] -12.624 14.215 -0.14293 -0.0006736 v Velocity[Z] -3.0653 2.9791 3.3544e-06 -5.3858e-08 v ǁVelocityǁ 0.002827 21.886 6.5179 8.0078 v Pressure -81771 2.1232e+05 66714 37521 v TurbVisc 2.6831e-21 0.0049682 0.00010384 5.6991e-06 v CourantNb 3.4063e-08 0.011767 0.00016639 4.8837e-06 v FourierNb 1.2425e-07 0.046749 0.00014542 1.6974e-07 v total_pressure 19554 3.1364e+05 1.6804e+05 1.3885e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0646 0.10529 0.0030549 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2169e-07 0.051937 0.00031182 5.0535e-06 INSTANT 0.875047000E-01 TIME STEP NUMBER 55245 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282750856E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.634897934E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13517E-01 0.21028E+01 Friction velocity uk : 0.13517E-01 0.21028E+01 Dimensionless distance yplus : 0.13076E-01 0.20648E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 2.362117141e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29425E+08 1 0.20943E-09 0.27182E+02 0.20561E+04 c Velocity[X] 0.13679E+02 c Velocity[Y] 0.13503E+02 c Velocity[Z] 0.47888E-05 c Pressure 0.16913E-03 24 0.80409E-04 0.33818E-02 0.19187E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -11.579 20.772 5.6057 7.9978 v Velocity[Y] -12.652 14.244 -0.14295 -0.00067366 v Velocity[Z] -3.0653 2.9791 3.3534e-06 -5.3858e-08 v ǁVelocityǁ 0.0027339 21.914 6.5192 8.0079 v Pressure -81002 2.1334e+05 67954 38268 v TurbVisc 3.4245e-21 0.0049682 0.000104 5.7155e-06 v CourantNb 2.0528e-08 0.011767 0.0001664 4.8838e-06 v FourierNb 1.2425e-07 0.046751 0.00014542 1.6986e-07 v total_pressure 20323 3.1467e+05 1.6928e+05 1.3959e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0648 0.10527 0.0030552 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.217e-07 0.051939 0.00031182 5.0537e-06 INSTANT 0.875048000E-01 TIME STEP NUMBER 55246 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282756833E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.635595313E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12970E-01 0.21029E+01 Friction velocity uk : 0.12970E-01 0.21029E+01 Dimensionless distance yplus : 0.12859E-01 0.20649E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 2.628858839e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29425E+08 1 0.20928E-09 0.27183E+02 0.20560E+04 c Velocity[X] 0.13683E+02 c Velocity[Y] 0.13500E+02 c Velocity[Z] 0.48491E-05 c Pressure 0.16545E-03 10 0.60827E-04 0.33027E-02 0.16232E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -11.604 20.8 5.6059 7.998 v Velocity[Y] -12.681 14.273 -0.14296 -0.0006733 v Velocity[Z] -3.0653 2.9792 3.3523e-06 -5.3858e-08 v ǁVelocityǁ 0.0025686 21.942 6.5206 8.0081 v Pressure -80186 2.1437e+05 69143 38911 v TurbVisc 3.8885e-21 0.0049682 0.00010415 5.7318e-06 v CourantNb 3.052e-08 0.011767 0.0001664 4.8839e-06 v FourierNb 1.2425e-07 0.046752 0.00014542 1.6998e-07 v total_pressure 21139 3.1569e+05 1.7047e+05 1.4024e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0649 0.10526 0.0030556 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2171e-07 0.05194 0.00031183 5.0539e-06 INSTANT 0.875049000E-01 TIME STEP NUMBER 55247 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282762924E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.636272955E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.14512E-01 0.21028E+01 Friction velocity uk : 0.14512E-01 0.21028E+01 Dimensionless distance yplus : 0.14039E-01 0.20648E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 2.874946357e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29426E+08 1 0.20913E-09 0.27184E+02 0.20560E+04 c Velocity[X] 0.13688E+02 c Velocity[Y] 0.13496E+02 c Velocity[Z] 0.49018E-05 c Pressure 0.16232E-03 56 0.99486E-04 0.32351E-02 0.16764E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -11.629 20.828 5.606 7.9981 v Velocity[Y] -12.71 14.301 -0.14298 -0.0006732 v Velocity[Z] -3.0652 2.9792 3.3512e-06 -5.3858e-08 v ǁVelocityǁ 0.0024439 21.969 6.5219 8.0083 v Pressure -79317 2.154e+05 70161 39557 v TurbVisc 4.5908e-21 0.0049682 0.0001043 5.7482e-06 v CourantNb 5.3041e-08 0.011767 0.00016641 4.884e-06 v FourierNb 1.2425e-07 0.046752 0.00014542 1.7009e-07 v total_pressure 22008 3.1672e+05 1.7149e+05 1.4088e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0648 0.10525 0.0030562 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2172e-07 0.05194 0.00031183 5.0541e-06 INSTANT 0.875050000E-01 TIME STEP NUMBER 55248 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282769089E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.636946895E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13319E-01 0.21027E+01 Friction velocity uk : 0.13319E-01 0.21027E+01 Dimensionless distance yplus : 0.12885E-01 0.20647E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 3.045095788e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29426E+08 1 0.20899E-09 0.27185E+02 0.20560E+04 c Velocity[X] 0.13692E+02 c Velocity[Y] 0.13493E+02 c Velocity[Z] 0.49471E-05 c Pressure 0.15856E-03 43 0.82517E-04 0.31549E-02 0.15182E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -11.654 20.857 5.6062 7.9982 v Velocity[Y] -12.738 14.328 -0.14299 -0.00067348 v Velocity[Z] -3.0652 2.9792 3.3502e-06 -5.3858e-08 v ǁVelocityǁ 0.0024164 21.996 6.5232 8.0085 v Pressure -78389 2.1643e+05 71282 40175 v TurbVisc 1.8e-21 0.0049683 0.00010445 5.7647e-06 v CourantNb 7.8647e-08 0.011767 0.00016641 4.8841e-06 v FourierNb 1.2425e-07 0.046751 0.00014542 1.7021e-07 v total_pressure 22936 3.1776e+05 1.7261e+05 1.415e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0647 0.10524 0.0030569 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2173e-07 0.051939 0.00031184 5.0544e-06 INSTANT 0.875051000E-01 TIME STEP NUMBER 55249 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282775369E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.637647318E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12147E-01 0.21025E+01 Friction velocity uk : 0.12147E-01 0.21025E+01 Dimensionless distance yplus : 0.11751E-01 0.20645E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 3.197755251e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29427E+08 1 0.20885E-09 0.27187E+02 0.20560E+04 c Velocity[X] 0.13695E+02 c Velocity[Y] 0.13492E+02 c Velocity[Z] 0.49931E-05 c Pressure 0.15542E-03 10 0.58163E-04 0.30873E-02 0.13592E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -11.679 20.885 5.6064 7.9983 v Velocity[Y] -12.766 14.356 -0.14301 -0.00067431 v Velocity[Z] -3.0652 2.9792 3.3491e-06 -5.3858e-08 v ǁVelocityǁ 0.0025264 22.023 6.5246 8.0087 v Pressure -77398 2.1749e+05 72354 40739 v TurbVisc 2.4386e-21 0.0049683 0.0001046 5.7811e-06 v CourantNb 8.8078e-08 0.011767 0.00016642 4.8843e-06 v FourierNb 1.2425e-07 0.04675 0.00014542 1.7033e-07 v total_pressure 23927 3.1882e+05 1.7368e+05 1.4206e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0645 0.10524 0.0030576 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2174e-07 0.051938 0.00031184 5.0546e-06 INSTANT 0.875052000E-01 TIME STEP NUMBER 55250 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282781788E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.638332556E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10990E-01 0.21022E+01 Friction velocity uk : 0.10990E-01 0.21022E+01 Dimensionless distance yplus : 0.10631E-01 0.20642E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 3.318266380e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29427E+08 1 0.20870E-09 0.27188E+02 0.20560E+04 c Velocity[X] 0.13700E+02 c Velocity[Y] 0.13487E+02 c Velocity[Z] 0.50294E-05 c Pressure 0.15299E-03 50 0.98077E-04 0.30339E-02 0.15336E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -11.704 20.914 5.6065 7.9985 v Velocity[Y] -12.795 14.383 -0.14303 -0.00067453 v Velocity[Z] -3.0652 2.9792 3.348e-06 -5.3858e-08 v ǁVelocityǁ 0.0027984 22.049 6.5259 8.0089 v Pressure -76348 2.1857e+05 73308 41362 v TurbVisc 2.1957e-21 0.0049683 0.00010476 5.7974e-06 v CourantNb 8.904e-08 0.011767 0.00016642 4.8844e-06 v FourierNb 1.2425e-07 0.046749 0.00014542 1.7045e-07 v total_pressure 24977 3.199e+05 1.7463e+05 1.4269e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0642 0.10524 0.0030584 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2175e-07 0.051936 0.00031185 5.0548e-06 INSTANT 0.875053000E-01 TIME STEP NUMBER 55251 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282788228E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.639018652E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.95540E-02 0.21020E+01 Friction velocity uk : 0.95540E-02 0.21020E+01 Dimensionless distance yplus : 0.92426E-02 0.20640E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 3.374217140e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29428E+08 1 0.20856E-09 0.27189E+02 0.20560E+04 c Velocity[X] 0.13705E+02 c Velocity[Y] 0.13484E+02 c Velocity[Z] 0.50553E-05 c Pressure 0.15038E-03 76 0.82729E-04 0.29774E-02 0.14068E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -11.728 20.943 5.6067 7.9986 v Velocity[Y] -12.823 14.41 -0.14305 -0.00067459 v Velocity[Z] -3.0652 2.9792 3.3469e-06 -5.3858e-08 v ǁVelocityǁ 0.0031715 22.075 6.5272 8.009 v Pressure -75239 2.1967e+05 74311 41966 v TurbVisc 1.8706e-21 0.0049683 0.00010491 5.814e-06 v CourantNb 6.6954e-08 0.011767 0.00016643 4.8845e-06 v FourierNb 1.2425e-07 0.046747 0.00014542 1.7057e-07 v total_pressure 26086 3.21e+05 1.7564e+05 1.4329e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.064 0.10523 0.0030592 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2176e-07 0.051934 0.00031186 5.055e-06 INSTANT 0.875054000E-01 TIME STEP NUMBER 55252 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282794780E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.639718063E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.87445E-02 0.21017E+01 Friction velocity uk : 0.87445E-02 0.21017E+01 Dimensionless distance yplus : 0.84232E-02 0.20637E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 3.394567472e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29429E+08 1 0.20843E-09 0.27191E+02 0.20560E+04 c Velocity[X] 0.13708E+02 c Velocity[Y] 0.13482E+02 c Velocity[Z] 0.50752E-05 c Pressure 0.14818E-03 10 0.56472E-04 0.29290E-02 0.11486E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -11.753 20.973 5.6069 7.9987 v Velocity[Y] -12.85 14.436 -0.14307 -0.00067436 v Velocity[Z] -3.0651 2.9793 3.3459e-06 -5.3858e-08 v ǁVelocityǁ 0.003598 22.102 6.5286 8.0092 v Pressure -74078 2.208e+05 75244 42456 v TurbVisc 1.4549e-21 0.0049683 0.00010506 5.8305e-06 v CourantNb 1.8599e-08 0.011767 0.00016644 4.8846e-06 v FourierNb 1.2425e-07 0.046745 0.00014542 1.7069e-07 v total_pressure 27247 3.2212e+05 1.7657e+05 1.4378e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0637 0.10522 0.0030599 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2177e-07 0.051932 0.00031186 5.0553e-06 INSTANT 0.875055000E-01 TIME STEP NUMBER 55253 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282801401E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.640413180E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.63211E-02 0.21014E+01 Friction velocity uk : 0.63211E-02 0.21014E+01 Dimensionless distance yplus : 0.63204E-02 0.20634E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 3.374615487e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29429E+08 1 0.20829E-09 0.27191E+02 0.20559E+04 c Velocity[X] 0.13712E+02 c Velocity[Y] 0.13479E+02 c Velocity[Z] 0.50853E-05 c Pressure 0.14653E-03 157 0.74568E-04 0.28916E-02 0.12308E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -11.778 21.002 5.607 7.9989 v Velocity[Y] -12.878 14.463 -0.14309 -0.00067496 v Velocity[Z] -3.0651 2.9793 3.3448e-06 -5.3858e-08 v ǁVelocityǁ 0.0040369 22.128 6.5299 8.0094 v Pressure -72876 2.2194e+05 76131 42942 v TurbVisc 1.4285e-21 0.0049684 0.00010521 5.8471e-06 v CourantNb 6.9743e-08 0.011766 0.00016644 4.8847e-06 v FourierNb 1.2425e-07 0.046744 0.00014542 1.708e-07 v total_pressure 28449 3.2326e+05 1.7746e+05 1.4427e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0634 0.1052 0.0030606 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2178e-07 0.05193 0.00031187 5.0555e-06 INSTANT 0.875056000E-01 TIME STEP NUMBER 55254 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282808099E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.641118531E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.65337E-02 0.21012E+01 Friction velocity uk : 0.65337E-02 0.21012E+01 Dimensionless distance yplus : 0.62937E-02 0.20632E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 3.312412071e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29430E+08 1 0.20815E-09 0.27192E+02 0.20559E+04 c Velocity[X] 0.13716E+02 c Velocity[Y] 0.13476E+02 c Velocity[Z] 0.50850E-05 c Pressure 0.14505E-03 58 0.78670E-04 0.28577E-02 0.12017E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -11.802 21.031 5.6072 7.999 v Velocity[Y] -12.905 14.489 -0.1431 -0.00067465 v Velocity[Z] -3.0651 2.9793 3.3438e-06 -5.3858e-08 v ǁVelocityǁ 0.0043162 22.154 6.5313 8.0096 v Pressure -71641 2.2309e+05 76991 43437 v TurbVisc 1.2397e-21 0.0049684 0.00010536 5.8636e-06 v CourantNb 5.6559e-08 0.011766 0.00016645 4.8848e-06 v FourierNb 1.2425e-07 0.046742 0.00014542 1.7092e-07 v total_pressure 29684 3.2441e+05 1.7832e+05 1.4476e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0632 0.10523 0.0030616 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2179e-07 0.051928 0.00031187 5.0557e-06 INSTANT 0.875057000E-01 TIME STEP NUMBER 55255 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282814820E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.641822640E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.94914E-02 0.21010E+01 Friction velocity uk : 0.94914E-02 0.21010E+01 Dimensionless distance yplus : 0.91427E-02 0.20630E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 3.194889410e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29430E+08 1 0.20802E-09 0.27192E+02 0.20559E+04 c Velocity[X] 0.13719E+02 c Velocity[Y] 0.13474E+02 c Velocity[Z] 0.50739E-05 c Pressure 0.14360E-03 221 0.90119E-04 0.28246E-02 0.10281E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -11.826 21.061 5.6074 7.9992 v Velocity[Y] -12.932 14.516 -0.14312 -0.0006754 v Velocity[Z] -3.0651 2.9793 3.3427e-06 -5.3858e-08 v ǁVelocityǁ 0.0041771 22.18 6.5326 8.0098 v Pressure -70384 2.2425e+05 77805 43848 v TurbVisc 8.4712e-22 0.0049684 0.00010551 5.8803e-06 v CourantNb 4.2984e-08 0.011766 0.00016645 4.8849e-06 v FourierNb 1.2425e-07 0.046742 0.00014542 1.7104e-07 v total_pressure 30941 3.2558e+05 1.7913e+05 1.4517e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.063 0.10526 0.0030625 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.218e-07 0.051927 0.00031188 5.0559e-06 INSTANT 0.875058000E-01 TIME STEP NUMBER 55256 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282821733E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.642536945E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11121E-01 0.21009E+01 Friction velocity uk : 0.11121E-01 0.21009E+01 Dimensionless distance yplus : 0.10758E-01 0.20629E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 3.040712215e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29431E+08 1 0.20789E-09 0.27191E+02 0.20558E+04 c Velocity[X] 0.13722E+02 c Velocity[Y] 0.13469E+02 c Velocity[Z] 0.50534E-05 c Pressure 0.14218E-03 129 0.75544E-04 0.27921E-02 0.10449E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -11.85 21.09 5.6075 7.9993 v Velocity[Y] -12.959 14.542 -0.14314 -0.00067549 v Velocity[Z] -3.0651 2.9793 3.3416e-06 -5.3858e-08 v ǁVelocityǁ 0.0040626 22.206 6.534 8.01 v Pressure -69119 2.2541e+05 78579 44298 v TurbVisc 6.9171e-22 0.0049684 0.00010567 5.8969e-06 v CourantNb 3.5893e-08 0.011766 0.00016646 4.885e-06 v FourierNb 1.2425e-07 0.046741 0.00014542 1.7116e-07 v total_pressure 32206 3.2674e+05 1.799e+05 1.4562e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0629 0.10527 0.0030633 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2181e-07 0.051927 0.00031188 5.0562e-06 INSTANT 0.875059000E-01 TIME STEP NUMBER 55257 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282828631E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.643258331E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.99705E-02 0.21009E+01 Friction velocity uk : 0.99705E-02 0.21009E+01 Dimensionless distance yplus : 0.96455E-02 0.20629E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 2.857609396e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29432E+08 1 0.20776E-09 0.27193E+02 0.20558E+04 c Velocity[X] 0.13725E+02 c Velocity[Y] 0.13468E+02 c Velocity[Z] 0.50275E-05 c Pressure 0.14006E-03 9 0.52698E-04 0.27460E-02 0.75482E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -11.874 21.119 5.6077 7.9994 v Velocity[Y] -12.985 14.569 -0.14315 -0.00067522 v Velocity[Z] -3.065 2.9793 3.3406e-06 -5.3858e-08 v ǁVelocityǁ 0.0039736 22.232 6.5353 8.0102 v Pressure -67863 2.2656e+05 79253 44633 v TurbVisc 6.4182e-22 0.0049684 0.00010582 5.9136e-06 v CourantNb 2.835e-08 0.011766 0.00016646 4.8851e-06 v FourierNb 1.2425e-07 0.046742 0.00014542 1.7128e-07 v total_pressure 33462 3.2789e+05 1.8058e+05 1.4596e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0629 0.10528 0.0030638 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2182e-07 0.051928 0.00031188 5.0564e-06 INSTANT 0.875060000E-01 TIME STEP NUMBER 55258 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282835600E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.643988032E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.97464E-02 0.21010E+01 Friction velocity uk : 0.97464E-02 0.21010E+01 Dimensionless distance yplus : 0.94287E-02 0.20630E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 2.612317493e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29432E+08 1 0.20763E-09 0.27192E+02 0.20557E+04 c Velocity[X] 0.13728E+02 c Velocity[Y] 0.13464E+02 c Velocity[Z] 0.49901E-05 c Pressure 0.13827E-03 142 0.93910E-04 0.27063E-02 0.90630E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -11.898 21.149 5.6078 7.9996 v Velocity[Y] -13.012 14.595 -0.14317 -0.00067513 v Velocity[Z] -3.065 2.9794 3.3395e-06 -5.3858e-08 v ǁVelocityǁ 0.0039073 22.258 6.5367 8.0104 v Pressure -66637 2.2769e+05 80019 45032 v TurbVisc 5.9566e-22 0.0049685 0.00010597 5.9303e-06 v CourantNb 5.0259e-08 0.011766 0.00016647 4.8852e-06 v FourierNb 1.2425e-07 0.046743 0.00014542 1.714e-07 v total_pressure 34688 3.2901e+05 1.8134e+05 1.4636e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.063 0.10527 0.0030641 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2183e-07 0.051929 0.00031189 5.0566e-06 INSTANT 0.875061000E-01 TIME STEP NUMBER 55259 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282842625E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.644737338E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12449E-01 0.21013E+01 Friction velocity uk : 0.12449E-01 0.21013E+01 Dimensionless distance yplus : 0.12044E-01 0.20632E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 2.399200144e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29433E+08 1 0.20751E-09 0.27193E+02 0.20556E+04 c Velocity[X] 0.13731E+02 c Velocity[Y] 0.13462E+02 c Velocity[Z] 0.49439E-05 c Pressure 0.13649E-03 34 0.77834E-04 0.26673E-02 0.70394E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -11.922 21.178 5.608 7.9997 v Velocity[Y] -13.038 14.622 -0.14318 -0.00067537 v Velocity[Z] -3.065 2.9794 3.3384e-06 -5.3858e-08 v ǁVelocityǁ 0.0036579 22.284 6.538 8.0106 v Pressure -65454 2.2877e+05 80639 45352 v TurbVisc 2.7129e-22 0.0049685 0.00010612 5.9471e-06 v CourantNb 2.6442e-08 0.011766 0.00016647 4.8853e-06 v FourierNb 1.2425e-07 0.046745 0.00014542 1.7152e-07 v total_pressure 35871 3.301e+05 1.8196e+05 1.4668e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0632 0.10526 0.0030642 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2185e-07 0.051932 0.00031189 5.0569e-06 INSTANT 0.875062000E-01 TIME STEP NUMBER 55260 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282849699E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.645467665E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.14157E-01 0.21016E+01 Friction velocity uk : 0.14157E-01 0.21016E+01 Dimensionless distance yplus : 0.14084E-01 0.20636E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 2.129025590e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29434E+08 1 0.20739E-09 0.27196E+02 0.20557E+04 c Velocity[X] 0.13733E+02 c Velocity[Y] 0.13462E+02 c Velocity[Z] 0.48939E-05 c Pressure 0.13408E-03 9 0.49535E-04 0.26158E-02 0.61438E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -11.945 21.207 5.6081 7.9999 v Velocity[Y] -13.064 14.65 -0.14319 -0.00067612 v Velocity[Z] -3.065 2.9794 3.3374e-06 -5.3858e-08 v ǁVelocityǁ 0.0034123 22.311 6.5393 8.0108 v Pressure -64327 2.2982e+05 81188 45628 v TurbVisc 2.0647e-22 0.0049685 0.00010627 5.9638e-06 v CourantNb 5.8538e-09 0.011766 0.00016647 4.8855e-06 v FourierNb 1.2425e-07 0.046748 0.00014542 1.7164e-07 v total_pressure 36998 3.3114e+05 1.8251e+05 1.4695e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0636 0.10523 0.003064 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2186e-07 0.051936 0.00031189 5.0571e-06 INSTANT 0.875063000E-01 TIME STEP NUMBER 55261 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282856859E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.646222355E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11560E-01 0.21020E+01 Friction velocity uk : 0.11560E-01 0.21020E+01 Dimensionless distance yplus : 0.11500E-01 0.20640E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.814145323e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29434E+08 1 0.20726E-09 0.27196E+02 0.20557E+04 c Velocity[X] 0.13737E+02 c Velocity[Y] 0.13460E+02 c Velocity[Z] 0.48433E-05 c Pressure 0.13166E-03 22 0.92184E-04 0.25645E-02 0.79171E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -11.969 21.236 5.6083 8 v Velocity[Y] -13.09 14.677 -0.1432 -0.00067635 v Velocity[Z] -3.065 2.9794 3.3363e-06 -5.3858e-08 v ǁVelocityǁ 0.0031863 22.338 6.5407 8.011 v Pressure -63273 2.3081e+05 81826 45982 v TurbVisc 4.6347e-22 0.0049685 0.00010643 5.9805e-06 v CourantNb 1.4442e-08 0.011766 0.00016648 4.8856e-06 v FourierNb 1.2425e-07 0.046752 0.00014542 1.7176e-07 v total_pressure 38052 3.3213e+05 1.8315e+05 1.4731e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.064 0.1052 0.0030635 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2187e-07 0.051941 0.00031189 5.0573e-06 INSTANT 0.875064000E-01 TIME STEP NUMBER 55262 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282864021E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.646997928E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15127E-01 0.21026E+01 Friction velocity uk : 0.15127E-01 0.21026E+01 Dimensionless distance yplus : 0.15049E-01 0.20646E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.565628046e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29435E+08 1 0.20715E-09 0.27198E+02 0.20557E+04 c Velocity[X] 0.13740E+02 c Velocity[Y] 0.13459E+02 c Velocity[Z] 0.47894E-05 c Pressure 0.12924E-03 102 0.78020E-04 0.25132E-02 0.55889E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -11.992 21.264 5.6084 8.0002 v Velocity[Y] -13.116 14.705 -0.14321 -0.00067631 v Velocity[Z] -3.0649 2.9794 3.3352e-06 -5.3858e-08 v ǁVelocityǁ 0.0029634 22.365 6.542 8.0112 v Pressure -62304 2.3173e+05 82327 46243 v TurbVisc 4.2455e-23 0.0049685 0.00010658 5.9974e-06 v CourantNb 2.3796e-08 0.011766 0.00016648 4.8857e-06 v FourierNb 1.2425e-07 0.046757 0.00014542 1.7188e-07 v total_pressure 39021 3.3305e+05 1.8365e+05 1.4757e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0646 0.10515 0.0030628 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2188e-07 0.051947 0.0003119 5.0576e-06 INSTANT 0.875065000E-01 TIME STEP NUMBER 55263 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282871224E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.647747388E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.35772E-02 0.21033E+01 Friction velocity uk : 0.35772E-02 0.21033E+01 Dimensionless distance yplus : 0.35438E-02 0.20652E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.240875299e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29436E+08 1 0.20703E-09 0.27203E+02 0.20558E+04 c Velocity[X] 0.13743E+02 c Velocity[Y] 0.13460E+02 c Velocity[Z] 0.47324E-05 c Pressure 0.12634E-03 9 0.50204E-04 0.24528E-02 0.43905E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -12.015 21.293 5.6085 8.0003 v Velocity[Y] -13.142 14.733 -0.14322 -0.00067592 v Velocity[Z] -3.0649 2.9794 3.3342e-06 -5.3858e-08 v ǁVelocityǁ 0.0027751 22.392 6.5433 8.0114 v Pressure -61432 2.3258e+05 82701 46435 v TurbVisc 7.0994e-23 0.0049685 0.00010673 6.0142e-06 v CourantNb 3.4091e-08 0.011766 0.00016648 4.8858e-06 v FourierNb 1.2425e-07 0.046762 0.00014542 1.72e-07 v total_pressure 39893 3.339e+05 1.8403e+05 1.4776e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0652 0.10509 0.0030619 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2189e-07 0.051953 0.0003119 5.0578e-06 INSTANT 0.875066000E-01 TIME STEP NUMBER 55264 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282878449E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.648520632E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.34521E-02 0.21041E+01 Friction velocity uk : 0.34521E-02 0.21041E+01 Dimensionless distance yplus : 0.34198E-02 0.20660E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 9.261772268e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29436E+08 1 0.20691E-09 0.27204E+02 0.20558E+04 c Velocity[X] 0.13745E+02 c Velocity[Y] 0.13459E+02 c Velocity[Z] 0.46790E-05 c Pressure 0.12373E-03 44 0.94095E-04 0.23982E-02 0.49431E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -12.039 21.321 5.6087 8.0004 v Velocity[Y] -13.167 14.762 -0.14322 -0.00067578 v Velocity[Z] -3.0649 2.9795 3.3331e-06 -5.3858e-08 v ǁVelocityǁ 0.0025952 22.419 6.5446 8.0116 v Pressure -60670 2.3334e+05 83206 46654 v TurbVisc 1.282e-22 0.0049686 0.00010688 6.031e-06 v CourantNb 3.4347e-08 0.011766 0.00016648 4.8859e-06 v FourierNb 1.2425e-07 0.046768 0.00014541 1.7212e-07 v total_pressure 40655 3.3467e+05 1.8453e+05 1.4798e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.066 0.10504 0.0030607 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.219e-07 0.051962 0.0003119 5.058e-06 INSTANT 0.875067000E-01 TIME STEP NUMBER 55265 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282885727E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.649313973E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.24283E-02 0.21049E+01 Friction velocity uk : 0.24283E-02 0.21049E+01 Dimensionless distance yplus : 0.24056E-02 0.20668E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 6.823275232e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29437E+08 1 0.20679E-09 0.27207E+02 0.20558E+04 c Velocity[X] 0.13748E+02 c Velocity[Y] 0.13459E+02 c Velocity[Z] 0.46286E-05 c Pressure 0.12123E-03 39 0.79239E-04 0.23460E-02 0.36396E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -12.062 21.349 5.6088 8.0006 v Velocity[Y] -13.193 14.79 -0.14323 -0.00067592 v Velocity[Z] -3.0649 2.9795 3.3321e-06 -5.3858e-08 v ǁVelocityǁ 0.0024431 22.447 6.546 8.0118 v Pressure -60024 2.3401e+05 83531 46819 v TurbVisc 1.5779e-22 0.0049686 0.00010703 6.048e-06 v CourantNb 3.025e-08 0.011766 0.00016649 4.886e-06 v FourierNb 1.2425e-07 0.046775 0.00014541 1.7224e-07 v total_pressure 41301 3.3533e+05 1.8486e+05 1.4814e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0668 0.10497 0.0030594 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2192e-07 0.05197 0.0003119 5.0583e-06 INSTANT 0.875068000E-01 TIME STEP NUMBER 55266 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282893033E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.650078487E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12998E-01 0.21059E+01 Friction velocity uk : 0.12998E-01 0.21059E+01 Dimensionless distance yplus : 0.12500E-01 0.20678E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 3.918057982e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29438E+08 1 0.20668E-09 0.27212E+02 0.20559E+04 c Velocity[X] 0.13750E+02 c Velocity[Y] 0.13462E+02 c Velocity[Z] 0.45781E-05 c Pressure 0.11867E-03 8 0.51375E-04 0.22926E-02 0.29985E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -12.085 21.377 5.6089 8.0007 v Velocity[Y] -13.219 14.82 -0.14323 -0.0006766 v Velocity[Z] -3.0648 2.9795 3.331e-06 -5.3858e-08 v ǁVelocityǁ 0.0023213 22.475 6.5473 8.012 v Pressure -59500 2.3457e+05 83782 46930 v TurbVisc 4.5064e-23 0.0049686 0.00010718 6.0649e-06 v CourantNb 2.7925e-08 0.011766 0.00016649 4.8861e-06 v FourierNb 1.2425e-07 0.046783 0.00014541 1.7236e-07 v total_pressure 41825 3.359e+05 1.8511e+05 1.4825e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0678 0.1049 0.0030578 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2193e-07 0.051979 0.0003119 5.0585e-06 INSTANT 0.875069000E-01 TIME STEP NUMBER 55267 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282900382E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.650864783E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.89855E-02 0.21069E+01 Friction velocity uk : 0.89855E-02 0.21069E+01 Dimensionless distance yplus : 0.86413E-02 0.20688E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 9.718401822e-03 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29438E+08 1 0.20656E-09 0.27213E+02 0.20559E+04 c Velocity[X] 0.13752E+02 c Velocity[Y] 0.13461E+02 c Velocity[Z] 0.45324E-05 c Pressure 0.11691E-03 15 0.96499E-04 0.22549E-02 0.48128E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -12.108 21.405 5.609 8.0009 v Velocity[Y] -13.245 14.849 -0.14323 -0.00067665 v Velocity[Z] -3.0648 2.9795 3.3299e-06 -5.3858e-08 v ǁVelocityǁ 0.0022093 22.504 6.5486 8.0122 v Pressure -59107 2.3504e+05 84126 47146 v TurbVisc 3.6594e-23 0.0049686 0.00010734 6.0817e-06 v CourantNb 1.796e-08 0.011766 0.00016649 4.8862e-06 v FourierNb 1.2425e-07 0.046791 0.00014541 1.7248e-07 v total_pressure 42218 3.3636e+05 1.8545e+05 1.4847e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0688 0.10482 0.003056 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2194e-07 0.051989 0.0003119 5.0587e-06 INSTANT 0.875070000E-01 TIME STEP NUMBER 55268 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282907747E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.651661908E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.66308E-02 0.21079E+01 Friction velocity uk : 0.66308E-02 0.21079E+01 Dimensionless distance yplus : 0.63769E-02 0.20698E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -9.393891123e-03 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29439E+08 1 0.20645E-09 0.27215E+02 0.20560E+04 c Velocity[X] 0.13754E+02 c Velocity[Y] 0.13462E+02 c Velocity[Z] 0.44942E-05 c Pressure 0.11538E-03 105 0.81399E-04 0.22217E-02 0.20379E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -12.132 21.432 5.6091 8.001 v Velocity[Y] -13.271 14.878 -0.14323 -0.00067656 v Velocity[Z] -3.0648 2.9795 3.3289e-06 -5.3858e-08 v ǁVelocityǁ 0.0021081 22.532 6.5499 8.0124 v Pressure -58843 2.3539e+05 84315 47227 v TurbVisc 1.5259e-22 0.0049686 0.00010749 6.0986e-06 v CourantNb 7.5838e-09 0.011766 0.00016649 4.8864e-06 v FourierNb 1.2425e-07 0.046799 0.00014541 1.7261e-07 v total_pressure 42482 3.3671e+05 1.8564e+05 1.4855e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0698 0.10474 0.0030542 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2195e-07 0.052 0.0003119 5.059e-06 INSTANT 0.875071000E-01 TIME STEP NUMBER 55269 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282915102E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.652434514E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.94693E-02 0.21090E+01 Friction velocity uk : 0.94693E-02 0.21090E+01 Dimensionless distance yplus : 0.91067E-02 0.20709E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -3.209365541e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29440E+08 1 0.20633E-09 0.27219E+02 0.20560E+04 c Velocity[X] 0.13755E+02 c Velocity[Y] 0.13464E+02 c Velocity[Z] 0.44599E-05 c Pressure 0.11421E-03 7 0.51711E-04 0.21955E-02 0.19740E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -12.155 21.46 5.6092 8.0012 v Velocity[Y] -13.297 14.908 -0.14323 -0.00067606 v Velocity[Z] -3.0648 2.9795 3.3278e-06 -5.3858e-08 v ǁVelocityǁ 0.0020395 22.561 6.5512 8.0126 v Pressure -58710 2.3563e+05 84406 47262 v TurbVisc 8.5988e-24 0.0049687 0.00010764 6.1156e-06 v CourantNb 3.0137e-09 0.011766 0.00016649 4.8865e-06 v FourierNb 1.2425e-07 0.046807 0.00014541 1.7273e-07 v total_pressure 42615 3.3696e+05 1.8573e+05 1.4859e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0709 0.10466 0.0030524 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2196e-07 0.05201 0.0003119 5.0592e-06 INSTANT 0.875072000E-01 TIME STEP NUMBER 55270 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282922441E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.653219382E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.47082E-02 0.21101E+01 Friction velocity uk : 0.47082E-02 0.21101E+01 Dimensionless distance yplus : 0.46759E-02 0.20719E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -5.145300881e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29440E+08 1 0.20622E-09 0.27220E+02 0.20560E+04 c Velocity[X] 0.13756E+02 c Velocity[Y] 0.13464E+02 c Velocity[Z] 0.44336E-05 c Pressure 0.11414E-03 31 0.98833E-04 0.21906E-02 0.21201E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -12.178 21.487 5.6092 8.0013 v Velocity[Y] -13.323 14.938 -0.14322 -0.00067581 v Velocity[Z] -3.0647 2.9795 3.3268e-06 -5.3858e-08 v ǁVelocityǁ 0.0019704 22.59 6.5525 8.0129 v Pressure -58705 2.3577e+05 84575 47346 v TurbVisc 1.6605e-23 0.0049687 0.00010779 6.1325e-06 v CourantNb 1.373e-08 0.011766 0.00016649 4.8866e-06 v FourierNb 1.2425e-07 0.046816 0.00014541 1.7285e-07 v total_pressure 42620 3.3709e+05 1.859e+05 1.4867e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0719 0.10458 0.0030507 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2198e-07 0.05202 0.0003119 5.0594e-06 INSTANT 0.875073000E-01 TIME STEP NUMBER 55271 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282929841E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.654009179E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.16928E-01 0.21112E+01 Friction velocity uk : 0.16928E-01 0.21112E+01 Dimensionless distance yplus : 0.16462E-01 0.20730E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -6.451906731e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29441E+08 1 0.20610E-09 0.27221E+02 0.20560E+04 c Velocity[X] 0.13756E+02 c Velocity[Y] 0.13465E+02 c Velocity[Z] 0.44142E-05 c Pressure 0.11427E-03 462 0.83252E-04 0.21896E-02 0.13420E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -12.202 21.515 5.6093 8.0015 v Velocity[Y] -13.35 14.968 -0.14322 -0.00067581 v Velocity[Z] -3.0647 2.9796 3.3257e-06 -5.3858e-08 v ǁVelocityǁ 0.0019222 22.619 6.5538 8.0131 v Pressure -58823 2.3579e+05 84609 47373 v TurbVisc 1.4043e-22 0.0049687 0.00010794 6.1496e-06 v CourantNb 2.9206e-08 0.011766 0.00016649 4.8867e-06 v FourierNb 1.2425e-07 0.046824 0.00014541 1.7297e-07 v total_pressure 42502 3.3712e+05 1.8593e+05 1.487e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.073 0.1045 0.0030489 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2199e-07 0.052031 0.0003119 5.0596e-06 INSTANT 0.875074000E-01 TIME STEP NUMBER 55272 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282937233E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.654782637E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13815E-01 0.21122E+01 Friction velocity uk : 0.13815E-01 0.21122E+01 Dimensionless distance yplus : 0.13476E-01 0.20740E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -7.666908534e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29441E+08 1 0.20599E-09 0.27222E+02 0.20560E+04 c Velocity[X] 0.13756E+02 c Velocity[Y] 0.13467E+02 c Velocity[Z] 0.44017E-05 c Pressure 0.11485E-03 7 0.53110E-04 0.21970E-02 0.19532E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -12.225 21.542 5.6094 8.0016 v Velocity[Y] -13.376 14.998 -0.14321 -0.00067635 v Velocity[Z] -3.0647 2.9796 3.3246e-06 -5.3858e-08 v ǁVelocityǁ 0.0018711 22.649 6.5551 8.0133 v Pressure -59059 2.3571e+05 84607 47363 v TurbVisc 1.0292e-22 0.0049687 0.00010809 6.1666e-06 v CourantNb 4.4492e-08 0.011766 0.00016649 4.8868e-06 v FourierNb 1.2425e-07 0.046832 0.00014541 1.7309e-07 v total_pressure 42266 3.3704e+05 1.8593e+05 1.4869e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.074 0.10442 0.003047 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.22e-07 0.05204 0.0003119 5.0599e-06 INSTANT 0.875075000E-01 TIME STEP NUMBER 55273 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282944650E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.655559424E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.17118E-01 0.21132E+01 Friction velocity uk : 0.17118E-01 0.21132E+01 Dimensionless distance yplus : 0.16743E-01 0.20750E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -8.601567638e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29442E+08 1 0.20588E-09 0.27222E+02 0.20559E+04 c Velocity[X] 0.13755E+02 c Velocity[Y] 0.13467E+02 c Velocity[Z] 0.43967E-05 c Pressure 0.11644E-03 34 0.75758E-04 0.22239E-02 0.41175E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -12.249 21.57 5.6094 8.0018 v Velocity[Y] -13.403 15.029 -0.1432 -0.00067581 v Velocity[Z] -3.0647 2.9796 3.3236e-06 -5.3858e-08 v ǁVelocityǁ 0.0015546 22.678 6.5564 8.0135 v Pressure -59406 2.3554e+05 84528 47344 v TurbVisc 8.845e-23 0.0049687 0.00010824 6.1835e-06 v CourantNb 5.9158e-08 0.011766 0.00016649 4.8869e-06 v FourierNb 1.2425e-07 0.046839 0.00014541 1.7321e-07 v total_pressure 41919 3.3686e+05 1.8585e+05 1.4867e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.075 0.10433 0.0030451 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2201e-07 0.05205 0.0003119 5.0601e-06 INSTANT 0.875076000E-01 TIME STEP NUMBER 55274 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282951993E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.656328815E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19553E-01 0.21141E+01 Friction velocity uk : 0.19553E-01 0.21141E+01 Dimensionless distance yplus : 0.19196E-01 0.20759E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -9.015512473e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29443E+08 1 0.20577E-09 0.27222E+02 0.20558E+04 c Velocity[X] 0.13754E+02 c Velocity[Y] 0.13468E+02 c Velocity[Z] 0.43970E-05 c Pressure 0.11819E-03 100 0.79769E-04 0.22535E-02 0.44692E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -12.272 21.597 5.6095 8.0019 v Velocity[Y] -13.43 15.059 -0.14319 -0.00067625 v Velocity[Z] -3.0646 2.9796 3.3225e-06 -5.3858e-08 v ǁVelocityǁ 0.001806 22.708 6.5576 8.0137 v Pressure -59856 2.3526e+05 84426 47286 v TurbVisc 7.8688e-23 0.0049687 0.00010839 6.2006e-06 v CourantNb 7.2745e-08 0.011766 0.00016649 4.887e-06 v FourierNb 1.2425e-07 0.046846 0.00014541 1.7333e-07 v total_pressure 41469 3.3659e+05 1.8575e+05 1.4861e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0759 0.10425 0.0030432 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2202e-07 0.052058 0.0003119 5.0603e-06 INSTANT 0.875077000E-01 TIME STEP NUMBER 55275 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282959424E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.657100411E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15869E-01 0.21150E+01 Friction velocity uk : 0.15869E-01 0.21150E+01 Dimensionless distance yplus : 0.15480E-01 0.20767E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -9.134849160e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29443E+08 1 0.20566E-09 0.27221E+02 0.20557E+04 c Velocity[X] 0.13752E+02 c Velocity[Y] 0.13469E+02 c Velocity[Z] 0.44074E-05 c Pressure 0.12029E-03 268 0.92466E-04 0.22898E-02 0.50948E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -12.296 21.624 5.6095 8.0021 v Velocity[Y] -13.457 15.089 -0.14318 -0.00067549 v Velocity[Z] -3.0646 2.9796 3.3215e-06 -5.3858e-08 v ǁVelocityǁ 0.0017427 22.737 6.5589 8.0139 v Pressure -60400 2.349e+05 84277 47230 v TurbVisc 2.377e-22 0.0049688 0.00010855 6.2175e-06 v CourantNb 8.2239e-08 0.011766 0.00016649 4.8871e-06 v FourierNb 1.2425e-07 0.046853 0.00014541 1.7346e-07 v total_pressure 40925 3.3623e+05 1.856e+05 1.4855e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0767 0.10418 0.0030414 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2203e-07 0.052066 0.0003119 5.0606e-06 INSTANT 0.875078000E-01 TIME STEP NUMBER 55276 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282966736E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.657865005E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15334E-01 0.21157E+01 Friction velocity uk : 0.15334E-01 0.21157E+01 Dimensionless distance yplus : 0.15130E-01 0.20774E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -8.982128428e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29444E+08 1 0.20555E-09 0.27218E+02 0.20555E+04 c Velocity[X] 0.13750E+02 c Velocity[Y] 0.13468E+02 c Velocity[Z] 0.44240E-05 c Pressure 0.12258E-03 80 0.77744E-04 0.23295E-02 0.40909E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -12.32 21.652 5.6096 8.0022 v Velocity[Y] -13.484 15.119 -0.14317 -0.00067545 v Velocity[Z] -3.0646 2.9796 3.3204e-06 -5.3858e-08 v ǁVelocityǁ 0.0018179 22.767 6.5603 8.0141 v Pressure -61031 2.3446e+05 84061 47097 v TurbVisc 1.8641e-23 0.0049688 0.0001087 6.2347e-06 v CourantNb 7.9562e-08 0.011766 0.00016649 4.8872e-06 v FourierNb 1.2425e-07 0.046858 0.00014541 1.7358e-07 v total_pressure 40294 3.3579e+05 1.8539e+05 1.4842e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0774 0.1041 0.0030397 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2205e-07 0.052073 0.0003119 5.0608e-06 INSTANT 0.875079000E-01 TIME STEP NUMBER 55277 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282974098E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.658625880E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15312E-01 0.21163E+01 Friction velocity uk : 0.15312E-01 0.21163E+01 Dimensionless distance yplus : 0.15033E-01 0.20780E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -8.482572679e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29445E+08 1 0.20544E-09 0.27216E+02 0.20554E+04 c Velocity[X] 0.13747E+02 c Velocity[Y] 0.13469E+02 c Velocity[Z] 0.44471E-05 c Pressure 0.12416E-03 8 0.53077E-04 0.23558E-02 0.27607E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -12.344 21.68 5.6096 8.0024 v Velocity[Y] -13.511 15.149 -0.14316 -0.00067583 v Velocity[Z] -3.0646 2.9796 3.3194e-06 -5.3858e-08 v ǁVelocityǁ 0.0018126 22.796 6.5616 8.0143 v Pressure -61738 2.3395e+05 83865 47005 v TurbVisc 4.0599e-24 0.0049688 0.00010885 6.2517e-06 v CourantNb 6.0885e-08 0.011766 0.00016649 4.8873e-06 v FourierNb 1.2425e-07 0.046863 0.00014541 1.737e-07 v total_pressure 39587 3.3528e+05 1.8519e+05 1.4833e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.078 0.10404 0.0030381 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2206e-07 0.052079 0.00031191 5.061e-06 INSTANT 0.875080000E-01 TIME STEP NUMBER 55278 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282981454E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.659383481E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.14030E-01 0.21168E+01 Friction velocity uk : 0.14030E-01 0.21168E+01 Dimensionless distance yplus : 0.13774E-01 0.20785E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -7.670990198e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29445E+08 1 0.20533E-09 0.27214E+02 0.20553E+04 c Velocity[X] 0.13745E+02 c Velocity[Y] 0.13469E+02 c Velocity[Z] 0.44756E-05 c Pressure 0.12651E-03 44 0.97670E-04 0.23964E-02 0.36619E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -12.368 21.707 5.6097 8.0025 v Velocity[Y] -13.539 15.179 -0.14315 -0.0006759 v Velocity[Z] -3.0645 2.9797 3.3183e-06 -5.3858e-08 v ǁVelocityǁ 0.0018138 22.825 6.5629 8.0145 v Pressure -62507 2.3338e+05 83473 46852 v TurbVisc 7.1353e-24 0.0049688 0.000109 6.2687e-06 v CourantNb 4.4157e-08 0.011766 0.0001665 4.8874e-06 v FourierNb 1.2425e-07 0.046867 0.00014541 1.7382e-07 v total_pressure 38818 3.3471e+05 1.848e+05 1.4818e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0785 0.10398 0.0030366 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2207e-07 0.052084 0.00031191 5.0613e-06 INSTANT 0.875081000E-01 TIME STEP NUMBER 55279 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282988759E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.660126236E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15019E-01 0.21172E+01 Friction velocity uk : 0.15019E-01 0.21172E+01 Dimensionless distance yplus : 0.14725E-01 0.20789E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -6.649624878e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29446E+08 1 0.20522E-09 0.27211E+02 0.20551E+04 c Velocity[X] 0.13742E+02 c Velocity[Y] 0.13469E+02 c Velocity[Z] 0.45044E-05 c Pressure 0.12870E-03 21 0.81774E-04 0.24340E-02 0.38870E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -12.392 21.735 5.6097 8.0027 v Velocity[Y] -13.566 15.208 -0.14314 -0.00067563 v Velocity[Z] -3.0645 2.9797 3.3173e-06 -5.3858e-08 v ǁVelocityǁ 0.0018102 22.855 6.5642 8.0147 v Pressure -63329 2.3276e+05 83147 46679 v TurbVisc 2.872e-23 0.0049688 0.00010915 6.2858e-06 v CourantNb 3.0824e-08 0.011767 0.0001665 4.8875e-06 v FourierNb 1.2425e-07 0.04687 0.00014541 1.7394e-07 v total_pressure 37996 3.3409e+05 1.8447e+05 1.48e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0789 0.10394 0.0030353 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2208e-07 0.052088 0.00031191 5.0615e-06 INSTANT 0.875082000E-01 TIME STEP NUMBER 55280 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282996031E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.660892324E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12795E-01 0.21175E+01 Friction velocity uk : 0.12795E-01 0.21175E+01 Dimensionless distance yplus : 0.12545E-01 0.20792E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -5.411376805e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29447E+08 1 0.20511E-09 0.27209E+02 0.20550E+04 c Velocity[X] 0.13739E+02 c Velocity[Y] 0.13470E+02 c Velocity[Z] 0.45463E-05 c Pressure 0.13055E-03 12 0.52672E-04 0.24649E-02 0.38858E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -12.416 21.763 5.6097 8.0028 v Velocity[Y] -13.594 15.238 -0.14313 -0.00067477 v Velocity[Z] -3.0645 2.9797 3.3162e-06 -5.3858e-08 v ǁVelocityǁ 0.0018093 22.884 6.5655 8.0149 v Pressure -64195 2.321e+05 82808 46522 v TurbVisc 1.2663e-23 0.0049688 0.0001093 6.3029e-06 v CourantNb 2.2246e-08 0.011767 0.0001665 4.8876e-06 v FourierNb 1.2425e-07 0.046872 0.00014541 1.7407e-07 v total_pressure 37130 3.3342e+05 1.8413e+05 1.4785e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0792 0.1039 0.0030342 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2209e-07 0.052091 0.00031191 5.0617e-06 INSTANT 0.875083000E-01 TIME STEP NUMBER 55281 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283003253E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.661641235E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11989E-01 0.21176E+01 Friction velocity uk : 0.11989E-01 0.21176E+01 Dimensionless distance yplus : 0.11695E-01 0.20793E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -3.864313059e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29447E+08 1 0.20501E-09 0.27207E+02 0.20548E+04 c Velocity[X] 0.13736E+02 c Velocity[Y] 0.13471E+02 c Velocity[Z] 0.45866E-05 c Pressure 0.13259E-03 21 0.98796E-04 0.24993E-02 0.70711E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -12.44 21.791 5.6098 8.003 v Velocity[Y] -13.621 15.267 -0.14312 -0.00067448 v Velocity[Z] -3.0645 2.9797 3.3152e-06 -5.3858e-08 v ǁVelocityǁ 0.0018034 22.912 6.5668 8.0151 v Pressure -65094 2.3139e+05 82252 46204 v TurbVisc 3.2445e-23 0.0049689 0.00010945 6.3199e-06 v CourantNb 2.2505e-08 0.011767 0.0001665 4.8877e-06 v FourierNb 1.2425e-07 0.046874 0.00014542 1.7419e-07 v total_pressure 36231 3.3272e+05 1.8358e+05 1.4753e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0793 0.10387 0.0030332 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2211e-07 0.052092 0.00031192 5.0619e-06 INSTANT 0.875084000E-01 TIME STEP NUMBER 55282 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283010451E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.662376150E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10601E-01 0.21176E+01 Friction velocity uk : 0.10601E-01 0.21176E+01 Dimensionless distance yplus : 0.10340E-01 0.20793E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -2.461130726e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29448E+08 1 0.20490E-09 0.27204E+02 0.20546E+04 c Velocity[X] 0.13732E+02 c Velocity[Y] 0.13472E+02 c Velocity[Z] 0.46246E-05 c Pressure 0.13455E-03 91 0.83625E-04 0.25321E-02 0.54074E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -12.464 21.82 5.6098 8.0031 v Velocity[Y] -13.649 15.296 -0.1431 -0.00067446 v Velocity[Z] -3.0644 2.9797 3.3141e-06 -5.3858e-08 v ǁVelocityǁ 0.0018037 22.941 6.5681 8.0153 v Pressure -66021 2.3066e+05 81778 45958 v TurbVisc 2.8467e-23 0.0049689 0.0001096 6.3371e-06 v CourantNb 2.2433e-08 0.011767 0.0001665 4.8879e-06 v FourierNb 1.2425e-07 0.046874 0.00014542 1.7431e-07 v total_pressure 35304 3.3199e+05 1.831e+05 1.4728e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0793 0.10385 0.0030324 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2212e-07 0.052093 0.00031192 5.0622e-06 INSTANT 0.875085000E-01 TIME STEP NUMBER 55283 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283017622E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.663143411E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11240E-01 0.21176E+01 Friction velocity uk : 0.11240E-01 0.21176E+01 Dimensionless distance yplus : 0.10964E-01 0.20793E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -6.531725968e-03 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29449E+08 1 0.20480E-09 0.27202E+02 0.20545E+04 c Velocity[X] 0.13729E+02 c Velocity[Y] 0.13473E+02 c Velocity[Z] 0.46740E-05 c Pressure 0.13610E-03 9 0.53721E-04 0.25572E-02 0.58439E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -12.488 21.848 5.6098 8.0032 v Velocity[Y] -13.676 15.325 -0.14309 -0.00067479 v Velocity[Z] -3.0644 2.9797 3.3131e-06 -5.3858e-08 v ǁVelocityǁ 0.0017953 22.969 6.5695 8.0155 v Pressure -66967 2.2991e+05 81315 45704 v TurbVisc 8.7617e-23 0.0049689 0.00010975 6.3542e-06 v CourantNb 2.2987e-08 0.011767 0.0001665 4.888e-06 v FourierNb 1.2425e-07 0.046874 0.00014542 1.7443e-07 v total_pressure 34358 3.3124e+05 1.8264e+05 1.4703e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0793 0.10384 0.0030318 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2213e-07 0.052092 0.00031192 5.0624e-06 INSTANT 0.875086000E-01 TIME STEP NUMBER 55284 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283024758E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.663894264E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10785E-01 0.21174E+01 Friction velocity uk : 0.10785E-01 0.21174E+01 Dimensionless distance yplus : 0.10520E-01 0.20791E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.146406439e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29449E+08 1 0.20469E-09 0.27200E+02 0.20544E+04 c Velocity[X] 0.13726E+02 c Velocity[Y] 0.13474E+02 c Velocity[Z] 0.47126E-05 c Pressure 0.13790E-03 266 0.75762E-04 0.25868E-02 0.83150E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -12.512 21.877 5.6099 8.0034 v Velocity[Y] -13.704 15.353 -0.14308 -0.00067412 v Velocity[Z] -3.0644 2.9797 3.312e-06 -5.3858e-08 v ǁVelocityǁ 0.0017806 22.998 6.5708 8.0157 v Pressure -67925 2.2915e+05 80629 45387 v TurbVisc 6.4701e-23 0.0049689 0.0001099 6.3712e-06 v CourantNb 2.208e-08 0.011767 0.00016651 4.8881e-06 v FourierNb 1.2425e-07 0.046873 0.00014542 1.7455e-07 v total_pressure 33400 3.3048e+05 1.8195e+05 1.4671e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0791 0.10383 0.0030314 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2214e-07 0.052091 0.00031193 5.0626e-06 INSTANT 0.875087000E-01 TIME STEP NUMBER 55285 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283031808E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.664632571E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11771E-01 0.21171E+01 Friction velocity uk : 0.11771E-01 0.21171E+01 Dimensionless distance yplus : 0.11482E-01 0.20788E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 2.589013690e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29450E+08 1 0.20459E-09 0.27197E+02 0.20542E+04 c Velocity[X] 0.13721E+02 c Velocity[Y] 0.13476E+02 c Velocity[Z] 0.47499E-05 c Pressure 0.13995E-03 67 0.79993E-04 0.26211E-02 0.87326E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -12.536 21.905 5.6099 8.0035 v Velocity[Y] -13.731 15.381 -0.14307 -0.0006745 v Velocity[Z] -3.0643 2.9798 3.311e-06 -5.3858e-08 v ǁVelocityǁ 0.0017631 23.025 6.5722 8.0159 v Pressure -68944 2.2838e+05 80049 45052 v TurbVisc 1.7579e-22 0.0049689 0.00011005 6.3884e-06 v CourantNb 2.1655e-08 0.011767 0.00016651 4.8882e-06 v FourierNb 1.2425e-07 0.046871 0.00014542 1.7468e-07 v total_pressure 32381 3.2971e+05 1.8137e+05 1.4638e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0788 0.10384 0.0030311 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2215e-07 0.052089 0.00031193 5.0628e-06 INSTANT 0.875088000E-01 TIME STEP NUMBER 55286 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283038880E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.665403220E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12796E-01 0.21167E+01 Friction velocity uk : 0.12796E-01 0.21167E+01 Dimensionless distance yplus : 0.12545E-01 0.20784E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 4.511205389e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29451E+08 1 0.20449E-09 0.27195E+02 0.20540E+04 c Velocity[X] 0.13718E+02 c Velocity[Y] 0.13477E+02 c Velocity[Z] 0.47897E-05 c Pressure 0.14183E-03 313 0.92526E-04 0.26520E-02 0.94163E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -12.561 21.934 5.6099 8.0037 v Velocity[Y] -13.759 15.409 -0.14306 -0.00067366 v Velocity[Z] -3.0643 2.9798 3.3099e-06 -5.3858e-08 v ǁVelocityǁ 0.0017406 23.053 6.5735 8.0161 v Pressure -69981 2.2761e+05 79373 44693 v TurbVisc 1.2263e-22 0.004969 0.00011019 6.4054e-06 v CourantNb 2.1112e-08 0.011768 0.00016651 4.8883e-06 v FourierNb 1.2425e-07 0.046869 0.00014542 1.748e-07 v total_pressure 31344 3.2894e+05 1.807e+05 1.4602e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0784 0.10384 0.003031 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2216e-07 0.052086 0.00031193 5.0631e-06 INSTANT 0.875089000E-01 TIME STEP NUMBER 55287 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283045771E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.666157817E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.16155E-01 0.21163E+01 Friction velocity uk : 0.16155E-01 0.21163E+01 Dimensionless distance yplus : 0.15839E-01 0.20780E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 6.243905236e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29451E+08 1 0.20438E-09 0.27189E+02 0.20538E+04 c Velocity[X] 0.13713E+02 c Velocity[Y] 0.13476E+02 c Velocity[Z] 0.48237E-05 c Pressure 0.14392E-03 119 0.78179E-04 0.26868E-02 0.96138E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -12.585 21.963 5.61 8.0038 v Velocity[Y] -13.786 15.437 -0.14305 -0.00067358 v Velocity[Z] -3.0643 2.9798 3.3089e-06 -5.3858e-08 v ǁVelocityǁ 0.0017118 23.081 6.5749 8.0163 v Pressure -71012 2.2684e+05 78664 44287 v TurbVisc 3.668e-22 0.004969 0.00011034 6.4226e-06 v CourantNb 2.5211e-08 0.011768 0.00016651 4.8884e-06 v FourierNb 1.2425e-07 0.046866 0.00014542 1.7492e-07 v total_pressure 30313 3.2817e+05 1.7999e+05 1.4561e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.078 0.10386 0.003031 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2217e-07 0.052082 0.00031194 5.0633e-06 INSTANT 0.875090000E-01 TIME STEP NUMBER 55288 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283052675E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.666917247E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10189E-01 0.21158E+01 Friction velocity uk : 0.10189E-01 0.21158E+01 Dimensionless distance yplus : 0.10004E-01 0.20775E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 7.797222696e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29452E+08 1 0.20428E-09 0.27185E+02 0.20536E+04 c Velocity[X] 0.13709E+02 c Velocity[Y] 0.13477E+02 c Velocity[Z] 0.48606E-05 c Pressure 0.14549E-03 9 0.54841E-04 0.27117E-02 0.84339E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -12.609 21.992 5.61 8.0039 v Velocity[Y] -13.813 15.464 -0.14304 -0.00067392 v Velocity[Z] -3.0643 2.9798 3.3078e-06 -5.3858e-08 v ǁVelocityǁ 0.0016808 23.108 6.5762 8.0165 v Pressure -72032 2.2608e+05 77944 43919 v TurbVisc 3.1898e-22 0.004969 0.00011049 6.4397e-06 v CourantNb 1.4882e-08 0.011768 0.00016652 4.8885e-06 v FourierNb 1.2425e-07 0.046863 0.00014543 1.7504e-07 v total_pressure 29293 3.274e+05 1.7927e+05 1.4524e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0775 0.10387 0.0030311 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2219e-07 0.052078 0.00031194 5.0635e-06 INSTANT 0.875091000E-01 TIME STEP NUMBER 55289 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283059496E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.667677774E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12667E-01 0.21153E+01 Friction velocity uk : 0.12667E-01 0.21153E+01 Dimensionless distance yplus : 0.12559E-01 0.20770E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 9.469727631e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29452E+08 1 0.20419E-09 0.27179E+02 0.20533E+04 c Velocity[X] 0.13703E+02 c Velocity[Y] 0.13476E+02 c Velocity[Z] 0.48791E-05 c Pressure 0.14798E-03 117 0.97701E-04 0.27538E-02 0.11318E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -12.633 22.022 5.61 8.0041 v Velocity[Y] -13.841 15.492 -0.14303 -0.00067404 v Velocity[Z] -3.0642 2.9798 3.3068e-06 -5.3858e-08 v ǁVelocityǁ 0.001641 23.135 6.5776 8.0167 v Pressure -73036 2.2532e+05 77107 43437 v TurbVisc 2.8374e-22 0.004969 0.00011064 6.4568e-06 v CourantNb 6.4615e-09 0.011768 0.00016652 4.8886e-06 v FourierNb 1.2425e-07 0.046859 0.00014543 1.7517e-07 v total_pressure 28289 3.2665e+05 1.7843e+05 1.4476e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.077 0.10389 0.0030312 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.222e-07 0.052074 0.00031195 5.0637e-06 INSTANT 0.875092000E-01 TIME STEP NUMBER 55290 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283066247E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.668433673E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13756E-01 0.21147E+01 Friction velocity uk : 0.13756E-01 0.21147E+01 Dimensionless distance yplus : 0.13707E-01 0.20765E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.047991855e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29453E+08 1 0.20409E-09 0.27173E+02 0.20530E+04 c Velocity[X] 0.13698E+02 c Velocity[Y] 0.13475E+02 c Velocity[Z] 0.48941E-05 c Pressure 0.15059E-03 33 0.81047E-04 0.27978E-02 0.10560E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -12.657 22.051 5.6101 8.0042 v Velocity[Y] -13.868 15.519 -0.14302 -0.00067377 v Velocity[Z] -3.0642 2.9798 3.3057e-06 -5.3858e-08 v ǁVelocityǁ 0.0015977 23.162 6.579 8.0169 v Pressure -74026 2.2458e+05 76282 42978 v TurbVisc 6.2071e-22 0.004969 0.00011079 6.474e-06 v CourantNb 2.4726e-08 0.011768 0.00016652 4.8887e-06 v FourierNb 1.2425e-07 0.046856 0.00014543 1.7529e-07 v total_pressure 27299 3.259e+05 1.7761e+05 1.443e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0765 0.10391 0.0030315 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2221e-07 0.05207 0.00031195 5.064e-06 INSTANT 0.875093000E-01 TIME STEP NUMBER 55291 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283072922E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.669203104E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19204E-01 0.21142E+01 Friction velocity uk : 0.19204E-01 0.21142E+01 Dimensionless distance yplus : 0.19025E-01 0.20759E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.168555952e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29454E+08 1 0.20399E-09 0.27168E+02 0.20527E+04 c Velocity[X] 0.13693E+02 c Velocity[Y] 0.13475E+02 c Velocity[Z] 0.49089E-05 c Pressure 0.15321E-03 10 0.54302E-04 0.28419E-02 0.10650E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -12.681 22.08 5.6101 8.0043 v Velocity[Y] -13.895 15.546 -0.14302 -0.00067293 v Velocity[Z] -3.0642 2.9798 3.3047e-06 -5.3858e-08 v ǁVelocityǁ 0.001567 23.188 6.5804 8.0171 v Pressure -75005 2.2384e+05 75402 42520 v TurbVisc 4.7888e-22 0.0049691 0.00011094 6.4911e-06 v CourantNb 4.4024e-08 0.011768 0.00016653 4.8888e-06 v FourierNb 1.2425e-07 0.046852 0.00014543 1.7541e-07 v total_pressure 26320 3.2516e+05 1.7673e+05 1.4384e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0759 0.10393 0.0030317 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2222e-07 0.052066 0.00031196 5.0642e-06 INSTANT 0.875094000E-01 TIME STEP NUMBER 55292 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283079472E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.669965128E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.89086E-02 0.21137E+01 Friction velocity uk : 0.89086E-02 0.21137E+01 Dimensionless distance yplus : 0.87463E-02 0.20755E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.280445501e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29454E+08 1 0.20389E-09 0.27158E+02 0.20523E+04 c Velocity[X] 0.13685E+02 c Velocity[Y] 0.13473E+02 c Velocity[Z] 0.49089E-05 c Pressure 0.15647E-03 46 0.97065E-04 0.28978E-02 0.14205E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -12.705 22.11 5.6102 8.0045 v Velocity[Y] -13.922 15.573 -0.14301 -0.00067274 v Velocity[Z] -3.0641 2.9798 3.3036e-06 -5.3858e-08 v ǁVelocityǁ 0.0015262 23.215 6.5818 8.0173 v Pressure -75972 2.231e+05 74502 41932 v TurbVisc 3.4289e-22 0.0049691 0.00011108 6.5082e-06 v CourantNb 6.2995e-08 0.011768 0.00016653 4.8889e-06 v FourierNb 1.2425e-07 0.046849 0.00014543 1.7553e-07 v total_pressure 25353 3.2442e+05 1.7583e+05 1.4326e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0755 0.10394 0.003032 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2223e-07 0.052062 0.00031196 5.0644e-06 INSTANT 0.875095000E-01 TIME STEP NUMBER 55293 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283085995E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.670726868E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15186E-01 0.21132E+01 Friction velocity uk : 0.15186E-01 0.21132E+01 Dimensionless distance yplus : 0.14670E-01 0.20750E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.331217925e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29455E+08 1 0.20379E-09 0.27149E+02 0.20519E+04 c Velocity[X] 0.13678E+02 c Velocity[Y] 0.13471E+02 c Velocity[Z] 0.49036E-05 c Pressure 0.15949E-03 101 0.82359E-04 0.29492E-02 0.13829E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -12.729 22.139 5.6103 8.0046 v Velocity[Y] -13.948 15.6 -0.143 -0.00067274 v Velocity[Z] -3.0641 2.9799 3.3026e-06 -5.3858e-08 v ǁVelocityǁ 0.0014961 23.241 6.5831 8.0175 v Pressure -76933 2.2237e+05 73534 41347 v TurbVisc 3.0898e-22 0.0049691 0.00011123 6.5254e-06 v CourantNb 7.9411e-08 0.011768 0.00016653 4.889e-06 v FourierNb 1.2425e-07 0.046846 0.00014543 1.7566e-07 v total_pressure 24392 3.2369e+05 1.7486e+05 1.4267e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.075 0.10397 0.0030324 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2224e-07 0.052058 0.00031197 5.0646e-06 INSTANT 0.875096000E-01 TIME STEP NUMBER 55294 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283092410E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.671485220E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.17184E-01 0.21128E+01 Friction velocity uk : 0.17184E-01 0.21128E+01 Dimensionless distance yplus : 0.16610E-01 0.20746E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.396110456e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29455E+08 1 0.20370E-09 0.27142E+02 0.20516E+04 c Velocity[X] 0.13672E+02 c Velocity[Y] 0.13470E+02 c Velocity[Z] 0.48929E-05 c Pressure 0.16260E-03 10 0.57762E-04 0.30019E-02 0.13139E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -12.752 22.168 5.6103 8.0047 v Velocity[Y] -13.975 15.626 -0.143 -0.00067313 v Velocity[Z] -3.0641 2.9799 3.3015e-06 -5.3858e-08 v ǁVelocityǁ 0.0014747 23.268 6.5845 8.0177 v Pressure -77892 2.2163e+05 72502 40804 v TurbVisc 2.3002e-22 0.0049691 0.00011138 6.5426e-06 v CourantNb 8.8977e-08 0.011768 0.00016654 4.8891e-06 v FourierNb 1.2425e-07 0.046843 0.00014543 1.7578e-07 v total_pressure 23433 3.2296e+05 1.7383e+05 1.4213e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0746 0.10399 0.0030327 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2225e-07 0.052055 0.00031197 5.0649e-06 INSTANT 0.875097000E-01 TIME STEP NUMBER 55295 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283098733E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.672241320E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15433E-01 0.21125E+01 Friction velocity uk : 0.15433E-01 0.21125E+01 Dimensionless distance yplus : 0.14918E-01 0.20743E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.441276851e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29456E+08 1 0.20360E-09 0.27131E+02 0.20511E+04 c Velocity[X] 0.13663E+02 c Velocity[Y] 0.13468E+02 c Velocity[Z] 0.48707E-05 c Pressure 0.16632E-03 126 0.75099E-04 0.30657E-02 0.15907E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -12.776 22.197 5.6104 8.0049 v Velocity[Y] -14.001 15.653 -0.14299 -0.00067256 v Velocity[Z] -3.0641 2.9799 3.3005e-06 -5.3858e-08 v ǁVelocityǁ 0.0014655 23.294 6.5859 8.0179 v Pressure -78851 2.2089e+05 71548 40204 v TurbVisc 9.8679e-22 0.0049691 0.00011152 6.5596e-06 v CourantNb 8.9824e-08 0.011768 0.00016654 4.8892e-06 v FourierNb 1.2425e-07 0.046841 0.00014543 1.759e-07 v total_pressure 22474 3.2222e+05 1.7287e+05 1.4153e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0743 0.104 0.0030329 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2226e-07 0.052053 0.00031198 5.0651e-06 INSTANT 0.875098000E-01 TIME STEP NUMBER 55296 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283104973E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.672999280E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.14953E-01 0.21122E+01 Friction velocity uk : 0.14953E-01 0.21122E+01 Dimensionless distance yplus : 0.14454E-01 0.20740E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.439005726e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29456E+08 1 0.20351E-09 0.27121E+02 0.20507E+04 c Velocity[X] 0.13655E+02 c Velocity[Y] 0.13466E+02 c Velocity[Z] 0.48444E-05 c Pressure 0.16945E-03 166 0.80115E-04 0.31185E-02 0.17529E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -12.8 22.227 5.6105 8.005 v Velocity[Y] -14.028 15.679 -0.14299 -0.00067314 v Velocity[Z] -3.064 2.9799 3.2994e-06 -5.3858e-08 v ǁVelocityǁ 0.0014737 23.32 6.5873 8.0181 v Pressure -79815 2.2015e+05 70436 39528 v TurbVisc 1.172e-21 0.0049691 0.00011167 6.5768e-06 v CourantNb 9.0315e-08 0.011768 0.00016655 4.8893e-06 v FourierNb 1.2425e-07 0.04684 0.00014544 1.7602e-07 v total_pressure 21510 3.2147e+05 1.7176e+05 1.4085e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.074 0.10401 0.003033 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2227e-07 0.052051 0.00031198 5.0653e-06 INSTANT 0.875099000E-01 TIME STEP NUMBER 55297 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283111139E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.673737076E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13766E-01 0.21120E+01 Friction velocity uk : 0.13766E-01 0.21120E+01 Dimensionless distance yplus : 0.13428E-01 0.20738E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.443377556e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29457E+08 1 0.20342E-09 0.27110E+02 0.20502E+04 c Velocity[X] 0.13648E+02 c Velocity[Y] 0.13462E+02 c Velocity[Z] 0.48083E-05 c Pressure 0.17288E-03 190 0.92306E-04 0.31766E-02 0.15602E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -12.823 22.256 5.6105 8.0051 v Velocity[Y] -14.054 15.706 -0.14298 -0.00067233 v Velocity[Z] -3.064 2.9799 3.2984e-06 -5.3858e-08 v ǁVelocityǁ 0.0014995 23.347 6.5887 8.0183 v Pressure -80792 2.1939e+05 69344 38957 v TurbVisc 3.2351e-22 0.0049692 0.00011182 6.5939e-06 v CourantNb 9.0886e-08 0.011768 0.00016655 4.8894e-06 v FourierNb 1.2425e-07 0.046839 0.00014544 1.7615e-07 v total_pressure 20533 3.2071e+05 1.7067e+05 1.4028e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0738 0.10401 0.0030329 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2228e-07 0.05205 0.00031198 5.0655e-06 INSTANT 0.875100000E-01 TIME STEP NUMBER 55298 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283117105E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.674476466E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.90079E-02 0.21120E+01 Friction velocity uk : 0.90079E-02 0.21120E+01 Dimensionless distance yplus : 0.89758E-02 0.20738E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.425479041e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29458E+08 1 0.20333E-09 0.27097E+02 0.20496E+04 c Velocity[X] 0.13639E+02 c Velocity[Y] 0.13458E+02 c Velocity[Z] 0.47700E-05 c Pressure 0.17616E-03 507 0.78369E-04 0.32318E-02 0.19047E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -12.847 22.285 5.6106 8.0052 v Velocity[Y] -14.08 15.733 -0.14298 -0.00067226 v Velocity[Z] -3.064 2.9799 3.2974e-06 -5.3859e-08 v ǁVelocityǁ 0.001547 23.373 6.5901 8.0184 v Pressure -81814 2.1861e+05 68194 38229 v TurbVisc 1.4247e-21 0.0049692 0.00011196 6.6112e-06 v CourantNb 9.3476e-08 0.011768 0.00016655 4.8895e-06 v FourierNb 1.2425e-07 0.046839 0.00014544 1.7627e-07 v total_pressure 19511 3.1994e+05 1.6952e+05 1.3955e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0738 0.104 0.0030328 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2229e-07 0.05205 0.00031199 5.0658e-06 INSTANT 0.875101000E-01 TIME STEP NUMBER 55299 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283123029E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.675204278E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.75242E-02 0.21120E+01 Friction velocity uk : 0.75242E-02 0.21120E+01 Dimensionless distance yplus : 0.74727E-02 0.20738E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.388036187e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29458E+08 1 0.20324E-09 0.27088E+02 0.20492E+04 c Velocity[X] 0.13632E+02 c Velocity[Y] 0.13456E+02 c Velocity[Z] 0.47323E-05 c Pressure 0.17877E-03 10 0.61705E-04 0.32746E-02 0.16607E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -12.87 22.314 5.6107 8.0053 v Velocity[Y] -14.106 15.759 -0.14298 -0.00067284 v Velocity[Z] -3.0639 2.9799 3.2963e-06 -5.3859e-08 v ǁVelocityǁ 0.0016098 23.4 6.5916 8.0186 v Pressure -82944 2.1781e+05 66962 37588 v TurbVisc 1.1385e-21 0.0049692 0.00011211 6.6283e-06 v CourantNb 1.0111e-07 0.011768 0.00016655 4.8896e-06 v FourierNb 1.2425e-07 0.04684 0.00014544 1.7639e-07 v total_pressure 18381 3.1913e+05 1.6829e+05 1.3891e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0738 0.10398 0.0030325 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.223e-07 0.052052 0.00031199 5.066e-06 INSTANT 0.875102000E-01 TIME STEP NUMBER 55300 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283128786E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.675921646E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.59250E-02 0.21122E+01 Friction velocity uk : 0.59250E-02 0.21122E+01 Dimensionless distance yplus : 0.58567E-02 0.20740E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.342883668e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29459E+08 1 0.20315E-09 0.27075E+02 0.20487E+04 c Velocity[X] 0.13622E+02 c Velocity[Y] 0.13453E+02 c Velocity[Z] 0.46836E-05 c Pressure 0.18223E-03 556 0.74720E-04 0.33329E-02 0.21522E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -12.894 22.342 5.6108 8.0055 v Velocity[Y] -14.132 15.786 -0.14298 -0.00067221 v Velocity[Z] -3.0639 2.9799 3.2953e-06 -5.3859e-08 v ǁVelocityǁ 0.001705 23.426 6.593 8.0188 v Pressure -84118 2.1697e+05 65851 36833 v TurbVisc 9.4686e-22 0.0049692 0.00011225 6.6454e-06 v CourantNb 1.0627e-07 0.011768 0.00016656 4.8897e-06 v FourierNb 1.2425e-07 0.046842 0.00014544 1.7651e-07 v total_pressure 17207 3.183e+05 1.6718e+05 1.3816e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.074 0.10396 0.003032 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2231e-07 0.052054 0.00031199 5.0662e-06 INSTANT 0.875103000E-01 TIME STEP NUMBER 55301 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283134494E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.676639608E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.70166E-02 0.21125E+01 Friction velocity uk : 0.70166E-02 0.21125E+01 Dimensionless distance yplus : 0.69357E-02 0.20743E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.270489705e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29459E+08 1 0.20306E-09 0.27063E+02 0.20482E+04 c Velocity[X] 0.13613E+02 c Velocity[Y] 0.13450E+02 c Velocity[Z] 0.46337E-05 c Pressure 0.18482E-03 31 0.80475E-04 0.33750E-02 0.22265E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -12.917 22.371 5.6109 8.0056 v Velocity[Y] -14.158 15.813 -0.14298 -0.00067301 v Velocity[Z] -3.0639 2.98 3.2942e-06 -5.3859e-08 v ǁVelocityǁ 0.0018123 23.453 6.5944 8.019 v Pressure -85343 2.1611e+05 64526 36038 v TurbVisc 1.3816e-21 0.0049692 0.0001124 6.6626e-06 v CourantNb 1.0958e-07 0.011768 0.00016656 4.8898e-06 v FourierNb 1.2425e-07 0.046845 0.00014544 1.7664e-07 v total_pressure 15982 3.1743e+05 1.6585e+05 1.3736e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0743 0.10393 0.0030314 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2232e-07 0.052058 0.000312 5.0664e-06 INSTANT 0.875104000E-01 TIME STEP NUMBER 55302 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283140095E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.677322646E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.69835E-02 0.21129E+01 Friction velocity uk : 0.69835E-02 0.21129E+01 Dimensionless distance yplus : 0.67160E-02 0.20747E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.211383134e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29460E+08 1 0.20297E-09 0.27052E+02 0.20477E+04 c Velocity[X] 0.13605E+02 c Velocity[Y] 0.13447E+02 c Velocity[Z] 0.45773E-05 c Pressure 0.18787E-03 147 0.92922E-04 0.34253E-02 0.20012E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -12.94 22.4 5.611 8.0057 v Velocity[Y] -14.183 15.839 -0.14298 -0.00067225 v Velocity[Z] -3.0638 2.98 3.2932e-06 -5.3859e-08 v ǁVelocityǁ 0.0019381 23.48 6.5958 8.0192 v Pressure -86628 2.152e+05 63250 35361 v TurbVisc 1.7463e-21 0.0049693 0.00011255 6.6797e-06 v CourantNb 1.104e-07 0.011768 0.00016656 4.8899e-06 v FourierNb 1.2425e-07 0.046849 0.00014544 1.7676e-07 v total_pressure 14697 3.1652e+05 1.6457e+05 1.3669e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0747 0.10389 0.0030307 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2233e-07 0.052062 0.000312 5.0667e-06 INSTANT 0.875105000E-01 TIME STEP NUMBER 55303 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283145484E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.678011802E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.70217E-02 0.21134E+01 Friction velocity uk : 0.70217E-02 0.21134E+01 Dimensionless distance yplus : 0.69407E-02 0.20752E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.135791287e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29460E+08 1 0.20288E-09 0.27038E+02 0.20471E+04 c Velocity[X] 0.13596E+02 c Velocity[Y] 0.13442E+02 c Velocity[Z] 0.45263E-05 c Pressure 0.19075E-03 171 0.78944E-04 0.34725E-02 0.24430E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -12.964 22.428 5.6111 8.0058 v Velocity[Y] -14.209 15.866 -0.14298 -0.00067237 v Velocity[Z] -3.0638 2.98 3.2921e-06 -5.3859e-08 v ǁVelocityǁ 0.0020777 23.507 6.5972 8.0193 v Pressure -87977 2.1424e+05 61908 34509 v TurbVisc 1.7693e-21 0.0049693 0.00011269 6.6969e-06 v CourantNb 1.0895e-07 0.011768 0.00016656 4.89e-06 v FourierNb 1.2425e-07 0.046853 0.00014544 1.7688e-07 v total_pressure 13348 3.1556e+05 1.6323e+05 1.3583e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0752 0.10385 0.0030298 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2234e-07 0.052068 0.000312 5.0669e-06 INSTANT 0.875106000E-01 TIME STEP NUMBER 55304 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283150806E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.678684167E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.47095E-02 0.21140E+01 Friction velocity uk : 0.47095E-02 0.21140E+01 Dimensionless distance yplus : 0.46772E-02 0.20758E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.060132856e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29461E+08 1 0.20280E-09 0.27028E+02 0.20467E+04 c Velocity[X] 0.13588E+02 c Velocity[Y] 0.13440E+02 c Velocity[Z] 0.44817E-05 c Pressure 0.19308E-03 10 0.63409E-04 0.35094E-02 0.20601E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -12.987 22.456 5.6112 8.0059 v Velocity[Y] -14.235 15.893 -0.14298 -0.00067291 v Velocity[Z] -3.0638 2.98 3.2911e-06 -5.3859e-08 v ǁVelocityǁ 0.0020539 23.534 6.5986 8.0195 v Pressure -89396 2.1322e+05 60509 33791 v TurbVisc 1.8113e-21 0.0049693 0.00011283 6.7141e-06 v CourantNb 1.0523e-07 0.011768 0.00016657 4.8901e-06 v FourierNb 1.2425e-07 0.046859 0.00014544 1.77e-07 v total_pressure 11929 3.1455e+05 1.6183e+05 1.3512e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0758 0.1038 0.0030288 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2234e-07 0.052075 0.000312 5.0671e-06 INSTANT 0.875107000E-01 TIME STEP NUMBER 55305 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283155953E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.679343503E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.36840E-02 0.21148E+01 Friction velocity uk : 0.36840E-02 0.21148E+01 Dimensionless distance yplus : 0.35429E-02 0.20765E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 9.821050950e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29461E+08 1 0.20271E-09 0.27015E+02 0.20462E+04 c Velocity[X] 0.13578E+02 c Velocity[Y] 0.13437E+02 c Velocity[Z] 0.44286E-05 c Pressure 0.19628E-03 541 0.75170E-04 0.35621E-02 0.27391E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -13.01 22.484 5.6113 8.006 v Velocity[Y] -14.26 15.92 -0.14299 -0.00067246 v Velocity[Z] -3.0637 2.98 3.2901e-06 -5.3859e-08 v ǁVelocityǁ 0.0017032 23.561 6.6 8.0197 v Pressure -90888 2.1214e+05 59192 32917 v TurbVisc 1.4385e-21 0.0049693 0.00011298 6.7311e-06 v CourantNb 9.9103e-08 0.011768 0.00016657 4.8902e-06 v FourierNb 1.2425e-07 0.046865 0.00014544 1.7712e-07 v total_pressure 10437 3.1347e+05 1.6052e+05 1.3424e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0765 0.10374 0.0030279 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2235e-07 0.052083 0.00031201 5.0673e-06 INSTANT 0.875108000E-01 TIME STEP NUMBER 55306 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283161035E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.679998323E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11515E-01 0.21156E+01 Friction velocity uk : 0.11515E-01 0.21156E+01 Dimensionless distance yplus : 0.11074E-01 0.20773E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 9.046699995e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29461E+08 1 0.20263E-09 0.27004E+02 0.20457E+04 c Velocity[X] 0.13569E+02 c Velocity[Y] 0.13434E+02 c Velocity[Z] 0.43799E-05 c Pressure 0.19889E-03 31 0.81107E-04 0.36038E-02 0.27432E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -13.033 22.511 5.6115 8.0061 v Velocity[Y] -14.286 15.948 -0.14299 -0.00067324 v Velocity[Z] -3.0637 2.98 3.289e-06 -5.3859e-08 v ǁVelocityǁ 0.0015897 23.589 6.6015 8.0198 v Pressure -92455 2.11e+05 57698 32037 v TurbVisc 1.2503e-21 0.0049693 0.00011312 6.7483e-06 v CourantNb 9.1484e-08 0.011768 0.00016657 4.8903e-06 v FourierNb 1.2425e-07 0.046871 0.00014544 1.7725e-07 v total_pressure 8870.4 3.1232e+05 1.5902e+05 1.3336e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0773 0.10368 0.0030269 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2236e-07 0.052091 0.00031201 5.0676e-06 INSTANT 0.875109000E-01 TIME STEP NUMBER 55307 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283166005E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.680624002E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.14400E-01 0.21165E+01 Friction velocity uk : 0.14400E-01 0.21165E+01 Dimensionless distance yplus : 0.14047E-01 0.20782E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 8.416648327e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29462E+08 1 0.20254E-09 0.26991E+02 0.20452E+04 c Velocity[X] 0.13561E+02 c Velocity[Y] 0.13431E+02 c Velocity[Z] 0.43328E-05 c Pressure 0.20199E-03 205 0.93323E-04 0.36544E-02 0.25213E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -13.056 22.539 5.6116 8.0062 v Velocity[Y] -14.311 15.975 -0.143 -0.00067251 v Velocity[Z] -3.0637 2.98 3.288e-06 -5.3859e-08 v ǁVelocityǁ 0.001874 23.616 6.6029 8.02 v Pressure -94099 2.0977e+05 56239 31266 v TurbVisc 1.6107e-21 0.0049693 0.00011327 6.7654e-06 v CourantNb 8.9786e-08 0.011768 0.00016657 4.8904e-06 v FourierNb 1.2425e-07 0.046879 0.00014544 1.7737e-07 v total_pressure 7225.9 3.111e+05 1.5756e+05 1.3259e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0782 0.10361 0.0030257 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2237e-07 0.0521 0.00031201 5.0678e-06 INSTANT 0.875110000E-01 TIME STEP NUMBER 55308 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283170736E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.681252814E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.14228E-01 0.21175E+01 Friction velocity uk : 0.14228E-01 0.21175E+01 Dimensionless distance yplus : 0.13879E-01 0.20792E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 7.802801740e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29462E+08 1 0.20245E-09 0.26976E+02 0.20445E+04 c Velocity[X] 0.13551E+02 c Velocity[Y] 0.13426E+02 c Velocity[Z] 0.42934E-05 c Pressure 0.20508E-03 211 0.79619E-04 0.37046E-02 0.30216E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -13.08 22.566 5.6117 8.0063 v Velocity[Y] -14.337 16.003 -0.143 -0.00067268 v Velocity[Z] -3.0636 2.98 3.2869e-06 -5.3859e-08 v ǁVelocityǁ 0.001811 23.644 6.6043 8.0202 v Pressure -95824 2.0847e+05 54724 30333 v TurbVisc 2.1459e-21 0.0049694 0.00011341 6.7827e-06 v CourantNb 6.8419e-08 0.011768 0.00016657 4.8905e-06 v FourierNb 1.2425e-07 0.046887 0.00014544 1.7749e-07 v total_pressure 5501.1 3.098e+05 1.5605e+05 1.3166e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0792 0.10354 0.0030245 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2238e-07 0.05211 0.00031201 5.068e-06 INSTANT 0.875111000E-01 TIME STEP NUMBER 55309 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283175398E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.681866627E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.17569E-01 0.21185E+01 Friction velocity uk : 0.17569E-01 0.21185E+01 Dimensionless distance yplus : 0.16972E-01 0.20802E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 7.289834482e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29463E+08 1 0.20237E-09 0.26965E+02 0.20440E+04 c Velocity[X] 0.13542E+02 c Velocity[Y] 0.13423E+02 c Velocity[Z] 0.42655E-05 c Pressure 0.20771E-03 10 0.64913E-04 0.37463E-02 0.26066E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -13.103 22.593 5.6118 8.0064 v Velocity[Y] -14.362 16.03 -0.14301 -0.00067329 v Velocity[Z] -3.0636 2.98 3.2859e-06 -5.3859e-08 v ǁVelocityǁ 0.0020189 23.672 6.6057 8.0203 v Pressure -97628 2.0709e+05 53185 29530 v TurbVisc 2.4238e-21 0.0049694 0.00011355 6.7998e-06 v CourantNb 7.462e-08 0.011768 0.00016658 4.8906e-06 v FourierNb 1.2425e-07 0.046895 0.00014544 1.7761e-07 v total_pressure 3696.9 3.0842e+05 1.5451e+05 1.3086e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0802 0.10346 0.0030231 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2238e-07 0.05212 0.00031201 5.0682e-06 INSTANT 0.875112000E-01 TIME STEP NUMBER 55310 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283179853E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.682469262E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15220E-01 0.21196E+01 Friction velocity uk : 0.15220E-01 0.21196E+01 Dimensionless distance yplus : 0.14703E-01 0.20813E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 6.864858840e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29463E+08 1 0.20228E-09 0.26951E+02 0.20435E+04 c Velocity[X] 0.13532E+02 c Velocity[Y] 0.13419E+02 c Velocity[Z] 0.42309E-05 c Pressure 0.21101E-03 145 0.76030E-04 0.38001E-02 0.33978E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -13.126 22.62 5.6119 8.0065 v Velocity[Y] -14.388 16.058 -0.14302 -0.0006729 v Velocity[Z] -3.0636 2.9801 3.2849e-06 -5.3859e-08 v ǁVelocityǁ 0.0018601 23.699 6.6072 8.0205 v Pressure -99506 2.0563e+05 51634 28582 v TurbVisc 2.2514e-21 0.0049694 0.00011369 6.8168e-06 v CourantNb 8.77e-08 0.011768 0.00016658 4.8907e-06 v FourierNb 1.2425e-07 0.046903 0.00014543 1.7774e-07 v total_pressure 1818.9 3.0695e+05 1.5296e+05 1.2991e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0813 0.10338 0.0030217 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2239e-07 0.052131 0.00031201 5.0684e-06 INSTANT 0.875113000E-01 TIME STEP NUMBER 55311 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283184259E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.683061304E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15455E-01 0.21207E+01 Friction velocity uk : 0.15455E-01 0.21207E+01 Dimensionless distance yplus : 0.15116E-01 0.20824E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 6.567434756e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29464E+08 1 0.20220E-09 0.26937E+02 0.20429E+04 c Velocity[X] 0.13521E+02 c Velocity[Y] 0.13416E+02 c Velocity[Z] 0.42014E-05 c Pressure 0.21421E-03 50 0.82281E-04 0.38518E-02 0.34950E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -13.149 22.647 5.6121 8.0066 v Velocity[Y] -14.414 16.086 -0.14303 -0.00067372 v Velocity[Z] -3.0635 2.9801 3.2838e-06 -5.3859e-08 v ǁVelocityǁ 0.0017249 23.727 6.6086 8.0206 v Pressure -1.0146e+05 2.0408e+05 49994 27601 v TurbVisc 3.8583e-21 0.0049694 0.00011384 6.834e-06 v CourantNb 8.6682e-08 0.011768 0.00016658 4.8908e-06 v FourierNb 1.2425e-07 0.046912 0.00014543 1.7786e-07 v total_pressure -135.05 3.0541e+05 1.5132e+05 1.2893e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0824 0.1033 0.0030203 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.224e-07 0.052141 0.00031201 5.0687e-06 INSTANT 0.875114000E-01 TIME STEP NUMBER 55312 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283188526E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.683647140E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.85702E-02 0.21218E+01 Friction velocity uk : 0.85702E-02 0.21218E+01 Dimensionless distance yplus : 0.84141E-02 0.20834E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 6.459168306e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29464E+08 1 0.20211E-09 0.26922E+02 0.20423E+04 c Velocity[X] 0.13511E+02 c Velocity[Y] 0.13411E+02 c Velocity[Z] 0.41792E-05 c Pressure 0.21748E-03 461 0.94520E-04 0.39047E-02 0.31245E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -13.172 22.674 5.6122 8.0067 v Velocity[Y] -14.439 16.113 -0.14304 -0.00067291 v Velocity[Z] -3.0635 2.9801 3.2828e-06 -5.3859e-08 v ǁVelocityǁ 0.0016084 23.755 6.61 8.0208 v Pressure -1.0349e+05 2.0246e+05 48377 26774 v TurbVisc 4.049e-21 0.0049694 0.00011398 6.851e-06 v CourantNb 8.5884e-08 0.011768 0.00016658 4.8909e-06 v FourierNb 1.2425e-07 0.04692 0.00014543 1.7798e-07 v total_pressure -2167.5 3.0378e+05 1.497e+05 1.281e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0834 0.10322 0.0030189 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2241e-07 0.052152 0.00031202 5.0689e-06 INSTANT 0.875115000E-01 TIME STEP NUMBER 55313 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283192549E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.684227982E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.18449E-01 0.21229E+01 Friction velocity uk : 0.18449E-01 0.21229E+01 Dimensionless distance yplus : 0.18356E-01 0.20845E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 6.438160326e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29464E+08 1 0.20202E-09 0.26905E+02 0.20416E+04 c Velocity[X] 0.13500E+02 c Velocity[Y] 0.13405E+02 c Velocity[Z] 0.41652E-05 c Pressure 0.22064E-03 377 0.80655E-04 0.39554E-02 0.37970E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -13.196 22.7 5.6123 8.0067 v Velocity[Y] -14.465 16.141 -0.14305 -0.00067313 v Velocity[Z] -3.0635 2.9801 3.2817e-06 -5.3859e-08 v ǁVelocityǁ 0.0015128 23.783 6.6115 8.0209 v Pressure -1.056e+05 2.0074e+05 46699 25766 v TurbVisc 4.1047e-21 0.0049694 0.00011412 6.8682e-06 v CourantNb 8.0821e-08 0.011768 0.00016658 4.891e-06 v FourierNb 1.2425e-07 0.046929 0.00014543 1.781e-07 v total_pressure -4270.9 3.0206e+05 1.4802e+05 1.2709e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0845 0.10317 0.0030177 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2241e-07 0.052162 0.00031202 5.0691e-06 INSTANT 0.875116000E-01 TIME STEP NUMBER 55314 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283196490E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.684798144E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.17322E-01 0.21240E+01 Friction velocity uk : 0.17322E-01 0.21240E+01 Dimensionless distance yplus : 0.17174E-01 0.20855E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 6.548549190e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29465E+08 1 0.20194E-09 0.26890E+02 0.20410E+04 c Velocity[X] 0.13489E+02 c Velocity[Y] 0.13401E+02 c Velocity[Z] 0.41647E-05 c Pressure 0.22319E-03 10 0.66104E-04 0.39952E-02 0.33260E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -13.219 22.727 5.6124 8.0068 v Velocity[Y] -14.491 16.169 -0.14306 -0.00067388 v Velocity[Z] -3.0634 2.9801 3.2807e-06 -5.3859e-08 v ǁVelocityǁ 0.0014465 23.811 6.6129 8.0211 v Pressure -1.0776e+05 1.9894e+05 45049 24891 v TurbVisc 4.8009e-21 0.0049695 0.00011426 6.8853e-06 v CourantNb 7.3188e-08 0.011768 0.00016659 4.8911e-06 v FourierNb 1.2425e-07 0.046937 0.00014543 1.7822e-07 v total_pressure -6437.7 3.0027e+05 1.4637e+05 1.2622e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0855 0.10312 0.0030165 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2242e-07 0.052173 0.00031202 5.0693e-06 INSTANT 0.875117000E-01 TIME STEP NUMBER 55315 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283200210E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.685360448E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12038E-01 0.21250E+01 Friction velocity uk : 0.12038E-01 0.21250E+01 Dimensionless distance yplus : 0.11976E-01 0.20866E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 6.729342472e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29465E+08 1 0.20185E-09 0.26874E+02 0.20403E+04 c Velocity[X] 0.13478E+02 c Velocity[Y] 0.13396E+02 c Velocity[Z] 0.41534E-05 c Pressure 0.22594E-03 198 0.76921E-04 0.40383E-02 0.42799E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -13.242 22.753 5.6126 8.0069 v Velocity[Y] -14.517 16.197 -0.14307 -0.0006735 v Velocity[Z] -3.0634 2.9801 3.2797e-06 -5.3859e-08 v ǁVelocityǁ 0.0014031 23.838 6.6144 8.0212 v Pressure -1.0998e+05 1.9707e+05 43269 23878 v TurbVisc 4.2663e-21 0.0049695 0.0001144 6.9023e-06 v CourantNb 6.2363e-08 0.011767 0.00016659 4.8912e-06 v FourierNb 1.2425e-07 0.046945 0.00014543 1.7835e-07 v total_pressure -8653.1 2.984e+05 1.4459e+05 1.252e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0866 0.10305 0.0030153 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2242e-07 0.052183 0.00031202 5.0695e-06 INSTANT 0.875118000E-01 TIME STEP NUMBER 55316 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283203878E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.685905339E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.73079E-02 0.21259E+01 Friction velocity uk : 0.73079E-02 0.21259E+01 Dimensionless distance yplus : 0.71748E-02 0.20875E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 7.080979223e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29465E+08 1 0.20176E-09 0.26858E+02 0.20397E+04 c Velocity[X] 0.13466E+02 c Velocity[Y] 0.13392E+02 c Velocity[Z] 0.41470E-05 c Pressure 0.22899E-03 45 0.82862E-04 0.40866E-02 0.44422E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -13.265 22.779 5.6127 8.007 v Velocity[Y] -14.543 16.225 -0.14309 -0.00067436 v Velocity[Z] -3.0634 2.9801 3.2786e-06 -5.3859e-08 v ǁVelocityǁ 0.0013932 23.866 6.6158 8.0213 v Pressure -1.1224e+05 1.9513e+05 41523 22828 v TurbVisc 6.2474e-21 0.0049695 0.00011454 6.9194e-06 v CourantNb 5.2799e-08 0.011767 0.00016659 4.8913e-06 v FourierNb 1.2425e-07 0.046952 0.00014543 1.7847e-07 v total_pressure -10915 2.9646e+05 1.4285e+05 1.2415e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0875 0.103 0.0030143 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2243e-07 0.052192 0.00031202 5.0697e-06 INSTANT 0.875119000E-01 TIME STEP NUMBER 55317 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283207396E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.686467829E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.95218E-02 0.21268E+01 Friction velocity uk : 0.95218E-02 0.21268E+01 Dimensionless distance yplus : 0.92577E-02 0.20884E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 7.528163839e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29466E+08 1 0.20168E-09 0.26841E+02 0.20390E+04 c Velocity[X] 0.13455E+02 c Velocity[Y] 0.13386E+02 c Velocity[Z] 0.41531E-05 c Pressure 0.23145E-03 205 0.95417E-04 0.41243E-02 0.39948E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -13.289 22.805 5.6128 8.007 v Velocity[Y] -14.569 16.252 -0.1431 -0.00067366 v Velocity[Z] -3.0633 2.9801 3.2776e-06 -5.3859e-08 v ǁVelocityǁ 0.0014121 23.893 6.6173 8.0215 v Pressure -1.1454e+05 1.9312e+05 39768 21942 v TurbVisc 5.7324e-21 0.0049695 0.00011468 6.9364e-06 v CourantNb 4.4658e-08 0.011767 0.0001666 4.8914e-06 v FourierNb 1.2425e-07 0.046959 0.00014543 1.7859e-07 v total_pressure -13215 2.9445e+05 1.4109e+05 1.2327e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0884 0.10295 0.0030133 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2244e-07 0.0522 0.00031203 5.0699e-06 INSTANT 0.875120000E-01 TIME STEP NUMBER 55318 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283210658E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.687013085E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12018E-01 0.21276E+01 Friction velocity uk : 0.12018E-01 0.21276E+01 Dimensionless distance yplus : 0.12058E-01 0.20892E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 8.059615311e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29466E+08 1 0.20159E-09 0.26822E+02 0.20382E+04 c Velocity[X] 0.13443E+02 c Velocity[Y] 0.13379E+02 c Velocity[Z] 0.41629E-05 c Pressure 0.23367E-03 100 0.81191E-04 0.41576E-02 0.48807E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -13.312 22.831 5.6129 8.0071 v Velocity[Y] -14.595 16.28 -0.14311 -0.00067389 v Velocity[Z] -3.0633 2.9801 3.2766e-06 -5.3859e-08 v ǁVelocityǁ 0.0014588 23.92 6.6187 8.0216 v Pressure -1.1687e+05 1.9105e+05 37959 20869 v TurbVisc 6.2981e-21 0.0049695 0.00011482 6.9535e-06 v CourantNb 3.8151e-08 0.011768 0.0001666 4.8914e-06 v FourierNb 1.2425e-07 0.046965 0.00014543 1.7871e-07 v total_pressure -15545 2.9237e+05 1.3928e+05 1.2219e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0892 0.10291 0.0030125 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2244e-07 0.052208 0.00031203 5.0702e-06 INSTANT 0.875121000E-01 TIME STEP NUMBER 55319 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283213831E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.687550330E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13196E-01 0.21284E+01 Friction velocity uk : 0.13196E-01 0.21284E+01 Dimensionless distance yplus : 0.12937E-01 0.20899E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 8.615773943e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29466E+08 1 0.20150E-09 0.26807E+02 0.20376E+04 c Velocity[X] 0.13432E+02 c Velocity[Y] 0.13374E+02 c Velocity[Z] 0.41765E-05 c Pressure 0.23514E-03 11 0.67210E-04 0.41775E-02 0.43053E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -13.335 22.857 5.613 8.0072 v Velocity[Y] -14.622 16.307 -0.14312 -0.00067453 v Velocity[Z] -3.0632 2.9801 3.2755e-06 -5.3859e-08 v ǁVelocityǁ 0.0015203 23.947 6.6202 8.0217 v Pressure -1.1922e+05 1.8892e+05 36208 19942 v TurbVisc 6.562e-21 0.0049696 0.00011496 6.9705e-06 v CourantNb 3.3351e-08 0.011768 0.0001666 4.8915e-06 v FourierNb 1.2425e-07 0.046971 0.00014543 1.7883e-07 v total_pressure -17892 2.9025e+05 1.3753e+05 1.2127e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0899 0.10287 0.0030119 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2245e-07 0.052215 0.00031203 5.0704e-06 INSTANT 0.875122000E-01 TIME STEP NUMBER 55320 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283216778E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.688079730E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12024E-01 0.21290E+01 Friction velocity uk : 0.12024E-01 0.21290E+01 Dimensionless distance yplus : 0.11922E-01 0.20905E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 9.118765558e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29466E+08 1 0.20141E-09 0.26790E+02 0.20369E+04 c Velocity[X] 0.13421E+02 c Velocity[Y] 0.13370E+02 c Velocity[Z] 0.41945E-05 c Pressure 0.23655E-03 438 0.77521E-04 0.41964E-02 0.56013E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -13.359 22.883 5.6131 8.0072 v Velocity[Y] -14.648 16.335 -0.14314 -0.00067403 v Velocity[Z] -3.0632 2.9802 3.2745e-06 -5.3859e-08 v ǁVelocityǁ 0.0016125 23.973 6.6216 8.0219 v Pressure -1.2156e+05 1.8675e+05 34268 18864 v TurbVisc 7.4515e-21 0.0049696 0.00011509 6.9874e-06 v CourantNb 2.9692e-08 0.011768 0.00016661 4.8916e-06 v FourierNb 1.2425e-07 0.046976 0.00014543 1.7895e-07 v total_pressure -20236 2.8808e+05 1.3559e+05 1.2019e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0905 0.10283 0.0030113 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2245e-07 0.052221 0.00031203 5.0706e-06 INSTANT 0.875123000E-01 TIME STEP NUMBER 55321 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283219666E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.688587370E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.69073E-02 0.21295E+01 Friction velocity uk : 0.69073E-02 0.21295E+01 Dimensionless distance yplus : 0.68481E-02 0.20910E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 9.789169092e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29467E+08 1 0.20132E-09 0.26774E+02 0.20362E+04 c Velocity[X] 0.13409E+02 c Velocity[Y] 0.13365E+02 c Velocity[Z] 0.42071E-05 c Pressure 0.23847E-03 65 0.83991E-04 0.42241E-02 0.57912E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -13.382 22.909 5.6132 8.0073 v Velocity[Y] -14.674 16.362 -0.14315 -0.00067501 v Velocity[Z] -3.0632 2.9802 3.2735e-06 -5.3859e-08 v ǁVelocityǁ 0.0017121 23.999 6.6231 8.022 v Pressure -1.239e+05 1.8455e+05 32433 17765 v TurbVisc 8.5679e-21 0.0049696 0.00011523 7.0044e-06 v CourantNb 2.8922e-08 0.011768 0.00016661 4.8917e-06 v FourierNb 1.2425e-07 0.04698 0.00014543 1.7907e-07 v total_pressure -22575 2.8588e+05 1.3376e+05 1.1909e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.091 0.10279 0.0030108 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2246e-07 0.052226 0.00031204 5.0708e-06 INSTANT 0.875124000E-01 TIME STEP NUMBER 55322 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283222396E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.689120071E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.96855E-02 0.21299E+01 Friction velocity uk : 0.96855E-02 0.21299E+01 Dimensionless distance yplus : 0.97262E-02 0.20914E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.035711157e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29467E+08 1 0.20123E-09 0.26757E+02 0.20356E+04 c Velocity[X] 0.13398E+02 c Velocity[Y] 0.13359E+02 c Velocity[Z] 0.42284E-05 c Pressure 0.23957E-03 219 0.96398E-04 0.42374E-02 0.53344E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -13.406 22.936 5.6133 8.0073 v Velocity[Y] -14.701 16.389 -0.14316 -0.00067428 v Velocity[Z] -3.0631 2.9802 3.2724e-06 -5.3859e-08 v ǁVelocityǁ 0.0018179 24.025 6.6245 8.0221 v Pressure -1.2623e+05 1.8232e+05 30576 16821 v TurbVisc 9.2756e-21 0.0049696 0.00011537 7.0213e-06 v CourantNb 2.9475e-08 0.011768 0.00016661 4.8918e-06 v FourierNb 1.2425e-07 0.046983 0.00014543 1.7919e-07 v total_pressure -24901 2.8365e+05 1.319e+05 1.1815e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0914 0.10279 0.0030107 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2246e-07 0.052231 0.00031204 5.071e-06 INSTANT 0.875125000E-01 TIME STEP NUMBER 55323 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283224858E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.689627384E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15214E-01 0.21302E+01 Friction velocity uk : 0.15214E-01 0.21302E+01 Dimensionless distance yplus : 0.14916E-01 0.20917E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.088885173e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29467E+08 1 0.20114E-09 0.26738E+02 0.20348E+04 c Velocity[X] 0.13386E+02 c Velocity[Y] 0.13352E+02 c Velocity[Z] 0.42478E-05 c Pressure 0.24049E-03 143 0.82165E-04 0.42475E-02 0.65406E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -13.429 22.962 5.6134 8.0074 v Velocity[Y] -14.727 16.415 -0.14317 -0.00067449 v Velocity[Z] -3.0631 2.9802 3.2714e-06 -5.3859e-08 v ǁVelocityǁ 0.00193 24.051 6.626 8.0222 v Pressure -1.2853e+05 1.8006e+05 28672 15692 v TurbVisc 9.8511e-21 0.0049696 0.0001155 7.0384e-06 v CourantNb 3.1853e-08 0.011768 0.00016662 4.8919e-06 v FourierNb 1.2425e-07 0.046986 0.00014543 1.7931e-07 v total_pressure -27201 2.8139e+05 1.3e+05 1.1702e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0917 0.10279 0.0030106 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2246e-07 0.052234 0.00031205 5.0712e-06 INSTANT 0.875126000E-01 TIME STEP NUMBER 55324 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283227228E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.690124726E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13424E-01 0.21304E+01 Friction velocity uk : 0.13424E-01 0.21304E+01 Dimensionless distance yplus : 0.13161E-01 0.20919E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.131827141e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29467E+08 1 0.20105E-09 0.26722E+02 0.20342E+04 c Velocity[X] 0.13376E+02 c Velocity[Y] 0.13347E+02 c Velocity[Z] 0.42683E-05 c Pressure 0.24074E-03 11 0.69069E-04 0.42457E-02 0.58337E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -13.452 22.988 5.6135 8.0074 v Velocity[Y] -14.754 16.442 -0.14319 -0.00067513 v Velocity[Z] -3.0631 2.9802 3.2704e-06 -5.3859e-08 v ǁVelocityǁ 0.0020312 24.076 6.6275 8.0223 v Pressure -1.3079e+05 1.7779e+05 26827 14715 v TurbVisc 1.0871e-20 0.0049696 0.00011564 7.0553e-06 v CourantNb 3.5936e-08 0.011768 0.00016662 4.8919e-06 v FourierNb 1.2425e-07 0.046988 0.00014543 1.7944e-07 v total_pressure -29463 2.7912e+05 1.2815e+05 1.1604e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0919 0.10278 0.0030106 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2247e-07 0.052236 0.00031205 5.0714e-06 INSTANT 0.875127000E-01 TIME STEP NUMBER 55325 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283229354E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.690611108E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.49610E-02 0.21305E+01 Friction velocity uk : 0.49610E-02 0.21305E+01 Dimensionless distance yplus : 0.48957E-02 0.20920E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.151711402e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29468E+08 1 0.20097E-09 0.26706E+02 0.20335E+04 c Velocity[X] 0.13364E+02 c Velocity[Y] 0.13341E+02 c Velocity[Z] 0.42897E-05 c Pressure 0.24113E-03 194 0.78692E-04 0.42464E-02 0.76067E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -13.475 23.014 5.6136 8.0075 v Velocity[Y] -14.78 16.468 -0.1432 -0.00067472 v Velocity[Z] -3.063 2.9802 3.2694e-06 -5.3859e-08 v ǁVelocityǁ 0.0021537 24.101 6.6289 8.0224 v Pressure -1.33e+05 1.7552e+05 24828 13594 v TurbVisc 1.0509e-20 0.0049697 0.00011577 7.0721e-06 v CourantNb 4.0635e-08 0.011768 0.00016663 4.892e-06 v FourierNb 1.2425e-07 0.046989 0.00014543 1.7955e-07 v total_pressure -31670 2.7684e+05 1.2615e+05 1.1492e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.092 0.10276 0.0030106 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2247e-07 0.052238 0.00031205 5.0716e-06 INSTANT 0.875128000E-01 TIME STEP NUMBER 55326 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283231429E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.691074711E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.62110E-02 0.21305E+01 Friction velocity uk : 0.62110E-02 0.21305E+01 Dimensionless distance yplus : 0.59999E-02 0.20920E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.187805084e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29468E+08 1 0.20087E-09 0.26689E+02 0.20328E+04 c Velocity[X] 0.13353E+02 c Velocity[Y] 0.13336E+02 c Velocity[Z] 0.43014E-05 c Pressure 0.24199E-03 53 0.84895E-04 0.42554E-02 0.81004E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -13.499 23.04 5.6137 8.0075 v Velocity[Y] -14.806 16.494 -0.14321 -0.00067557 v Velocity[Z] -3.063 2.9802 3.2683e-06 -5.3859e-08 v ǁVelocityǁ 0.0022626 24.126 6.6304 8.0225 v Pressure -1.3515e+05 1.7325e+05 22907 12429 v TurbVisc 1.0485e-20 0.0049697 0.00011591 7.089e-06 v CourantNb 4.7917e-08 0.011768 0.00016663 4.8921e-06 v FourierNb 1.2425e-07 0.04699 0.00014543 1.7968e-07 v total_pressure -33822 2.7458e+05 1.2423e+05 1.1375e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.092 0.10277 0.0030108 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2247e-07 0.052238 0.00031206 5.0718e-06 INSTANT 0.875129000E-01 TIME STEP NUMBER 55327 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283233334E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.691553642E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15765E-01 0.21304E+01 Friction velocity uk : 0.15765E-01 0.21304E+01 Dimensionless distance yplus : 0.15562E-01 0.20919E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.188284170e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29468E+08 1 0.20078E-09 0.26672E+02 0.20321E+04 c Velocity[X] 0.13342E+02 c Velocity[Y] 0.13329E+02 c Velocity[Z] 0.43168E-05 c Pressure 0.24233E-03 211 0.97716E-04 0.42552E-02 0.74192E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -13.522 23.067 5.6137 8.0076 v Velocity[Y] -14.832 16.519 -0.14322 -0.0006748 v Velocity[Z] -3.0629 2.9802 3.2673e-06 -5.3859e-08 v ǁVelocityǁ 0.0023647 24.15 6.6318 8.0227 v Pressure -1.3724e+05 1.7099e+05 20991 11447 v TurbVisc 1.0519e-20 0.0049697 0.00011604 7.1059e-06 v CourantNb 5.5598e-08 0.011768 0.00016664 4.8922e-06 v FourierNb 1.2425e-07 0.04699 0.00014543 1.798e-07 v total_pressure -35915 2.7231e+05 1.2232e+05 1.1277e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0919 0.10276 0.003011 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2248e-07 0.052238 0.00031206 5.072e-06 INSTANT 0.875130000E-01 TIME STEP NUMBER 55328 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283234961E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.692007686E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11545E-01 0.21303E+01 Friction velocity uk : 0.11545E-01 0.21303E+01 Dimensionless distance yplus : 0.11335E-01 0.20917E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.179059144e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29468E+08 1 0.20069E-09 0.26652E+02 0.20313E+04 c Velocity[X] 0.13331E+02 c Velocity[Y] 0.13321E+02 c Velocity[Z] 0.43275E-05 c Pressure 0.24263E-03 555 0.83271E-04 0.42544E-02 0.92667E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -13.545 23.093 5.6138 8.0076 v Velocity[Y] -14.859 16.544 -0.14322 -0.00067483 v Velocity[Z] -3.0629 2.9802 3.2663e-06 -5.3859e-08 v ǁVelocityǁ 0.002462 24.175 6.6333 8.0228 v Pressure -1.3927e+05 1.6874e+05 19031 10270 v TurbVisc 9.0332e-21 0.0049697 0.00011618 7.1228e-06 v CourantNb 4.3841e-08 0.011768 0.00016664 4.8922e-06 v FourierNb 1.2425e-07 0.046989 0.00014543 1.7992e-07 v total_pressure -37946 2.7006e+05 1.2036e+05 1.116e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0917 0.10275 0.0030112 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2248e-07 0.052237 0.00031207 5.0722e-06 INSTANT 0.875131000E-01 TIME STEP NUMBER 55329 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283236493E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.692447555E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.37314E-02 0.21300E+01 Friction velocity uk : 0.37314E-02 0.21300E+01 Dimensionless distance yplus : 0.37043E-02 0.20915E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.149673829e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29468E+08 1 0.20060E-09 0.26636E+02 0.20307E+04 c Velocity[X] 0.13321E+02 c Velocity[Y] 0.13315E+02 c Velocity[Z] 0.43334E-05 c Pressure 0.24240E-03 11 0.71060E-04 0.42443E-02 0.83354E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -13.568 23.12 5.6138 8.0076 v Velocity[Y] -14.885 16.569 -0.14323 -0.0006756 v Velocity[Z] -3.0629 2.9802 3.2652e-06 -5.3859e-08 v ǁVelocityǁ 0.002537 24.198 6.6347 8.0228 v Pressure -1.4124e+05 1.6651e+05 17104 9256 v TurbVisc 7.8396e-21 0.0049697 0.00011631 7.1396e-06 v CourantNb 7.2921e-08 0.011768 0.00016665 4.8923e-06 v FourierNb 1.2425e-07 0.046988 0.00014543 1.8004e-07 v total_pressure -39911 2.6783e+05 1.1843e+05 1.1058e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0915 0.10273 0.0030113 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2248e-07 0.052236 0.00031207 5.0724e-06 INSTANT 0.875132000E-01 TIME STEP NUMBER 55330 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283237773E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.692873169E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.59977E-02 0.21298E+01 Friction velocity uk : 0.59977E-02 0.21298E+01 Dimensionless distance yplus : 0.59463E-02 0.20913E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.084428029e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29468E+08 1 0.20051E-09 0.26617E+02 0.20299E+04 c Velocity[X] 0.13310E+02 c Velocity[Y] 0.13308E+02 c Velocity[Z] 0.43370E-05 c Pressure 0.24269E-03 218 0.79659E-04 0.42434E-02 0.10997E+07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -13.591 23.146 5.6139 8.0076 v Velocity[Y] -14.911 16.594 -0.14324 -0.00067511 v Velocity[Z] -3.0628 2.9802 3.2642e-06 -5.3859e-08 v ǁVelocityǁ 0.0026313 24.222 6.6362 8.0229 v Pressure -1.4313e+05 1.643e+05 15124 8093.6 v TurbVisc 7.6456e-21 0.0049697 0.00011644 7.1564e-06 v CourantNb 8.1039e-08 0.011768 0.00016665 4.8924e-06 v FourierNb 1.2425e-07 0.046987 0.00014543 1.8015e-07 v total_pressure -41802 2.6562e+05 1.1645e+05 1.0942e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0913 0.10273 0.0030115 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2249e-07 0.052234 0.00031208 5.0725e-06 INSTANT 0.875133000E-01 TIME STEP NUMBER 55331 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283238998E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.693281078E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.26871E-02 0.21294E+01 Friction velocity uk : 0.26871E-02 0.21294E+01 Dimensionless distance yplus : 0.26641E-02 0.20909E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.038215870e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29468E+08 1 0.20041E-09 0.26599E+02 0.20292E+04 c Velocity[X] 0.13299E+02 c Velocity[Y] 0.13301E+02 c Velocity[Z] 0.43283E-05 c Pressure 0.24303E-03 153 0.86082E-04 0.42434E-02 0.11874E+07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -13.614 23.173 5.6139 8.0077 v Velocity[Y] -14.937 16.618 -0.14324 -0.00067596 v Velocity[Z] -3.0628 2.9803 3.2632e-06 -5.3859e-08 v ǁVelocityǁ 0.002419 24.246 6.6376 8.023 v Pressure -1.4495e+05 1.6213e+05 13137 6882.7 v TurbVisc 5.9367e-21 0.0049698 0.00011657 7.1732e-06 v CourantNb 7.7564e-08 0.011769 0.00016665 4.8924e-06 v FourierNb 1.2425e-07 0.046985 0.00014543 1.8027e-07 v total_pressure -43626 2.6345e+05 1.1446e+05 1.0821e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0909 0.10273 0.0030116 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2249e-07 0.052232 0.00031208 5.0727e-06 INSTANT 0.875134000E-01 TIME STEP NUMBER 55332 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283240045E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.693685335E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.14205E-01 0.21291E+01 Friction velocity uk : 0.14205E-01 0.21291E+01 Dimensionless distance yplus : 0.14154E-01 0.20906E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 9.470862823e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29468E+08 1 0.20032E-09 0.26581E+02 0.20285E+04 c Velocity[X] 0.13288E+02 c Velocity[Y] 0.13293E+02 c Velocity[Z] 0.43165E-05 c Pressure 0.24330E-03 142 0.98965E-04 0.42422E-02 0.10682E+07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -13.636 23.199 5.6139 8.0077 v Velocity[Y] -14.962 16.643 -0.14325 -0.00067513 v Velocity[Z] -3.0628 2.9803 3.2622e-06 -5.3859e-08 v ǁVelocityǁ 0.00215 24.269 6.6391 8.0231 v Pressure -1.4671e+05 1.5999e+05 11201 5882.5 v TurbVisc 5.219e-21 0.0049698 0.0001167 7.19e-06 v CourantNb 6.3721e-08 0.011769 0.00016666 4.8925e-06 v FourierNb 1.2425e-07 0.046983 0.00014543 1.8039e-07 v total_pressure -45388 2.6131e+05 1.1253e+05 1.0721e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0906 0.10273 0.0030117 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2249e-07 0.052229 0.00031209 5.0729e-06 INSTANT 0.875135000E-01 TIME STEP NUMBER 55333 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283240811E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.694074345E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.40206E-02 0.21287E+01 Friction velocity uk : 0.40206E-02 0.21287E+01 Dimensionless distance yplus : 0.39280E-02 0.20902E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 8.408351089e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29468E+08 1 0.20023E-09 0.26559E+02 0.20276E+04 c Velocity[X] 0.13277E+02 c Velocity[Y] 0.13282E+02 c Velocity[Z] 0.42991E-05 c Pressure 0.24348E-03 590 0.84291E-04 0.42393E-02 0.13556E+07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -13.659 23.226 5.6139 8.0077 v Velocity[Y] -14.988 16.667 -0.14325 -0.0006751 v Velocity[Z] -3.0627 2.9803 3.2611e-06 -5.3859e-08 v ǁVelocityǁ 0.0019436 24.292 6.6405 8.0232 v Pressure -1.4842e+05 1.5787e+05 9208.3 4665.8 v TurbVisc 4.6542e-21 0.0049698 0.00011683 7.2068e-06 v CourantNb 7.891e-08 0.011769 0.00016666 4.8926e-06 v FourierNb 1.2425e-07 0.046981 0.00014543 1.8051e-07 v total_pressure -47095 2.592e+05 1.1053e+05 1.0599e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0902 0.10272 0.0030117 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2249e-07 0.052227 0.00031209 5.0731e-06 INSTANT 0.875136000E-01 TIME STEP NUMBER 55334 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283241480E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.694445831E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.77555E-02 0.21283E+01 Friction velocity uk : 0.77555E-02 0.21283E+01 Dimensionless distance yplus : 0.75608E-02 0.20898E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 7.211437235e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29469E+08 1 0.20014E-09 0.26542E+02 0.20269E+04 c Velocity[X] 0.13267E+02 c Velocity[Y] 0.13275E+02 c Velocity[Z] 0.42757E-05 c Pressure 0.24313E-03 11 0.72893E-04 0.42273E-02 0.11982E+07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -13.681 23.253 5.6139 8.0077 v Velocity[Y] -15.013 16.69 -0.14325 -0.00067585 v Velocity[Z] -3.0627 2.9803 3.2601e-06 -5.3859e-08 v ǁVelocityǁ 0.0018194 24.315 6.6419 8.0233 v Pressure -1.5008e+05 1.5581e+05 7230.5 3625.7 v TurbVisc 4.3239e-21 0.0049698 0.00011696 7.2236e-06 v CourantNb 4.8586e-08 0.011769 0.00016666 4.8926e-06 v FourierNb 1.2425e-07 0.046978 0.00014543 1.8063e-07 v total_pressure -48751 2.5714e+05 1.0856e+05 1.0495e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0898 0.10274 0.0030119 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2249e-07 0.052224 0.0003121 5.0733e-06 INSTANT 0.875137000E-01 TIME STEP NUMBER 55335 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283241888E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.694804101E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.68572E-02 0.21280E+01 Friction velocity uk : 0.68572E-02 0.21280E+01 Dimensionless distance yplus : 0.67554E-02 0.20895E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 5.632991677e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29469E+08 1 0.20005E-09 0.26522E+02 0.20261E+04 c Velocity[X] 0.13256E+02 c Velocity[Y] 0.13265E+02 c Velocity[Z] 0.42493E-05 c Pressure 0.24348E-03 440 0.80757E-04 0.42276E-02 0.15455E+07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -13.703 23.279 5.6139 8.0077 v Velocity[Y] -15.038 16.714 -0.14325 -0.00067517 v Velocity[Z] -3.0626 2.9803 3.2591e-06 -5.3859e-08 v ǁVelocityǁ 0.0017711 24.338 6.6433 8.0234 v Pressure -1.5189e+05 1.539e+05 5300.8 2430.8 v TurbVisc 5.1698e-21 0.0049698 0.00011709 7.2402e-06 v CourantNb 2.1723e-08 0.011769 0.00016667 4.8927e-06 v FourierNb 1.2425e-07 0.046977 0.00014543 1.8075e-07 v total_pressure -50567 2.5522e+05 1.0663e+05 1.0376e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0895 0.10275 0.003012 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2249e-07 0.052222 0.0003121 5.0734e-06 INSTANT 0.875138000E-01 TIME STEP NUMBER 55336 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283242241E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.695152926E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.58367E-02 0.21276E+01 Friction velocity uk : 0.58367E-02 0.21276E+01 Dimensionless distance yplus : 0.58560E-02 0.20891E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 4.341667331e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29469E+08 1 0.19995E-09 0.26502E+02 0.20254E+04 c Velocity[X] 0.13246E+02 c Velocity[Y] 0.13257E+02 c Velocity[Z] 0.42117E-05 c Pressure 0.24330E-03 181 0.87200E-04 0.42186E-02 0.15596E+07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -13.726 23.306 5.6139 8.0077 v Velocity[Y] -15.063 16.738 -0.14325 -0.0006761 v Velocity[Z] -3.0626 2.9803 3.2581e-06 -5.3859e-08 v ǁVelocityǁ 0.0017815 24.361 6.6447 8.0234 v Pressure -1.5393e+05 1.5202e+05 3277.9 1213.8 v TurbVisc 3.615e-21 0.0049699 0.00011722 7.257e-06 v CourantNb 4.4158e-08 0.011769 0.00016667 4.8927e-06 v FourierNb 1.2425e-07 0.046974 0.00014544 1.8087e-07 v total_pressure -52606 2.5334e+05 1.046e+05 1.0254e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0891 0.10278 0.0030121 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2249e-07 0.052219 0.00031211 5.0736e-06 INSTANT 0.875139000E-01 TIME STEP NUMBER 55337 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283242416E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.695482408E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15127E-01 0.21273E+01 Friction velocity uk : 0.15127E-01 0.21273E+01 Dimensionless distance yplus : 0.14720E-01 0.20888E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 2.659827467e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29469E+08 1 0.19986E-09 0.26480E+02 0.20245E+04 c Velocity[X] 0.13236E+02 c Velocity[Y] 0.13245E+02 c Velocity[Z] 0.41691E-05 c Pressure 0.24334E-03 171 0.74927E-04 0.42135E-02 0.13474E+07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -13.748 23.332 5.6139 8.0077 v Velocity[Y] -15.088 16.761 -0.14325 -0.00067591 v Velocity[Z] -3.0625 2.9803 3.257e-06 -5.3859e-08 v ǁVelocityǁ 0.0018239 24.384 6.6462 8.0235 v Pressure -1.5594e+05 1.5026e+05 1333.6 172.3 v TurbVisc 3.4571e-21 0.0049699 0.00011735 7.2736e-06 v CourantNb 6.1454e-08 0.011769 0.00016667 4.8928e-06 v FourierNb 1.2425e-07 0.046973 0.00014544 1.8099e-07 v total_pressure -54616 2.5159e+05 1.0266e+05 1.015e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0888 0.1028 0.003012 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2249e-07 0.052217 0.00031211 5.0738e-06 INSTANT 0.875140000E-01 TIME STEP NUMBER 55338 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283242368E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.695810025E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12691E-01 0.21270E+01 Friction velocity uk : 0.12691E-01 0.21270E+01 Dimensionless distance yplus : 0.12349E-01 0.20885E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 9.330051052e-03 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29469E+08 1 0.19977E-09 0.26463E+02 0.20238E+04 c Velocity[X] 0.13227E+02 c Velocity[Y] 0.13237E+02 c Velocity[Z] 0.41236E-05 c Pressure 0.24266E-03 11 0.70146E-04 0.41960E-02 0.13335E+07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -13.77 23.358 5.6139 8.0077 v Velocity[Y] -15.113 16.785 -0.14325 -0.00067526 v Velocity[Z] -3.0625 2.9803 3.256e-06 -5.3859e-08 v ǁVelocityǁ 0.0018661 24.407 6.6476 8.0236 v Pressure -1.5793e+05 1.4872e+05 -668.73 -907.61 v TurbVisc 3.4666e-21 0.0049699 0.00011747 7.2903e-06 v CourantNb 6.6171e-08 0.011769 0.00016667 4.8929e-06 v FourierNb 1.2425e-07 0.046971 0.00014544 1.8111e-07 v total_pressure -56604 2.5004e+05 1.0066e+05 1.0042e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0885 0.1028 0.0030116 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2249e-07 0.052215 0.00031211 5.074e-06 INSTANT 0.875141000E-01 TIME STEP NUMBER 55339 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283241987E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.696121202E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13659E-01 0.21267E+01 Friction velocity uk : 0.13659E-01 0.21267E+01 Dimensionless distance yplus : 0.13291E-01 0.20883E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.049143412e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29469E+08 1 0.19968E-09 0.26442E+02 0.20230E+04 c Velocity[X] 0.13216E+02 c Velocity[Y] 0.13225E+02 c Velocity[Z] 0.40770E-05 c Pressure 0.24264E-03 38 0.96083E-04 0.41899E-02 0.15193E+07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -13.791 23.384 5.6138 8.0077 v Velocity[Y] -15.137 16.808 -0.14325 -0.0006751 v Velocity[Z] -3.0625 2.9803 3.255e-06 -5.3859e-08 v ǁVelocityǁ 0.001896 24.431 6.6489 8.0236 v Pressure -1.599e+05 1.4718e+05 -2564.3 -2112.3 v TurbVisc 3.8516e-21 0.0049699 0.0001176 7.307e-06 v CourantNb 5.4479e-08 0.011769 0.00016668 4.8929e-06 v FourierNb 1.2425e-07 0.04697 0.00014544 1.8123e-07 v total_pressure -58574 2.4851e+05 98761 99213 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0883 0.10279 0.003011 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2249e-07 0.052214 0.00031212 5.0741e-06 INSTANT 0.875142000E-01 TIME STEP NUMBER 55340 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283241624E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.696428272E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.16360E-01 0.21265E+01 Friction velocity uk : 0.16360E-01 0.21265E+01 Dimensionless distance yplus : 0.16035E-01 0.20880E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -2.634064677e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29469E+08 1 0.19959E-09 0.26422E+02 0.20222E+04 c Velocity[X] 0.13207E+02 c Velocity[Y] 0.13215E+02 c Velocity[Z] 0.40241E-05 c Pressure 0.24170E-03 24 0.80960E-04 0.41681E-02 0.14212E+07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -13.813 23.41 5.6138 8.0077 v Velocity[Y] -15.162 16.832 -0.14324 -0.00067517 v Velocity[Z] -3.0624 2.9803 3.254e-06 -5.3859e-08 v ǁVelocityǁ 0.0019025 24.454 6.6503 8.0237 v Pressure -1.6186e+05 1.4565e+05 -4596.2 -3336.3 v TurbVisc 6.1639e-21 0.0049699 0.00011773 7.3237e-06 v CourantNb 3.4352e-08 0.01177 0.00016668 4.8929e-06 v FourierNb 1.2425e-07 0.046969 0.00014544 1.8134e-07 v total_pressure -60539 2.4697e+05 96729 97989 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.088 0.10277 0.0030101 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2249e-07 0.052213 0.00031212 5.0743e-06 INSTANT 0.875143000E-01 TIME STEP NUMBER 55341 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283241055E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.696707472E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.64308E-02 0.21263E+01 Friction velocity uk : 0.64308E-02 0.21263E+01 Dimensionless distance yplus : 0.64139E-02 0.20879E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -4.453088649e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29468E+08 1 0.19949E-09 0.26406E+02 0.20215E+04 c Velocity[X] 0.13199E+02 c Velocity[Y] 0.13206E+02 c Velocity[Z] 0.39654E-05 c Pressure 0.24109E-03 11 0.68199E-04 0.41519E-02 0.12059E+07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -13.835 23.436 5.6138 8.0077 v Velocity[Y] -15.186 16.855 -0.14324 -0.00067572 v Velocity[Z] -3.0624 2.9803 3.2529e-06 -5.3859e-08 v ǁVelocityǁ 0.0018742 24.477 6.6517 8.0237 v Pressure -1.6383e+05 1.4411e+05 -6593.9 -4442.3 v TurbVisc 6.2256e-21 0.0049699 0.00011785 7.3403e-06 v CourantNb 2.2904e-08 0.01177 0.00016668 4.893e-06 v FourierNb 1.2425e-07 0.046969 0.00014545 1.8146e-07 v total_pressure -62506 2.4543e+05 94731 96883 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0879 0.10273 0.0030089 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2249e-07 0.052212 0.00031212 5.0745e-06 INSTANT 0.875144000E-01 TIME STEP NUMBER 55342 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283240275E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.696995565E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.33711E-02 0.21262E+01 Friction velocity uk : 0.33711E-02 0.21262E+01 Dimensionless distance yplus : 0.32865E-02 0.20878E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -6.387907702e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29468E+08 1 0.19940E-09 0.26386E+02 0.20207E+04 c Velocity[X] 0.13191E+02 c Velocity[Y] 0.13195E+02 c Velocity[Z] 0.39154E-05 c Pressure 0.24080E-03 192 0.74325E-04 0.41414E-02 0.12334E+07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -13.856 23.462 5.6137 8.0077 v Velocity[Y] -15.21 16.879 -0.14323 -0.00067515 v Velocity[Z] -3.0623 2.9803 3.2519e-06 -5.3859e-08 v ǁVelocityǁ 0.0018303 24.501 6.6531 8.0238 v Pressure -1.658e+05 1.4256e+05 -8463.6 -5575.4 v TurbVisc 4.8749e-21 0.00497 0.00011798 7.3569e-06 v CourantNb 7.4415e-08 0.01177 0.00016668 4.893e-06 v FourierNb 1.2425e-07 0.046969 0.00014545 1.8158e-07 v total_pressure -64475 2.4388e+05 92861 95750 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0878 0.10268 0.0030075 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2249e-07 0.052212 0.00031213 5.0746e-06 INSTANT 0.875145000E-01 TIME STEP NUMBER 55343 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283239407E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.697280306E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.39046E-02 0.21261E+01 Friction velocity uk : 0.39046E-02 0.21261E+01 Dimensionless distance yplus : 0.38345E-02 0.20877E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -7.904529397e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29468E+08 1 0.19931E-09 0.26368E+02 0.20200E+04 c Velocity[X] 0.13183E+02 c Velocity[Y] 0.13185E+02 c Velocity[Z] 0.38590E-05 c Pressure 0.23967E-03 47 0.79546E-04 0.41165E-02 0.11609E+07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -13.878 23.487 5.6136 8.0076 v Velocity[Y] -15.234 16.903 -0.14323 -0.0006758 v Velocity[Z] -3.0623 2.9803 3.2509e-06 -5.3859e-08 v ǁVelocityǁ 0.0017869 24.524 6.6545 8.0238 v Pressure -1.6778e+05 1.4098e+05 -10479 -6780.7 v TurbVisc 5.0184e-21 0.00497 0.0001181 7.3735e-06 v CourantNb 7.901e-08 0.01177 0.00016668 4.8931e-06 v FourierNb 1.2425e-07 0.046969 0.00014545 1.817e-07 v total_pressure -66457 2.4231e+05 90846 94544 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0877 0.10264 0.0030061 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2249e-07 0.052212 0.00031213 5.0748e-06 INSTANT 0.875146000E-01 TIME STEP NUMBER 55344 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283238354E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.697537932E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.42651E-02 0.21261E+01 Friction velocity uk : 0.42651E-02 0.21261E+01 Dimensionless distance yplus : 0.42167E-02 0.20876E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -9.540679540e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29468E+08 1 0.19921E-09 0.26349E+02 0.20193E+04 c Velocity[X] 0.13175E+02 c Velocity[Y] 0.13175E+02 c Velocity[Z] 0.38016E-05 c Pressure 0.23894E-03 206 0.91282E-04 0.40984E-02 0.92721E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -13.899 23.513 5.6136 8.0076 v Velocity[Y] -15.259 16.927 -0.14322 -0.0006749 v Velocity[Z] -3.0623 2.9804 3.2499e-06 -5.3859e-08 v ǁVelocityǁ 0.0017701 24.548 6.6558 8.0239 v Pressure -1.6978e+05 1.3937e+05 -12403 -7784.9 v TurbVisc 5.6098e-21 0.00497 0.00011823 7.39e-06 v CourantNb 6.5063e-08 0.01177 0.00016668 4.8931e-06 v FourierNb 1.2425e-07 0.046969 0.00014545 1.8182e-07 v total_pressure -68457 2.407e+05 88922 93540 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0876 0.10261 0.0030047 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2249e-07 0.052213 0.00031213 5.0749e-06 INSTANT 0.875147000E-01 TIME STEP NUMBER 55345 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283237007E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.697801777E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.72129E-02 0.21261E+01 Friction velocity uk : 0.72129E-02 0.21261E+01 Dimensionless distance yplus : 0.71755E-02 0.20876E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.103630924e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29468E+08 1 0.19912E-09 0.26329E+02 0.20185E+04 c Velocity[X] 0.13167E+02 c Velocity[Y] 0.13162E+02 c Velocity[Z] 0.37489E-05 c Pressure 0.23802E-03 286 0.77793E-04 0.40772E-02 0.10079E+07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -13.921 23.538 5.6135 8.0076 v Velocity[Y] -15.283 16.95 -0.14321 -0.00067492 v Velocity[Z] -3.0622 2.9804 3.2489e-06 -5.3859e-08 v ǁVelocityǁ 0.0018085 24.572 6.6572 8.0239 v Pressure -1.7181e+05 1.3773e+05 -14360 -8991.5 v TurbVisc 6.3645e-21 0.00497 0.00011835 7.4067e-06 v CourantNb 4.9426e-08 0.01177 0.00016668 4.8932e-06 v FourierNb 1.2425e-07 0.04697 0.00014546 1.8193e-07 v total_pressure -70481 2.3905e+05 86965 92333 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0876 0.1026 0.0030034 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2248e-07 0.052214 0.00031213 5.0751e-06 INSTANT 0.875148000E-01 TIME STEP NUMBER 55346 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283235560E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.698052602E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.69458E-02 0.21261E+01 Friction velocity uk : 0.69458E-02 0.21261E+01 Dimensionless distance yplus : 0.69097E-02 0.20877E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.233846954e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29468E+08 1 0.19902E-09 0.26312E+02 0.20178E+04 c Velocity[X] 0.13160E+02 c Velocity[Y] 0.13153E+02 c Velocity[Z] 0.36988E-05 c Pressure 0.23660E-03 11 0.67943E-04 0.40475E-02 0.77141E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -13.942 23.563 5.6134 8.0076 v Velocity[Y] -15.307 16.974 -0.14321 -0.00067531 v Velocity[Z] -3.0622 2.9804 3.2478e-06 -5.3859e-08 v ǁVelocityǁ 0.0019272 24.596 6.6585 8.0239 v Pressure -1.7385e+05 1.3604e+05 -16294 -9990.2 v TurbVisc 6.7442e-21 0.00497 0.00011847 7.4232e-06 v CourantNb 3.237e-08 0.01177 0.00016668 4.8932e-06 v FourierNb 1.2425e-07 0.046971 0.00014546 1.8205e-07 v total_pressure -72529 2.3736e+05 85031 91335 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0877 0.10257 0.0030019 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2248e-07 0.052215 0.00031213 5.0752e-06 INSTANT 0.875149000E-01 TIME STEP NUMBER 55347 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283233874E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.698295943E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.55367E-02 0.21262E+01 Friction velocity uk : 0.55367E-02 0.21262E+01 Dimensionless distance yplus : 0.54966E-02 0.20878E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.361477960e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29468E+08 1 0.19893E-09 0.26293E+02 0.20171E+04 c Velocity[X] 0.13153E+02 c Velocity[Y] 0.13141E+02 c Velocity[Z] 0.36533E-05 c Pressure 0.23582E-03 320 0.74305E-04 0.40288E-02 0.89440E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -13.963 23.588 5.6133 8.0075 v Velocity[Y] -15.331 16.998 -0.1432 -0.00067472 v Velocity[Z] -3.0621 2.9804 3.2468e-06 -5.3859e-08 v ǁVelocityǁ 0.0021322 24.62 6.6599 8.024 v Pressure -1.7592e+05 1.3431e+05 -18184 -11165 v TurbVisc 8.9849e-21 0.0049701 0.0001186 7.4397e-06 v CourantNb 1.7429e-08 0.01177 0.00016668 4.8932e-06 v FourierNb 1.2425e-07 0.046972 0.00014546 1.8217e-07 v total_pressure -74599 2.3563e+05 83141 90160 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0878 0.10253 0.0030002 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2248e-07 0.052217 0.00031214 5.0754e-06 INSTANT 0.875150000E-01 TIME STEP NUMBER 55348 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283232127E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.698535297E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.75395E-02 0.21263E+01 Friction velocity uk : 0.75395E-02 0.21263E+01 Dimensionless distance yplus : 0.75004E-02 0.20878E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.439658693e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29468E+08 1 0.19883E-09 0.26275E+02 0.20164E+04 c Velocity[X] 0.13146E+02 c Velocity[Y] 0.13129E+02 c Velocity[Z] 0.36074E-05 c Pressure 0.23468E-03 47 0.80229E-04 0.40040E-02 0.81199E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -13.984 23.612 5.6132 8.0075 v Velocity[Y] -15.354 17.023 -0.14319 -0.00067534 v Velocity[Z] -3.0621 2.9804 3.2458e-06 -5.3859e-08 v ǁVelocityǁ 0.0024069 24.644 6.6612 8.024 v Pressure -1.7802e+05 1.3252e+05 -20154 -12351 v TurbVisc 9.5705e-21 0.0049701 0.00011872 7.4562e-06 v CourantNb 2.8965e-08 0.01177 0.00016667 4.8933e-06 v FourierNb 1.2425e-07 0.046973 0.00014546 1.8229e-07 v total_pressure -76695 2.3385e+05 81171 88974 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0878 0.10252 0.0029985 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2248e-07 0.052218 0.00031214 5.0755e-06 INSTANT 0.875151000E-01 TIME STEP NUMBER 55349 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283230208E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.698762236E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.86195E-02 0.21264E+01 Friction velocity uk : 0.86195E-02 0.21264E+01 Dimensionless distance yplus : 0.85748E-02 0.20879E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.513914773e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29467E+08 1 0.19874E-09 0.26256E+02 0.20156E+04 c Velocity[X] 0.13138E+02 c Velocity[Y] 0.13118E+02 c Velocity[Z] 0.35654E-05 c Pressure 0.23377E-03 199 0.92074E-04 0.39834E-02 0.64837E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -14.006 23.637 5.6131 8.0074 v Velocity[Y] -15.378 17.047 -0.14318 -0.00067439 v Velocity[Z] -3.062 2.9804 3.2448e-06 -5.3859e-08 v ǁVelocityǁ 0.0023515 24.669 6.6626 8.024 v Pressure -1.8014e+05 1.3069e+05 -22040 -13327 v TurbVisc 1.0824e-20 0.0049701 0.00011884 7.4727e-06 v CourantNb 4.919e-08 0.01177 0.00016667 4.8933e-06 v FourierNb 1.2425e-07 0.046975 0.00014547 1.824e-07 v total_pressure -78817 2.3201e+05 79285 87998 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0879 0.10248 0.0029967 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2247e-07 0.05222 0.00031214 5.0757e-06 INSTANT 0.875152000E-01 TIME STEP NUMBER 55350 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283228010E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.698991108E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.70314E-02 0.21264E+01 Friction velocity uk : 0.70314E-02 0.21264E+01 Dimensionless distance yplus : 0.69949E-02 0.20880E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.566251859e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29467E+08 1 0.19864E-09 0.26234E+02 0.20148E+04 c Velocity[X] 0.13131E+02 c Velocity[Y] 0.13104E+02 c Velocity[Z] 0.35295E-05 c Pressure 0.23275E-03 204 0.78240E-04 0.39607E-02 0.70785E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -14.027 23.661 5.613 8.0074 v Velocity[Y] -15.402 17.071 -0.14317 -0.00067437 v Velocity[Z] -3.062 2.9804 3.2438e-06 -5.3859e-08 v ǁVelocityǁ 0.0022738 24.693 6.6639 8.0241 v Pressure -1.8229e+05 1.288e+05 -23954 -14496 v TurbVisc 1.3723e-20 0.0049701 0.00011896 7.4893e-06 v CourantNb 6.9588e-08 0.01177 0.00016667 4.8933e-06 v FourierNb 1.2425e-07 0.046976 0.00014547 1.8252e-07 v total_pressure -80966 2.3012e+05 77371 86829 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.088 0.10244 0.0029948 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2247e-07 0.052222 0.00031214 5.0758e-06 INSTANT 0.875153000E-01 TIME STEP NUMBER 55351 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283225714E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.699206922E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.76654E-02 0.21265E+01 Friction velocity uk : 0.76654E-02 0.21265E+01 Dimensionless distance yplus : 0.76256E-02 0.20880E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.594847041e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29467E+08 1 0.19854E-09 0.26216E+02 0.20141E+04 c Velocity[X] 0.13123E+02 c Velocity[Y] 0.13093E+02 c Velocity[Z] 0.34984E-05 c Pressure 0.23119E-03 11 0.66251E-04 0.39291E-02 0.54274E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -14.048 23.685 5.6129 8.0073 v Velocity[Y] -15.427 17.095 -0.14316 -0.00067474 v Velocity[Z] -3.0619 2.9804 3.2427e-06 -5.3859e-08 v ǁVelocityǁ 0.0021833 24.718 6.6653 8.0241 v Pressure -1.8446e+05 1.2686e+05 -25808 -15454 v TurbVisc 1.1793e-20 0.0049701 0.00011908 7.5057e-06 v CourantNb 6.9553e-08 0.01177 0.00016667 4.8934e-06 v FourierNb 1.2425e-07 0.046977 0.00014547 1.8264e-07 v total_pressure -83135 2.2818e+05 75517 85871 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.088 0.1024 0.0029928 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2247e-07 0.052223 0.00031214 5.076e-06 INSTANT 0.875154000E-01 TIME STEP NUMBER 55352 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283223188E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.699412917E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10415E-01 0.21266E+01 Friction velocity uk : 0.10415E-01 0.21266E+01 Dimensionless distance yplus : 0.10361E-01 0.20881E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.609722968e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29467E+08 1 0.19845E-09 0.26196E+02 0.20133E+04 c Velocity[X] 0.13117E+02 c Velocity[Y] 0.13080E+02 c Velocity[Z] 0.34737E-05 c Pressure 0.23005E-03 199 0.74568E-04 0.39046E-02 0.63687E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -14.07 23.709 5.6128 8.0073 v Velocity[Y] -15.451 17.119 -0.14315 -0.00067412 v Velocity[Z] -3.0619 2.9804 3.2417e-06 -5.3859e-08 v ǁVelocityǁ 0.0021176 24.742 6.6666 8.0241 v Pressure -1.8664e+05 1.2487e+05 -27698 -16575 v TurbVisc 1.0852e-20 0.0049701 0.0001192 7.522e-06 v CourantNb 4.9879e-08 0.01177 0.00016667 4.8934e-06 v FourierNb 1.2425e-07 0.046979 0.00014548 1.8275e-07 v total_pressure -85315 2.2619e+05 73627 84750 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0881 0.10235 0.0029909 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2246e-07 0.052225 0.00031215 5.0761e-06 INSTANT 0.875155000E-01 TIME STEP NUMBER 55353 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283220597E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.699604267E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.62296E-02 0.21266E+01 Friction velocity uk : 0.62296E-02 0.21266E+01 Dimensionless distance yplus : 0.60179E-02 0.20881E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.590536307e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29467E+08 1 0.19835E-09 0.26177E+02 0.20125E+04 c Velocity[X] 0.13109E+02 c Velocity[Y] 0.13067E+02 c Velocity[Z] 0.34480E-05 c Pressure 0.22895E-03 62 0.80541E-04 0.38811E-02 0.58914E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -14.091 23.733 5.6127 8.0072 v Velocity[Y] -15.475 17.143 -0.14314 -0.00067471 v Velocity[Z] -3.0619 2.9804 3.2407e-06 -5.3859e-08 v ǁVelocityǁ 0.0020392 24.767 6.6679 8.0241 v Pressure -1.8883e+05 1.2284e+05 -29586 -17711 v TurbVisc 1.0089e-20 0.0049702 0.00011932 7.5385e-06 v CourantNb 4.7521e-08 0.01177 0.00016667 4.8934e-06 v FourierNb 1.2425e-07 0.046979 0.00014548 1.8287e-07 v total_pressure -87504 2.2417e+05 71739 83614 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0881 0.10233 0.0029891 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2246e-07 0.052226 0.00031215 5.0763e-06 INSTANT 0.875156000E-01 TIME STEP NUMBER 55354 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283217847E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.699796210E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.76646E-02 0.21265E+01 Friction velocity uk : 0.76646E-02 0.21265E+01 Dimensionless distance yplus : 0.76248E-02 0.20881E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.552563805e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29466E+08 1 0.19824E-09 0.26156E+02 0.20117E+04 c Velocity[X] 0.13101E+02 c Velocity[Y] 0.13055E+02 c Velocity[Z] 0.34306E-05 c Pressure 0.22767E-03 206 0.92336E-04 0.38543E-02 0.47145E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -14.113 23.757 5.6126 8.0072 v Velocity[Y] -15.499 17.167 -0.14313 -0.00067374 v Velocity[Z] -3.0618 2.9804 3.2397e-06 -5.3859e-08 v ǁVelocityǁ 0.0019627 24.791 6.6693 8.0241 v Pressure -1.9102e+05 1.2077e+05 -31404 -18633 v TurbVisc 1.056e-20 0.0049702 0.00011943 7.5549e-06 v CourantNb 6.381e-08 0.011771 0.00016667 4.8934e-06 v FourierNb 1.2425e-07 0.04698 0.00014548 1.8298e-07 v total_pressure -89700 2.221e+05 69921 82692 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0881 0.10231 0.0029873 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2245e-07 0.052226 0.00031215 5.0764e-06 INSTANT 0.875157000E-01 TIME STEP NUMBER 55355 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283214826E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.699976832E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.58955E-02 0.21265E+01 Friction velocity uk : 0.58955E-02 0.21265E+01 Dimensionless distance yplus : 0.58649E-02 0.20880E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.498270115e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29466E+08 1 0.19814E-09 0.26133E+02 0.20108E+04 c Velocity[X] 0.13094E+02 c Velocity[Y] 0.13039E+02 c Velocity[Z] 0.34183E-05 c Pressure 0.22618E-03 292 0.78405E-04 0.38242E-02 0.52778E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -14.134 23.78 5.6125 8.0071 v Velocity[Y] -15.523 17.191 -0.14312 -0.0006737 v Velocity[Z] -3.0618 2.9804 3.2387e-06 -5.3859e-08 v ǁVelocityǁ 0.0018911 24.815 6.6706 8.0241 v Pressure -1.9322e+05 1.1867e+05 -33249 -19755 v TurbVisc 1.0361e-20 0.0049702 0.00011955 7.5713e-06 v CourantNb 8.0146e-08 0.011771 0.00016667 4.8935e-06 v FourierNb 1.2425e-07 0.04698 0.00014549 1.831e-07 v total_pressure -91893 2.1999e+05 68076 81570 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.088 0.10228 0.0029856 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2245e-07 0.052227 0.00031215 5.0766e-06 INSTANT 0.875158000E-01 TIME STEP NUMBER 55356 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283211715E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.700143156E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.32780E-02 0.21263E+01 Friction velocity uk : 0.32780E-02 0.21263E+01 Dimensionless distance yplus : 0.32610E-02 0.20879E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.428788087e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29466E+08 1 0.19804E-09 0.26114E+02 0.20101E+04 c Velocity[X] 0.13086E+02 c Velocity[Y] 0.13028E+02 c Velocity[Z] 0.34181E-05 c Pressure 0.22401E-03 10 0.64471E-04 0.37828E-02 0.39351E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -14.156 23.804 5.6124 8.007 v Velocity[Y] -15.547 17.214 -0.14311 -0.00067407 v Velocity[Z] -3.0617 2.9804 3.2376e-06 -5.3859e-08 v ǁVelocityǁ 0.0018148 24.839 6.672 8.0241 v Pressure -1.954e+05 1.1654e+05 -34995 -20639 v TurbVisc 9.3864e-21 0.0049702 0.00011967 7.5877e-06 v CourantNb 7.0898e-08 0.011771 0.00016667 4.8935e-06 v FourierNb 1.2425e-07 0.04698 0.00014549 1.8322e-07 v total_pressure -94074 2.1787e+05 66330 80686 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0879 0.10225 0.0029839 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2244e-07 0.052226 0.00031216 5.0767e-06 INSTANT 0.875159000E-01 TIME STEP NUMBER 55357 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283208389E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.700297194E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.61313E-02 0.21262E+01 Friction velocity uk : 0.61313E-02 0.21262E+01 Dimensionless distance yplus : 0.60995E-02 0.20877E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.343319199e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29465E+08 1 0.19794E-09 0.26093E+02 0.20093E+04 c Velocity[X] 0.13080E+02 c Velocity[Y] 0.13014E+02 c Velocity[Z] 0.34084E-05 c Pressure 0.22196E-03 418 0.74536E-04 0.37434E-02 0.48909E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -14.178 23.828 5.6123 8.007 v Velocity[Y] -15.572 17.238 -0.1431 -0.00067331 v Velocity[Z] -3.0617 2.9804 3.2366e-06 -5.3859e-08 v ǁVelocityǁ 0.0017572 24.863 6.6733 8.0241 v Pressure -1.9755e+05 1.144e+05 -36854 -21719 v TurbVisc 8.0807e-21 0.0049702 0.00011978 7.6039e-06 v CourantNb 6.3504e-08 0.011771 0.00016666 4.8935e-06 v FourierNb 1.2425e-07 0.04698 0.00014549 1.8333e-07 v total_pressure -96226 2.1573e+05 64471 79606 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0877 0.10223 0.0029824 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2244e-07 0.052226 0.00031216 5.0768e-06 INSTANT 0.875160000E-01 TIME STEP NUMBER 55358 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283204995E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.700426968E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.43339E-02 0.21259E+01 Friction velocity uk : 0.43339E-02 0.21259E+01 Dimensionless distance yplus : 0.42613E-02 0.20875E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.250078811e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29465E+08 1 0.19784E-09 0.26073E+02 0.20085E+04 c Velocity[X] 0.13072E+02 c Velocity[Y] 0.13000E+02 c Velocity[Z] 0.34000E-05 c Pressure 0.22028E-03 33 0.80601E-04 0.37104E-02 0.43967E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -14.199 23.852 5.6122 8.0069 v Velocity[Y] -15.596 17.261 -0.14309 -0.00067403 v Velocity[Z] -3.0616 2.9804 3.2356e-06 -5.3859e-08 v ǁVelocityǁ 0.0016988 24.887 6.6747 8.0241 v Pressure -1.9967e+05 1.1226e+05 -38615 -22768 v TurbVisc 9.452e-21 0.0049702 0.0001199 7.6203e-06 v CourantNb 5.3333e-08 0.011771 0.00016666 4.8935e-06 v FourierNb 1.2425e-07 0.046979 0.0001455 1.8345e-07 v total_pressure -98347 2.1359e+05 62710 78557 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0875 0.10221 0.002981 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2243e-07 0.052224 0.00031216 5.077e-06 INSTANT 0.875161000E-01 TIME STEP NUMBER 55359 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283201457E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.700570007E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.93629E-02 0.21256E+01 Friction velocity uk : 0.93629E-02 0.21256E+01 Dimensionless distance yplus : 0.92754E-02 0.20872E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.137671977e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29465E+08 1 0.19774E-09 0.26052E+02 0.20076E+04 c Velocity[X] 0.13065E+02 c Velocity[Y] 0.12988E+02 c Velocity[Z] 0.34027E-05 c Pressure 0.21794E-03 210 0.92363E-04 0.36665E-02 0.36498E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -14.221 23.875 5.6121 8.0068 v Velocity[Y] -15.62 17.284 -0.14308 -0.00067306 v Velocity[Z] -3.0616 2.9804 3.2346e-06 -5.3859e-08 v ǁVelocityǁ 0.0016434 24.91 6.6761 8.0241 v Pressure -2.0176e+05 1.1012e+05 -40341 -23642 v TurbVisc 9.1769e-21 0.0049703 0.00012001 7.6365e-06 v CourantNb 4.3738e-08 0.011771 0.00016666 4.8935e-06 v FourierNb 1.2425e-07 0.046977 0.0001455 1.8356e-07 v total_pressure -1.0043e+05 2.1144e+05 60984 77683 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0872 0.10219 0.0029797 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2243e-07 0.052222 0.00031216 5.0771e-06 INSTANT 0.875162000E-01 TIME STEP NUMBER 55360 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283197656E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.700688063E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13504E-01 0.21253E+01 Friction velocity uk : 0.13504E-01 0.21253E+01 Dimensionless distance yplus : 0.13208E-01 0.20868E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.018891759e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29464E+08 1 0.19763E-09 0.26029E+02 0.20067E+04 c Velocity[X] 0.13057E+02 c Velocity[Y] 0.12972E+02 c Velocity[Z] 0.34080E-05 c Pressure 0.21542E-03 269 0.78544E-04 0.36195E-02 0.40635E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -14.243 23.899 5.612 8.0068 v Velocity[Y] -15.645 17.306 -0.14308 -0.00067303 v Velocity[Z] -3.0615 2.9805 3.2336e-06 -5.386e-08 v ǁVelocityǁ 0.001596 24.933 6.6774 8.0241 v Pressure -2.0379e+05 1.0798e+05 -42078 -24692 v TurbVisc 8.9351e-21 0.0049703 0.00012012 7.6529e-06 v CourantNb 3.6148e-08 0.011771 0.00016667 4.8936e-06 v FourierNb 1.2425e-07 0.046975 0.0001455 1.8368e-07 v total_pressure -1.0247e+05 2.093e+05 59247 76633 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0868 0.10218 0.0029786 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2242e-07 0.05222 0.00031217 5.0772e-06 INSTANT 0.875163000E-01 TIME STEP NUMBER 55361 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283193776E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.700791892E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.14850E-01 0.21248E+01 Friction velocity uk : 0.14850E-01 0.21248E+01 Dimensionless distance yplus : 0.14354E-01 0.20864E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -9.024829620e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29464E+08 1 0.19753E-09 0.26010E+02 0.20060E+04 c Velocity[X] 0.13050E+02 c Velocity[Y] 0.12960E+02 c Velocity[Z] 0.34217E-05 c Pressure 0.21212E-03 10 0.62890E-04 0.35597E-02 0.30287E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -14.264 23.923 5.6119 8.0067 v Velocity[Y] -15.669 17.329 -0.14307 -0.00067342 v Velocity[Z] -3.0615 2.9804 3.2326e-06 -5.386e-08 v ǁVelocityǁ 0.0015484 24.956 6.6788 8.0241 v Pressure -2.0578e+05 1.0586e+05 -43706 -25513 v TurbVisc 8.0952e-21 0.0049703 0.00012024 7.6691e-06 v CourantNb 3.0477e-08 0.011771 0.00016667 4.8936e-06 v FourierNb 1.2425e-07 0.046973 0.0001455 1.8379e-07 v total_pressure -1.0445e+05 2.0719e+05 57619 75812 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0864 0.10218 0.0029776 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2241e-07 0.052217 0.00031217 5.0774e-06 INSTANT 0.875164000E-01 TIME STEP NUMBER 55362 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283189697E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.700881221E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15811E-01 0.21244E+01 Friction velocity uk : 0.15811E-01 0.21244E+01 Dimensionless distance yplus : 0.15622E-01 0.20860E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -7.768608377e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29464E+08 1 0.19743E-09 0.25989E+02 0.20052E+04 c Velocity[X] 0.13043E+02 c Velocity[Y] 0.12946E+02 c Velocity[Z] 0.34241E-05 c Pressure 0.20896E-03 296 0.74637E-04 0.35024E-02 0.37847E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -14.286 23.947 5.6118 8.0066 v Velocity[Y] -15.693 17.351 -0.14306 -0.00067279 v Velocity[Z] -3.0614 2.9805 3.2316e-06 -5.386e-08 v ǁVelocityǁ 0.0015166 24.979 6.6802 8.0241 v Pressure -2.077e+05 1.0378e+05 -45449 -26512 v TurbVisc 6.8568e-21 0.0049703 0.00012035 7.6853e-06 v CourantNb 2.6296e-08 0.011771 0.00016667 4.8936e-06 v FourierNb 1.2425e-07 0.046971 0.00014551 1.8391e-07 v total_pressure -1.0637e+05 2.0511e+05 55876 74813 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.086 0.10217 0.0029768 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2241e-07 0.052214 0.00031217 5.0775e-06 INSTANT 0.875165000E-01 TIME STEP NUMBER 55363 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283185548E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.700943374E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10596E-01 0.21238E+01 Friction velocity uk : 0.10596E-01 0.21238E+01 Dimensionless distance yplus : 0.10236E-01 0.20854E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -6.765129338e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29463E+08 1 0.19732E-09 0.25969E+02 0.20044E+04 c Velocity[X] 0.13036E+02 c Velocity[Y] 0.12933E+02 c Velocity[Z] 0.34246E-05 c Pressure 0.20624E-03 35 0.80432E-04 0.34525E-02 0.35045E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -14.308 23.97 5.6117 8.0065 v Velocity[Y] -15.717 17.373 -0.14305 -0.00067342 v Velocity[Z] -3.0614 2.9805 3.2305e-06 -5.386e-08 v ǁVelocityǁ 0.0014873 25.001 6.6815 8.0241 v Pressure -2.0955e+05 1.0175e+05 -47086 -27501 v TurbVisc 6.233e-21 0.0049703 0.00012046 7.7015e-06 v CourantNb 2.425e-08 0.011771 0.00016667 4.8936e-06 v FourierNb 1.2425e-07 0.046967 0.00014551 1.8402e-07 v total_pressure -1.0822e+05 2.0307e+05 54239 73824 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0854 0.10216 0.0029761 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.224e-07 0.05221 0.00031218 5.0776e-06 INSTANT 0.875166000E-01 TIME STEP NUMBER 55364 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283181272E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.701020413E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.33438E-02 0.21233E+01 Friction velocity uk : 0.33438E-02 0.21233E+01 Dimensionless distance yplus : 0.33372E-02 0.20849E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -5.504781435e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29463E+08 1 0.19721E-09 0.25948E+02 0.20036E+04 c Velocity[X] 0.13028E+02 c Velocity[Y] 0.12920E+02 c Velocity[Z] 0.34320E-05 c Pressure 0.20294E-03 222 0.92334E-04 0.33933E-02 0.28277E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -14.329 23.994 5.6116 8.0064 v Velocity[Y] -15.741 17.394 -0.14304 -0.00067249 v Velocity[Z] -3.0614 2.9805 3.2295e-06 -5.386e-08 v ǁVelocityǁ 0.0014614 25.023 6.6829 8.0241 v Pressure -2.1132e+05 99756 -48671 -28292 v TurbVisc 6.1903e-21 0.0049704 0.00012057 7.7177e-06 v CourantNb 2.3432e-08 0.011772 0.00016667 4.8936e-06 v FourierNb 1.2425e-07 0.046964 0.00014551 1.8414e-07 v total_pressure -1.1e+05 2.0108e+05 52654 73033 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0849 0.10215 0.0029755 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2239e-07 0.052206 0.00031218 5.0778e-06 INSTANT 0.875167000E-01 TIME STEP NUMBER 55365 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283176747E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.701070301E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.59495E-02 0.21227E+01 Friction velocity uk : 0.59495E-02 0.21227E+01 Dimensionless distance yplus : 0.57274E-02 0.20843E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -4.415012783e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29463E+08 1 0.19711E-09 0.25925E+02 0.20027E+04 c Velocity[X] 0.13021E+02 c Velocity[Y] 0.12904E+02 c Velocity[Z] 0.34389E-05 c Pressure 0.19956E-03 371 0.78500E-04 0.33327E-02 0.31869E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -14.351 24.018 5.6115 8.0063 v Velocity[Y] -15.765 17.416 -0.14304 -0.00067236 v Velocity[Z] -3.0613 2.9805 3.2285e-06 -5.386e-08 v ǁVelocityǁ 0.0014418 25.045 6.6843 8.024 v Pressure -2.1303e+05 97813 -50261 -29252 v TurbVisc 6.8524e-21 0.0049704 0.00012068 7.734e-06 v CourantNb 2.4205e-08 0.011772 0.00016667 4.8936e-06 v FourierNb 1.2425e-07 0.046961 0.00014551 1.8425e-07 v total_pressure -1.117e+05 1.9914e+05 51064 72073 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0843 0.10216 0.0029751 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2239e-07 0.052201 0.00031218 5.0779e-06 INSTANT 0.875168000E-01 TIME STEP NUMBER 55366 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283172159E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.701105925E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.94553E-02 0.21221E+01 Friction velocity uk : 0.94553E-02 0.21221E+01 Dimensionless distance yplus : 0.92969E-02 0.20837E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -3.461608450e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29462E+08 1 0.19700E-09 0.25905E+02 0.20019E+04 c Velocity[X] 0.13013E+02 c Velocity[Y] 0.12892E+02 c Velocity[Z] 0.34494E-05 c Pressure 0.19549E-03 10 0.61856E-04 0.32607E-02 0.25181E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -14.372 24.042 5.6115 8.0062 v Velocity[Y] -15.789 17.436 -0.14303 -0.00067294 v Velocity[Z] -3.0613 2.9805 3.2275e-06 -5.386e-08 v ǁVelocityǁ 0.0014233 25.067 6.6857 8.024 v Pressure -2.1466e+05 95932 -51771 -30046 v TurbVisc 7.5115e-21 0.0049704 0.00012079 7.7501e-06 v CourantNb 2.6154e-08 0.011772 0.00016667 4.8936e-06 v FourierNb 1.2425e-07 0.046957 0.00014552 1.8437e-07 v total_pressure -1.1333e+05 1.9726e+05 49554 71279 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0837 0.10218 0.002975 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2238e-07 0.052197 0.00031219 5.078e-06 INSTANT 0.875169000E-01 TIME STEP NUMBER 55367 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283167368E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.701127522E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10496E-01 0.21215E+01 Friction velocity uk : 0.10496E-01 0.21215E+01 Dimensionless distance yplus : 0.10388E-01 0.20831E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -2.520089436e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29462E+08 1 0.19690E-09 0.25884E+02 0.20011E+04 c Velocity[X] 0.13006E+02 c Velocity[Y] 0.12878E+02 c Velocity[Z] 0.34467E-05 c Pressure 0.19195E-03 110 0.74572E-04 0.31979E-02 0.29401E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -14.394 24.066 5.6114 8.0061 v Velocity[Y] -15.812 17.457 -0.14303 -0.00067234 v Velocity[Z] -3.0612 2.9805 3.2265e-06 -5.386e-08 v ǁVelocityǁ 0.0014153 25.088 6.6871 8.024 v Pressure -2.162e+05 94121 -53320 -30932 v TurbVisc 7.215e-21 0.0049704 0.0001209 7.7662e-06 v CourantNb 2.8876e-08 0.011772 0.00016667 4.8937e-06 v FourierNb 1.2425e-07 0.046953 0.00014552 1.8448e-07 v total_pressure -1.1487e+05 1.9545e+05 48005 70393 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0831 0.10219 0.0029749 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2237e-07 0.052192 0.00031219 5.0781e-06 INSTANT 0.875170000E-01 TIME STEP NUMBER 55368 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283162528E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.701127903E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.14214E-01 0.21208E+01 Friction velocity uk : 0.14214E-01 0.21208E+01 Dimensionless distance yplus : 0.13683E-01 0.20825E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.979803885e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29461E+08 1 0.19679E-09 0.25863E+02 0.20003E+04 c Velocity[X] 0.12999E+02 c Velocity[Y] 0.12864E+02 c Velocity[Z] 0.34390E-05 c Pressure 0.18864E-03 49 0.80349E-04 0.31390E-02 0.28484E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -14.415 24.089 5.6113 8.006 v Velocity[Y] -15.836 17.478 -0.14302 -0.00067302 v Velocity[Z] -3.0612 2.9805 3.2255e-06 -5.386e-08 v ǁVelocityǁ 0.0014065 25.109 6.6885 8.024 v Pressure -2.1766e+05 92384 -54813 -31849 v TurbVisc 6.7737e-21 0.0049704 0.000121 7.7824e-06 v CourantNb 3.2203e-08 0.011772 0.00016668 4.8937e-06 v FourierNb 1.2425e-07 0.046949 0.00014552 1.8459e-07 v total_pressure -1.1633e+05 1.9371e+05 46512 69476 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0825 0.10222 0.0029749 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2236e-07 0.052187 0.0003122 5.0783e-06 INSTANT 0.875171000E-01 TIME STEP NUMBER 55369 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283157572E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.701134761E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15772E-01 0.21202E+01 Friction velocity uk : 0.15772E-01 0.21202E+01 Dimensionless distance yplus : 0.15196E-01 0.20818E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.256361245e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29461E+08 1 0.19668E-09 0.25841E+02 0.19994E+04 c Velocity[X] 0.12990E+02 c Velocity[Y] 0.12851E+02 c Velocity[Z] 0.34326E-05 c Pressure 0.18517E-03 230 0.92326E-04 0.30776E-02 0.22726E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -14.437 24.113 5.6112 8.0059 v Velocity[Y] -15.859 17.498 -0.14302 -0.00067212 v Velocity[Z] -3.0611 2.9805 3.2245e-06 -5.386e-08 v ǁVelocityǁ 0.0014004 25.129 6.6899 8.0239 v Pressure -2.1904e+05 90717 -56234 -32565 v TurbVisc 8.3638e-21 0.0049704 0.00012111 7.7984e-06 v CourantNb 3.5947e-08 0.011772 0.00016668 4.8937e-06 v FourierNb 1.2425e-07 0.046945 0.00014552 1.8471e-07 v total_pressure -1.1771e+05 1.9204e+05 45091 68760 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0818 0.10224 0.0029749 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2235e-07 0.052182 0.0003122 5.0784e-06 INSTANT 0.875172000E-01 TIME STEP NUMBER 55370 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283152379E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.701122259E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12316E-01 0.21196E+01 Friction velocity uk : 0.12316E-01 0.21196E+01 Dimensionless distance yplus : 0.12061E-01 0.20813E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -7.813613797e-03 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29460E+08 1 0.19657E-09 0.25816E+02 0.19985E+04 c Velocity[X] 0.12982E+02 c Velocity[Y] 0.12834E+02 c Velocity[Z] 0.34228E-05 c Pressure 0.18172E-03 158 0.78464E-04 0.30168E-02 0.25468E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -14.458 24.137 5.6112 8.0058 v Velocity[Y] -15.882 17.518 -0.14301 -0.00067219 v Velocity[Z] -3.0611 2.9805 3.2235e-06 -5.386e-08 v ǁVelocityǁ 0.0013969 25.15 6.6913 8.0239 v Pressure -2.2034e+05 89123 -57651 -33432 v TurbVisc 8.2565e-21 0.0049705 0.00012122 7.8146e-06 v CourantNb 3.9858e-08 0.011772 0.00016668 4.8937e-06 v FourierNb 1.2425e-07 0.046942 0.00014552 1.8482e-07 v total_pressure -1.1902e+05 1.9045e+05 43674 67893 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0813 0.10226 0.002975 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2235e-07 0.052178 0.00031221 5.0785e-06 INSTANT 0.875173000E-01 TIME STEP NUMBER 55371 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283147134E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.701096756E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.53859E-02 0.21190E+01 Friction velocity uk : 0.53859E-02 0.21190E+01 Dimensionless distance yplus : 0.51849E-02 0.20807E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -4.874762753e-03 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29460E+08 1 0.19646E-09 0.25795E+02 0.19976E+04 c Velocity[X] 0.12973E+02 c Velocity[Y] 0.12822E+02 c Velocity[Z] 0.34147E-05 c Pressure 0.17762E-03 10 0.60287E-04 0.29453E-02 0.19971E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -14.479 24.161 5.6111 8.0057 v Velocity[Y] -15.905 17.538 -0.14301 -0.0006727 v Velocity[Z] -3.061 2.9805 3.2224e-06 -5.386e-08 v ǁVelocityǁ 0.0013935 25.17 6.6927 8.0239 v Pressure -2.2157e+05 87608 -59015 -34139 v TurbVisc 8.1687e-21 0.0049705 0.00012132 7.8307e-06 v CourantNb 4.3584e-08 0.011773 0.00016668 4.8937e-06 v FourierNb 1.2425e-07 0.046938 0.00014552 1.8494e-07 v total_pressure -1.2025e+05 1.8893e+05 42310 67186 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0807 0.10228 0.002975 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2234e-07 0.052174 0.00031221 5.0786e-06 INSTANT 0.875174000E-01 TIME STEP NUMBER 55372 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283141719E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.701059216E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10764E-01 0.21185E+01 Friction velocity uk : 0.10764E-01 0.21185E+01 Dimensionless distance yplus : 0.10584E-01 0.20802E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -2.634692720e-03 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29459E+08 1 0.19636E-09 0.25770E+02 0.19967E+04 c Velocity[X] 0.12964E+02 c Velocity[Y] 0.12806E+02 c Velocity[Z] 0.33921E-05 c Pressure 0.17442E-03 56 0.99871E-04 0.28889E-02 0.23135E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -14.5 24.184 5.6111 8.0056 v Velocity[Y] -15.928 17.558 -0.14301 -0.00067303 v Velocity[Z] -3.061 2.9805 3.2214e-06 -5.386e-08 v ǁVelocityǁ 0.0013949 25.19 6.6941 8.0238 v Pressure -2.2273e+05 86173 -60324 -34948 v TurbVisc 7.1878e-21 0.0049705 0.00012143 7.8467e-06 v CourantNb 4.6929e-08 0.011773 0.00016669 4.8937e-06 v FourierNb 1.2425e-07 0.046935 0.00014553 1.8505e-07 v total_pressure -1.214e+05 1.875e+05 41001 66377 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0802 0.10231 0.0029752 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2233e-07 0.05217 0.00031221 5.0788e-06 INSTANT 0.875175000E-01 TIME STEP NUMBER 55373 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283136235E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.701010375E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13864E-01 0.21180E+01 Friction velocity uk : 0.13864E-01 0.21180E+01 Dimensionless distance yplus : 0.13357E-01 0.20797E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -3.921996520e-03 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29459E+08 1 0.19625E-09 0.25746E+02 0.19957E+04 c Velocity[X] 0.12955E+02 c Velocity[Y] 0.12791E+02 c Velocity[Z] 0.33652E-05 c Pressure 0.17083E-03 43 0.82211E-04 0.28263E-02 0.20201E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -14.52 24.207 5.611 8.0055 v Velocity[Y] -15.951 17.577 -0.14301 -0.0006729 v Velocity[Z] -3.0609 2.9805 3.2204e-06 -5.386e-08 v ǁVelocityǁ 0.001394 25.209 6.6955 8.0238 v Pressure -2.2384e+05 84937 -61644 -35689 v TurbVisc 6.4723e-21 0.0049705 0.00012153 7.8628e-06 v CourantNb 4.9228e-08 0.011773 0.00016669 4.8937e-06 v FourierNb 1.2425e-07 0.046933 0.00014553 1.8516e-07 v total_pressure -1.2252e+05 1.8626e+05 39681 65636 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0797 0.10234 0.0029753 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2232e-07 0.052166 0.00031222 5.0789e-06 INSTANT 0.875176000E-01 TIME STEP NUMBER 55374 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283130625E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.700951341E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13018E-01 0.21176E+01 Friction velocity uk : 0.13018E-01 0.21176E+01 Dimensionless distance yplus : 0.12821E-01 0.20793E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -4.338472814e-03 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29458E+08 1 0.19614E-09 0.25724E+02 0.19949E+04 c Velocity[X] 0.12946E+02 c Velocity[Y] 0.12778E+02 c Velocity[Z] 0.33407E-05 c Pressure 0.16729E-03 10 0.57359E-04 0.27645E-02 0.17983E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -14.541 24.231 5.6109 8.0054 v Velocity[Y] -15.974 17.597 -0.14301 -0.00067208 v Velocity[Z] -3.0609 2.9805 3.2194e-06 -5.386e-08 v ǁVelocityǁ 0.0013932 25.229 6.6969 8.0237 v Pressure -2.2504e+05 83775 -62931 -36366 v TurbVisc 8.2867e-21 0.0049705 0.00012164 7.8788e-06 v CourantNb 5.0824e-08 0.011773 0.00016669 4.8937e-06 v FourierNb 1.2425e-07 0.04693 0.00014553 1.8528e-07 v total_pressure -1.2372e+05 1.851e+05 38394 64959 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0793 0.10235 0.0029753 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2231e-07 0.052163 0.00031222 5.079e-06 INSTANT 0.875177000E-01 TIME STEP NUMBER 55375 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283124845E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.700887213E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10700E-01 0.21173E+01 Friction velocity uk : 0.10700E-01 0.21173E+01 Dimensionless distance yplus : 0.10336E-01 0.20790E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -6.462162148e-03 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29458E+08 1 0.19603E-09 0.25697E+02 0.19938E+04 c Velocity[X] 0.12937E+02 c Velocity[Y] 0.12761E+02 c Velocity[Z] 0.33048E-05 c Pressure 0.16436E-03 29 0.97486E-04 0.27130E-02 0.20935E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -14.561 24.254 5.6109 8.0053 v Velocity[Y] -15.996 17.616 -0.14301 -0.00067197 v Velocity[Z] -3.0608 2.9805 3.2184e-06 -5.386e-08 v ǁVelocityǁ 0.0013941 25.248 6.6983 8.0237 v Pressure -2.2616e+05 82674 -64096 -37144 v TurbVisc 7.3418e-21 0.0049705 0.00012174 7.8948e-06 v CourantNb 5.1365e-08 0.011773 0.0001667 4.8937e-06 v FourierNb 1.2425e-07 0.046929 0.00014553 1.8539e-07 v total_pressure -1.2484e+05 1.84e+05 37229 64181 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.079 0.10236 0.0029752 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.223e-07 0.052161 0.00031222 5.0791e-06 INSTANT 0.875178000E-01 TIME STEP NUMBER 55376 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283119029E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.700817690E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12181E-01 0.21170E+01 Friction velocity uk : 0.12181E-01 0.21170E+01 Dimensionless distance yplus : 0.11942E-01 0.20787E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.087086313e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29457E+08 1 0.19592E-09 0.25672E+02 0.19929E+04 c Velocity[X] 0.12927E+02 c Velocity[Y] 0.12745E+02 c Velocity[Z] 0.32682E-05 c Pressure 0.16073E-03 98 0.83212E-04 0.26501E-02 0.18651E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -14.582 24.277 5.6109 8.0051 v Velocity[Y] -16.018 17.636 -0.14302 -0.00067219 v Velocity[Z] -3.0608 2.9805 3.2174e-06 -5.386e-08 v ǁVelocityǁ 0.0013955 25.267 6.6997 8.0236 v Pressure -2.2721e+05 81628 -65299 -37874 v TurbVisc 9.0144e-21 0.0049706 0.00012184 7.911e-06 v CourantNb 5.0166e-08 0.011773 0.0001667 4.8937e-06 v FourierNb 1.2425e-07 0.046927 0.00014553 1.855e-07 v total_pressure -1.2589e+05 1.8295e+05 36026 63451 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0787 0.10237 0.0029751 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2229e-07 0.05216 0.00031223 5.0792e-06 INSTANT 0.875179000E-01 TIME STEP NUMBER 55377 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283113088E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.700727161E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11512E-01 0.21167E+01 Friction velocity uk : 0.11512E-01 0.21167E+01 Dimensionless distance yplus : 0.11286E-01 0.20784E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.516651336e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29457E+08 1 0.19581E-09 0.25649E+02 0.19920E+04 c Velocity[X] 0.12918E+02 c Velocity[Y] 0.12732E+02 c Velocity[Z] 0.32305E-05 c Pressure 0.15722E-03 10 0.58926E-04 0.25892E-02 0.15920E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -14.602 24.3 5.6108 8.005 v Velocity[Y] -16.04 17.655 -0.14302 -0.00067283 v Velocity[Z] -3.0607 2.9805 3.2164e-06 -5.386e-08 v ǁVelocityǁ 0.0013951 25.287 6.7011 8.0236 v Pressure -2.282e+05 80633 -66493 -38501 v TurbVisc 6.3752e-21 0.0049706 0.00012194 7.927e-06 v CourantNb 4.7888e-08 0.011773 0.0001667 4.8938e-06 v FourierNb 1.2425e-07 0.046927 0.00014553 1.8562e-07 v total_pressure -1.2688e+05 1.8196e+05 34832 62824 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0784 0.10237 0.0029749 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2228e-07 0.052159 0.00031223 5.0794e-06 INSTANT 0.875180000E-01 TIME STEP NUMBER 55378 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283107040E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.700636269E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12111E-01 0.21166E+01 Friction velocity uk : 0.12111E-01 0.21166E+01 Dimensionless distance yplus : 0.11669E-01 0.20783E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.954047675e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29456E+08 1 0.19570E-09 0.25623E+02 0.19910E+04 c Velocity[X] 0.12908E+02 c Velocity[Y] 0.12715E+02 c Velocity[Z] 0.31858E-05 c Pressure 0.15439E-03 188 0.76296E-04 0.25398E-02 0.17144E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -14.622 24.322 5.6108 8.0049 v Velocity[Y] -16.062 17.674 -0.14302 -0.00067235 v Velocity[Z] -3.0607 2.9805 3.2154e-06 -5.386e-08 v ǁVelocityǁ 0.0013958 25.306 6.7025 8.0235 v Pressure -2.2913e+05 79685 -67499 -39129 v TurbVisc 9.0677e-21 0.0049706 0.00012204 7.9428e-06 v CourantNb 4.4272e-08 0.011773 0.0001667 4.8938e-06 v FourierNb 1.2425e-07 0.046927 0.00014553 1.8573e-07 v total_pressure -1.278e+05 1.8101e+05 33826 62196 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0783 0.10236 0.0029745 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2227e-07 0.052159 0.00031223 5.0795e-06 INSTANT 0.875181000E-01 TIME STEP NUMBER 55379 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283100904E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.700544211E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11639E-01 0.21165E+01 Friction velocity uk : 0.11639E-01 0.21165E+01 Dimensionless distance yplus : 0.11213E-01 0.20783E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -2.626885280e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29456E+08 1 0.19560E-09 0.25598E+02 0.19900E+04 c Velocity[X] 0.12898E+02 c Velocity[Y] 0.12700E+02 c Velocity[Z] 0.31421E-05 c Pressure 0.15082E-03 65 0.80895E-04 0.24783E-02 0.17465E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -14.642 24.345 5.6107 8.0048 v Velocity[Y] -16.084 17.694 -0.14303 -0.00067316 v Velocity[Z] -3.0606 2.9805 3.2144e-06 -5.386e-08 v ǁVelocityǁ 0.0013959 25.325 6.7039 8.0235 v Pressure -2.3e+05 78781 -68610 -39804 v TurbVisc 9.486e-21 0.0049706 0.00012214 7.9589e-06 v CourantNb 3.8633e-08 0.011773 0.00016671 4.8938e-06 v FourierNb 1.2425e-07 0.046927 0.00014553 1.8584e-07 v total_pressure -1.2867e+05 1.8011e+05 32715 61521 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0783 0.10235 0.0029741 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2226e-07 0.052159 0.00031224 5.0796e-06 INSTANT 0.875182000E-01 TIME STEP NUMBER 55380 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283094709E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.700427221E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10887E-01 0.21166E+01 Friction velocity uk : 0.10887E-01 0.21166E+01 Dimensionless distance yplus : 0.10489E-01 0.20783E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -3.154307975e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29455E+08 1 0.19549E-09 0.25573E+02 0.19890E+04 c Velocity[X] 0.12887E+02 c Velocity[Y] 0.12686E+02 c Velocity[Z] 0.30941E-05 c Pressure 0.14764E-03 369 0.93261E-04 0.24234E-02 0.14122E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -14.662 24.367 5.6107 8.0046 v Velocity[Y] -16.105 17.713 -0.14304 -0.00067238 v Velocity[Z] -3.0606 2.9805 3.2134e-06 -5.386e-08 v ǁVelocityǁ 0.0013957 25.344 6.7053 8.0234 v Pressure -2.3082e+05 77914 -69613 -40317 v TurbVisc 1.0507e-20 0.0049706 0.00012224 7.9749e-06 v CourantNb 3.1745e-08 0.011773 0.00016671 4.8938e-06 v FourierNb 1.2425e-07 0.046928 0.00014553 1.8595e-07 v total_pressure -1.295e+05 1.7924e+05 31712 61008 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0783 0.10234 0.0029735 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2225e-07 0.052161 0.00031224 5.0797e-06 INSTANT 0.875183000E-01 TIME STEP NUMBER 55381 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283088310E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.700314226E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.98102E-02 0.21166E+01 Friction velocity uk : 0.98102E-02 0.21166E+01 Dimensionless distance yplus : 0.94517E-02 0.20783E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -3.788416256e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29455E+08 1 0.19538E-09 0.25544E+02 0.19879E+04 c Velocity[X] 0.12877E+02 c Velocity[Y] 0.12667E+02 c Velocity[Z] 0.30481E-05 c Pressure 0.14440E-03 112 0.78841E-04 0.23676E-02 0.15578E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -14.681 24.389 5.6107 8.0045 v Velocity[Y] -16.127 17.733 -0.14305 -0.00067258 v Velocity[Z] -3.0605 2.9805 3.2123e-06 -5.386e-08 v ǁVelocityǁ 0.0013958 25.363 6.7067 8.0234 v Pressure -2.3161e+05 77080 -70599 -40950 v TurbVisc 7.7228e-21 0.0049707 0.00012234 7.9909e-06 v CourantNb 2.3303e-08 0.011774 0.00016671 4.8938e-06 v FourierNb 1.2425e-07 0.04693 0.00014553 1.8607e-07 v total_pressure -1.3028e+05 1.784e+05 30726 60375 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0783 0.10232 0.0029728 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2224e-07 0.052162 0.00031224 5.0798e-06 INSTANT 0.875184000E-01 TIME STEP NUMBER 55382 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283081896E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.700190994E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.84048E-02 0.21168E+01 Friction velocity uk : 0.84048E-02 0.21168E+01 Dimensionless distance yplus : 0.80976E-02 0.20785E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -4.399714659e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29454E+08 1 0.19527E-09 0.25520E+02 0.19870E+04 c Velocity[X] 0.12867E+02 c Velocity[Y] 0.12654E+02 c Velocity[Z] 0.30062E-05 c Pressure 0.14024E-03 10 0.56845E-04 0.22968E-02 0.11645E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -14.701 24.411 5.6106 8.0044 v Velocity[Y] -16.149 17.752 -0.14306 -0.00067325 v Velocity[Z] -3.0605 2.9805 3.2113e-06 -5.386e-08 v ǁVelocityǁ 0.0013954 25.382 6.7081 8.0233 v Pressure -2.3235e+05 76276 -71563 -41437 v TurbVisc 8.1664e-21 0.0049707 0.00012244 8.0069e-06 v CourantNb 1.5696e-08 0.011774 0.00016671 4.8938e-06 v FourierNb 1.2425e-07 0.046932 0.00014553 1.8618e-07 v total_pressure -1.3102e+05 1.776e+05 29762 59888 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0785 0.10229 0.002972 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2223e-07 0.052165 0.00031224 5.08e-06 INSTANT 0.875185000E-01 TIME STEP NUMBER 55383 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283075377E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.700060678E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.65534E-02 0.21170E+01 Friction velocity uk : 0.65534E-02 0.21170E+01 Dimensionless distance yplus : 0.63139E-02 0.20787E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -4.957602330e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29453E+08 1 0.19516E-09 0.25492E+02 0.19859E+04 c Velocity[X] 0.12856E+02 c Velocity[Y] 0.12636E+02 c Velocity[Z] 0.29580E-05 c Pressure 0.13735E-03 74 0.99223E-04 0.22470E-02 0.13616E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -14.72 24.432 5.6106 8.0043 v Velocity[Y] -16.17 17.772 -0.14307 -0.00067368 v Velocity[Z] -3.0604 2.9805 3.2103e-06 -5.386e-08 v ǁVelocityǁ 0.0013953 25.401 6.7095 8.0232 v Pressure -2.3306e+05 75498 -72385 -42001 v TurbVisc 8.0513e-21 0.0049707 0.00012254 8.0227e-06 v CourantNb 2.0609e-08 0.011774 0.00016671 4.8938e-06 v FourierNb 1.2425e-07 0.046934 0.00014553 1.8629e-07 v total_pressure -1.3173e+05 1.7682e+05 28940 59324 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0787 0.10226 0.0029711 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2222e-07 0.052168 0.00031225 5.0801e-06 INSTANT 0.875186000E-01 TIME STEP NUMBER 55384 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283068794E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.699931073E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.60558E-02 0.21173E+01 Friction velocity uk : 0.60558E-02 0.21173E+01 Dimensionless distance yplus : 0.58345E-02 0.20790E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -5.546509369e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29453E+08 1 0.19505E-09 0.25465E+02 0.19848E+04 c Velocity[X] 0.12845E+02 c Velocity[Y] 0.12620E+02 c Velocity[Z] 0.29142E-05 c Pressure 0.13370E-03 34 0.82207E-04 0.21849E-02 0.11422E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -14.74 24.454 5.6106 8.0041 v Velocity[Y] -16.191 17.791 -0.14308 -0.00067367 v Velocity[Z] -3.0603 2.9805 3.2093e-06 -5.386e-08 v ǁVelocityǁ 0.0013951 25.421 6.7109 8.0232 v Pressure -2.3374e+05 74743 -73277 -42492 v TurbVisc 9.3502e-21 0.0049707 0.00012264 8.0388e-06 v CourantNb 3.3296e-08 0.011774 0.00016671 4.8938e-06 v FourierNb 1.2425e-07 0.046937 0.00014553 1.864e-07 v total_pressure -1.3242e+05 1.7607e+05 28048 58833 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.079 0.10223 0.0029701 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2221e-07 0.052171 0.00031225 5.0802e-06 INSTANT 0.875187000E-01 TIME STEP NUMBER 55385 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283062130E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.699779222E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.57219E-02 0.21176E+01 Friction velocity uk : 0.57219E-02 0.21176E+01 Dimensionless distance yplus : 0.55128E-02 0.20792E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -5.963116955e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29452E+08 1 0.19494E-09 0.25440E+02 0.19838E+04 c Velocity[X] 0.12834E+02 c Velocity[Y] 0.12606E+02 c Velocity[Z] 0.28783E-05 c Pressure 0.13029E-03 9 0.53444E-04 0.21268E-02 0.99625E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -14.759 24.475 5.6105 8.004 v Velocity[Y] -16.213 17.811 -0.14309 -0.000673 v Velocity[Z] -3.0603 2.9805 3.2083e-06 -5.386e-08 v ǁVelocityǁ 0.0013952 25.44 6.7123 8.0231 v Pressure -2.344e+05 74005 -74124 -42924 v TurbVisc 9.2963e-21 0.0049707 0.00012273 8.0546e-06 v CourantNb 3.911e-08 0.011774 0.00016672 4.8938e-06 v FourierNb 1.2425e-07 0.04694 0.00014553 1.8652e-07 v total_pressure -1.3307e+05 1.7533e+05 27201 58401 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0792 0.10219 0.0029689 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.222e-07 0.052175 0.00031225 5.0803e-06 INSTANT 0.875188000E-01 TIME STEP NUMBER 55386 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283055351E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.699635017E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.41537E-02 0.21179E+01 Friction velocity uk : 0.41537E-02 0.21179E+01 Dimensionless distance yplus : 0.40019E-02 0.20796E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -6.369980782e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29452E+08 1 0.19483E-09 0.25411E+02 0.19827E+04 c Velocity[X] 0.12823E+02 c Velocity[Y] 0.12588E+02 c Velocity[Z] 0.28319E-05 c Pressure 0.12768E-03 42 0.97628E-04 0.20821E-02 0.12317E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -14.778 24.496 5.6105 8.0039 v Velocity[Y] -16.234 17.831 -0.1431 -0.00067306 v Velocity[Z] -3.0602 2.9806 3.2073e-06 -5.386e-08 v ǁVelocityǁ 0.0013945 25.459 6.7136 8.0231 v Pressure -2.3503e+05 73286 -74843 -43451 v TurbVisc 9.5265e-21 0.0049707 0.00012283 8.0706e-06 v CourantNb 4.4108e-08 0.011774 0.00016672 4.8938e-06 v FourierNb 1.2425e-07 0.046944 0.00014553 1.8663e-07 v total_pressure -1.337e+05 1.7461e+05 26482 57874 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0796 0.10215 0.0029677 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2219e-07 0.05218 0.00031225 5.0804e-06 INSTANT 0.875189000E-01 TIME STEP NUMBER 55387 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283048557E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.699489231E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.60505E-02 0.21182E+01 Friction velocity uk : 0.60505E-02 0.21182E+01 Dimensionless distance yplus : 0.58294E-02 0.20799E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -6.677981386e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29451E+08 1 0.19472E-09 0.25383E+02 0.19816E+04 c Velocity[X] 0.12812E+02 c Velocity[Y] 0.12571E+02 c Velocity[Z] 0.27928E-05 c Pressure 0.12447E-03 99 0.82993E-04 0.20275E-02 0.10007E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -14.797 24.517 5.6104 8.0037 v Velocity[Y] -16.255 17.85 -0.14311 -0.00067333 v Velocity[Z] -3.0602 2.9806 3.2063e-06 -5.386e-08 v ǁVelocityǁ 0.0013941 25.478 6.715 8.023 v Pressure -2.3564e+05 72581 -75599 -43900 v TurbVisc 9.0459e-21 0.0049708 0.00012292 8.0866e-06 v CourantNb 3.7225e-08 0.011774 0.00016672 4.8938e-06 v FourierNb 1.2425e-07 0.046947 0.00014554 1.8674e-07 v total_pressure -1.3432e+05 1.7391e+05 25726 57425 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0799 0.10211 0.0029664 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2218e-07 0.052184 0.00031225 5.0805e-06 INSTANT 0.875190000E-01 TIME STEP NUMBER 55388 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283041688E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.699324554E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.61662E-02 0.21186E+01 Friction velocity uk : 0.61662E-02 0.21186E+01 Dimensionless distance yplus : 0.59408E-02 0.20803E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -6.923441317e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29450E+08 1 0.19461E-09 0.25357E+02 0.19806E+04 c Velocity[X] 0.12800E+02 c Velocity[Y] 0.12557E+02 c Velocity[Z] 0.27618E-05 c Pressure 0.12147E-03 9 0.54452E-04 0.19764E-02 0.82434E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -14.816 24.537 5.6104 8.0036 v Velocity[Y] -16.276 17.87 -0.14312 -0.00067403 v Velocity[Z] -3.0601 2.9806 3.2053e-06 -5.386e-08 v ǁVelocityǁ 0.0013944 25.498 6.7164 8.0229 v Pressure -2.3635e+05 71889 -76309 -44257 v TurbVisc 9.7037e-21 0.0049708 0.00012302 8.1025e-06 v CourantNb 7.3444e-08 0.011774 0.00016672 4.8938e-06 v FourierNb 1.2425e-07 0.046951 0.00014554 1.8685e-07 v total_pressure -1.3502e+05 1.7321e+05 25016 57068 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0803 0.10206 0.0029651 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2217e-07 0.052188 0.00031225 5.0807e-06 INSTANT 0.875191000E-01 TIME STEP NUMBER 55389 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283034781E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.699163241E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.45600E-02 0.21190E+01 Friction velocity uk : 0.45600E-02 0.21190E+01 Dimensionless distance yplus : 0.43933E-02 0.20806E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -7.028932233e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29450E+08 1 0.19450E-09 0.25328E+02 0.19795E+04 c Velocity[X] 0.12788E+02 c Velocity[Y] 0.12540E+02 c Velocity[Z] 0.27275E-05 c Pressure 0.11935E-03 384 0.75694E-04 0.19400E-02 0.96007E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -14.835 24.558 5.6104 8.0034 v Velocity[Y] -16.298 17.89 -0.14314 -0.00067361 v Velocity[Z] -3.0601 2.9806 3.2043e-06 -5.386e-08 v ǁVelocityǁ 0.0013932 25.517 6.7178 8.0229 v Pressure -2.3712e+05 71213 -76913 -44618 v TurbVisc 1.1211e-20 0.0049708 0.00012311 8.1183e-06 v CourantNb 8.8531e-08 0.011774 0.00016672 4.8938e-06 v FourierNb 1.2425e-07 0.046954 0.00014554 1.8696e-07 v total_pressure -1.358e+05 1.7254e+05 24412 56707 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0806 0.10202 0.0029638 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2216e-07 0.052193 0.00031226 5.0808e-06 INSTANT 0.875192000E-01 TIME STEP NUMBER 55390 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283027776E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.698998216E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.63636E-02 0.21193E+01 Friction velocity uk : 0.63636E-02 0.21193E+01 Dimensionless distance yplus : 0.61311E-02 0.20810E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -7.056179455e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29449E+08 1 0.19439E-09 0.25300E+02 0.19784E+04 c Velocity[X] 0.12776E+02 c Velocity[Y] 0.12524E+02 c Velocity[Z] 0.26982E-05 c Pressure 0.11701E-03 62 0.79995E-04 0.18998E-02 0.94742E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -14.854 24.578 5.6103 8.0033 v Velocity[Y] -16.319 17.909 -0.14315 -0.00067438 v Velocity[Z] -3.06 2.9806 3.2033e-06 -5.386e-08 v ǁVelocityǁ 0.0013931 25.536 6.7192 8.0228 v Pressure -2.3789e+05 70553 -77532 -44976 v TurbVisc 1.1932e-20 0.0049708 0.00012321 8.1343e-06 v CourantNb 1.0302e-07 0.011774 0.00016672 4.8938e-06 v FourierNb 1.2425e-07 0.046958 0.00014554 1.8708e-07 v total_pressure -1.3657e+05 1.7188e+05 23793 56349 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.081 0.10198 0.0029625 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2214e-07 0.052197 0.00031226 5.0809e-06 INSTANT 0.875193000E-01 TIME STEP NUMBER 55391 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283020808E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.698824892E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11396E-01 0.21196E+01 Friction velocity uk : 0.11396E-01 0.21196E+01 Dimensionless distance yplus : 0.10979E-01 0.20813E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -6.994462137e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29449E+08 1 0.19428E-09 0.25271E+02 0.19773E+04 c Velocity[X] 0.12763E+02 c Velocity[Y] 0.12508E+02 c Velocity[Z] 0.26741E-05 c Pressure 0.11506E-03 715 0.92977E-04 0.18662E-02 0.87741E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -14.873 24.599 5.6103 8.0032 v Velocity[Y] -16.34 17.929 -0.14316 -0.00067373 v Velocity[Z] -3.06 2.9806 3.2023e-06 -5.386e-08 v ǁVelocityǁ 0.0013935 25.556 6.7206 8.0227 v Pressure -2.3866e+05 70024 -78091 -45276 v TurbVisc 1.1293e-20 0.0049708 0.0001233 8.1501e-06 v CourantNb 9.9574e-08 0.011774 0.00016672 4.8938e-06 v FourierNb 1.2425e-07 0.046961 0.00014554 1.8719e-07 v total_pressure -1.3733e+05 1.7135e+05 23234 56049 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0813 0.10194 0.0029611 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2213e-07 0.052201 0.00031226 5.081e-06 INSTANT 0.875194000E-01 TIME STEP NUMBER 55392 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283013650E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.698650626E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15120E-01 0.21199E+01 Friction velocity uk : 0.15120E-01 0.21199E+01 Dimensionless distance yplus : 0.14568E-01 0.20815E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -6.835184760e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29448E+08 1 0.19417E-09 0.25238E+02 0.19760E+04 c Velocity[X] 0.12750E+02 c Velocity[Y] 0.12488E+02 c Velocity[Z] 0.26542E-05 c Pressure 0.11333E-03 67 0.78331E-04 0.18363E-02 0.75769E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -14.892 24.619 5.6102 8.003 v Velocity[Y] -16.361 17.948 -0.14317 -0.000674 v Velocity[Z] -3.0599 2.9806 3.2013e-06 -5.386e-08 v ǁVelocityǁ 0.0013927 25.575 6.7219 8.0226 v Pressure -2.3942e+05 69535 -78605 -45583 v TurbVisc 8.4206e-21 0.0049708 0.00012339 8.1661e-06 v CourantNb 5.1905e-08 0.011774 0.00016672 4.8938e-06 v FourierNb 1.2425e-07 0.046964 0.00014554 1.873e-07 v total_pressure -1.3809e+05 1.7086e+05 22720 55742 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0815 0.10189 0.0029598 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2212e-07 0.052204 0.00031226 5.0811e-06 INSTANT 0.875195000E-01 TIME STEP NUMBER 55393 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283006542E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.698473211E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10627E-01 0.21201E+01 Friction velocity uk : 0.10627E-01 0.21201E+01 Dimensionless distance yplus : 0.10466E-01 0.20817E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -6.608570859e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29447E+08 1 0.19407E-09 0.25209E+02 0.19749E+04 c Velocity[X] 0.12736E+02 c Velocity[Y] 0.12473E+02 c Velocity[Z] 0.26393E-05 c Pressure 0.11057E-03 9 0.52870E-04 0.17897E-02 0.50319E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -14.911 24.639 5.6101 8.0029 v Velocity[Y] -16.383 17.968 -0.14318 -0.00067475 v Velocity[Z] -3.0599 2.9806 3.2003e-06 -5.386e-08 v ǁVelocityǁ 0.0013928 25.594 6.7233 8.0226 v Pressure -2.4016e+05 69074 -79042 -45792 v TurbVisc 1.2199e-20 0.0049709 0.00012348 8.1819e-06 v CourantNb 4.3091e-08 0.011774 0.00016672 4.8938e-06 v FourierNb 1.2425e-07 0.046966 0.00014554 1.8741e-07 v total_pressure -1.3884e+05 1.704e+05 22283 55533 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0817 0.10185 0.0029585 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2211e-07 0.052207 0.00031226 5.0812e-06 INSTANT 0.875196000E-01 TIME STEP NUMBER 55394 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282999402E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.698292889E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.88740E-02 0.21202E+01 Friction velocity uk : 0.88740E-02 0.21202E+01 Dimensionless distance yplus : 0.87910E-02 0.20819E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -6.328737320e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29447E+08 1 0.19396E-09 0.25177E+02 0.19736E+04 c Velocity[X] 0.12723E+02 c Velocity[Y] 0.12454E+02 c Velocity[Z] 0.26240E-05 c Pressure 0.10933E-03 140 0.98615E-04 0.17678E-02 0.63258E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -14.929 24.659 5.6101 8.0027 v Velocity[Y] -16.404 17.987 -0.1432 -0.00067516 v Velocity[Z] -3.0598 2.9806 3.1993e-06 -5.386e-08 v ǁVelocityǁ 0.0013926 25.614 6.7247 8.0225 v Pressure -2.4088e+05 68642 -79505 -46066 v TurbVisc 1.0048e-20 0.0049709 0.00012358 8.1977e-06 v CourantNb 3.583e-08 0.011774 0.00016672 4.8938e-06 v FourierNb 1.2425e-07 0.046968 0.00014554 1.8752e-07 v total_pressure -1.3956e+05 1.6997e+05 21820 55259 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0819 0.10182 0.0029572 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.221e-07 0.052209 0.00031226 5.0813e-06 INSTANT 0.875197000E-01 TIME STEP NUMBER 55395 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282992207E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.698105117E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.16880E-01 0.21203E+01 Friction velocity uk : 0.16880E-01 0.21203E+01 Dimensionless distance yplus : 0.16651E-01 0.20820E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -5.961252118e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29446E+08 1 0.19385E-09 0.25146E+02 0.19724E+04 c Velocity[X] 0.12709E+02 c Velocity[Y] 0.12437E+02 c Velocity[Z] 0.26111E-05 c Pressure 0.10778E-03 43 0.82628E-04 0.17408E-02 0.41065E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -14.948 24.679 5.61 8.0026 v Velocity[Y] -16.425 18.006 -0.14321 -0.00067515 v Velocity[Z] -3.0598 2.9806 3.1983e-06 -5.386e-08 v ǁVelocityǁ 0.0013926 25.633 6.726 8.0224 v Pressure -2.4158e+05 68243 -79869 -46245 v TurbVisc 1.0479e-20 0.0049709 0.00012367 8.2136e-06 v CourantNb 3.7085e-08 0.011774 0.00016672 4.8938e-06 v FourierNb 1.2425e-07 0.04697 0.00014554 1.8763e-07 v total_pressure -1.4026e+05 1.6957e+05 21456 55080 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.082 0.10179 0.0029561 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2209e-07 0.052211 0.00031227 5.0814e-06 INSTANT 0.875198000E-01 TIME STEP NUMBER 55396 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282984991E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.697927282E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13979E-01 0.21204E+01 Friction velocity uk : 0.13979E-01 0.21204E+01 Dimensionless distance yplus : 0.13488E-01 0.20820E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -5.635842620e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29445E+08 1 0.19374E-09 0.25116E+02 0.19712E+04 c Velocity[X] 0.12694E+02 c Velocity[Y] 0.12422E+02 c Velocity[Z] 0.26064E-05 c Pressure 0.10611E-03 12 0.52690E-04 0.17121E-02 0.38230E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -14.967 24.699 5.6099 8.0024 v Velocity[Y] -16.446 18.025 -0.14322 -0.00067444 v Velocity[Z] -3.0597 2.9806 3.1973e-06 -5.386e-08 v ǁVelocityǁ 0.0013931 25.652 6.7274 8.0224 v Pressure -2.4225e+05 67875 -80172 -46388 v TurbVisc 1.1359e-20 0.0049709 0.00012376 8.2294e-06 v CourantNb 2.158e-08 0.011774 0.00016672 4.8938e-06 v FourierNb 1.2425e-07 0.046971 0.00014554 1.8775e-07 v total_pressure -1.4092e+05 1.692e+05 21153 54937 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.082 0.10177 0.002955 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2207e-07 0.052213 0.00031227 5.0815e-06 INSTANT 0.875199000E-01 TIME STEP NUMBER 55397 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282977722E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.697741636E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19585E-01 0.21203E+01 Friction velocity uk : 0.19585E-01 0.21203E+01 Dimensionless distance yplus : 0.19351E-01 0.20819E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -5.300397647e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29445E+08 1 0.19363E-09 0.25084E+02 0.19700E+04 c Velocity[X] 0.12681E+02 c Velocity[Y] 0.12403E+02 c Velocity[Z] 0.26013E-05 c Pressure 0.10533E-03 541 0.75571E-04 0.16977E-02 0.82155E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -14.985 24.719 5.6099 8.0023 v Velocity[Y] -16.468 18.044 -0.14322 -0.00067539 v Velocity[Z] -3.0596 2.9806 3.1963e-06 -5.386e-08 v ǁVelocityǁ 0.001393 25.671 6.7288 8.0223 v Pressure -2.4288e+05 67543 -80545 -46684 v TurbVisc 9.051e-21 0.0049709 0.00012385 8.2452e-06 v CourantNb 5.7404e-09 0.011774 0.00016672 4.8938e-06 v FourierNb 1.2425e-07 0.046971 0.00014555 1.8786e-07 v total_pressure -1.4155e+05 1.6887e+05 20780 54641 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0819 0.10176 0.0029539 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2206e-07 0.052213 0.00031227 5.0816e-06 INSTANT 0.875200000E-01 TIME STEP NUMBER 55398 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282970492E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.697547426E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.16929E-01 0.21202E+01 Friction velocity uk : 0.16929E-01 0.21202E+01 Dimensionless distance yplus : 0.16334E-01 0.20818E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -4.838922310e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29444E+08 1 0.19352E-09 0.25053E+02 0.19688E+04 c Velocity[X] 0.12665E+02 c Velocity[Y] 0.12388E+02 c Velocity[Z] 0.25961E-05 c Pressure 0.10438E-03 146 0.79774E-04 0.16808E-02 0.55123E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -15.004 24.739 5.6098 8.0021 v Velocity[Y] -16.489 18.063 -0.14323 -0.00067468 v Velocity[Z] -3.0596 2.9806 3.1953e-06 -5.386e-08 v ǁVelocityǁ 0.001394 25.689 6.7302 8.0222 v Pressure -2.4346e+05 67252 -80730 -46687 v TurbVisc 1.124e-20 0.0049709 0.00012394 8.2611e-06 v CourantNb 9.3272e-09 0.011774 0.00016673 4.8938e-06 v FourierNb 1.2425e-07 0.046971 0.00014555 1.8797e-07 v total_pressure -1.4213e+05 1.6858e+05 20595 54638 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0818 0.10174 0.002953 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2205e-07 0.052213 0.00031227 5.0817e-06 INSTANT 0.875201000E-01 TIME STEP NUMBER 55399 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282963167E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.697370394E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15770E-01 0.21199E+01 Friction velocity uk : 0.15770E-01 0.21199E+01 Dimensionless distance yplus : 0.15215E-01 0.20816E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -4.553254301e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29443E+08 1 0.19342E-09 0.25021E+02 0.19675E+04 c Velocity[X] 0.12650E+02 c Velocity[Y] 0.12371E+02 c Velocity[Z] 0.25966E-05 c Pressure 0.10362E-03 113 0.92936E-04 0.16667E-02 0.67464E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -15.022 24.759 5.6097 8.002 v Velocity[Y] -16.51 18.081 -0.14324 -0.00067555 v Velocity[Z] -3.0595 2.9806 3.1943e-06 -5.386e-08 v ǁVelocityǁ 0.0013956 25.708 6.7315 8.0221 v Pressure -2.4399e+05 67003 -80926 -46813 v TurbVisc 8.4509e-21 0.004971 0.00012402 8.277e-06 v CourantNb 2.5309e-08 0.011774 0.00016673 4.8938e-06 v FourierNb 1.2425e-07 0.04697 0.00014555 1.8808e-07 v total_pressure -1.4267e+05 1.6833e+05 20399 54512 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0816 0.10173 0.0029521 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2204e-07 0.052211 0.00031228 5.0819e-06 INSTANT 0.875202000E-01 TIME STEP NUMBER 55400 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282955940E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.697181314E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12945E-01 0.21196E+01 Friction velocity uk : 0.12945E-01 0.21196E+01 Dimensionless distance yplus : 0.12501E-01 0.20813E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -4.250830797e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29443E+08 1 0.19331E-09 0.24986E+02 0.19662E+04 c Velocity[X] 0.12634E+02 c Velocity[Y] 0.12352E+02 c Velocity[Z] 0.25977E-05 c Pressure 0.10302E-03 116 0.78434E-04 0.16554E-02 0.36734E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -15.041 24.779 5.6096 8.0018 v Velocity[Y] -16.531 18.1 -0.14325 -0.00067551 v Velocity[Z] -3.0595 2.9806 3.1933e-06 -5.386e-08 v ǁVelocityǁ 0.0013984 25.727 6.7329 8.0221 v Pressure -2.4447e+05 66799 -81068 -46855 v TurbVisc 9.6498e-21 0.004971 0.00012411 8.2928e-06 v CourantNb 3.8992e-08 0.011774 0.00016673 4.8938e-06 v FourierNb 1.2425e-07 0.046969 0.00014555 1.8819e-07 v total_pressure -1.4315e+05 1.6812e+05 20257 54470 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0813 0.10173 0.0029514 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2203e-07 0.052209 0.00031228 5.082e-06 INSTANT 0.875203000E-01 TIME STEP NUMBER 55401 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282948629E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.696992073E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10467E-01 0.21192E+01 Friction velocity uk : 0.10467E-01 0.21192E+01 Dimensionless distance yplus : 0.10099E-01 0.20808E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -4.040837146e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29442E+08 1 0.19320E-09 0.24955E+02 0.19649E+04 c Velocity[X] 0.12618E+02 c Velocity[Y] 0.12337E+02 c Velocity[Z] 0.26009E-05 c Pressure 0.10125E-03 7 0.52847E-04 0.16253E-02 0.22762E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -15.059 24.799 5.6095 8.0017 v Velocity[Y] -16.552 18.118 -0.14325 -0.00067496 v Velocity[Z] -3.0594 2.9806 3.1923e-06 -5.386e-08 v ǁVelocityǁ 0.001402 25.745 6.7342 8.022 v Pressure -2.4488e+05 66645 -81106 -46867 v TurbVisc 5.984e-21 0.004971 0.0001242 8.3086e-06 v CourantNb 5.0612e-08 0.011774 0.00016673 4.8938e-06 v FourierNb 1.2425e-07 0.046967 0.00014555 1.883e-07 v total_pressure -1.4356e+05 1.6797e+05 20219 54458 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0808 0.10173 0.0029507 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2202e-07 0.052206 0.00031228 5.0821e-06 INSTANT 0.875204000E-01 TIME STEP NUMBER 55402 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282941293E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.696802345E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.14407E-01 0.21187E+01 Friction velocity uk : 0.14407E-01 0.21187E+01 Dimensionless distance yplus : 0.13919E-01 0.20804E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -4.070556648e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29441E+08 1 0.19310E-09 0.24922E+02 0.19636E+04 c Velocity[X] 0.12603E+02 c Velocity[Y] 0.12318E+02 c Velocity[Z] 0.26030E-05 c Pressure 0.10127E-03 24 0.98724E-04 0.16241E-02 0.27779E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -15.078 24.82 5.6094 8.0015 v Velocity[Y] -16.573 18.136 -0.14325 -0.00067478 v Velocity[Z] -3.0594 2.9806 3.1913e-06 -5.386e-08 v ǁVelocityǁ 0.0014096 25.763 6.7356 8.0219 v Pressure -2.4523e+05 66545 -81266 -46962 v TurbVisc 6.3938e-21 0.004971 0.00012428 8.3244e-06 v CourantNb 5.1896e-08 0.011774 0.00016673 4.8937e-06 v FourierNb 1.2425e-07 0.046964 0.00014556 1.8841e-07 v total_pressure -1.439e+05 1.6787e+05 20059 54363 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0804 0.10173 0.0029501 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.22e-07 0.052203 0.00031228 5.0822e-06 INSTANT 0.875205000E-01 TIME STEP NUMBER 55403 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282933989E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.696602645E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.16414E-01 0.21181E+01 Friction velocity uk : 0.16414E-01 0.21181E+01 Dimensionless distance yplus : 0.15837E-01 0.20798E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -3.770354768e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29441E+08 1 0.19299E-09 0.24889E+02 0.19623E+04 c Velocity[X] 0.12587E+02 c Velocity[Y] 0.12301E+02 c Velocity[Z] 0.26020E-05 c Pressure 0.10085E-03 548 0.82842E-04 0.16157E-02 0.16083E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -15.096 24.84 5.6093 8.0014 v Velocity[Y] -16.594 18.154 -0.14326 -0.00067484 v Velocity[Z] -3.0593 2.9806 3.1903e-06 -5.386e-08 v ǁVelocityǁ 0.0014211 25.781 6.737 8.0218 v Pressure -2.4549e+05 66506 -81230 -46923 v TurbVisc 9.4847e-21 0.004971 0.00012437 8.3404e-06 v CourantNb 6.7748e-08 0.011774 0.00016673 4.8937e-06 v FourierNb 1.2425e-07 0.04696 0.00014556 1.8852e-07 v total_pressure -1.4417e+05 1.6783e+05 20095 54402 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0798 0.10174 0.0029497 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2199e-07 0.052198 0.00031229 5.0823e-06 INSTANT 0.875206000E-01 TIME STEP NUMBER 55404 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282926709E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.696423994E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.16013E-01 0.21174E+01 Friction velocity uk : 0.16013E-01 0.21174E+01 Dimensionless distance yplus : 0.15450E-01 0.20791E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -3.961924148e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29440E+08 1 0.19289E-09 0.24857E+02 0.19611E+04 c Velocity[X] 0.12571E+02 c Velocity[Y] 0.12286E+02 c Velocity[Z] 0.26077E-05 c Pressure 0.10060E-03 7 0.51863E-04 0.16100E-02 0.23675E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -15.114 24.86 5.6092 8.0013 v Velocity[Y] -16.615 18.171 -0.14326 -0.0006756 v Velocity[Z] -3.0592 2.9806 3.1893e-06 -5.386e-08 v ǁVelocityǁ 0.0014384 25.799 6.7383 8.0218 v Pressure -2.4567e+05 66524 -81171 -46920 v TurbVisc 4.8712e-21 0.004971 0.00012446 8.3561e-06 v CourantNb 6.235e-08 0.011774 0.00016673 4.8937e-06 v FourierNb 1.2425e-07 0.046956 0.00014556 1.8863e-07 v total_pressure -1.4435e+05 1.6785e+05 20154 54405 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0791 0.10176 0.0029493 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2198e-07 0.052193 0.00031229 5.0824e-06 INSTANT 0.875207000E-01 TIME STEP NUMBER 55405 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282919453E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.696232553E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.66883E-02 0.21167E+01 Friction velocity uk : 0.66883E-02 0.21167E+01 Dimensionless distance yplus : 0.64532E-02 0.20784E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -4.258314053e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29439E+08 1 0.19278E-09 0.24824E+02 0.19598E+04 c Velocity[X] 0.12554E+02 c Velocity[Y] 0.12270E+02 c Velocity[Z] 0.26097E-05 c Pressure 0.10155E-03 30 0.75453E-04 0.16236E-02 0.57911E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -15.132 24.88 5.6091 8.0011 v Velocity[Y] -16.635 18.188 -0.14326 -0.00067502 v Velocity[Z] -3.0592 2.9806 3.1883e-06 -5.386e-08 v ǁVelocityǁ 0.0014574 25.816 6.7397 8.0217 v Pressure -2.4577e+05 66605 -81073 -46775 v TurbVisc 7.4618e-21 0.0049711 0.00012454 8.3718e-06 v CourantNb 5.39e-08 0.011774 0.00016673 4.8937e-06 v FourierNb 1.2425e-07 0.046952 0.00014556 1.8874e-07 v total_pressure -1.4444e+05 1.6793e+05 20252 54550 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0784 0.10177 0.0029489 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2197e-07 0.052187 0.00031229 5.0825e-06 INSTANT 0.875208000E-01 TIME STEP NUMBER 55406 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282912140E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.696036909E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10268E-01 0.21159E+01 Friction velocity uk : 0.10268E-01 0.21159E+01 Dimensionless distance yplus : 0.99828E-02 0.20776E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -4.523005413e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29439E+08 1 0.19268E-09 0.24791E+02 0.19585E+04 c Velocity[X] 0.12537E+02 c Velocity[Y] 0.12254E+02 c Velocity[Z] 0.26098E-05 c Pressure 0.10233E-03 58 0.79460E-04 0.16346E-02 0.53048E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -15.151 24.901 5.6089 8.001 v Velocity[Y] -16.656 18.205 -0.14326 -0.0006757 v Velocity[Z] -3.0591 2.9806 3.1873e-06 -5.386e-08 v ǁVelocityǁ 0.0014875 25.834 6.741 8.0216 v Pressure -2.4577e+05 66750 -80928 -46717 v TurbVisc 3.3222e-21 0.0049711 0.00012463 8.3877e-06 v CourantNb 4.6256e-08 0.011774 0.00016673 4.8937e-06 v FourierNb 1.2425e-07 0.046946 0.00014557 1.8886e-07 v total_pressure -1.4444e+05 1.6808e+05 20397 54608 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0776 0.10179 0.0029486 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2196e-07 0.052181 0.0003123 5.0826e-06 INSTANT 0.875209000E-01 TIME STEP NUMBER 55407 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282904954E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.695849198E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10235E-01 0.21151E+01 Friction velocity uk : 0.10235E-01 0.21151E+01 Dimensionless distance yplus : 0.98758E-02 0.20768E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -5.040110967e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29438E+08 1 0.19257E-09 0.24757E+02 0.19572E+04 c Velocity[X] 0.12519E+02 c Velocity[Y] 0.12238E+02 c Velocity[Z] 0.26096E-05 c Pressure 0.10371E-03 100 0.92657E-04 0.16549E-02 0.68411E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -15.169 24.921 5.6088 8.0008 v Velocity[Y] -16.676 18.222 -0.14325 -0.00067487 v Velocity[Z] -3.0591 2.9806 3.1863e-06 -5.386e-08 v ǁVelocityǁ 0.0015269 25.851 6.7424 8.0215 v Pressure -2.4568e+05 66964 -80726 -46580 v TurbVisc 2.5665e-21 0.0049711 0.00012471 8.4034e-06 v CourantNb 4.4468e-08 0.011775 0.00016673 4.8937e-06 v FourierNb 1.2425e-07 0.046941 0.00014557 1.8897e-07 v total_pressure -1.4435e+05 1.6829e+05 20599 54745 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0768 0.10181 0.0029484 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2194e-07 0.052174 0.0003123 5.0827e-06 INSTANT 0.875210000E-01 TIME STEP NUMBER 55408 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282897661E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.695655078E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15476E-01 0.21142E+01 Friction velocity uk : 0.15476E-01 0.21142E+01 Dimensionless distance yplus : 0.14932E-01 0.20760E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -5.719400897e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29438E+08 1 0.19247E-09 0.24721E+02 0.19557E+04 c Velocity[X] 0.12502E+02 c Velocity[Y] 0.12219E+02 c Velocity[Z] 0.26067E-05 c Pressure 0.10545E-03 557 0.78307E-04 0.16811E-02 0.45204E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -15.187 24.941 5.6087 8.0007 v Velocity[Y] -16.696 18.239 -0.14325 -0.00067483 v Velocity[Z] -3.059 2.9806 3.1853e-06 -5.386e-08 v ǁVelocityǁ 0.0015773 25.868 6.7437 8.0215 v Pressure -2.4549e+05 67247 -80476 -46440 v TurbVisc 2.0314e-21 0.0049711 0.00012479 8.4193e-06 v CourantNb 2.1622e-08 0.011775 0.00016674 4.8937e-06 v FourierNb 1.2425e-07 0.046935 0.00014557 1.8908e-07 v total_pressure -1.4417e+05 1.6857e+05 20849 54885 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.076 0.10183 0.0029482 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2193e-07 0.052167 0.00031231 5.0828e-06 INSTANT 0.875211000E-01 TIME STEP NUMBER 55409 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282890479E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.695460678E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10510E-01 0.21133E+01 Friction velocity uk : 0.10510E-01 0.21133E+01 Dimensionless distance yplus : 0.10350E-01 0.20751E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -6.491788167e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29437E+08 1 0.19237E-09 0.24688E+02 0.19544E+04 c Velocity[X] 0.12485E+02 c Velocity[Y] 0.12203E+02 c Velocity[Z] 0.26082E-05 c Pressure 0.10625E-03 7 0.53485E-04 0.16922E-02 0.29425E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -15.205 24.962 5.6085 8.0005 v Velocity[Y] -16.717 18.255 -0.14324 -0.00067558 v Velocity[Z] -3.059 2.9806 3.1843e-06 -5.386e-08 v ǁVelocityǁ 0.0016501 25.885 6.745 8.0214 v Pressure -2.4521e+05 67596 -80219 -46372 v TurbVisc 1.0632e-21 0.0049711 0.00012488 8.4351e-06 v CourantNb 5.8156e-08 0.011775 0.00016674 4.8937e-06 v FourierNb 1.2425e-07 0.046929 0.00014557 1.8919e-07 v total_pressure -1.4388e+05 1.6892e+05 21106 54953 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0751 0.10186 0.002948 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2192e-07 0.052159 0.00031231 5.0829e-06 INSTANT 0.875212000E-01 TIME STEP NUMBER 55410 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282883335E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.695264549E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.95201E-02 0.21124E+01 Friction velocity uk : 0.95201E-02 0.21124E+01 Dimensionless distance yplus : 0.91856E-02 0.20742E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -7.551380199e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29436E+08 1 0.19226E-09 0.24652E+02 0.19530E+04 c Velocity[X] 0.12465E+02 c Velocity[Y] 0.12187E+02 c Velocity[Z] 0.25960E-05 c Pressure 0.10888E-03 15 0.99008E-04 0.17324E-02 0.72295E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -15.222 24.982 5.6084 8.0004 v Velocity[Y] -16.737 18.272 -0.14324 -0.00067559 v Velocity[Z] -3.0589 2.9806 3.1833e-06 -5.386e-08 v ǁVelocityǁ 0.0017182 25.902 6.7464 8.0213 v Pressure -2.4483e+05 68016 -79818 -46043 v TurbVisc 1.6326e-21 0.0049712 0.00012496 8.4508e-06 v CourantNb 4.9488e-08 0.011775 0.00016674 4.8937e-06 v FourierNb 1.2425e-07 0.046923 0.00014558 1.893e-07 v total_pressure -1.435e+05 1.6934e+05 21507 55282 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0742 0.10188 0.0029478 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2191e-07 0.052152 0.00031231 5.083e-06 INSTANT 0.875213000E-01 TIME STEP NUMBER 55411 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282876226E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.695069909E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11008E-01 0.21115E+01 Friction velocity uk : 0.11008E-01 0.21115E+01 Dimensionless distance yplus : 0.10621E-01 0.20733E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -8.446667147e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29436E+08 1 0.19216E-09 0.24617E+02 0.19516E+04 c Velocity[X] 0.12447E+02 c Velocity[Y] 0.12170E+02 c Velocity[Z] 0.25841E-05 c Pressure 0.11122E-03 37 0.82883E-04 0.17679E-02 0.42007E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -15.24 25.003 5.6082 8.0002 v Velocity[Y] -16.756 18.288 -0.14323 -0.00067538 v Velocity[Z] -3.0588 2.9806 3.1823e-06 -5.386e-08 v ǁVelocityǁ 0.0018121 25.918 6.7477 8.0212 v Pressure -2.4435e+05 68502 -79453 -45858 v TurbVisc 3.9546e-22 0.0049712 0.00012504 8.4667e-06 v CourantNb 5.2786e-08 0.011775 0.00016674 4.8937e-06 v FourierNb 1.2425e-07 0.046917 0.00014558 1.8941e-07 v total_pressure -1.4303e+05 1.6983e+05 21872 55467 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0733 0.10191 0.0029475 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.219e-07 0.052144 0.00031232 5.0831e-06 INSTANT 0.875214000E-01 TIME STEP NUMBER 55412 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282869109E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.694868626E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.14062E-01 0.21105E+01 Friction velocity uk : 0.14062E-01 0.21105E+01 Dimensionless distance yplus : 0.13567E-01 0.20724E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -9.557086266e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29435E+08 1 0.19206E-09 0.24583E+02 0.19503E+04 c Velocity[X] 0.12428E+02 c Velocity[Y] 0.12155E+02 c Velocity[Z] 0.25725E-05 c Pressure 0.11361E-03 9 0.51882E-04 0.18042E-02 0.52490E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -15.258 25.023 5.6081 8.0001 v Velocity[Y] -16.776 18.304 -0.14322 -0.00067468 v Velocity[Z] -3.0588 2.9806 3.1813e-06 -5.386e-08 v ǁVelocityǁ 0.0019205 25.935 6.7491 8.0212 v Pressure -2.4378e+05 69056 -79021 -45637 v TurbVisc 1.8527e-22 0.0049712 0.00012512 8.4825e-06 v CourantNb 5.859e-08 0.011775 0.00016674 4.8936e-06 v FourierNb 1.2425e-07 0.046911 0.00014558 1.8952e-07 v total_pressure -1.4245e+05 1.7038e+05 22304 55688 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0724 0.10193 0.0029473 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2189e-07 0.052136 0.00031232 5.0832e-06 INSTANT 0.875215000E-01 TIME STEP NUMBER 55413 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282862027E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.694668458E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15300E-01 0.21096E+01 Friction velocity uk : 0.15300E-01 0.21096E+01 Dimensionless distance yplus : 0.14759E-01 0.20715E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.095443167e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29434E+08 1 0.19196E-09 0.24546E+02 0.19488E+04 c Velocity[X] 0.12408E+02 c Velocity[Y] 0.12138E+02 c Velocity[Z] 0.25566E-05 c Pressure 0.11691E-03 226 0.99989E-04 0.18548E-02 0.71355E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -15.275 25.044 5.6079 7.9999 v Velocity[Y] -16.796 18.32 -0.14321 -0.0006743 v Velocity[Z] -3.0587 2.9806 3.1803e-06 -5.3861e-08 v ǁVelocityǁ 0.002044 25.952 6.7504 8.0211 v Pressure -2.4311e+05 69676 -78505 -45326 v TurbVisc 3.2718e-22 0.0049712 0.0001252 8.4983e-06 v CourantNb 6.0842e-08 0.011775 0.00016674 4.8936e-06 v FourierNb 1.2425e-07 0.046905 0.00014559 1.8963e-07 v total_pressure -1.4179e+05 1.71e+05 22820 55999 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0715 0.10196 0.002947 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2188e-07 0.052129 0.00031233 5.0833e-06 INSTANT 0.875216000E-01 TIME STEP NUMBER 55414 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282855008E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.694469945E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.14318E-01 0.21087E+01 Friction velocity uk : 0.14318E-01 0.21087E+01 Dimensionless distance yplus : 0.13812E-01 0.20706E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.201149773e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29434E+08 1 0.19186E-09 0.24510E+02 0.19474E+04 c Velocity[X] 0.12389E+02 c Velocity[Y] 0.12121E+02 c Velocity[Z] 0.25377E-05 c Pressure 0.11985E-03 36 0.84531E-04 0.18997E-02 0.53863E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -15.293 25.064 5.6077 7.9998 v Velocity[Y] -16.815 18.336 -0.1432 -0.0006743 v Velocity[Z] -3.0587 2.9806 3.1793e-06 -5.3861e-08 v ǁVelocityǁ 0.0021828 25.968 6.7517 8.021 v Pressure -2.4236e+05 70361 -77988 -45084 v TurbVisc 4.8651e-22 0.0049712 0.00012528 8.5143e-06 v CourantNb 4.0456e-08 0.011776 0.00016674 4.8936e-06 v FourierNb 1.2425e-07 0.046899 0.00014559 1.8974e-07 v total_pressure -1.4104e+05 1.7169e+05 23337 56241 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0706 0.10197 0.0029466 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2186e-07 0.052121 0.00031233 5.0834e-06 INSTANT 0.875217000E-01 TIME STEP NUMBER 55415 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282848041E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.694262309E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.34028E-02 0.21079E+01 Friction velocity uk : 0.34028E-02 0.21079E+01 Dimensionless distance yplus : 0.34024E-02 0.20698E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.342038850e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29433E+08 1 0.19176E-09 0.24476E+02 0.19461E+04 c Velocity[X] 0.12370E+02 c Velocity[Y] 0.12106E+02 c Velocity[Z] 0.25178E-05 c Pressure 0.12264E-03 9 0.54479E-04 0.19419E-02 0.67388E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -15.31 25.085 5.6076 7.9997 v Velocity[Y] -16.834 18.352 -0.14319 -0.00067503 v Velocity[Z] -3.0586 2.9806 3.1783e-06 -5.3861e-08 v ǁVelocityǁ 0.002336 25.984 6.753 8.021 v Pressure -2.4153e+05 71109 -77420 -44792 v TurbVisc 1.3369e-22 0.0049712 0.00012536 8.5301e-06 v CourantNb 2.1491e-08 0.011776 0.00016674 4.8936e-06 v FourierNb 1.2425e-07 0.046894 0.00014559 1.8985e-07 v total_pressure -1.402e+05 1.7243e+05 23905 56533 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0698 0.10199 0.0029461 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2185e-07 0.052115 0.00031233 5.0835e-06 INSTANT 0.875218000E-01 TIME STEP NUMBER 55416 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282841172E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.694058753E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.99259E-02 0.21071E+01 Friction velocity uk : 0.99259E-02 0.21071E+01 Dimensionless distance yplus : 0.95814E-02 0.20690E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.488355348e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29432E+08 1 0.19166E-09 0.24440E+02 0.19446E+04 c Velocity[X] 0.12348E+02 c Velocity[Y] 0.12092E+02 c Velocity[Z] 0.24956E-05 c Pressure 0.12613E-03 641 0.77437E-04 0.19954E-02 0.12771E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -15.327 25.105 5.6074 7.9995 v Velocity[Y] -16.853 18.368 -0.14318 -0.00067406 v Velocity[Z] -3.0585 2.9806 3.1773e-06 -5.3861e-08 v ǁVelocityǁ 0.0025031 26.001 6.7543 8.0209 v Pressure -2.4061e+05 71914 -76723 -44288 v TurbVisc 1.1692e-21 0.0049713 0.00012544 8.5458e-06 v CourantNb 1.8469e-08 0.011776 0.00016674 4.8936e-06 v FourierNb 1.2425e-07 0.046888 0.00014559 1.8996e-07 v total_pressure -1.3929e+05 1.7324e+05 24602 57037 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.069 0.10201 0.0029456 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2184e-07 0.052108 0.00031234 5.0836e-06 INSTANT 0.875219000E-01 TIME STEP NUMBER 55417 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282834256E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.693859320E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.56606E-02 0.21064E+01 Friction velocity uk : 0.56606E-02 0.21064E+01 Dimensionless distance yplus : 0.56322E-02 0.20683E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.599097074e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29432E+08 1 0.19156E-09 0.24405E+02 0.19432E+04 c Velocity[X] 0.12329E+02 c Velocity[Y] 0.12075E+02 c Velocity[Z] 0.24708E-05 c Pressure 0.12953E-03 271 0.81742E-04 0.20472E-02 0.81273E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -15.345 25.125 5.6072 7.9994 v Velocity[Y] -16.872 18.384 -0.14317 -0.00067472 v Velocity[Z] -3.0585 2.9806 3.1763e-06 -5.3861e-08 v ǁVelocityǁ 0.00235 26.017 6.7557 8.0208 v Pressure -2.3963e+05 72771 -76088 -44036 v TurbVisc 8.2929e-22 0.0049713 0.00012552 8.5618e-06 v CourantNb 4.0446e-08 0.011776 0.00016674 4.8936e-06 v FourierNb 1.2425e-07 0.046883 0.0001456 1.9008e-07 v total_pressure -1.3831e+05 1.741e+05 25237 57289 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0683 0.10203 0.002945 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2183e-07 0.052102 0.00031234 5.0837e-06 INSTANT 0.875220000E-01 TIME STEP NUMBER 55418 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282827507E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.693644852E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.98189E-02 0.21057E+01 Friction velocity uk : 0.98189E-02 0.21057E+01 Dimensionless distance yplus : 0.94865E-02 0.20676E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.739236921e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29431E+08 1 0.19146E-09 0.24369E+02 0.19418E+04 c Velocity[X] 0.12308E+02 c Velocity[Y] 0.12061E+02 c Velocity[Z] 0.24439E-05 c Pressure 0.13280E-03 32 0.95463E-04 0.20969E-02 0.11894E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -15.362 25.146 5.6071 7.9992 v Velocity[Y] -16.891 18.4 -0.14316 -0.00067362 v Velocity[Z] -3.0584 2.9806 3.1753e-06 -5.3861e-08 v ǁVelocityǁ 0.0021801 26.034 6.757 8.0208 v Pressure -2.3858e+05 73679 -75366 -43608 v TurbVisc 2.0141e-22 0.0049713 0.0001256 8.5776e-06 v CourantNb 7.5033e-08 0.011776 0.00016674 4.8936e-06 v FourierNb 1.2425e-07 0.046879 0.0001456 1.9019e-07 v total_pressure -1.3726e+05 1.75e+05 25959 57717 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0676 0.10206 0.0029444 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2182e-07 0.052097 0.00031234 5.0838e-06 INSTANT 0.875221000E-01 TIME STEP NUMBER 55419 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282820720E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.693438960E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11712E-01 0.21051E+01 Friction velocity uk : 0.11712E-01 0.21051E+01 Dimensionless distance yplus : 0.11379E-01 0.20670E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.864298321e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29431E+08 1 0.19137E-09 0.24331E+02 0.19403E+04 c Velocity[X] 0.12288E+02 c Velocity[Y] 0.12043E+02 c Velocity[Z] 0.24157E-05 c Pressure 0.13606E-03 201 0.80566E-04 0.21464E-02 0.96526E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -15.379 25.166 5.6069 7.9991 v Velocity[Y] -16.91 18.416 -0.14315 -0.00067368 v Velocity[Z] -3.0584 2.9806 3.1743e-06 -5.3861e-08 v ǁVelocityǁ 0.0020173 26.05 6.7583 8.0207 v Pressure -2.3747e+05 74635 -74601 -43227 v TurbVisc 7.2835e-23 0.0049713 0.00012568 8.5936e-06 v CourantNb 5.5192e-08 0.011776 0.00016674 4.8936e-06 v FourierNb 1.2425e-07 0.046875 0.0001456 1.903e-07 v total_pressure -1.3614e+05 1.7596e+05 26724 58098 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.067 0.10208 0.0029437 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2181e-07 0.052092 0.00031234 5.0839e-06 INSTANT 0.875222000E-01 TIME STEP NUMBER 55420 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282814057E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.693233491E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15292E-01 0.21045E+01 Friction velocity uk : 0.15292E-01 0.21045E+01 Dimensionless distance yplus : 0.14752E-01 0.20664E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.974920984e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29430E+08 1 0.19127E-09 0.24297E+02 0.19389E+04 c Velocity[X] 0.12268E+02 c Velocity[Y] 0.12028E+02 c Velocity[Z] 0.23913E-05 c Pressure 0.13820E-03 9 0.56198E-04 0.21782E-02 0.89976E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -15.396 25.186 5.6067 7.999 v Velocity[Y] -16.928 18.432 -0.14314 -0.00067421 v Velocity[Z] -3.0583 2.9806 3.1733e-06 -5.3861e-08 v ǁVelocityǁ 0.0018642 26.067 6.7596 8.0206 v Pressure -2.3631e+05 75630 -73827 -42833 v TurbVisc 2.9564e-22 0.0049713 0.00012576 8.6095e-06 v CourantNb 3.0963e-08 0.011776 0.00016674 4.8936e-06 v FourierNb 1.2425e-07 0.046872 0.0001456 1.9041e-07 v total_pressure -1.3498e+05 1.7696e+05 27498 58492 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0664 0.1021 0.0029429 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.218e-07 0.052088 0.00031235 5.084e-06 INSTANT 0.875223000E-01 TIME STEP NUMBER 55421 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282807538E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.693028431E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10396E-01 0.21040E+01 Friction velocity uk : 0.10396E-01 0.21040E+01 Dimensionless distance yplus : 0.10239E-01 0.20660E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -2.079111573e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29430E+08 1 0.19117E-09 0.24261E+02 0.19375E+04 c Velocity[X] 0.12246E+02 c Velocity[Y] 0.12014E+02 c Velocity[Z] 0.23625E-05 c Pressure 0.14143E-03 31 0.76098E-04 0.22269E-02 0.15997E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -15.413 25.206 5.6066 7.9988 v Velocity[Y] -16.947 18.448 -0.14312 -0.00067323 v Velocity[Z] -3.0582 2.9806 3.1724e-06 -5.3861e-08 v ǁVelocityǁ 0.0017257 26.084 6.7609 8.0206 v Pressure -2.351e+05 76660 -72898 -42205 v TurbVisc 1.1687e-21 0.0049713 0.00012584 8.6252e-06 v CourantNb 2.0472e-08 0.011777 0.00016674 4.8936e-06 v FourierNb 1.2425e-07 0.046869 0.00014561 1.9052e-07 v total_pressure -1.3378e+05 1.7798e+05 28427 59120 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.066 0.10211 0.002942 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2179e-07 0.052084 0.00031235 5.0841e-06 INSTANT 0.875224000E-01 TIME STEP NUMBER 55422 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282800955E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.692831689E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.14910E-01 0.21036E+01 Friction velocity uk : 0.14910E-01 0.21036E+01 Dimensionless distance yplus : 0.14384E-01 0.20655E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -2.148188016e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29429E+08 1 0.19108E-09 0.24226E+02 0.19361E+04 c Velocity[X] 0.12227E+02 c Velocity[Y] 0.11999E+02 c Velocity[Z] 0.23325E-05 c Pressure 0.14471E-03 559 0.80696E-04 0.22764E-02 0.11261E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -15.429 25.226 5.6064 7.9987 v Velocity[Y] -16.965 18.465 -0.14311 -0.00067399 v Velocity[Z] -3.0582 2.9806 3.1714e-06 -5.3861e-08 v ǁVelocityǁ 0.0016105 26.1 6.7622 8.0205 v Pressure -2.3386e+05 77717 -72033 -41805 v TurbVisc 3.4051e-22 0.0049714 0.00012591 8.6413e-06 v CourantNb 1.6149e-08 0.011777 0.00016674 4.8936e-06 v FourierNb 1.2425e-07 0.046867 0.00014561 1.9063e-07 v total_pressure -1.3253e+05 1.7904e+05 29292 59520 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0655 0.10213 0.0029409 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2178e-07 0.052081 0.00031235 5.0842e-06 INSTANT 0.875225000E-01 TIME STEP NUMBER 55423 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282794550E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.692620781E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13032E-01 0.21032E+01 Friction velocity uk : 0.13032E-01 0.21032E+01 Dimensionless distance yplus : 0.12674E-01 0.20652E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -2.220494757e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29428E+08 1 0.19098E-09 0.24192E+02 0.19347E+04 c Velocity[X] 0.12205E+02 c Velocity[Y] 0.11986E+02 c Velocity[Z] 0.23035E-05 c Pressure 0.14779E-03 34 0.94202E-04 0.23227E-02 0.15397E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -15.446 25.246 5.6063 7.9986 v Velocity[Y] -16.984 18.481 -0.1431 -0.00067277 v Velocity[Z] -3.0581 2.9806 3.1704e-06 -5.3861e-08 v ǁVelocityǁ 0.0015194 26.117 6.7635 8.0205 v Pressure -2.3258e+05 78805 -71096 -41234 v TurbVisc 5.7636e-22 0.0049714 0.00012599 8.6572e-06 v CourantNb 3.2215e-08 0.011777 0.00016674 4.8935e-06 v FourierNb 1.2425e-07 0.046865 0.00014561 1.9074e-07 v total_pressure -1.3126e+05 1.8013e+05 30229 60091 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0652 0.10213 0.0029398 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2177e-07 0.052079 0.00031235 5.0843e-06 INSTANT 0.875226000E-01 TIME STEP NUMBER 55424 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282788149E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.692420989E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12900E-01 0.21029E+01 Friction velocity uk : 0.12900E-01 0.21029E+01 Dimensionless distance yplus : 0.12442E-01 0.20649E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -2.266484145e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29428E+08 1 0.19089E-09 0.24154E+02 0.19332E+04 c Velocity[X] 0.12185E+02 c Velocity[Y] 0.11968E+02 c Velocity[Z] 0.22756E-05 c Pressure 0.15088E-03 183 0.79474E-04 0.23691E-02 0.12603E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -15.463 25.265 5.6061 7.9984 v Velocity[Y] -17.002 18.497 -0.14309 -0.00067282 v Velocity[Z] -3.058 2.9806 3.1694e-06 -5.3861e-08 v ǁVelocityǁ 0.0014598 26.134 6.7648 8.0204 v Pressure -2.3128e+05 79917 -70124 -40749 v TurbVisc 8.947e-22 0.0049714 0.00012607 8.6732e-06 v CourantNb 2.8833e-08 0.011777 0.00016674 4.8935e-06 v FourierNb 1.2425e-07 0.046864 0.00014561 1.9086e-07 v total_pressure -1.2995e+05 1.8124e+05 31201 60576 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0649 0.10214 0.0029386 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2176e-07 0.052077 0.00031235 5.0844e-06 INSTANT 0.875227000E-01 TIME STEP NUMBER 55425 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282781871E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.692225164E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.87824E-02 0.21027E+01 Friction velocity uk : 0.87824E-02 0.21027E+01 Dimensionless distance yplus : 0.84740E-02 0.20647E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -2.290397103e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29427E+08 1 0.19080E-09 0.24120E+02 0.19319E+04 c Velocity[X] 0.12165E+02 c Velocity[Y] 0.11955E+02 c Velocity[Z] 0.22501E-05 c Pressure 0.15302E-03 10 0.57007E-04 0.24005E-02 0.12361E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -15.48 25.285 5.606 7.9983 v Velocity[Y] -17.02 18.514 -0.14308 -0.00067335 v Velocity[Z] -3.058 2.9806 3.1684e-06 -5.3861e-08 v ǁVelocityǁ 0.0014348 26.151 6.7662 8.0204 v Pressure -2.2995e+05 81048 -69130 -40231 v TurbVisc 1.6776e-21 0.0049714 0.00012615 8.6892e-06 v CourantNb 2.2147e-08 0.011777 0.00016674 4.8935e-06 v FourierNb 1.2425e-07 0.046863 0.00014561 1.9097e-07 v total_pressure -1.2862e+05 1.8237e+05 32195 61094 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0647 0.10214 0.0029373 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2174e-07 0.052076 0.00031235 5.0845e-06 INSTANT 0.875228000E-01 TIME STEP NUMBER 55426 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282775779E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.692033258E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.42299E-02 0.21025E+01 Friction velocity uk : 0.42299E-02 0.21025E+01 Dimensionless distance yplus : 0.40822E-02 0.20645E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -2.283992154e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29427E+08 1 0.19070E-09 0.24084E+02 0.19304E+04 c Velocity[X] 0.12144E+02 c Velocity[Y] 0.11940E+02 c Velocity[Z] 0.22291E-05 c Pressure 0.15620E-03 28 0.99355E-04 0.24481E-02 0.16950E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -15.496 25.305 5.6058 7.9982 v Velocity[Y] -17.038 18.531 -0.14306 -0.00067327 v Velocity[Z] -3.0579 2.9806 3.1674e-06 -5.3861e-08 v ǁVelocityǁ 0.0011897 26.168 6.7675 8.0203 v Pressure -2.2861e+05 82192 -68050 -39564 v TurbVisc 2.28e-21 0.0049714 0.00012622 8.705e-06 v CourantNb 5.0174e-08 0.011777 0.00016674 4.8935e-06 v FourierNb 1.2425e-07 0.046863 0.00014561 1.9108e-07 v total_pressure -1.2728e+05 1.8352e+05 33275 61761 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0645 0.10215 0.0029362 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2173e-07 0.052076 0.00031235 5.0846e-06 INSTANT 0.875229000E-01 TIME STEP NUMBER 55427 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282769678E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.691850737E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10580E-01 0.21024E+01 Friction velocity uk : 0.10580E-01 0.21024E+01 Dimensionless distance yplus : 0.10211E-01 0.20644E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -2.265958095e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29426E+08 1 0.19061E-09 0.24049E+02 0.19290E+04 c Velocity[X] 0.12123E+02 c Velocity[Y] 0.11926E+02 c Velocity[Z] 0.22067E-05 c Pressure 0.15919E-03 388 0.83404E-04 0.24926E-02 0.16472E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -15.513 25.324 5.6057 7.9981 v Velocity[Y] -17.057 18.547 -0.14305 -0.0006731 v Velocity[Z] -3.0579 2.9806 3.1664e-06 -5.3861e-08 v ǁVelocityǁ 0.00090956 26.186 6.7688 8.0203 v Pressure -2.2725e+05 83346 -66944 -38907 v TurbVisc 2.2743e-21 0.0049714 0.0001263 8.7212e-06 v CourantNb 4.4124e-08 0.011777 0.00016674 4.8935e-06 v FourierNb 1.2425e-07 0.046863 0.00014561 1.9119e-07 v total_pressure -1.2593e+05 1.8467e+05 34381 62418 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0644 0.10216 0.002935 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2173e-07 0.052076 0.00031235 5.0847e-06 INSTANT 0.875230000E-01 TIME STEP NUMBER 55428 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282763678E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.691663828E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13668E-01 0.21023E+01 Friction velocity uk : 0.13668E-01 0.21023E+01 Dimensionless distance yplus : 0.13482E-01 0.20643E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -2.220733930e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29426E+08 1 0.19052E-09 0.24016E+02 0.19277E+04 c Velocity[X] 0.12103E+02 c Velocity[Y] 0.11914E+02 c Velocity[Z] 0.21854E-05 c Pressure 0.16198E-03 10 0.56305E-04 0.25340E-02 0.15478E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -15.529 25.343 5.6056 7.998 v Velocity[Y] -17.075 18.564 -0.14304 -0.00067227 v Velocity[Z] -3.0578 2.9806 3.1654e-06 -5.3861e-08 v ǁVelocityǁ 0.00067313 26.203 6.7701 8.0202 v Pressure -2.2589e+05 84512 -65806 -38300 v TurbVisc 2.7914e-21 0.0049715 0.00012638 8.7372e-06 v CourantNb 6.8139e-08 0.011777 0.00016674 4.8935e-06 v FourierNb 1.2425e-07 0.046863 0.00014562 1.913e-07 v total_pressure -1.2456e+05 1.8584e+05 35519 63025 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0643 0.10216 0.0029337 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2172e-07 0.052076 0.00031235 5.0848e-06 INSTANT 0.875231000E-01 TIME STEP NUMBER 55429 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282757784E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.691485779E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10425E-01 0.21023E+01 Friction velocity uk : 0.10425E-01 0.21023E+01 Dimensionless distance yplus : 0.10284E-01 0.20642E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -2.129862696e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29425E+08 1 0.19043E-09 0.23982E+02 0.19263E+04 c Velocity[X] 0.12082E+02 c Velocity[Y] 0.11900E+02 c Velocity[Z] 0.21691E-05 c Pressure 0.16535E-03 262 0.75840E-04 0.25844E-02 0.18711E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -15.546 25.363 5.6054 7.9978 v Velocity[Y] -17.093 18.581 -0.14303 -0.00067273 v Velocity[Z] -3.0577 2.9806 3.1644e-06 -5.3861e-08 v ǁVelocityǁ 0.00053613 26.22 6.7714 8.0202 v Pressure -2.2452e+05 85687 -64655 -37641 v TurbVisc 2.9993e-21 0.0049715 0.00012645 8.7532e-06 v CourantNb 3.8434e-08 0.011778 0.00016674 4.8935e-06 v FourierNb 1.2425e-07 0.046863 0.00014562 1.9142e-07 v total_pressure -1.2319e+05 1.8701e+05 36670 63684 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0642 0.10216 0.0029324 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2171e-07 0.052076 0.00031235 5.085e-06 INSTANT 0.875232000E-01 TIME STEP NUMBER 55430 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282751978E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.691315333E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.92147E-02 0.21022E+01 Friction velocity uk : 0.92147E-02 0.21022E+01 Dimensionless distance yplus : 0.89023E-02 0.20642E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -2.059774255e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29425E+08 1 0.19034E-09 0.23948E+02 0.19250E+04 c Velocity[X] 0.12061E+02 c Velocity[Y] 0.11887E+02 c Velocity[Z] 0.21527E-05 c Pressure 0.16850E-03 59 0.80666E-04 0.26311E-02 0.20445E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -15.562 25.382 5.6053 7.9977 v Velocity[Y] -17.111 18.598 -0.14303 -0.00067181 v Velocity[Z] -3.0577 2.9806 3.1634e-06 -5.3861e-08 v ǁVelocityǁ 0.00053766 26.238 6.7728 8.0201 v Pressure -2.2313e+05 86868 -63431 -36902 v TurbVisc 1.9715e-21 0.0049715 0.00012653 8.7693e-06 v CourantNb 8.5129e-08 0.011778 0.00016674 4.8935e-06 v FourierNb 1.2425e-07 0.046864 0.00014562 1.9153e-07 v total_pressure -1.2181e+05 1.8819e+05 37894 64423 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0642 0.10216 0.0029312 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.217e-07 0.052077 0.00031235 5.0851e-06 INSTANT 0.875233000E-01 TIME STEP NUMBER 55431 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282746245E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.691148620E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13699E-01 0.21022E+01 Friction velocity uk : 0.13699E-01 0.21022E+01 Dimensionless distance yplus : 0.13221E-01 0.20642E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.933855166e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29424E+08 1 0.19025E-09 0.23915E+02 0.19236E+04 c Velocity[X] 0.12042E+02 c Velocity[Y] 0.11873E+02 c Velocity[Z] 0.21398E-05 c Pressure 0.17172E-03 199 0.93328E-04 0.26790E-02 0.18309E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -15.579 25.401 5.6052 7.9976 v Velocity[Y] -17.13 18.615 -0.14302 -0.00067262 v Velocity[Z] -3.0576 2.9806 3.1624e-06 -5.3861e-08 v ǁVelocityǁ 0.00055024 26.255 6.7741 8.0201 v Pressure -2.2174e+05 88060 -62208 -36282 v TurbVisc 1.2346e-21 0.0049715 0.00012661 8.7854e-06 v CourantNb 9.1338e-08 0.011778 0.00016673 4.8935e-06 v FourierNb 1.2425e-07 0.046865 0.00014562 1.9164e-07 v total_pressure -1.2042e+05 1.8939e+05 39117 65043 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0642 0.10215 0.0029299 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2169e-07 0.052078 0.00031235 5.0852e-06 INSTANT 0.875234000E-01 TIME STEP NUMBER 55432 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282740733E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.690990050E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.72097E-02 0.21022E+01 Friction velocity uk : 0.72097E-02 0.21022E+01 Dimensionless distance yplus : 0.69645E-02 0.20642E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.792986100e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29424E+08 1 0.19016E-09 0.23878E+02 0.19222E+04 c Velocity[X] 0.12021E+02 c Velocity[Y] 0.11858E+02 c Velocity[Z] 0.21304E-05 c Pressure 0.17493E-03 81 0.79420E-04 0.27265E-02 0.22134E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -15.595 25.42 5.6051 7.9975 v Velocity[Y] -17.148 18.631 -0.14301 -0.00067241 v Velocity[Z] -3.0575 2.9806 3.1614e-06 -5.3861e-08 v ǁVelocityǁ 0.00052971 26.273 6.7754 8.02 v Pressure -2.2034e+05 89263 -60923 -35488 v TurbVisc 1.3587e-21 0.0049715 0.00012668 8.8015e-06 v CourantNb 9.8704e-08 0.011778 0.00016673 4.8936e-06 v FourierNb 1.2425e-07 0.046866 0.00014562 1.9175e-07 v total_pressure -1.1902e+05 1.9059e+05 40402 65837 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0642 0.10215 0.0029287 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2168e-07 0.052079 0.00031235 5.0853e-06 INSTANT 0.875235000E-01 TIME STEP NUMBER 55433 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282735264E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.690840220E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12275E-01 0.21022E+01 Friction velocity uk : 0.12275E-01 0.21022E+01 Dimensionless distance yplus : 0.11889E-01 0.20642E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.636069131e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29423E+08 1 0.19008E-09 0.23846E+02 0.19209E+04 c Velocity[X] 0.12001E+02 c Velocity[Y] 0.11845E+02 c Velocity[Z] 0.21233E-05 c Pressure 0.17730E-03 10 0.59707E-04 0.27609E-02 0.18869E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -15.611 25.439 5.605 7.9974 v Velocity[Y] -17.166 18.648 -0.143 -0.00067171 v Velocity[Z] -3.0575 2.9806 3.1604e-06 -5.3861e-08 v ǁVelocityǁ 0.00051991 26.29 6.7768 8.02 v Pressure -2.1893e+05 90471 -59607 -34807 v TurbVisc 1.6931e-21 0.0049715 0.00012676 8.8176e-06 v CourantNb 9.7645e-08 0.011778 0.00016673 4.8936e-06 v FourierNb 1.2425e-07 0.046867 0.00014562 1.9187e-07 v total_pressure -1.176e+05 1.918e+05 41718 66518 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0642 0.10214 0.0029275 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2167e-07 0.05208 0.00031235 5.0854e-06 INSTANT 0.875236000E-01 TIME STEP NUMBER 55434 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282729954E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.690698195E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.56763E-02 0.21022E+01 Friction velocity uk : 0.56763E-02 0.21022E+01 Dimensionless distance yplus : 0.54833E-02 0.20641E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.437704404e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29423E+08 1 0.18999E-09 0.23813E+02 0.19195E+04 c Velocity[X] 0.11981E+02 c Velocity[Y] 0.11832E+02 c Velocity[Z] 0.21200E-05 c Pressure 0.18072E-03 130 0.75448E-04 0.28116E-02 0.24512E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -15.628 25.458 5.6049 7.9973 v Velocity[Y] -17.185 18.665 -0.143 -0.00067224 v Velocity[Z] -3.0574 2.9806 3.1595e-06 -5.3861e-08 v ǁVelocityǁ 0.00052062 26.307 6.7781 8.02 v Pressure -2.175e+05 91691 -58302 -34004 v TurbVisc 2.6567e-21 0.0049716 0.00012683 8.8337e-06 v CourantNb 8.6913e-08 0.011778 0.00016673 4.8936e-06 v FourierNb 1.2425e-07 0.046868 0.00014562 1.9198e-07 v total_pressure -1.1618e+05 1.9302e+05 43023 67321 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0641 0.10214 0.0029264 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2166e-07 0.052081 0.00031236 5.0856e-06 INSTANT 0.875237000E-01 TIME STEP NUMBER 55435 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282724713E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.690560672E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.72445E-02 0.21022E+01 Friction velocity uk : 0.72445E-02 0.21022E+01 Dimensionless distance yplus : 0.71698E-02 0.20641E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.283655038e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29422E+08 1 0.18990E-09 0.23781E+02 0.19182E+04 c Velocity[X] 0.11961E+02 c Velocity[Y] 0.11820E+02 c Velocity[Z] 0.21159E-05 c Pressure 0.18363E-03 29 0.81471E-04 0.28544E-02 0.26058E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -15.644 25.477 5.6048 7.9972 v Velocity[Y] -17.203 18.682 -0.14299 -0.00067136 v Velocity[Z] -3.0573 2.9805 3.1585e-06 -5.3861e-08 v ǁVelocityǁ 0.00052696 26.325 6.7795 8.0199 v Pressure -2.1607e+05 92920 -56884 -33141 v TurbVisc 1.6243e-21 0.0049716 0.00012691 8.8499e-06 v CourantNb 7.8038e-08 0.011778 0.00016674 4.8936e-06 v FourierNb 1.2425e-07 0.046869 0.00014562 1.9209e-07 v total_pressure -1.1474e+05 1.9424e+05 44441 68184 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0641 0.10214 0.0029256 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2165e-07 0.052082 0.00031236 5.0857e-06 INSTANT 0.875238000E-01 TIME STEP NUMBER 55436 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282719565E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.690435996E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11729E-01 0.21021E+01 Friction velocity uk : 0.11729E-01 0.21021E+01 Dimensionless distance yplus : 0.11324E-01 0.20641E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.074979456e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29422E+08 1 0.18982E-09 0.23750E+02 0.19170E+04 c Velocity[X] 0.11943E+02 c Velocity[Y] 0.11807E+02 c Velocity[Z] 0.21154E-05 c Pressure 0.18677E-03 342 0.94140E-04 0.29005E-02 0.23200E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -15.66 25.496 5.6047 7.9971 v Velocity[Y] -17.221 18.699 -0.14299 -0.00067227 v Velocity[Z] -3.0573 2.9805 3.1575e-06 -5.3861e-08 v ǁVelocityǁ 0.00056544 26.342 6.7808 8.0199 v Pressure -2.1461e+05 94168 -55491 -32418 v TurbVisc 1.8075e-21 0.0049716 0.00012698 8.8662e-06 v CourantNb 6.9612e-08 0.011778 0.00016674 4.8936e-06 v FourierNb 1.2425e-07 0.046869 0.00014562 1.922e-07 v total_pressure -1.1328e+05 1.9549e+05 45834 68907 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0641 0.10214 0.0029247 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2164e-07 0.052083 0.00031236 5.0858e-06 INSTANT 0.875239000E-01 TIME STEP NUMBER 55437 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282714653E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.690312005E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10187E-01 0.21020E+01 Friction velocity uk : 0.10187E-01 0.21020E+01 Dimensionless distance yplus : 0.98348E-02 0.20640E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -8.641656993e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29421E+08 1 0.18973E-09 0.23715E+02 0.19156E+04 c Velocity[X] 0.11923E+02 c Velocity[Y] 0.11792E+02 c Velocity[Z] 0.21186E-05 c Pressure 0.18979E-03 90 0.80216E-04 0.29446E-02 0.27732E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -15.677 25.515 5.6047 7.997 v Velocity[Y] -17.24 18.715 -0.14299 -0.00067212 v Velocity[Z] -3.0572 2.9805 3.1565e-06 -5.3861e-08 v ǁVelocityǁ 0.00064109 26.359 6.7822 8.0199 v Pressure -2.1312e+05 95438 -54041 -31521 v TurbVisc 1.9109e-21 0.0049716 0.00012706 8.8824e-06 v CourantNb 5.9694e-08 0.011778 0.00016674 4.8936e-06 v FourierNb 1.2425e-07 0.04687 0.00014562 1.9232e-07 v total_pressure -1.118e+05 1.9676e+05 47284 69804 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.064 0.10213 0.002924 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2164e-07 0.052083 0.00031236 5.0859e-06 INSTANT 0.875240000E-01 TIME STEP NUMBER 55438 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282709799E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.690198751E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12751E-01 0.21019E+01 Friction velocity uk : 0.12751E-01 0.21019E+01 Dimensionless distance yplus : 0.12310E-01 0.20639E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -6.541403764e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29421E+08 1 0.18965E-09 0.23686E+02 0.19144E+04 c Velocity[X] 0.11905E+02 c Velocity[Y] 0.11781E+02 c Velocity[Z] 0.21232E-05 c Pressure 0.19194E-03 10 0.61971E-04 0.29754E-02 0.23902E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -15.693 25.534 5.6046 7.9969 v Velocity[Y] -17.258 18.732 -0.14299 -0.00067149 v Velocity[Z] -3.0571 2.9805 3.1555e-06 -5.3861e-08 v ǁVelocityǁ 0.00072949 26.377 6.7836 8.0199 v Pressure -2.1161e+05 96731 -52553 -30748 v TurbVisc 1.3738e-21 0.0049716 0.00012713 8.8986e-06 v CourantNb 4.913e-08 0.011778 0.00016674 4.8936e-06 v FourierNb 1.2425e-07 0.04687 0.00014562 1.9243e-07 v total_pressure -1.1028e+05 1.9806e+05 48772 70577 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0639 0.10213 0.0029233 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2163e-07 0.052083 0.00031236 5.0861e-06 INSTANT 0.875241000E-01 TIME STEP NUMBER 55439 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282705128E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.690094077E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.17168E-01 0.21018E+01 Friction velocity uk : 0.17168E-01 0.21018E+01 Dimensionless distance yplus : 0.16575E-01 0.20638E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -4.135811517e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29420E+08 1 0.18956E-09 0.23655E+02 0.19131E+04 c Velocity[X] 0.11886E+02 c Velocity[Y] 0.11769E+02 c Velocity[Z] 0.21305E-05 c Pressure 0.19511E-03 137 0.76405E-04 0.30217E-02 0.30877E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -15.709 25.553 5.6046 7.9968 v Velocity[Y] -17.276 18.748 -0.14299 -0.00067209 v Velocity[Z] -3.0571 2.9805 3.1545e-06 -5.3861e-08 v ǁVelocityǁ 0.00079975 26.394 6.785 8.0198 v Pressure -2.1007e+05 98053 -51106 -29843 v TurbVisc 2.2373e-21 0.0049716 0.00012721 8.9148e-06 v CourantNb 3.6116e-08 0.011778 0.00016674 4.8936e-06 v FourierNb 1.2425e-07 0.04687 0.00014562 1.9254e-07 v total_pressure -1.0874e+05 1.9938e+05 50219 71482 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0638 0.10213 0.0029228 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2162e-07 0.052082 0.00031236 5.0862e-06 INSTANT 0.875242000E-01 TIME STEP NUMBER 55440 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282700526E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.689992540E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.16996E-01 0.21016E+01 Friction velocity uk : 0.16996E-01 0.21016E+01 Dimensionless distance yplus : 0.16392E-01 0.20636E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -2.444226655e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29420E+08 1 0.18948E-09 0.23626E+02 0.19119E+04 c Velocity[X] 0.11868E+02 c Velocity[Y] 0.11758E+02 c Velocity[Z] 0.21349E-05 c Pressure 0.19763E-03 30 0.82457E-04 0.30580E-02 0.32508E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -15.726 25.572 5.6045 7.9967 v Velocity[Y] -17.295 18.764 -0.14299 -0.00067127 v Velocity[Z] -3.057 2.9805 3.1535e-06 -5.3861e-08 v ǁVelocityǁ 0.00086377 26.41 6.7864 8.0198 v Pressure -2.0849e+05 99402 -49522 -28884 v TurbVisc 1.6376e-21 0.0049717 0.00012728 8.9311e-06 v CourantNb 2.452e-08 0.011778 0.00016674 4.8937e-06 v FourierNb 1.2425e-07 0.046869 0.00014562 1.9266e-07 v total_pressure -1.0716e+05 2.0073e+05 51803 72441 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0636 0.10212 0.0029224 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2161e-07 0.052082 0.00031236 5.0863e-06 INSTANT 0.875243000E-01 TIME STEP NUMBER 55441 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282696035E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.689907934E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12815E-01 0.21014E+01 Friction velocity uk : 0.12815E-01 0.21014E+01 Dimensionless distance yplus : 0.12360E-01 0.20634E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -2.802280815e-03 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29420E+08 1 0.18940E-09 0.23598E+02 0.19108E+04 c Velocity[X] 0.11851E+02 c Velocity[Y] 0.11747E+02 c Velocity[Z] 0.21433E-05 c Pressure 0.20046E-03 217 0.95249E-04 0.30990E-02 0.28996E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -15.742 25.591 5.6045 7.9966 v Velocity[Y] -17.313 18.781 -0.14299 -0.00067226 v Velocity[Z] -3.057 2.9805 3.1525e-06 -5.3861e-08 v ǁVelocityǁ 0.00091096 26.427 6.7877 8.0198 v Pressure -2.0694e+05 1.0079e+05 -47975 -28079 v TurbVisc 1.8898e-21 0.0049717 0.00012735 8.9475e-06 v CourantNb 2.382e-08 0.011778 0.00016674 4.8937e-06 v FourierNb 1.2425e-07 0.046869 0.00014562 1.9277e-07 v total_pressure -1.0562e+05 2.0211e+05 53350 73246 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0634 0.10211 0.002922 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2161e-07 0.052081 0.00031237 5.0865e-06 INSTANT 0.875244000E-01 TIME STEP NUMBER 55442 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282691802E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.689820539E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.93147E-02 0.21012E+01 Friction velocity uk : 0.93147E-02 0.21012E+01 Dimensionless distance yplus : 0.89837E-02 0.20632E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.719036267e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29419E+08 1 0.18932E-09 0.23567E+02 0.19095E+04 c Velocity[X] 0.11834E+02 c Velocity[Y] 0.11733E+02 c Velocity[Z] 0.21522E-05 c Pressure 0.20315E-03 132 0.81129E-04 0.31377E-02 0.34790E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -15.758 25.61 5.6045 7.9965 v Velocity[Y] -17.331 18.797 -0.14299 -0.00067219 v Velocity[Z] -3.0569 2.9805 3.1516e-06 -5.3861e-08 v ǁVelocityǁ 0.00094097 26.444 6.7891 8.0198 v Pressure -2.0541e+05 1.0222e+05 -46372 -27092 v TurbVisc 1.9038e-21 0.0049717 0.00012743 8.9638e-06 v CourantNb 4.0847e-08 0.011778 0.00016674 4.8937e-06 v FourierNb 1.2425e-07 0.046868 0.00014563 1.9289e-07 v total_pressure -1.0408e+05 2.0354e+05 54953 74233 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0632 0.10211 0.0029218 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.216e-07 0.05208 0.00031237 5.0866e-06 INSTANT 0.875245000E-01 TIME STEP NUMBER 55443 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282687633E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.689744121E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.68435E-02 0.21010E+01 Friction velocity uk : 0.68435E-02 0.21010E+01 Dimensionless distance yplus : 0.66004E-02 0.20630E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 3.527874471e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29419E+08 1 0.18924E-09 0.23540E+02 0.19084E+04 c Velocity[X] 0.11817E+02 c Velocity[Y] 0.11723E+02 c Velocity[Z] 0.21626E-05 c Pressure 0.20503E-03 10 0.63780E-04 0.31639E-02 0.30092E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -15.774 25.629 5.6044 7.9964 v Velocity[Y] -17.349 18.812 -0.143 -0.00067162 v Velocity[Z] -3.0568 2.9805 3.1506e-06 -5.3861e-08 v ǁVelocityǁ 0.00095674 26.46 6.7906 8.0198 v Pressure -2.0381e+05 1.0369e+05 -44742 -26243 v TurbVisc 2.1229e-21 0.0049717 0.0001275 8.9801e-06 v CourantNb 4.9642e-08 0.011778 0.00016675 4.8937e-06 v FourierNb 1.2425e-07 0.046867 0.00014563 1.93e-07 v total_pressure -1.0249e+05 2.0501e+05 56583 75082 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.063 0.1021 0.0029216 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2159e-07 0.052079 0.00031237 5.0867e-06 INSTANT 0.875246000E-01 TIME STEP NUMBER 55444 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282683670E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.689675740E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.61321E-02 0.21007E+01 Friction velocity uk : 0.61321E-02 0.21007E+01 Dimensionless distance yplus : 0.60690E-02 0.20627E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 5.465697662e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29419E+08 1 0.18916E-09 0.23513E+02 0.19073E+04 c Velocity[X] 0.11801E+02 c Velocity[Y] 0.11712E+02 c Velocity[Z] 0.21735E-05 c Pressure 0.20786E-03 443 0.77395E-04 0.32047E-02 0.39240E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -15.79 25.648 5.6044 7.9964 v Velocity[Y] -17.368 18.828 -0.143 -0.00067243 v Velocity[Z] -3.0568 2.9805 3.1496e-06 -5.3861e-08 v ǁVelocityǁ 0.00094224 26.477 6.792 8.0198 v Pressure -2.0216e+05 1.0521e+05 -43136 -25246 v TurbVisc 3.5999e-21 0.0049717 0.00012757 8.9965e-06 v CourantNb 6.5142e-08 0.011778 0.00016675 4.8938e-06 v FourierNb 1.2425e-07 0.046866 0.00014563 1.9311e-07 v total_pressure -1.0084e+05 2.0653e+05 58189 76079 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0627 0.1021 0.0029216 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2159e-07 0.052077 0.00031238 5.0869e-06 INSTANT 0.875247000E-01 TIME STEP NUMBER 55445 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282679773E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.689611676E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.16442E-01 0.21004E+01 Friction velocity uk : 0.16442E-01 0.21004E+01 Dimensionless distance yplus : 0.15858E-01 0.20624E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 6.607492822e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29418E+08 1 0.18908E-09 0.23488E+02 0.19063E+04 c Velocity[X] 0.11785E+02 c Velocity[Y] 0.11703E+02 c Velocity[Z] 0.21789E-05 c Pressure 0.21020E-03 30 0.83632E-04 0.32379E-02 0.40347E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -15.806 25.668 5.6044 7.9963 v Velocity[Y] -17.386 18.844 -0.14301 -0.00067153 v Velocity[Z] -3.0567 2.9805 3.1486e-06 -5.3861e-08 v ǁVelocityǁ 0.00091906 26.493 6.7934 8.0198 v Pressure -2.0045e+05 1.0677e+05 -41417 -24220 v TurbVisc 2.0547e-21 0.0049717 0.00012765 9.0129e-06 v CourantNb 7.8548e-08 0.011778 0.00016675 4.8938e-06 v FourierNb 1.2425e-07 0.046865 0.00014563 1.9323e-07 v total_pressure -99126 2.0809e+05 59908 77105 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0624 0.10209 0.0029216 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2158e-07 0.052076 0.00031238 5.087e-06 INSTANT 0.875248000E-01 TIME STEP NUMBER 55446 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282676007E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.689560088E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.16649E-01 0.21001E+01 Friction velocity uk : 0.16649E-01 0.21001E+01 Dimensionless distance yplus : 0.16191E-01 0.20621E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 8.011371679e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29418E+08 1 0.18901E-09 0.23463E+02 0.19052E+04 c Velocity[X] 0.11770E+02 c Velocity[Y] 0.11693E+02 c Velocity[Z] 0.21879E-05 c Pressure 0.21278E-03 222 0.96513E-04 0.32746E-02 0.36727E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -15.822 25.687 5.6044 7.9962 v Velocity[Y] -17.404 18.859 -0.14302 -0.0006726 v Velocity[Z] -3.0566 2.9805 3.1476e-06 -5.3861e-08 v ǁVelocityǁ 0.000882 26.509 6.7948 8.0198 v Pressure -1.9878e+05 1.0838e+05 -39731 -23343 v TurbVisc 2.271e-21 0.0049718 0.00012772 9.0294e-06 v CourantNb 9.1856e-08 0.011778 0.00016675 4.8938e-06 v FourierNb 1.2425e-07 0.046864 0.00014563 1.9334e-07 v total_pressure -97451 2.0971e+05 61594 77982 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0621 0.10208 0.0029217 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2157e-07 0.052074 0.00031238 5.0872e-06 INSTANT 0.875249000E-01 TIME STEP NUMBER 55447 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282672512E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.689507872E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11524E-01 0.20998E+01 Friction velocity uk : 0.11524E-01 0.20998E+01 Dimensionless distance yplus : 0.11207E-01 0.20618E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 9.141534218e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29418E+08 1 0.18893E-09 0.23434E+02 0.19041E+04 c Velocity[X] 0.11754E+02 c Velocity[Y] 0.11680E+02 c Velocity[Z] 0.21948E-05 c Pressure 0.21524E-03 102 0.82260E-04 0.33096E-02 0.43971E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -15.838 25.706 5.6044 7.9961 v Velocity[Y] -17.422 18.874 -0.14303 -0.00067258 v Velocity[Z] -3.0565 2.9805 3.1466e-06 -5.3861e-08 v ǁVelocityǁ 0.00083519 26.525 6.7962 8.0198 v Pressure -1.9706e+05 1.1011e+05 -37993 -22283 v TurbVisc 2.2659e-21 0.0049718 0.00012779 9.0458e-06 v CourantNb 1.0577e-07 0.011778 0.00016676 4.8938e-06 v FourierNb 1.2425e-07 0.046862 0.00014563 1.9346e-07 v total_pressure -95737 2.1144e+05 63332 79042 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0618 0.10207 0.0029218 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2157e-07 0.052072 0.00031239 5.0873e-06 INSTANT 0.875250000E-01 TIME STEP NUMBER 55448 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282669090E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.689466250E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12006E-01 0.20995E+01 Friction velocity uk : 0.12006E-01 0.20995E+01 Dimensionless distance yplus : 0.11686E-01 0.20616E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.000004434e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29417E+08 1 0.18885E-09 0.23412E+02 0.19031E+04 c Velocity[X] 0.11740E+02 c Velocity[Y] 0.11671E+02 c Velocity[Z] 0.22021E-05 c Pressure 0.21691E-03 10 0.65125E-04 0.33323E-02 0.38262E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -15.854 25.726 5.6044 7.9961 v Velocity[Y] -17.439 18.89 -0.14303 -0.00067207 v Velocity[Z] -3.0565 2.9805 3.1456e-06 -5.3861e-08 v ǁVelocityǁ 0.00078636 26.541 6.7977 8.0198 v Pressure -1.9528e+05 1.1203e+05 -36252 -21373 v TurbVisc 2.6142e-21 0.0049718 0.00012787 9.0623e-06 v CourantNb 1.1894e-07 0.011778 0.00016676 4.8939e-06 v FourierNb 1.2425e-07 0.046861 0.00014563 1.9357e-07 v total_pressure -93959 2.1336e+05 65073 79952 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0616 0.10206 0.0029219 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2156e-07 0.052071 0.00031239 5.0875e-06 INSTANT 0.875251000E-01 TIME STEP NUMBER 55449 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282665888E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.689432722E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11396E-01 0.20992E+01 Friction velocity uk : 0.11396E-01 0.20992E+01 Dimensionless distance yplus : 0.11008E-01 0.20612E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.078159862e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29417E+08 1 0.18878E-09 0.23387E+02 0.19021E+04 c Velocity[X] 0.11726E+02 c Velocity[Y] 0.11662E+02 c Velocity[Z] 0.22073E-05 c Pressure 0.21937E-03 401 0.78279E-04 0.33671E-02 0.49803E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -15.87 25.745 5.6044 7.996 v Velocity[Y] -17.457 18.905 -0.14304 -0.00067293 v Velocity[Z] -3.0564 2.9805 3.1447e-06 -5.3861e-08 v ǁVelocityǁ 0.00071863 26.557 6.7991 8.0198 v Pressure -1.9345e+05 1.14e+05 -34484 -20311 v TurbVisc 3.8409e-21 0.0049718 0.00012794 9.0788e-06 v CourantNb 7.0013e-08 0.011778 0.00016676 4.8939e-06 v FourierNb 1.2425e-07 0.04686 0.00014563 1.9369e-07 v total_pressure -92124 2.1533e+05 66841 81014 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0612 0.10205 0.002922 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2156e-07 0.052069 0.00031239 5.0876e-06 INSTANT 0.875252000E-01 TIME STEP NUMBER 55450 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282662757E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.689408317E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.42240E-02 0.20990E+01 Friction velocity uk : 0.42240E-02 0.20990E+01 Dimensionless distance yplus : 0.40742E-02 0.20610E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.099922397e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29417E+08 1 0.18870E-09 0.23365E+02 0.19012E+04 c Velocity[X] 0.11712E+02 c Velocity[Y] 0.11653E+02 c Velocity[Z] 0.22062E-05 c Pressure 0.22164E-03 30 0.84709E-04 0.33988E-02 0.51448E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -15.886 25.765 5.6044 7.9959 v Velocity[Y] -17.474 18.92 -0.14305 -0.00067205 v Velocity[Z] -3.0563 2.9805 3.1437e-06 -5.3861e-08 v ǁVelocityǁ 0.00066032 26.573 6.8005 8.0198 v Pressure -1.9155e+05 1.1601e+05 -32658 -19222 v TurbVisc 2.2666e-21 0.0049718 0.00012801 9.0954e-06 v CourantNb 2.7528e-08 0.011778 0.00016677 4.894e-06 v FourierNb 1.2425e-07 0.046859 0.00014563 1.938e-07 v total_pressure -90229 2.1733e+05 68667 82103 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.061 0.10204 0.0029222 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2155e-07 0.052068 0.0003124 5.0878e-06 INSTANT 0.875253000E-01 TIME STEP NUMBER 55451 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282659767E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.689386541E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11610E-01 0.20987E+01 Friction velocity uk : 0.11610E-01 0.20987E+01 Dimensionless distance yplus : 0.11198E-01 0.20608E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.119399326e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29417E+08 1 0.18863E-09 0.23344E+02 0.19003E+04 c Velocity[X] 0.11699E+02 c Velocity[Y] 0.11644E+02 c Velocity[Z] 0.22062E-05 c Pressure 0.22386E-03 222 0.97688E-04 0.34298E-02 0.46923E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -15.902 25.785 5.6045 7.9959 v Velocity[Y] -17.492 18.935 -0.14307 -0.00067319 v Velocity[Z] -3.0563 2.9805 3.1427e-06 -5.3861e-08 v ǁVelocityǁ 0.00060359 26.588 6.802 8.0199 v Pressure -1.896e+05 1.1806e+05 -30856 -18294 v TurbVisc 2.7746e-21 0.0049719 0.00012809 9.112e-06 v CourantNb 6.9065e-08 0.011778 0.00016677 4.894e-06 v FourierNb 1.2425e-07 0.046858 0.00014563 1.9392e-07 v total_pressure -88274 2.1938e+05 70469 83031 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0608 0.10203 0.0029224 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2155e-07 0.052066 0.0003124 5.0879e-06 INSTANT 0.875254000E-01 TIME STEP NUMBER 55452 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282657061E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.689370783E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10358E-01 0.20985E+01 Friction velocity uk : 0.10358E-01 0.20985E+01 Dimensionless distance yplus : 0.10005E-01 0.20606E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.112335555e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29416E+08 1 0.18856E-09 0.23319E+02 0.18993E+04 c Velocity[X] 0.11686E+02 c Velocity[Y] 0.11633E+02 c Velocity[Z] 0.22033E-05 c Pressure 0.22594E-03 383 0.83301E-04 0.34586E-02 0.56253E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -15.917 25.804 5.6045 7.9958 v Velocity[Y] -17.509 18.95 -0.14308 -0.00067333 v Velocity[Z] -3.0562 2.9805 3.1417e-06 -5.3861e-08 v ǁVelocityǁ 0.0005606 26.604 6.8034 8.0199 v Pressure -1.8759e+05 1.2015e+05 -29008 -17184 v TurbVisc 2.8668e-21 0.0049719 0.00012816 9.1286e-06 v CourantNb 8.2649e-08 0.011778 0.00016677 4.894e-06 v FourierNb 1.2425e-07 0.046857 0.00014563 1.9404e-07 v total_pressure -86262 2.2147e+05 72317 84141 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0606 0.10202 0.0029226 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2154e-07 0.052066 0.00031241 5.0881e-06 INSTANT 0.875255000E-01 TIME STEP NUMBER 55453 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282654430E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.689365310E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.97059E-02 0.20984E+01 Friction velocity uk : 0.97059E-02 0.20984E+01 Dimensionless distance yplus : 0.95743E-02 0.20604E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.083977300e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29416E+08 1 0.18849E-09 0.23299E+02 0.18985E+04 c Velocity[X] 0.11674E+02 c Velocity[Y] 0.11626E+02 c Velocity[Z] 0.22012E-05 c Pressure 0.22717E-03 10 0.66653E-04 0.34743E-02 0.50072E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -15.933 25.824 5.6045 7.9958 v Velocity[Y] -17.526 18.965 -0.14309 -0.0006727 v Velocity[Z] -3.0561 2.9805 3.1407e-06 -5.3861e-08 v ǁVelocityǁ 0.00053847 26.619 6.8049 8.0199 v Pressure -1.8552e+05 1.2227e+05 -27177 -16214 v TurbVisc 3.382e-21 0.0049719 0.00012823 9.1452e-06 v CourantNb 4.3878e-08 0.011778 0.00016678 4.8941e-06 v FourierNb 1.2425e-07 0.046857 0.00014563 1.9415e-07 v total_pressure -84199 2.2359e+05 74148 85111 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0604 0.102 0.0029228 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2154e-07 0.052065 0.00031241 5.0882e-06 INSTANT 0.875256000E-01 TIME STEP NUMBER 55454 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282652045E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.689368873E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12409E-01 0.20982E+01 Friction velocity uk : 0.12409E-01 0.20982E+01 Dimensionless distance yplus : 0.11988E-01 0.20603E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.034742875e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29416E+08 1 0.18841E-09 0.23279E+02 0.18976E+04 c Velocity[X] 0.11661E+02 c Velocity[Y] 0.11617E+02 c Velocity[Z] 0.21960E-05 c Pressure 0.22897E-03 410 0.79512E-04 0.34987E-02 0.64580E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -15.948 25.843 5.6045 7.9957 v Velocity[Y] -17.543 18.98 -0.1431 -0.00067359 v Velocity[Z] -3.0561 2.9805 3.1397e-06 -5.3861e-08 v ǁVelocityǁ 0.00052203 26.635 6.8063 8.0199 v Pressure -1.8342e+05 1.2442e+05 -25273 -15106 v TurbVisc 4.5698e-21 0.0049719 0.00012831 9.1619e-06 v CourantNb 5.961e-08 0.011778 0.00016678 4.8941e-06 v FourierNb 1.2425e-07 0.046857 0.00014563 1.9427e-07 v total_pressure -82096 2.2575e+05 76052 86219 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0603 0.10199 0.0029229 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2153e-07 0.052065 0.00031241 5.0884e-06 INSTANT 0.875257000E-01 TIME STEP NUMBER 55455 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282649721E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.689387055E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.81202E-02 0.20982E+01 Friction velocity uk : 0.81202E-02 0.20982E+01 Dimensionless distance yplus : 0.80231E-02 0.20602E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 9.713136035e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29416E+08 1 0.18834E-09 0.23260E+02 0.18968E+04 c Velocity[X] 0.11650E+02 c Velocity[Y] 0.11610E+02 c Velocity[Z] 0.21850E-05 c Pressure 0.23083E-03 41 0.85827E-04 0.35240E-02 0.66996E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -15.964 25.863 5.6046 7.9957 v Velocity[Y] -17.56 18.995 -0.14311 -0.00067271 v Velocity[Z] -3.056 2.9805 3.1388e-06 -5.3861e-08 v ǁVelocityǁ 0.00052172 26.651 6.8077 8.02 v Pressure -1.8128e+05 1.2659e+05 -23369 -13970 v TurbVisc 2.9263e-21 0.0049719 0.00012838 9.1786e-06 v CourantNb 8.4622e-08 0.011778 0.00016678 4.8942e-06 v FourierNb 1.2425e-07 0.046857 0.00014563 1.9439e-07 v total_pressure -79954 2.2792e+05 77956 87355 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0602 0.10198 0.0029229 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2153e-07 0.052066 0.00031242 5.0885e-06 INSTANT 0.875258000E-01 TIME STEP NUMBER 55456 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282647550E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.689398191E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10937E-01 0.20982E+01 Friction velocity uk : 0.10937E-01 0.20982E+01 Dimensionless distance yplus : 0.10566E-01 0.20602E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 8.813801206e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29415E+08 1 0.18828E-09 0.23242E+02 0.18961E+04 c Velocity[X] 0.11639E+02 c Velocity[Y] 0.11603E+02 c Velocity[Z] 0.21746E-05 c Pressure 0.23232E-03 146 0.99032E-04 0.35436E-02 0.61396E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -15.979 25.883 5.6046 7.9956 v Velocity[Y] -17.577 19.01 -0.14312 -0.00067385 v Velocity[Z] -3.0559 2.9805 3.1378e-06 -5.3861e-08 v ǁVelocityǁ 0.00051628 26.666 6.8092 8.02 v Pressure -1.791e+05 1.2879e+05 -21484 -13004 v TurbVisc 3.5543e-21 0.0049719 0.00012845 9.1954e-06 v CourantNb 7.4564e-08 0.011778 0.00016679 4.8942e-06 v FourierNb 1.2425e-07 0.046858 0.00014563 1.945e-07 v total_pressure -77775 2.3011e+05 79841 88321 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0602 0.10196 0.0029228 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2153e-07 0.052067 0.00031242 5.0887e-06 INSTANT 0.875259000E-01 TIME STEP NUMBER 55457 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282645676E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.689422987E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.92961E-02 0.20982E+01 Friction velocity uk : 0.92961E-02 0.20982E+01 Dimensionless distance yplus : 0.89662E-02 0.20603E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 7.796609794e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29415E+08 1 0.18821E-09 0.23221E+02 0.18952E+04 c Velocity[X] 0.11629E+02 c Velocity[Y] 0.11593E+02 c Velocity[Z] 0.21624E-05 c Pressure 0.23362E-03 356 0.84391E-04 0.35603E-02 0.74024E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -15.994 25.902 5.6046 7.9956 v Velocity[Y] -17.594 19.026 -0.14314 -0.00067402 v Velocity[Z] -3.0559 2.9805 3.1368e-06 -5.3861e-08 v ǁVelocityǁ 0.00050933 26.682 6.8106 8.02 v Pressure -1.7689e+05 1.31e+05 -19545 -11852 v TurbVisc 3.8853e-21 0.004972 0.00012853 9.2122e-06 v CourantNb 6.7774e-08 0.011778 0.00016679 4.8943e-06 v FourierNb 1.2425e-07 0.04686 0.00014563 1.9462e-07 v total_pressure -75564 2.3233e+05 81780 89473 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0603 0.10194 0.0029227 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2152e-07 0.052068 0.00031242 5.0889e-06 INSTANT 0.875260000E-01 TIME STEP NUMBER 55458 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282643876E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.689458771E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.95073E-02 0.20983E+01 Friction velocity uk : 0.95073E-02 0.20983E+01 Dimensionless distance yplus : 0.91700E-02 0.20604E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 6.678432929e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29415E+08 1 0.18814E-09 0.23207E+02 0.18946E+04 c Velocity[X] 0.11619E+02 c Velocity[Y] 0.11588E+02 c Velocity[Z] 0.21523E-05 c Pressure 0.23404E-03 10 0.67778E-04 0.35635E-02 0.66087E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -16.009 25.922 5.6046 7.9956 v Velocity[Y] -17.611 19.041 -0.14315 -0.00067336 v Velocity[Z] -3.0558 2.9805 3.1358e-06 -5.3861e-08 v ǁVelocityǁ 0.00051541 26.698 6.8121 8.0201 v Pressure -1.7466e+05 1.3323e+05 -17655 -10848 v TurbVisc 4.1387e-21 0.004972 0.0001286 9.2289e-06 v CourantNb 6.7735e-08 0.011778 0.00016679 4.8943e-06 v FourierNb 1.2425e-07 0.046861 0.00014563 1.9474e-07 v total_pressure -73330 2.3455e+05 83670 90477 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0604 0.10191 0.0029224 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2152e-07 0.05207 0.00031242 5.089e-06 INSTANT 0.875261000E-01 TIME STEP NUMBER 55459 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282642334E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.689503497E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13787E-01 0.20985E+01 Friction velocity uk : 0.13787E-01 0.20985E+01 Dimensionless distance yplus : 0.13297E-01 0.20605E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 5.372906749e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29415E+08 1 0.18807E-09 0.23190E+02 0.18939E+04 c Velocity[X] 0.11610E+02 c Velocity[Y] 0.11581E+02 c Velocity[Z] 0.21401E-05 c Pressure 0.23491E-03 209 0.80439E-04 0.35735E-02 0.85110E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -16.024 25.941 5.6047 7.9955 v Velocity[Y] -17.627 19.057 -0.14316 -0.00067413 v Velocity[Z] -3.0557 2.9805 3.1348e-06 -5.3861e-08 v ǁVelocityǁ 0.00051587 26.714 6.8135 8.0201 v Pressure -1.7241e+05 1.3546e+05 -15663 -9707.8 v TurbVisc 5.4676e-21 0.004972 0.00012867 9.2458e-06 v CourantNb 6.7567e-08 0.011778 0.00016679 4.8944e-06 v FourierNb 1.2425e-07 0.046863 0.00014563 1.9485e-07 v total_pressure -71087 2.3678e+05 85662 91617 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0605 0.10189 0.0029221 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2152e-07 0.052072 0.00031243 5.0892e-06 INSTANT 0.875262000E-01 TIME STEP NUMBER 55460 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282640855E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.689566842E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13579E-01 0.20987E+01 Friction velocity uk : 0.13579E-01 0.20987E+01 Dimensionless distance yplus : 0.13417E-01 0.20607E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 4.371053382e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29415E+08 1 0.18801E-09 0.23177E+02 0.18933E+04 c Velocity[X] 0.11601E+02 c Velocity[Y] 0.11576E+02 c Velocity[Z] 0.21235E-05 c Pressure 0.23597E-03 54 0.86798E-04 0.35865E-02 0.89500E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -16.039 25.96 5.6047 7.9955 v Velocity[Y] -17.644 19.072 -0.14317 -0.00067333 v Velocity[Z] -3.0556 2.9805 3.1339e-06 -5.3861e-08 v ǁVelocityǁ 0.00051062 26.73 6.8149 8.0202 v Pressure -1.7016e+05 1.3768e+05 -13705 -8525.9 v TurbVisc 3.8853e-21 0.004972 0.00012875 9.2626e-06 v CourantNb 8.2713e-08 0.011778 0.0001668 4.8944e-06 v FourierNb 1.2425e-07 0.046866 0.00014563 1.9497e-07 v total_pressure -68834 2.3901e+05 87620 92799 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0607 0.10186 0.0029216 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2152e-07 0.052076 0.00031243 5.0894e-06 INSTANT 0.875263000E-01 TIME STEP NUMBER 55461 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282639537E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.689618708E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.88455E-02 0.20989E+01 Friction velocity uk : 0.88455E-02 0.20989E+01 Dimensionless distance yplus : 0.87397E-02 0.20610E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 2.943674610e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29415E+08 1 0.18794E-09 0.23160E+02 0.18926E+04 c Velocity[X] 0.11593E+02 c Velocity[Y] 0.11567E+02 c Velocity[Z] 0.21091E-05 c Pressure 0.23655E-03 175 0.74958E-04 0.35920E-02 0.79614E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -16.054 25.98 5.6047 7.9955 v Velocity[Y] -17.661 19.088 -0.14318 -0.00067365 v Velocity[Z] -3.0556 2.9804 3.1329e-06 -5.3862e-08 v ǁVelocityǁ 0.00051187 26.746 6.8164 8.0202 v Pressure -1.679e+05 1.3991e+05 -11763 -7518 v TurbVisc 4.8897e-21 0.004972 0.00012882 9.2797e-06 v CourantNb 7.0781e-08 0.011778 0.0001668 4.8945e-06 v FourierNb 1.2425e-07 0.046869 0.00014563 1.9509e-07 v total_pressure -66575 2.4123e+05 89562 93807 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.061 0.10184 0.0029211 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2151e-07 0.052079 0.00031243 5.0895e-06 INSTANT 0.875264000E-01 TIME STEP NUMBER 55462 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282638449E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.689688703E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11408E-01 0.20992E+01 Friction velocity uk : 0.11408E-01 0.20992E+01 Dimensionless distance yplus : 0.11021E-01 0.20613E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.615507451e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29415E+08 1 0.18788E-09 0.23149E+02 0.18921E+04 c Velocity[X] 0.11586E+02 c Velocity[Y] 0.11563E+02 c Velocity[Z] 0.20973E-05 c Pressure 0.23634E-03 11 0.64537E-04 0.35856E-02 0.80980E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -16.069 25.999 5.6048 7.9955 v Velocity[Y] -17.677 19.104 -0.14319 -0.00067447 v Velocity[Z] -3.0555 2.9804 3.1319e-06 -5.3862e-08 v ǁVelocityǁ 0.00051323 26.762 6.8178 8.0203 v Pressure -1.6564e+05 1.4212e+05 -9830.1 -6492.2 v TurbVisc 4.76e-21 0.004972 0.0001289 9.2966e-06 v CourantNb 3.7868e-08 0.011778 0.0001668 4.8945e-06 v FourierNb 1.2425e-07 0.046872 0.00014563 1.9521e-07 v total_pressure -64316 2.4344e+05 91495 94833 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0613 0.10181 0.0029204 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2151e-07 0.052083 0.00031243 5.0897e-06 INSTANT 0.875265000E-01 TIME STEP NUMBER 55463 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282637687E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.689769889E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.93915E-02 0.20996E+01 Friction velocity uk : 0.93915E-02 0.20996E+01 Dimensionless distance yplus : 0.90731E-02 0.20616E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.997717254e-03 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29415E+08 1 0.18781E-09 0.23136E+02 0.18916E+04 c Velocity[X] 0.11579E+02 c Velocity[Y] 0.11557E+02 c Velocity[Z] 0.20795E-05 c Pressure 0.23651E-03 29 0.96253E-04 0.35850E-02 0.10413E+07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -16.084 26.018 5.6048 7.9955 v Velocity[Y] -17.694 19.12 -0.1432 -0.00067474 v Velocity[Z] -3.0554 2.9804 3.1309e-06 -5.3862e-08 v ǁVelocityǁ 0.00052007 26.778 6.8193 8.0203 v Pressure -1.6339e+05 1.4432e+05 -7829.8 -5298.3 v TurbVisc 5.5096e-21 0.0049721 0.00012897 9.3134e-06 v CourantNb 6.2342e-08 0.011778 0.0001668 4.8946e-06 v FourierNb 1.2425e-07 0.046875 0.00014563 1.9533e-07 v total_pressure -62069 2.4565e+05 93495 96027 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0616 0.10178 0.0029197 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2151e-07 0.052087 0.00031243 5.0899e-06 INSTANT 0.875266000E-01 TIME STEP NUMBER 55464 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282636913E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.689869957E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11900E-01 0.21000E+01 Friction velocity uk : 0.11900E-01 0.21000E+01 Dimensionless distance yplus : 0.11496E-01 0.20620E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -7.811457625e-03 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29415E+08 1 0.18775E-09 0.23125E+02 0.18911E+04 c Velocity[X] 0.11573E+02 c Velocity[Y] 0.11552E+02 c Velocity[Z] 0.20680E-05 c Pressure 0.23664E-03 67 0.81255E-04 0.35838E-02 0.10482E+07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -16.099 26.037 5.6048 7.9954 v Velocity[Y] -17.71 19.137 -0.14321 -0.00067461 v Velocity[Z] -3.0554 2.9804 3.1299e-06 -5.3862e-08 v ǁVelocityǁ 0.00052247 26.795 6.8207 8.0204 v Pressure -1.6116e+05 1.465e+05 -5820.9 -4105.3 v TurbVisc 5.761e-21 0.0049721 0.00012904 9.3306e-06 v CourantNb 8.6509e-08 0.011778 0.00016681 4.8946e-06 v FourierNb 1.2425e-07 0.046879 0.00014563 1.9545e-07 v total_pressure -59831 2.4783e+05 95504 97220 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.062 0.10175 0.0029189 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2151e-07 0.052092 0.00031243 5.0901e-06 INSTANT 0.875267000E-01 TIME STEP NUMBER 55465 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282636341E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.689964698E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11918E-01 0.21004E+01 Friction velocity uk : 0.11918E-01 0.21004E+01 Dimensionless distance yplus : 0.11601E-01 0.20624E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -2.051572364e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29415E+08 1 0.18769E-09 0.23116E+02 0.18907E+04 c Velocity[X] 0.11567E+02 c Velocity[Y] 0.11549E+02 c Velocity[Z] 0.20606E-05 c Pressure 0.23640E-03 10 0.63193E-04 0.35768E-02 0.97398E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -16.114 26.057 5.6048 7.9954 v Velocity[Y] -17.727 19.153 -0.14322 -0.00067412 v Velocity[Z] -3.0553 2.9804 3.129e-06 -5.3862e-08 v ǁVelocityǁ 0.00052362 26.811 6.8221 8.0205 v Pressure -1.5893e+05 1.4866e+05 -3847.8 -3025.8 v TurbVisc 5.3492e-21 0.0049721 0.00012912 9.3476e-06 v CourantNb 3.7049e-08 0.011778 0.00016681 4.8947e-06 v FourierNb 1.2425e-07 0.046884 0.00014563 1.9556e-07 v total_pressure -57606 2.4999e+05 97477 98299 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0624 0.10172 0.0029181 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2151e-07 0.052097 0.00031243 5.0902e-06 INSTANT 0.875268000E-01 TIME STEP NUMBER 55466 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282635966E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.690073832E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12438E-01 0.21007E+01 Friction velocity uk : 0.12438E-01 0.21007E+01 Dimensionless distance yplus : 0.12414E-01 0.20628E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -3.124752782e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29415E+08 1 0.18763E-09 0.23107E+02 0.18903E+04 c Velocity[X] 0.11562E+02 c Velocity[Y] 0.11545E+02 c Velocity[Z] 0.20537E-05 c Pressure 0.23634E-03 418 0.74362E-04 0.35727E-02 0.11158E+07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -16.128 26.076 5.6048 7.9954 v Velocity[Y] -17.743 19.17 -0.14322 -0.00067487 v Velocity[Z] -3.0552 2.9804 3.128e-06 -5.3862e-08 v ǁVelocityǁ 0.0005236 26.828 6.8235 8.0205 v Pressure -1.5673e+05 1.508e+05 -1861.3 -1892.3 v TurbVisc 6.9359e-21 0.0049721 0.00012919 9.3646e-06 v CourantNb 5.6261e-08 0.011778 0.00016681 4.8947e-06 v FourierNb 1.2425e-07 0.046887 0.00014563 1.9568e-07 v total_pressure -55404 2.5213e+05 99464 99433 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0628 0.10169 0.0029172 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2151e-07 0.052101 0.00031244 5.0904e-06 INSTANT 0.875269000E-01 TIME STEP NUMBER 55467 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282635703E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.690199707E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10734E-01 0.21012E+01 Friction velocity uk : 0.10734E-01 0.21012E+01 Dimensionless distance yplus : 0.10324E-01 0.20632E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -3.848616592e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29415E+08 1 0.18757E-09 0.23100E+02 0.18900E+04 c Velocity[X] 0.11558E+02 c Velocity[Y] 0.11542E+02 c Velocity[Z] 0.20415E-05 c Pressure 0.23624E-03 30 0.79764E-04 0.35680E-02 0.11247E+07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -16.143 26.095 5.6049 7.9954 v Velocity[Y] -17.76 19.186 -0.14323 -0.000674 v Velocity[Z] -3.0551 2.9804 3.127e-06 -5.3862e-08 v ǁVelocityǁ 0.00052255 26.845 6.825 8.0206 v Pressure -1.5455e+05 1.5292e+05 130.01 -713.29 v TurbVisc 5.394e-21 0.0049721 0.00012927 9.3818e-06 v CourantNb 8.3273e-08 0.011778 0.00016681 4.8948e-06 v FourierNb 1.2425e-07 0.046892 0.00014562 1.958e-07 v total_pressure -53221 2.5424e+05 1.0146e+05 1.0061e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0632 0.10165 0.0029162 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2151e-07 0.052106 0.00031244 5.0906e-06 INSTANT 0.875270000E-01 TIME STEP NUMBER 55468 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282635608E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.690322726E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.84151E-02 0.21016E+01 Friction velocity uk : 0.84151E-02 0.21016E+01 Dimensionless distance yplus : 0.80938E-02 0.20636E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -4.818402634e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29415E+08 1 0.18751E-09 0.23094E+02 0.18897E+04 c Velocity[X] 0.11554E+02 c Velocity[Y] 0.11539E+02 c Velocity[Z] 0.20344E-05 c Pressure 0.23590E-03 207 0.91727E-04 0.35596E-02 0.98041E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -16.158 26.114 5.6049 7.9954 v Velocity[Y] -17.776 19.203 -0.14323 -0.00067497 v Velocity[Z] -3.0551 2.9804 3.126e-06 -5.3862e-08 v ǁVelocityǁ 0.00051908 26.862 6.8264 8.0207 v Pressure -1.5238e+05 1.5505e+05 2087.2 290.69 v TurbVisc 6.0507e-21 0.0049721 0.00012934 9.399e-06 v CourantNb 6.0883e-08 0.011778 0.00016681 4.8949e-06 v FourierNb 1.2425e-07 0.046896 0.00014562 1.9592e-07 v total_pressure -51057 2.5637e+05 1.0341e+05 1.0162e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0636 0.10163 0.0029152 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2151e-07 0.052111 0.00031244 5.0908e-06 INSTANT 0.875271000E-01 TIME STEP NUMBER 55469 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282635825E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.690462683E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.57221E-02 0.21021E+01 Friction velocity uk : 0.57221E-02 0.21021E+01 Dimensionless distance yplus : 0.55188E-02 0.20640E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -5.531667356e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29415E+08 1 0.18745E-09 0.23084E+02 0.18893E+04 c Velocity[X] 0.11551E+02 c Velocity[Y] 0.11533E+02 c Velocity[Z] 0.20301E-05 c Pressure 0.23546E-03 679 0.78270E-04 0.35498E-02 0.11283E+07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -16.172 26.133 5.6049 7.9954 v Velocity[Y] -17.793 19.22 -0.14324 -0.00067507 v Velocity[Z] -3.055 2.9804 3.1251e-06 -5.3862e-08 v ǁVelocityǁ 0.00051669 26.879 6.8278 8.0208 v Pressure -1.5024e+05 1.5718e+05 4078.7 1495.4 v TurbVisc 6.2939e-21 0.0049722 0.00012942 9.4162e-06 v CourantNb 4.089e-08 0.011778 0.00016681 4.8949e-06 v FourierNb 1.2425e-07 0.0469 0.00014562 1.9604e-07 v total_pressure -48915 2.5851e+05 1.054e+05 1.0282e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.064 0.1016 0.0029142 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2151e-07 0.052116 0.00031244 5.091e-06 INSTANT 0.875272000E-01 TIME STEP NUMBER 55470 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282636129E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.690614982E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.56408E-02 0.21025E+01 Friction velocity uk : 0.56408E-02 0.21025E+01 Dimensionless distance yplus : 0.54255E-02 0.20644E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -6.026468750e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29415E+08 1 0.18739E-09 0.23081E+02 0.18891E+04 c Velocity[X] 0.11548E+02 c Velocity[Y] 0.11532E+02 c Velocity[Z] 0.20310E-05 c Pressure 0.23432E-03 10 0.65147E-04 0.35294E-02 0.92133E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -16.187 26.152 5.6049 7.9954 v Velocity[Y] -17.81 19.237 -0.14324 -0.00067434 v Velocity[Z] -3.0549 2.9804 3.1241e-06 -5.3862e-08 v ǁVelocityǁ 0.00051328 26.896 6.8293 8.0209 v Pressure -1.4812e+05 1.5928e+05 6042.1 2518.3 v TurbVisc 7.1998e-21 0.0049722 0.00012949 9.4334e-06 v CourantNb 2.6336e-08 0.011778 0.00016682 4.895e-06 v FourierNb 1.2425e-07 0.046904 0.00014562 1.9616e-07 v total_pressure -46798 2.606e+05 1.0737e+05 1.0384e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0644 0.10157 0.0029132 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2151e-07 0.052121 0.00031244 5.0911e-06 INSTANT 0.875273000E-01 TIME STEP NUMBER 55471 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282636690E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.690778726E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.58720E-02 0.21028E+01 Friction velocity uk : 0.58720E-02 0.21028E+01 Dimensionless distance yplus : 0.56478E-02 0.20648E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -6.472820318e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29415E+08 1 0.18732E-09 0.23076E+02 0.18889E+04 c Velocity[X] 0.11547E+02 c Velocity[Y] 0.11529E+02 c Velocity[Z] 0.20331E-05 c Pressure 0.23386E-03 152 0.74544E-04 0.35193E-02 0.11020E+07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -16.202 26.171 5.6049 7.9955 v Velocity[Y] -17.826 19.254 -0.14324 -0.00067493 v Velocity[Z] -3.0548 2.9804 3.1231e-06 -5.3862e-08 v ǁVelocityǁ 0.00051763 26.913 6.8307 8.0209 v Pressure -1.4604e+05 1.6135e+05 8006.1 3703.7 v TurbVisc 7.838e-21 0.0049722 0.00012957 9.4506e-06 v CourantNb 2.6342e-08 0.011778 0.00016682 4.8951e-06 v FourierNb 1.2425e-07 0.046907 0.00014562 1.9628e-07 v total_pressure -44714 2.6267e+05 1.0933e+05 1.0503e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0648 0.10155 0.0029122 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2151e-07 0.052125 0.00031244 5.0913e-06 INSTANT 0.875274000E-01 TIME STEP NUMBER 55472 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282637319E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.690954816E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.69301E-02 0.21032E+01 Friction velocity uk : 0.69301E-02 0.21032E+01 Dimensionless distance yplus : 0.66655E-02 0.20651E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -6.471865362e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29415E+08 1 0.18727E-09 0.23073E+02 0.18887E+04 c Velocity[X] 0.11546E+02 c Velocity[Y] 0.11528E+02 c Velocity[Z] 0.20309E-05 c Pressure 0.23317E-03 41 0.80534E-04 0.35057E-02 0.10410E+07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -16.216 26.19 5.6049 7.9955 v Velocity[Y] -17.843 19.271 -0.14324 -0.00067409 v Velocity[Z] -3.0548 2.9804 3.1221e-06 -5.3862e-08 v ǁVelocityǁ 0.00052288 26.93 6.8321 8.021 v Pressure -1.4398e+05 1.6338e+05 10011 4913.2 v TurbVisc 6.6606e-21 0.0049722 0.00012965 9.4679e-06 v CourantNb 1.8687e-08 0.011779 0.00016682 4.8951e-06 v FourierNb 1.2425e-07 0.046911 0.00014562 1.964e-07 v total_pressure -42656 2.6471e+05 1.1134e+05 1.0624e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0651 0.10152 0.0029113 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2151e-07 0.052129 0.00031244 5.0915e-06 INSTANT 0.875275000E-01 TIME STEP NUMBER 55473 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282638113E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.691136584E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.39580E-02 0.21035E+01 Friction velocity uk : 0.39580E-02 0.21035E+01 Dimensionless distance yplus : 0.38069E-02 0.20655E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -6.662083165e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29415E+08 1 0.18721E-09 0.23072E+02 0.18886E+04 c Velocity[X] 0.11545E+02 c Velocity[Y] 0.11527E+02 c Velocity[Z] 0.20357E-05 c Pressure 0.23248E-03 147 0.92684E-04 0.34922E-02 0.84715E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -16.231 26.209 5.6049 7.9955 v Velocity[Y] -17.86 19.288 -0.14324 -0.00067503 v Velocity[Z] -3.0547 2.9804 3.1212e-06 -5.3862e-08 v ǁVelocityǁ 0.00052192 26.948 6.8335 8.0211 v Pressure -1.4195e+05 1.6539e+05 11945 5908.7 v TurbVisc 7.0627e-21 0.0049722 0.00012972 9.4854e-06 v CourantNb 3.1016e-08 0.011779 0.00016682 4.8952e-06 v FourierNb 1.2425e-07 0.046914 0.00014562 1.9652e-07 v total_pressure -40622 2.6672e+05 1.1327e+05 1.0723e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0655 0.1015 0.0029105 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2151e-07 0.052133 0.00031244 5.0917e-06 INSTANT 0.875276000E-01 TIME STEP NUMBER 55474 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282639206E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.691327297E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.83085E-02 0.21038E+01 Friction velocity uk : 0.83085E-02 0.21038E+01 Dimensionless distance yplus : 0.79913E-02 0.20657E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -6.586435538e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29415E+08 1 0.18715E-09 0.23067E+02 0.18884E+04 c Velocity[X] 0.11545E+02 c Velocity[Y] 0.11522E+02 c Velocity[Z] 0.20422E-05 c Pressure 0.23164E-03 368 0.78891E-04 0.34763E-02 0.94248E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -16.246 26.229 5.6049 7.9955 v Velocity[Y] -17.877 19.305 -0.14324 -0.00067504 v Velocity[Z] -3.0546 2.9804 3.1202e-06 -5.3862e-08 v ǁVelocityǁ 0.00051741 26.965 6.835 8.0212 v Pressure -1.3993e+05 1.6739e+05 13913 7114.1 v TurbVisc 6.7451e-21 0.0049722 0.0001298 9.5027e-06 v CourantNb 4.031e-08 0.011779 0.00016682 4.8953e-06 v FourierNb 1.2425e-07 0.046917 0.00014562 1.9665e-07 v total_pressure -38610 2.6871e+05 1.1524e+05 1.0844e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0657 0.10148 0.0029097 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2151e-07 0.052136 0.00031244 5.0919e-06 INSTANT 0.875277000E-01 TIME STEP NUMBER 55475 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282640391E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.691533280E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.75373E-02 0.21040E+01 Friction velocity uk : 0.75373E-02 0.21040E+01 Dimensionless distance yplus : 0.72495E-02 0.20659E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -6.351760023e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29415E+08 1 0.18710E-09 0.23068E+02 0.18884E+04 c Velocity[X] 0.11545E+02 c Velocity[Y] 0.11523E+02 c Velocity[Z] 0.20539E-05 c Pressure 0.23005E-03 10 0.65502E-04 0.34493E-02 0.74524E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -16.26 26.248 5.6049 7.9955 v Velocity[Y] -17.894 19.323 -0.14324 -0.00067428 v Velocity[Z] -3.0545 2.9804 3.1192e-06 -5.3862e-08 v ǁVelocityǁ 0.00051697 26.983 6.8364 8.0213 v Pressure -1.3813e+05 1.6935e+05 15862 8132.6 v TurbVisc 8.5529e-21 0.0049723 0.00012987 9.5201e-06 v CourantNb 4.8291e-08 0.011779 0.00016682 4.8953e-06 v FourierNb 1.2425e-07 0.046919 0.00014562 1.9677e-07 v total_pressure -36809 2.7068e+05 1.1719e+05 1.0946e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0659 0.10147 0.002909 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2152e-07 0.052139 0.00031244 5.0921e-06 INSTANT 0.875278000E-01 TIME STEP NUMBER 55476 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282641834E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.691751934E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11172E-01 0.21041E+01 Friction velocity uk : 0.11172E-01 0.21041E+01 Dimensionless distance yplus : 0.10745E-01 0.20660E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -5.966455956e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29415E+08 1 0.18704E-09 0.23068E+02 0.18884E+04 c Velocity[X] 0.11547E+02 c Velocity[Y] 0.11521E+02 c Velocity[Z] 0.20666E-05 c Pressure 0.22926E-03 441 0.75292E-04 0.34343E-02 0.86948E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -16.275 26.267 5.6049 7.9956 v Velocity[Y] -17.911 19.34 -0.14323 -0.00067496 v Velocity[Z] -3.0545 2.9804 3.1182e-06 -5.3862e-08 v ǁVelocityǁ 0.000522 27 6.8378 8.0214 v Pressure -1.3635e+05 1.713e+05 17763 9305.8 v TurbVisc 8.8341e-21 0.0049723 0.00012995 9.5375e-06 v CourantNb 5.2655e-08 0.011779 0.00016683 4.8954e-06 v FourierNb 1.2425e-07 0.046921 0.00014562 1.9689e-07 v total_pressure -35025 2.7262e+05 1.1909e+05 1.1063e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.066 0.10145 0.0029084 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2152e-07 0.052141 0.00031244 5.0923e-06 INSTANT 0.875279000E-01 TIME STEP NUMBER 55477 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282643340E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.691981054E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13814E-01 0.21042E+01 Friction velocity uk : 0.13814E-01 0.21042E+01 Dimensionless distance yplus : 0.13287E-01 0.20662E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -5.435301959e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29415E+08 1 0.18698E-09 0.23071E+02 0.18884E+04 c Velocity[X] 0.11549E+02 c Velocity[Y] 0.11522E+02 c Velocity[Z] 0.20742E-05 c Pressure 0.22798E-03 30 0.81514E-04 0.34121E-02 0.79215E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -16.29 26.287 5.6049 7.9956 v Velocity[Y] -17.928 19.357 -0.14323 -0.00067391 v Velocity[Z] -3.0544 2.9803 3.1173e-06 -5.3862e-08 v ǁVelocityǁ 0.00052931 27.018 6.8392 8.0215 v Pressure -1.3457e+05 1.7322e+05 19731 10478 v TurbVisc 7.5976e-21 0.0049723 0.00013003 9.555e-06 v CourantNb 5.6986e-08 0.011779 0.00016683 4.8955e-06 v FourierNb 1.2425e-07 0.046922 0.00014562 1.9701e-07 v total_pressure -33250 2.7454e+05 1.2106e+05 1.118e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0662 0.10144 0.0029078 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2152e-07 0.052143 0.00031245 5.0925e-06 INSTANT 0.875280000E-01 TIME STEP NUMBER 55478 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282645008E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.692224163E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15878E-01 0.21042E+01 Friction velocity uk : 0.15878E-01 0.21042E+01 Dimensionless distance yplus : 0.15272E-01 0.20662E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -4.916318961e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29415E+08 1 0.18693E-09 0.23074E+02 0.18885E+04 c Velocity[X] 0.11552E+02 c Velocity[Y] 0.11522E+02 c Velocity[Z] 0.20891E-05 c Pressure 0.22686E-03 206 0.93772E-04 0.33922E-02 0.65710E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -16.304 26.306 5.6049 7.9956 v Velocity[Y] -17.945 19.374 -0.14323 -0.00067482 v Velocity[Z] -3.0543 2.9803 3.1163e-06 -5.3862e-08 v ǁVelocityǁ 0.00053019 27.035 6.8407 8.0217 v Pressure -1.328e+05 1.7525e+05 21626 11468 v TurbVisc 7.9033e-21 0.0049723 0.0001301 9.5726e-06 v CourantNb 5.9899e-08 0.011779 0.00016683 4.8955e-06 v FourierNb 1.2425e-07 0.046923 0.00014562 1.9713e-07 v total_pressure -31478 2.7657e+05 1.2295e+05 1.1279e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0662 0.10143 0.0029073 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2152e-07 0.052144 0.00031245 5.0927e-06 INSTANT 0.875281000E-01 TIME STEP NUMBER 55479 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282646973E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.692473086E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.17455E-01 0.21042E+01 Friction velocity uk : 0.17455E-01 0.21042E+01 Dimensionless distance yplus : 0.16789E-01 0.20662E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -4.245084176e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29416E+08 1 0.18687E-09 0.23074E+02 0.18885E+04 c Velocity[X] 0.11555E+02 c Velocity[Y] 0.11519E+02 c Velocity[Z] 0.21044E-05 c Pressure 0.22558E-03 142 0.79699E-04 0.33699E-02 0.71140E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -16.319 26.326 5.6048 7.9957 v Velocity[Y] -17.962 19.391 -0.14322 -0.00067463 v Velocity[Z] -3.0542 2.9803 3.1153e-06 -5.3862e-08 v ǁVelocityǁ 0.00053004 27.053 6.8421 8.0218 v Pressure -1.3103e+05 1.7727e+05 23542 12643 v TurbVisc 7.6148e-21 0.0049723 0.00013018 9.5901e-06 v CourantNb 5.943e-08 0.011779 0.00016683 4.8956e-06 v FourierNb 1.2425e-07 0.046924 0.00014562 1.9725e-07 v total_pressure -29704 2.7859e+05 1.2487e+05 1.1397e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0662 0.10142 0.0029068 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2153e-07 0.052144 0.00031245 5.0929e-06 INSTANT 0.875282000E-01 TIME STEP NUMBER 55480 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282649027E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.692737963E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.18613E-01 0.21041E+01 Friction velocity uk : 0.18613E-01 0.21041E+01 Dimensionless distance yplus : 0.17953E-01 0.20661E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -3.521187574e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29416E+08 1 0.18682E-09 0.23080E+02 0.18887E+04 c Velocity[X] 0.11559E+02 c Velocity[Y] 0.11521E+02 c Velocity[Z] 0.21231E-05 c Pressure 0.22350E-03 10 0.65028E-04 0.33358E-02 0.55995E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -16.334 26.346 5.6048 7.9957 v Velocity[Y] -17.979 19.408 -0.14321 -0.00067395 v Velocity[Z] -3.0542 2.9803 3.1144e-06 -5.3862e-08 v ǁVelocityǁ 0.00053898 27.07 6.8435 8.0219 v Pressure -1.2925e+05 1.7927e+05 25438 13627 v TurbVisc 8.9055e-21 0.0049723 0.00013026 9.6076e-06 v CourantNb 5.713e-08 0.011779 0.00016683 4.8957e-06 v FourierNb 1.2425e-07 0.046924 0.00014562 1.9738e-07 v total_pressure -27926 2.806e+05 1.2676e+05 1.1495e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0661 0.10142 0.0029065 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2153e-07 0.052144 0.00031245 5.0931e-06 INSTANT 0.875283000E-01 TIME STEP NUMBER 55481 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282651320E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.693016141E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.18662E-01 0.21040E+01 Friction velocity uk : 0.18662E-01 0.21040E+01 Dimensionless distance yplus : 0.18165E-01 0.20659E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -2.652090417e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29416E+08 1 0.18676E-09 0.23085E+02 0.18889E+04 c Velocity[X] 0.11564E+02 c Velocity[Y] 0.11521E+02 c Velocity[Z] 0.21407E-05 c Pressure 0.22228E-03 452 0.75831E-04 0.33146E-02 0.65813E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -16.349 26.366 5.6048 7.9958 v Velocity[Y] -17.996 19.425 -0.14321 -0.00067459 v Velocity[Z] -3.0541 2.9803 3.1134e-06 -5.3862e-08 v ǁVelocityǁ 0.0005404 27.088 6.845 8.022 v Pressure -1.2747e+05 1.8126e+05 27275 14769 v TurbVisc 9.3056e-21 0.0049724 0.00013034 9.6252e-06 v CourantNb 5.108e-08 0.011779 0.00016683 4.8958e-06 v FourierNb 1.2425e-07 0.046923 0.00014562 1.975e-07 v total_pressure -26146 2.8259e+05 1.286e+05 1.1609e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0659 0.10142 0.0029061 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2153e-07 0.052143 0.00031246 5.0933e-06 INSTANT 0.875284000E-01 TIME STEP NUMBER 55482 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282653685E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.693304696E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.18460E-01 0.21038E+01 Friction velocity uk : 0.18460E-01 0.21038E+01 Dimensionless distance yplus : 0.17820E-01 0.20657E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.915791820e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29416E+08 1 0.18671E-09 0.23092E+02 0.18891E+04 c Velocity[X] 0.11569E+02 c Velocity[Y] 0.11523E+02 c Velocity[Z] 0.21529E-05 c Pressure 0.22055E-03 30 0.81980E-04 0.32858E-02 0.60205E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -16.363 26.386 5.6048 7.9958 v Velocity[Y] -18.013 19.442 -0.1432 -0.0006735 v Velocity[Z] -3.054 2.9803 3.1124e-06 -5.3862e-08 v ǁVelocityǁ 0.00055514 27.105 6.8464 8.0221 v Pressure -1.2568e+05 1.8323e+05 29184 15906 v TurbVisc 7.9047e-21 0.0049724 0.00013041 9.6429e-06 v CourantNb 4.5117e-08 0.011779 0.00016684 4.8958e-06 v FourierNb 1.2425e-07 0.046923 0.00014562 1.9762e-07 v total_pressure -24355 2.8456e+05 1.3051e+05 1.1723e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0657 0.10142 0.0029059 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2154e-07 0.052143 0.00031246 5.0935e-06 INSTANT 0.875285000E-01 TIME STEP NUMBER 55483 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282656199E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.693609070E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.16565E-01 0.21036E+01 Friction velocity uk : 0.16565E-01 0.21036E+01 Dimensionless distance yplus : 0.15990E-01 0.20655E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.122424132e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29417E+08 1 0.18666E-09 0.23100E+02 0.18894E+04 c Velocity[X] 0.11575E+02 c Velocity[Y] 0.11525E+02 c Velocity[Z] 0.21712E-05 c Pressure 0.21902E-03 206 0.94317E-04 0.32600E-02 0.49826E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -16.378 26.407 5.6048 7.9959 v Velocity[Y] -18.03 19.459 -0.14319 -0.00067438 v Velocity[Z] -3.0539 2.9803 3.1115e-06 -5.3862e-08 v ǁVelocityǁ 0.0005751 27.123 6.8479 8.0223 v Pressure -1.2388e+05 1.8519e+05 31012 16856 v TurbVisc 8.1287e-21 0.0049724 0.00013049 9.6607e-06 v CourantNb 3.7947e-08 0.011779 0.00016684 4.8959e-06 v FourierNb 1.2425e-07 0.046922 0.00014562 1.9775e-07 v total_pressure -22551 2.8652e+05 1.3234e+05 1.1818e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0655 0.10142 0.0029057 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2154e-07 0.052141 0.00031246 5.0937e-06 INSTANT 0.875286000E-01 TIME STEP NUMBER 55484 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282659006E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.693918618E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.14524E-01 0.21033E+01 Friction velocity uk : 0.14524E-01 0.21033E+01 Dimensionless distance yplus : 0.14020E-01 0.20652E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -3.045417131e-03 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29417E+08 1 0.18661E-09 0.23104E+02 0.18895E+04 c Velocity[X] 0.11581E+02 c Velocity[Y] 0.11523E+02 c Velocity[Z] 0.21878E-05 c Pressure 0.21735E-03 390 0.80194E-04 0.32321E-02 0.53917E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -16.393 26.427 5.6048 7.9959 v Velocity[Y] -18.047 19.475 -0.14319 -0.0006743 v Velocity[Z] -3.0539 2.9803 3.1105e-06 -5.3862e-08 v ǁVelocityǁ 0.00060409 27.14 6.8493 8.0224 v Pressure -1.2205e+05 1.8715e+05 32852 17977 v TurbVisc 8.0428e-21 0.0049724 0.00013057 9.6784e-06 v CourantNb 2.7866e-08 0.011779 0.00016684 4.896e-06 v FourierNb 1.2425e-07 0.04692 0.00014562 1.9787e-07 v total_pressure -20729 2.8847e+05 1.3418e+05 1.193e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0652 0.10142 0.0029056 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2155e-07 0.052139 0.00031246 5.0939e-06 INSTANT 0.875287000E-01 TIME STEP NUMBER 55485 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282661887E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.694244290E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13579E-01 0.21030E+01 Friction velocity uk : 0.13579E-01 0.21030E+01 Dimensionless distance yplus : 0.13108E-01 0.20649E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 4.760249605e-03 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29417E+08 1 0.18656E-09 0.23115E+02 0.18899E+04 c Velocity[X] 0.11588E+02 c Velocity[Y] 0.11527E+02 c Velocity[Z] 0.22056E-05 c Pressure 0.21485E-03 10 0.64486E-04 0.31920E-02 0.43345E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -16.408 26.448 5.6048 7.996 v Velocity[Y] -18.064 19.492 -0.14318 -0.00067341 v Velocity[Z] -3.0538 2.9803 3.1095e-06 -5.3862e-08 v ǁVelocityǁ 0.00064062 27.158 6.8508 8.0225 v Pressure -1.2022e+05 1.8909e+05 34670 18935 v TurbVisc 8.7744e-21 0.0049724 0.00013065 9.6961e-06 v CourantNb 1.6744e-08 0.01178 0.00016684 4.8961e-06 v FourierNb 1.2425e-07 0.046918 0.00014563 1.9799e-07 v total_pressure -18891 2.9041e+05 1.3599e+05 1.2026e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0649 0.10142 0.0029055 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2155e-07 0.052137 0.00031247 5.0941e-06 INSTANT 0.875288000E-01 TIME STEP NUMBER 55486 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282665009E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.694583331E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15921E-01 0.21026E+01 Friction velocity uk : 0.15921E-01 0.21026E+01 Dimensionless distance yplus : 0.15369E-01 0.20646E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.338968844e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29417E+08 1 0.18650E-09 0.23124E+02 0.18902E+04 c Velocity[X] 0.11596E+02 c Velocity[Y] 0.11528E+02 c Velocity[Z] 0.22223E-05 c Pressure 0.21324E-03 442 0.76458E-04 0.31651E-02 0.50269E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -16.422 26.468 5.6048 7.996 v Velocity[Y] -18.081 19.509 -0.14317 -0.00067405 v Velocity[Z] -3.0537 2.9803 3.1086e-06 -5.3862e-08 v ǁVelocityǁ 0.00066915 27.175 6.8522 8.0227 v Pressure -1.1837e+05 1.9102e+05 36439 20010 v TurbVisc 9.9711e-21 0.0049724 0.00013073 9.7139e-06 v CourantNb 2.83e-08 0.01178 0.00016684 4.8962e-06 v FourierNb 1.2425e-07 0.046916 0.00014563 1.9812e-07 v total_pressure -17040 2.9234e+05 1.3776e+05 1.2134e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0646 0.10143 0.0029055 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2155e-07 0.052134 0.00031247 5.0943e-06 INSTANT 0.875289000E-01 TIME STEP NUMBER 55487 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282668187E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.694934522E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.14361E-01 0.21023E+01 Friction velocity uk : 0.14361E-01 0.21023E+01 Dimensionless distance yplus : 0.13851E-01 0.20642E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.895908467e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29418E+08 1 0.18645E-09 0.23135E+02 0.18906E+04 c Velocity[X] 0.11604E+02 c Velocity[Y] 0.11531E+02 c Velocity[Z] 0.22340E-05 c Pressure 0.21128E-03 53 0.82398E-04 0.31331E-02 0.46673E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -16.437 26.489 5.6047 7.9961 v Velocity[Y] -18.098 19.526 -0.14316 -0.00067292 v Velocity[Z] -3.0536 2.9803 3.1076e-06 -5.3862e-08 v ǁVelocityǁ 0.00070512 27.193 6.8537 8.0228 v Pressure -1.165e+05 1.9293e+05 38254 21094 v TurbVisc 7.796e-21 0.0049725 0.0001308 9.7318e-06 v CourantNb 3.4525e-08 0.01178 0.00016685 4.8962e-06 v FourierNb 1.2425e-07 0.046914 0.00014563 1.9824e-07 v total_pressure -15174 2.9425e+05 1.3958e+05 1.2242e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0642 0.10143 0.0029055 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2156e-07 0.052132 0.00031247 5.0945e-06 INSTANT 0.875290000E-01 TIME STEP NUMBER 55488 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282671508E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.695295761E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10120E-01 0.21019E+01 Friction velocity uk : 0.10120E-01 0.21019E+01 Dimensionless distance yplus : 0.97609E-02 0.20639E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 2.535550901e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29418E+08 1 0.18640E-09 0.23146E+02 0.18910E+04 c Velocity[X] 0.11612E+02 c Velocity[Y] 0.11534E+02 c Velocity[Z] 0.22467E-05 c Pressure 0.20941E-03 223 0.94767E-04 0.31025E-02 0.38649E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -16.452 26.51 5.6047 7.9962 v Velocity[Y] -18.115 19.542 -0.14315 -0.0006738 v Velocity[Z] -3.0536 2.9803 3.1066e-06 -5.3862e-08 v ǁVelocityǁ 0.00074407 27.21 6.8551 8.023 v Pressure -1.1462e+05 1.9483e+05 39992 21987 v TurbVisc 8.1093e-21 0.0049725 0.00013088 9.7497e-06 v CourantNb 4.1572e-08 0.01178 0.00016685 4.8963e-06 v FourierNb 1.2425e-07 0.046912 0.00014563 1.9837e-07 v total_pressure -13292 2.9615e+05 1.4132e+05 1.2331e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0639 0.10143 0.0029055 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2157e-07 0.052129 0.00031248 5.0947e-06 INSTANT 0.875291000E-01 TIME STEP NUMBER 55489 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282675109E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.695664810E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10386E-01 0.21015E+01 Friction velocity uk : 0.10386E-01 0.21015E+01 Dimensionless distance yplus : 0.10017E-01 0.20635E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 3.096639920e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29418E+08 1 0.18636E-09 0.23154E+02 0.18913E+04 c Velocity[X] 0.11621E+02 c Velocity[Y] 0.11533E+02 c Velocity[Z] 0.22568E-05 c Pressure 0.20742E-03 250 0.80694E-04 0.30703E-02 0.42141E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -16.467 26.531 5.6047 7.9962 v Velocity[Y] -18.132 19.559 -0.14314 -0.00067357 v Velocity[Z] -3.0535 2.9803 3.1057e-06 -5.3862e-08 v ǁVelocityǁ 0.00078735 27.228 6.8566 8.0231 v Pressure -1.1272e+05 1.9672e+05 41739 23049 v TurbVisc 8.1019e-21 0.0049725 0.00013096 9.7676e-06 v CourantNb 5.6369e-08 0.01178 0.00016685 4.8964e-06 v FourierNb 1.2425e-07 0.04691 0.00014563 1.9849e-07 v total_pressure -11394 2.9804e+05 1.4306e+05 1.2437e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0635 0.10144 0.0029056 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2157e-07 0.052126 0.00031248 5.0949e-06 INSTANT 0.875292000E-01 TIME STEP NUMBER 55490 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282678776E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.696048248E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.59976E-02 0.21012E+01 Friction velocity uk : 0.59976E-02 0.21012E+01 Dimensionless distance yplus : 0.57846E-02 0.20632E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 3.573680313e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29419E+08 1 0.18631E-09 0.23168E+02 0.18918E+04 c Velocity[X] 0.11630E+02 c Velocity[Y] 0.11538E+02 c Velocity[Z] 0.22676E-05 c Pressure 0.20456E-03 10 0.63123E-04 0.30250E-02 0.33424E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -16.481 26.552 5.6047 7.9963 v Velocity[Y] -18.149 19.575 -0.14314 -0.00067281 v Velocity[Z] -3.0534 2.9803 3.1047e-06 -5.3862e-08 v ǁVelocityǁ 0.00083773 27.245 6.8581 8.0233 v Pressure -1.1088e+05 1.9859e+05 43437 23936 v TurbVisc 8.583e-21 0.0049725 0.00013104 9.7856e-06 v CourantNb 7.0697e-08 0.01178 0.00016685 4.8965e-06 v FourierNb 1.2425e-07 0.046908 0.00014563 1.9862e-07 v total_pressure -9557.2 2.9991e+05 1.4476e+05 1.2526e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0632 0.10144 0.0029056 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2158e-07 0.052124 0.00031249 5.0951e-06 INSTANT 0.875293000E-01 TIME STEP NUMBER 55491 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282682665E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.696443465E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11186E-01 0.21008E+01 Friction velocity uk : 0.11186E-01 0.21008E+01 Dimensionless distance yplus : 0.10843E-01 0.20628E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 4.068751934e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29419E+08 1 0.18626E-09 0.23180E+02 0.18923E+04 c Velocity[X] 0.11640E+02 c Velocity[Y] 0.11540E+02 c Velocity[Z] 0.22766E-05 c Pressure 0.20250E-03 444 0.76714E-04 0.29918E-02 0.39525E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -16.496 26.574 5.6047 7.9964 v Velocity[Y] -18.166 19.592 -0.14313 -0.00067342 v Velocity[Z] -3.0533 2.9802 3.1037e-06 -5.3862e-08 v ǁVelocityǁ 0.00087272 27.263 6.8596 8.0234 v Pressure -1.0907e+05 2.0044e+05 45134 24943 v TurbVisc 1.0373e-20 0.0049725 0.00013112 9.8036e-06 v CourantNb 8.7499e-08 0.01178 0.00016686 4.8966e-06 v FourierNb 1.2425e-07 0.046906 0.00014563 1.9874e-07 v total_pressure -7749.6 3.0176e+05 1.4646e+05 1.2627e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0628 0.10144 0.0029056 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2158e-07 0.052121 0.00031249 5.0953e-06 INSTANT 0.875294000E-01 TIME STEP NUMBER 55492 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282686608E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.696853365E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.56943E-02 0.21005E+01 Friction velocity uk : 0.56943E-02 0.21005E+01 Dimensionless distance yplus : 0.56356E-02 0.20625E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 4.286155061e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29419E+08 1 0.18621E-09 0.23194E+02 0.18928E+04 c Velocity[X] 0.11650E+02 c Velocity[Y] 0.11544E+02 c Velocity[Z] 0.22795E-05 c Pressure 0.20034E-03 30 0.82726E-04 0.29571E-02 0.36936E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -16.511 26.595 5.6048 7.9965 v Velocity[Y] -18.183 19.609 -0.14312 -0.00067232 v Velocity[Z] -3.0532 2.9802 3.1028e-06 -5.3862e-08 v ǁVelocityǁ 0.00091656 27.28 6.861 8.0236 v Pressure -1.0727e+05 2.0226e+05 46822 25955 v TurbVisc 7.712e-21 0.0049725 0.0001312 9.8216e-06 v CourantNb 1.0417e-07 0.01178 0.00016686 4.8967e-06 v FourierNb 1.2425e-07 0.046905 0.00014564 1.9887e-07 v total_pressure -5946.3 3.0359e+05 1.4815e+05 1.2728e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0625 0.10144 0.0029056 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2159e-07 0.05212 0.00031249 5.0956e-06 INSTANT 0.875295000E-01 TIME STEP NUMBER 55493 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282690679E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.697263201E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10216E-01 0.21002E+01 Friction velocity uk : 0.10216E-01 0.21002E+01 Dimensionless distance yplus : 0.98543E-02 0.20623E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 4.524054025e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29420E+08 1 0.18617E-09 0.23209E+02 0.18933E+04 c Velocity[X] 0.11660E+02 c Velocity[Y] 0.11549E+02 c Velocity[Z] 0.22834E-05 c Pressure 0.19803E-03 224 0.95305E-04 0.29204E-02 0.30602E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -16.526 26.616 5.6048 7.9966 v Velocity[Y] -18.199 19.625 -0.14311 -0.00067319 v Velocity[Z] -3.0532 2.9802 3.1018e-06 -5.3862e-08 v ǁVelocityǁ 0.00096015 27.298 6.8625 8.0238 v Pressure -1.0547e+05 2.0407e+05 48447 26779 v TurbVisc 8.2072e-21 0.0049726 0.00013128 9.8398e-06 v CourantNb 1.1769e-07 0.01178 0.00016686 4.8968e-06 v FourierNb 1.2425e-07 0.046903 0.00014564 1.99e-07 v total_pressure -4148.4 3.0539e+05 1.4977e+05 1.281e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0623 0.10144 0.0029056 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.216e-07 0.052118 0.0003125 5.0958e-06 INSTANT 0.875296000E-01 TIME STEP NUMBER 55494 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282695019E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.697684566E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10778E-01 0.21000E+01 Friction velocity uk : 0.10778E-01 0.21000E+01 Dimensionless distance yplus : 0.10396E-01 0.20620E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 4.685353727e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29420E+08 1 0.18612E-09 0.23219E+02 0.18937E+04 c Velocity[X] 0.11671E+02 c Velocity[Y] 0.11549E+02 c Velocity[Z] 0.22851E-05 c Pressure 0.19562E-03 381 0.80985E-04 0.28820E-02 0.33218E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -16.54 26.638 5.6048 7.9967 v Velocity[Y] -18.216 19.642 -0.1431 -0.0006731 v Velocity[Z] -3.0531 2.9802 3.1008e-06 -5.3862e-08 v ǁVelocityǁ 0.0010037 27.316 6.864 8.0239 v Pressure -1.0368e+05 2.0585e+05 50071 27755 v TurbVisc 8.3628e-21 0.0049726 0.00013136 9.8579e-06 v CourantNb 1.278e-07 0.01178 0.00016686 4.8969e-06 v FourierNb 1.2425e-07 0.046902 0.00014564 1.9912e-07 v total_pressure -2359 3.0718e+05 1.514e+05 1.2908e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.062 0.10144 0.0029056 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.216e-07 0.052117 0.0003125 5.096e-06 INSTANT 0.875297000E-01 TIME STEP NUMBER 55495 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282699407E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.698116995E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10828E-01 0.20998E+01 Friction velocity uk : 0.10828E-01 0.20998E+01 Dimensionless distance yplus : 0.10454E-01 0.20619E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 4.783924594e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29420E+08 1 0.18608E-09 0.23236E+02 0.18943E+04 c Velocity[X] 0.11681E+02 c Velocity[Y] 0.11555E+02 c Velocity[Z] 0.22867E-05 c Pressure 0.19220E-03 10 0.61821E-04 0.28290E-02 0.26940E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -16.555 26.659 5.6048 7.9967 v Velocity[Y] -18.233 19.659 -0.1431 -0.0006722 v Velocity[Z] -3.053 2.9802 3.0999e-06 -5.3862e-08 v ǁVelocityǁ 0.0010495 27.334 6.8655 8.0241 v Pressure -1.0191e+05 2.076e+05 51634 28586 v TurbVisc 8.8929e-21 0.0049726 0.00013144 9.8761e-06 v CourantNb 1.3592e-07 0.01178 0.00016686 4.897e-06 v FourierNb 1.2425e-07 0.046902 0.00014564 1.9925e-07 v total_pressure -584.31 3.0893e+05 1.5296e+05 1.2991e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0619 0.10144 0.0029055 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2161e-07 0.052116 0.0003125 5.0962e-06 INSTANT 0.875298000E-01 TIME STEP NUMBER 55496 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282704003E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.698559173E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10951E-01 0.20997E+01 Friction velocity uk : 0.10951E-01 0.20997E+01 Dimensionless distance yplus : 0.10573E-01 0.20617E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 4.895024287e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29421E+08 1 0.18603E-09 0.23251E+02 0.18949E+04 c Velocity[X] 0.11693E+02 c Velocity[Y] 0.11558E+02 c Velocity[Z] 0.22877E-05 c Pressure 0.18956E-03 440 0.76869E-04 0.27875E-02 0.31185E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -16.57 26.681 5.6048 7.9968 v Velocity[Y] -18.249 19.676 -0.14309 -0.00067287 v Velocity[Z] -3.0529 2.9802 3.0989e-06 -5.3862e-08 v ǁVelocityǁ 0.0010016 27.352 6.867 8.0243 v Pressure -1.0016e+05 2.0932e+05 53221 29494 v TurbVisc 1.1256e-20 0.0049726 0.00013152 9.8943e-06 v CourantNb 1.3691e-07 0.01178 0.00016687 4.8971e-06 v FourierNb 1.2425e-07 0.046901 0.00014564 1.9938e-07 v total_pressure 1164.5 3.1065e+05 1.5455e+05 1.3082e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0617 0.10143 0.0029053 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2162e-07 0.052115 0.0003125 5.0965e-06 INSTANT 0.875299000E-01 TIME STEP NUMBER 55497 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282708652E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.699016063E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10694E-01 0.20997E+01 Friction velocity uk : 0.10694E-01 0.20997E+01 Dimensionless distance yplus : 0.10324E-01 0.20617E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 4.820619951e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29421E+08 1 0.18599E-09 0.23268E+02 0.18955E+04 c Velocity[X] 0.11705E+02 c Velocity[Y] 0.11563E+02 c Velocity[Z] 0.22836E-05 c Pressure 0.18694E-03 35 0.82746E-04 0.27465E-02 0.29826E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -16.585 26.702 5.6049 7.9969 v Velocity[Y] -18.266 19.693 -0.14308 -0.00067177 v Velocity[Z] -3.0528 2.9802 3.0979e-06 -5.3862e-08 v ǁVelocityǁ 0.00092168 27.37 6.8685 8.0244 v Pressure -98438 2.11e+05 54761 30425 v TurbVisc 8.456e-21 0.0049726 0.0001316 9.9126e-06 v CourantNb 1.3384e-07 0.01178 0.00016687 4.8972e-06 v FourierNb 1.2425e-07 0.046902 0.00014564 1.995e-07 v total_pressure 2887.1 3.1233e+05 1.5609e+05 1.3175e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0617 0.10142 0.0029051 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2163e-07 0.052116 0.00031251 5.0967e-06 INSTANT 0.875300000E-01 TIME STEP NUMBER 55498 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282713407E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.699465239E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10501E-01 0.20997E+01 Friction velocity uk : 0.10501E-01 0.20997E+01 Dimensionless distance yplus : 0.10138E-01 0.20617E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 4.771251837e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29422E+08 1 0.18595E-09 0.23285E+02 0.18962E+04 c Velocity[X] 0.11716E+02 c Velocity[Y] 0.11569E+02 c Velocity[Z] 0.22792E-05 c Pressure 0.18403E-03 231 0.95353E-04 0.27011E-02 0.24558E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -16.6 26.724 5.6049 7.997 v Velocity[Y] -18.282 19.71 -0.14308 -0.00067268 v Velocity[Z] -3.0528 2.9802 3.097e-06 -5.3862e-08 v ǁVelocityǁ 0.00082956 27.388 6.87 8.0246 v Pressure -96744 2.1276e+05 56244 31167 v TurbVisc 9.0103e-21 0.0049726 0.00013169 9.931e-06 v CourantNb 1.3239e-07 0.01178 0.00016687 4.8973e-06 v FourierNb 1.2425e-07 0.046903 0.00014564 1.9963e-07 v total_pressure 4580.7 3.1408e+05 1.5757e+05 1.3249e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0617 0.10141 0.0029049 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2163e-07 0.052117 0.00031251 5.0969e-06 INSTANT 0.875301000E-01 TIME STEP NUMBER 55499 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282718417E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.699927643E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11259E-01 0.20998E+01 Friction velocity uk : 0.11259E-01 0.20998E+01 Dimensionless distance yplus : 0.10870E-01 0.20618E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 4.693406278e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29422E+08 1 0.18591E-09 0.23298E+02 0.18967E+04 c Velocity[X] 0.11729E+02 c Velocity[Y] 0.11570E+02 c Velocity[Z] 0.22749E-05 c Pressure 0.18102E-03 499 0.80950E-04 0.26544E-02 0.26677E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -16.614 26.745 5.605 7.9971 v Velocity[Y] -18.299 19.727 -0.14307 -0.00067263 v Velocity[Z] -3.0527 2.9802 3.096e-06 -5.3862e-08 v ǁVelocityǁ 0.00073127 27.406 6.8715 8.0248 v Pressure -95083 2.1463e+05 57720 32053 v TurbVisc 9.343e-21 0.0049727 0.00013177 9.9493e-06 v CourantNb 1.3118e-07 0.01178 0.00016687 4.8974e-06 v FourierNb 1.2425e-07 0.046904 0.00014564 1.9976e-07 v total_pressure 6241.9 3.1595e+05 1.5904e+05 1.3338e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0618 0.10139 0.0029045 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2164e-07 0.052119 0.00031251 5.0971e-06 INSTANT 0.875302000E-01 TIME STEP NUMBER 55500 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282723462E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.700398073E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12455E-01 0.20999E+01 Friction velocity uk : 0.12455E-01 0.20999E+01 Dimensionless distance yplus : 0.12112E-01 0.20620E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 4.625378532e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29423E+08 1 0.18587E-09 0.23318E+02 0.18974E+04 c Velocity[X] 0.11741E+02 c Velocity[Y] 0.11577E+02 c Velocity[Z] 0.22713E-05 c Pressure 0.17692E-03 10 0.60306E-04 0.25918E-02 0.21643E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -16.629 26.767 5.605 7.9972 v Velocity[Y] -18.315 19.744 -0.14307 -0.00067174 v Velocity[Z] -3.0526 2.9802 3.095e-06 -5.3862e-08 v ǁVelocityǁ 0.00063185 27.425 6.873 8.025 v Pressure -93545 2.1646e+05 59129 32805 v TurbVisc 9.8916e-21 0.0049727 0.00013185 9.9677e-06 v CourantNb 1.3179e-07 0.01178 0.00016687 4.8975e-06 v FourierNb 1.2425e-07 0.046907 0.00014564 1.9989e-07 v total_pressure 7779.8 3.1779e+05 1.6045e+05 1.3413e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.062 0.10138 0.0029041 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2165e-07 0.052122 0.00031251 5.0974e-06 INSTANT 0.875303000E-01 TIME STEP NUMBER 55501 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282728692E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.700876166E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12362E-01 0.21001E+01 Friction velocity uk : 0.12362E-01 0.21001E+01 Dimensionless distance yplus : 0.12022E-01 0.20622E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 4.626890766e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29423E+08 1 0.18583E-09 0.23335E+02 0.18980E+04 c Velocity[X] 0.11753E+02 c Velocity[Y] 0.11581E+02 c Velocity[Z] 0.22687E-05 c Pressure 0.17372E-03 279 0.76856E-04 0.25425E-02 0.24833E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -16.644 26.788 5.6051 7.9973 v Velocity[Y] -18.332 19.762 -0.14307 -0.00067232 v Velocity[Z] -3.0525 2.9802 3.0941e-06 -5.3862e-08 v ǁVelocityǁ 0.00055369 27.443 6.8745 8.0252 v Pressure -92172 2.1826e+05 60557 33610 v TurbVisc 1.2745e-20 0.0049727 0.00013193 9.9861e-06 v CourantNb 1.3241e-07 0.01178 0.00016688 4.8976e-06 v FourierNb 1.2425e-07 0.046909 0.00014564 2.0002e-07 v total_pressure 9152.9 3.1959e+05 1.6188e+05 1.3493e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0622 0.10135 0.0029037 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2166e-07 0.052124 0.00031252 5.0976e-06 INSTANT 0.875304000E-01 TIME STEP NUMBER 55502 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282733978E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.701366800E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12759E-01 0.21005E+01 Friction velocity uk : 0.12759E-01 0.21005E+01 Dimensionless distance yplus : 0.12407E-01 0.20625E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 4.524655378e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29424E+08 1 0.18579E-09 0.23354E+02 0.18988E+04 c Velocity[X] 0.11767E+02 c Velocity[Y] 0.11587E+02 c Velocity[Z] 0.22630E-05 c Pressure 0.17053E-03 35 0.82437E-04 0.24935E-02 0.24351E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -16.659 26.809 5.6052 7.9974 v Velocity[Y] -18.348 19.779 -0.14306 -0.00067139 v Velocity[Z] -3.0524 2.9801 3.0931e-06 -5.3862e-08 v ǁVelocityǁ 0.00050703 27.462 6.876 8.0254 v Pressure -90858 2.2001e+05 61936 34452 v TurbVisc 6.9144e-21 0.0049727 0.00013202 1.0005e-05 v CourantNb 1.296e-07 0.01178 0.00016688 4.8977e-06 v FourierNb 1.2425e-07 0.046912 0.00014564 2.0015e-07 v total_pressure 10467 3.2134e+05 1.6326e+05 1.3578e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0625 0.10133 0.0029032 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2167e-07 0.052128 0.00031252 5.0978e-06 INSTANT 0.875305000E-01 TIME STEP NUMBER 55503 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282739344E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.701848976E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13537E-01 0.21008E+01 Friction velocity uk : 0.13537E-01 0.21008E+01 Dimensionless distance yplus : 0.13165E-01 0.20628E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 4.501542587e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29424E+08 1 0.18575E-09 0.23373E+02 0.18995E+04 c Velocity[X] 0.11779E+02 c Velocity[Y] 0.11594E+02 c Velocity[Z] 0.22578E-05 c Pressure 0.16713E-03 244 0.94813E-04 0.24414E-02 0.19774E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -16.674 26.831 5.6052 7.9976 v Velocity[Y] -18.365 19.797 -0.14306 -0.00067235 v Velocity[Z] -3.0524 2.9801 3.0922e-06 -5.3862e-08 v ǁVelocityǁ 0.00050496 27.481 6.8775 8.0255 v Pressure -89602 2.2173e+05 63249 35104 v TurbVisc 8.5034e-21 0.0049727 0.0001321 1.0023e-05 v CourantNb 1.1116e-07 0.01178 0.00016688 4.8978e-06 v FourierNb 1.2425e-07 0.046916 0.00014564 2.0028e-07 v total_pressure 11723 3.2305e+05 1.6457e+05 1.3643e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0628 0.1013 0.0029026 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2168e-07 0.052133 0.00031252 5.0981e-06 INSTANT 0.875306000E-01 TIME STEP NUMBER 55504 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282744952E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.702342233E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12177E-01 0.21013E+01 Friction velocity uk : 0.12177E-01 0.21013E+01 Dimensionless distance yplus : 0.11744E-01 0.20633E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 4.532810300e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29425E+08 1 0.18572E-09 0.23389E+02 0.19001E+04 c Velocity[X] 0.11792E+02 c Velocity[Y] 0.11597E+02 c Velocity[Z] 0.22551E-05 c Pressure 0.16368E-03 106 0.80477E-04 0.23888E-02 0.21760E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -16.689 26.852 5.6053 7.9977 v Velocity[Y] -18.381 19.815 -0.14306 -0.00067219 v Velocity[Z] -3.0523 2.9801 3.0912e-06 -5.3862e-08 v ǁVelocityǁ 0.00055243 27.5 6.879 8.0257 v Pressure -88406 2.2339e+05 64552 35901 v TurbVisc 1.9518e-21 0.0049727 0.00013218 1.0042e-05 v CourantNb 9.4784e-08 0.01178 0.00016688 4.8979e-06 v FourierNb 1.2425e-07 0.04692 0.00014564 2.0041e-07 v total_pressure 12919 3.2472e+05 1.6588e+05 1.3723e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0633 0.10127 0.002902 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2168e-07 0.052138 0.00031252 5.0983e-06 INSTANT 0.875307000E-01 TIME STEP NUMBER 55505 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282750586E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.702842143E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.71700E-02 0.21018E+01 Friction velocity uk : 0.71700E-02 0.21018E+01 Dimensionless distance yplus : 0.69152E-02 0.20637E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 4.633902958e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29425E+08 1 0.18568E-09 0.23410E+02 0.19009E+04 c Velocity[X] 0.11805E+02 c Velocity[Y] 0.11605E+02 c Velocity[Z] 0.22531E-05 c Pressure 0.15913E-03 10 0.58467E-04 0.23201E-02 0.16778E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -16.704 26.873 5.6054 7.9978 v Velocity[Y] -18.398 19.833 -0.14306 -0.0006715 v Velocity[Z] -3.0522 2.9801 3.0902e-06 -5.3863e-08 v ǁVelocityǁ 0.00065573 27.519 6.8806 8.0259 v Pressure -87274 2.2501e+05 65789 36538 v TurbVisc 1.1275e-20 0.0049728 0.00013227 1.006e-05 v CourantNb 7.6848e-08 0.01178 0.00016689 4.898e-06 v FourierNb 1.2425e-07 0.046925 0.00014563 2.0054e-07 v total_pressure 14051 3.2633e+05 1.6711e+05 1.3786e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0637 0.10124 0.0029013 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2169e-07 0.052144 0.00031252 5.0986e-06 INSTANT 0.875308000E-01 TIME STEP NUMBER 55506 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282756361E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.703348419E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.95754E-02 0.21023E+01 Friction velocity uk : 0.95754E-02 0.21023E+01 Dimensionless distance yplus : 0.92352E-02 0.20643E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 4.897334153e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29426E+08 1 0.18564E-09 0.23429E+02 0.19016E+04 c Velocity[X] 0.11819E+02 c Velocity[Y] 0.11611E+02 c Velocity[Z] 0.22530E-05 c Pressure 0.15575E-03 159 0.75726E-04 0.22686E-02 0.20231E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -16.719 26.895 5.6055 7.9979 v Velocity[Y] -18.414 19.851 -0.14306 -0.00067212 v Velocity[Z] -3.0521 2.9801 3.0893e-06 -5.3863e-08 v ǁVelocityǁ 0.00078799 27.538 6.8821 8.0261 v Pressure -86209 2.2656e+05 67017 37255 v TurbVisc 1.3801e-20 0.0049728 0.00013235 1.0079e-05 v CourantNb 5.7996e-08 0.01178 0.00016689 4.8982e-06 v FourierNb 1.2425e-07 0.04693 0.00014563 2.0067e-07 v total_pressure 15116 3.2789e+05 1.6834e+05 1.3858e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0643 0.1012 0.0029007 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.217e-07 0.052149 0.00031252 5.0988e-06 INSTANT 0.875309000E-01 TIME STEP NUMBER 55507 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282762215E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.703863438E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13348E-01 0.21029E+01 Friction velocity uk : 0.13348E-01 0.21029E+01 Dimensionless distance yplus : 0.13210E-01 0.20649E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 5.019888975e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29426E+08 1 0.18561E-09 0.23450E+02 0.19024E+04 c Velocity[X] 0.11833E+02 c Velocity[Y] 0.11618E+02 c Velocity[Z] 0.22521E-05 c Pressure 0.15224E-03 109 0.80887E-04 0.22154E-02 0.19735E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -16.734 26.916 5.6056 7.998 v Velocity[Y] -18.431 19.869 -0.14306 -0.00067126 v Velocity[Z] -3.052 2.9801 3.0883e-06 -5.3863e-08 v ǁVelocityǁ 0.00092335 27.557 6.8836 8.0263 v Pressure -85206 2.2805e+05 68216 37989 v TurbVisc 1.1137e-20 0.0049728 0.00013244 1.0098e-05 v CourantNb 4.4024e-08 0.01178 0.00016689 4.8983e-06 v FourierNb 1.2425e-07 0.046935 0.00014563 2.008e-07 v total_pressure 16119 3.2938e+05 1.6954e+05 1.3931e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0649 0.10116 0.0029 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2171e-07 0.052156 0.00031252 5.0991e-06 INSTANT 0.875310000E-01 TIME STEP NUMBER 55508 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282768118E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.704375980E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.68727E-02 0.21036E+01 Friction velocity uk : 0.68727E-02 0.21036E+01 Dimensionless distance yplus : 0.68019E-02 0.20655E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 5.368224341e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29427E+08 1 0.18557E-09 0.23471E+02 0.19031E+04 c Velocity[X] 0.11845E+02 c Velocity[Y] 0.11626E+02 c Velocity[Z] 0.22538E-05 c Pressure 0.14876E-03 195 0.93332E-04 0.21627E-02 0.15964E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -16.749 26.937 5.6057 7.9981 v Velocity[Y] -18.447 19.888 -0.14306 -0.00067226 v Velocity[Z] -3.0519 2.9801 3.0874e-06 -5.3863e-08 v ǁVelocityǁ 0.0008392 27.577 6.8852 8.0265 v Pressure -84264 2.2949e+05 69338 38543 v TurbVisc 1.2879e-20 0.0049728 0.00013252 1.0117e-05 v CourantNb 2.1907e-08 0.01178 0.00016689 4.8984e-06 v FourierNb 1.2425e-07 0.046941 0.00014563 2.0093e-07 v total_pressure 17061 3.3081e+05 1.7066e+05 1.3987e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0655 0.10112 0.0028993 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2172e-07 0.052163 0.00031252 5.0993e-06 INSTANT 0.875311000E-01 TIME STEP NUMBER 55509 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282774243E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.704895126E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13411E-01 0.21042E+01 Friction velocity uk : 0.13411E-01 0.21042E+01 Dimensionless distance yplus : 0.13000E-01 0.20662E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 5.777119844e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29427E+08 1 0.18554E-09 0.23488E+02 0.19038E+04 c Velocity[X] 0.11859E+02 c Velocity[Y] 0.11629E+02 c Velocity[Z] 0.22571E-05 c Pressure 0.14531E-03 113 0.79113E-04 0.21105E-02 0.17595E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -16.764 26.958 5.6058 7.9983 v Velocity[Y] -18.464 19.906 -0.14306 -0.00067214 v Velocity[Z] -3.0519 2.9801 3.0864e-06 -5.3863e-08 v ǁVelocityǁ 0.00074877 27.596 6.8867 8.0267 v Pressure -83380 2.3086e+05 70447 39237 v TurbVisc 1.1775e-20 0.0049728 0.00013261 1.0135e-05 v CourantNb 1.8986e-08 0.01178 0.0001669 4.8985e-06 v FourierNb 1.2425e-07 0.046947 0.00014563 2.0106e-07 v total_pressure 17945 3.3218e+05 1.7177e+05 1.4056e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0662 0.10108 0.0028986 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2173e-07 0.05217 0.00031253 5.0996e-06 INSTANT 0.875312000E-01 TIME STEP NUMBER 55510 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282780381E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.705420954E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11401E-01 0.21049E+01 Friction velocity uk : 0.11401E-01 0.21049E+01 Dimensionless distance yplus : 0.11051E-01 0.20669E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 6.276747853e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29428E+08 1 0.18550E-09 0.23510E+02 0.19046E+04 c Velocity[X] 0.11872E+02 c Velocity[Y] 0.11638E+02 c Velocity[Z] 0.22708E-05 c Pressure 0.14072E-03 9 0.56574E-04 0.20419E-02 0.12933E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -16.779 26.979 5.6059 7.9984 v Velocity[Y] -18.481 19.925 -0.14306 -0.00067151 v Velocity[Z] -3.0518 2.9801 3.0854e-06 -5.3863e-08 v ǁVelocityǁ 0.00065064 27.616 6.8883 8.0269 v Pressure -82554 2.3216e+05 71499 39763 v TurbVisc 1.1009e-20 0.0049728 0.00013269 1.0154e-05 v CourantNb 4.6431e-08 0.01178 0.0001669 4.8986e-06 v FourierNb 1.2425e-07 0.046953 0.00014563 2.0119e-07 v total_pressure 18771 3.3349e+05 1.7282e+05 1.4109e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0669 0.10103 0.0028979 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2174e-07 0.052178 0.00031253 5.0998e-06 INSTANT 0.875313000E-01 TIME STEP NUMBER 55511 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282786627E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.705952675E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10757E-01 0.21057E+01 Friction velocity uk : 0.10757E-01 0.21057E+01 Dimensionless distance yplus : 0.10427E-01 0.20676E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 6.975372789e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29428E+08 1 0.18547E-09 0.23529E+02 0.19053E+04 c Velocity[X] 0.11885E+02 c Velocity[Y] 0.11643E+02 c Velocity[Z] 0.22743E-05 c Pressure 0.13762E-03 135 0.99381E-04 0.19950E-02 0.15654E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -16.794 27.001 5.6061 7.9985 v Velocity[Y] -18.498 19.943 -0.14307 -0.00067118 v Velocity[Z] -3.0517 2.9801 3.0845e-06 -5.3863e-08 v ǁVelocityǁ 0.00057527 27.635 6.8898 8.0272 v Pressure -81787 2.334e+05 72496 40395 v TurbVisc 7.6984e-21 0.0049728 0.00013278 1.0173e-05 v CourantNb 3.5013e-08 0.01178 0.0001669 4.8987e-06 v FourierNb 1.2425e-07 0.046959 0.00014563 2.0132e-07 v total_pressure 19538 3.3472e+05 1.7382e+05 1.4172e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0676 0.10099 0.0028973 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2175e-07 0.052185 0.00031253 5.1001e-06 INSTANT 0.875314000E-01 TIME STEP NUMBER 55512 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282792956E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.706488446E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12003E-01 0.21064E+01 Friction velocity uk : 0.12003E-01 0.21064E+01 Dimensionless distance yplus : 0.11634E-01 0.20683E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 7.500826668e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29429E+08 1 0.18544E-09 0.23549E+02 0.19060E+04 c Velocity[X] 0.11898E+02 c Velocity[Y] 0.11651E+02 c Velocity[Z] 0.22759E-05 c Pressure 0.13386E-03 34 0.82320E-04 0.19385E-02 0.12738E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -16.809 27.022 5.6062 7.9986 v Velocity[Y] -18.515 19.962 -0.14307 -0.00067137 v Velocity[Z] -3.0516 2.98 3.0835e-06 -5.3863e-08 v ǁVelocityǁ 0.00053726 27.655 6.8914 8.0274 v Pressure -81074 2.3456e+05 73484 40932 v TurbVisc 9.052e-21 0.0049729 0.00013287 1.0192e-05 v CourantNb 5.248e-08 0.01178 0.00016691 4.8989e-06 v FourierNb 1.2425e-07 0.046965 0.00014562 2.0145e-07 v total_pressure 20251 3.3589e+05 1.7481e+05 1.4226e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0683 0.10094 0.0028967 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2176e-07 0.052193 0.00031253 5.1003e-06 INSTANT 0.875315000E-01 TIME STEP NUMBER 55513 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282799365E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.707033228E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13516E-01 0.21072E+01 Friction velocity uk : 0.13516E-01 0.21072E+01 Dimensionless distance yplus : 0.13101E-01 0.20690E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 8.251067524e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29430E+08 1 0.18540E-09 0.23571E+02 0.19069E+04 c Velocity[X] 0.11911E+02 c Velocity[Y] 0.11660E+02 c Velocity[Z] 0.22927E-05 c Pressure 0.13010E-03 9 0.53453E-04 0.18822E-02 0.11483E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -16.824 27.043 5.6063 7.9988 v Velocity[Y] -18.532 19.981 -0.14308 -0.00067234 v Velocity[Z] -3.0515 2.98 3.0826e-06 -5.3863e-08 v ǁVelocityǁ 0.00053185 27.674 6.893 8.0276 v Pressure -80410 2.3566e+05 74438 41418 v TurbVisc 7.839e-21 0.0049732 0.00013295 1.0211e-05 v CourantNb 6.471e-08 0.01178 0.00016691 4.899e-06 v FourierNb 1.2425e-07 0.046972 0.00014562 2.0159e-07 v total_pressure 20915 3.3699e+05 1.7576e+05 1.4274e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.069 0.10089 0.0028961 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2177e-07 0.052201 0.00031253 5.1006e-06 INSTANT 0.875316000E-01 TIME STEP NUMBER 55514 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282805905E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.707578583E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.68278E-02 0.21079E+01 Friction velocity uk : 0.68278E-02 0.21079E+01 Dimensionless distance yplus : 0.65909E-02 0.20698E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 9.193164477e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29430E+08 1 0.18537E-09 0.23590E+02 0.19076E+04 c Velocity[X] 0.11925E+02 c Velocity[Y] 0.11666E+02 c Velocity[Z] 0.23041E-05 c Pressure 0.12731E-03 27 0.97891E-04 0.18400E-02 0.14272E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -16.839 27.064 5.6065 7.9989 v Velocity[Y] -18.549 20 -0.14308 -0.00067247 v Velocity[Z] -3.0514 2.98 3.0816e-06 -5.3863e-08 v ǁVelocityǁ 0.00053519 27.694 6.8946 8.0278 v Pressure -79793 2.367e+05 75301 42018 v TurbVisc 7.8693e-21 0.0049913 0.00013304 1.023e-05 v CourantNb 4.6823e-08 0.01178 0.00016691 4.8991e-06 v FourierNb 1.2425e-07 0.046978 0.00014562 2.0172e-07 v total_pressure 21532 3.3802e+05 1.7663e+05 1.4334e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0698 0.10083 0.0028956 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2178e-07 0.052209 0.00031253 5.1008e-06 INSTANT 0.875317000E-01 TIME STEP NUMBER 55515 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282812465E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.708125740E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12044E-01 0.21086E+01 Friction velocity uk : 0.12044E-01 0.21086E+01 Dimensionless distance yplus : 0.11657E-01 0.20705E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 9.869161126e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29431E+08 1 0.18534E-09 0.23611E+02 0.19083E+04 c Velocity[X] 0.11938E+02 c Velocity[Y] 0.11673E+02 c Velocity[Z] 0.23108E-05 c Pressure 0.12369E-03 98 0.83244E-04 0.17860E-02 0.11666E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -16.855 27.085 5.6066 7.999 v Velocity[Y] -18.566 20.018 -0.14309 -0.0006724 v Velocity[Z] -3.0514 2.98 3.0807e-06 -5.3863e-08 v ǁVelocityǁ 0.00054348 27.713 6.8961 8.028 v Pressure -79217 2.3767e+05 76152 42533 v TurbVisc 6.9277e-21 0.0050094 0.00013313 1.0249e-05 v CourantNb 4.6758e-08 0.01178 0.00016692 4.8992e-06 v FourierNb 1.2425e-07 0.046984 0.00014562 2.0185e-07 v total_pressure 22108 3.3899e+05 1.7748e+05 1.4386e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0705 0.10078 0.0028952 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2179e-07 0.052216 0.00031254 5.1011e-06 INSTANT 0.875318000E-01 TIME STEP NUMBER 55516 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282819106E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.708687276E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.74253E-02 0.21094E+01 Friction velocity uk : 0.74253E-02 0.21094E+01 Dimensionless distance yplus : 0.72142E-02 0.20712E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.087548042e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29431E+08 1 0.18531E-09 0.23633E+02 0.19092E+04 c Velocity[X] 0.11950E+02 c Velocity[Y] 0.11683E+02 c Velocity[Z] 0.23316E-05 c Pressure 0.12012E-03 9 0.54828E-04 0.17328E-02 0.97606E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -16.87 27.106 5.6068 7.9992 v Velocity[Y] -18.583 20.037 -0.1431 -0.00067184 v Velocity[Z] -3.0513 2.98 3.0797e-06 -5.3863e-08 v ǁVelocityǁ 0.0005589 27.733 6.8977 8.0282 v Pressure -78678 2.3857e+05 76992 42952 v TurbVisc 6.6803e-21 0.0050275 0.00013321 1.0268e-05 v CourantNb 3.4309e-08 0.01178 0.00016692 4.8994e-06 v FourierNb 1.2425e-07 0.04699 0.00014562 2.0198e-07 v total_pressure 22647 3.399e+05 1.7832e+05 1.4428e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0712 0.10073 0.0028948 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.218e-07 0.052224 0.00031254 5.1014e-06 INSTANT 0.875319000E-01 TIME STEP NUMBER 55517 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282825795E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.709248883E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.63508E-02 0.21101E+01 Friction velocity uk : 0.63508E-02 0.21101E+01 Dimensionless distance yplus : 0.61291E-02 0.20719E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.184939333e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29432E+08 1 0.18528E-09 0.23653E+02 0.19099E+04 c Velocity[X] 0.11963E+02 c Velocity[Y] 0.11690E+02 c Velocity[Z] 0.23478E-05 c Pressure 0.11765E-03 394 0.75992E-04 0.16955E-02 0.11454E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -16.885 27.128 5.6069 7.9993 v Velocity[Y] -18.6 20.056 -0.1431 -0.00067256 v Velocity[Z] -3.0512 2.98 3.0788e-06 -5.3863e-08 v ǁVelocityǁ 0.00054979 27.752 6.8993 8.0284 v Pressure -78174 2.3942e+05 77690 43384 v TurbVisc 4.9814e-21 0.0050456 0.0001333 1.0287e-05 v CourantNb 2.0614e-08 0.01178 0.00016692 4.8995e-06 v FourierNb 1.2425e-07 0.046996 0.00014562 2.0212e-07 v total_pressure 23151 3.4074e+05 1.7902e+05 1.4471e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0719 0.10067 0.0028946 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2182e-07 0.052231 0.00031254 5.1016e-06 INSTANT 0.875320000E-01 TIME STEP NUMBER 55518 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282832599E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.709810802E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.14515E-01 0.21107E+01 Friction velocity uk : 0.14515E-01 0.21107E+01 Dimensionless distance yplus : 0.14069E-01 0.20726E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.262734865e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29433E+08 1 0.18525E-09 0.23675E+02 0.19107E+04 c Velocity[X] 0.11976E+02 c Velocity[Y] 0.11699E+02 c Velocity[Z] 0.23604E-05 c Pressure 0.11451E-03 55 0.80359E-04 0.16487E-02 0.11358E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -16.9 27.149 5.6071 7.9994 v Velocity[Y] -18.618 20.075 -0.14311 -0.00067194 v Velocity[Z] -3.0511 2.98 3.0778e-06 -5.3863e-08 v ǁVelocityǁ 0.00054828 27.772 6.9009 8.0287 v Pressure -77699 2.402e+05 78432 43818 v TurbVisc 4.4773e-21 0.0050637 0.00013339 1.0306e-05 v CourantNb 4.3587e-08 0.01178 0.00016693 4.8996e-06 v FourierNb 1.2425e-07 0.047002 0.00014561 2.0225e-07 v total_pressure 23626 3.4152e+05 1.7976e+05 1.4514e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0726 0.10062 0.0028944 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2183e-07 0.052238 0.00031254 5.1019e-06 INSTANT 0.875321000E-01 TIME STEP NUMBER 55519 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282839364E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.710389039E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10903E-01 0.21114E+01 Friction velocity uk : 0.10903E-01 0.21114E+01 Dimensionless distance yplus : 0.10527E-01 0.20732E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.362580197e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29433E+08 1 0.18522E-09 0.23696E+02 0.19115E+04 c Velocity[X] 0.11988E+02 c Velocity[Y] 0.11708E+02 c Velocity[Z] 0.23786E-05 c Pressure 0.11186E-03 728 0.93355E-04 0.16090E-02 0.10430E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -16.916 27.17 5.6072 7.9996 v Velocity[Y] -18.635 20.094 -0.14312 -0.00067294 v Velocity[Z] -3.051 2.98 3.0769e-06 -5.3863e-08 v ǁVelocityǁ 0.00067754 27.791 6.9025 8.0289 v Pressure -77249 2.4092e+05 79101 44184 v TurbVisc 4.1426e-21 0.0050818 0.00013348 1.0325e-05 v CourantNb 3.6112e-08 0.01178 0.00016693 4.8998e-06 v FourierNb 1.2425e-07 0.047007 0.00014561 2.0239e-07 v total_pressure 24076 3.4225e+05 1.8043e+05 1.4551e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0732 0.10058 0.0028944 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2184e-07 0.052245 0.00031255 5.1021e-06 INSTANT 0.875322000E-01 TIME STEP NUMBER 55520 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282846353E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.710965966E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11329E-01 0.21120E+01 Friction velocity uk : 0.11329E-01 0.21120E+01 Dimensionless distance yplus : 0.10982E-01 0.20738E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.455697038e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29434E+08 1 0.18519E-09 0.23713E+02 0.19121E+04 c Velocity[X] 0.12000E+02 c Velocity[Y] 0.11713E+02 c Velocity[Z] 0.23959E-05 c Pressure 0.10934E-03 308 0.78858E-04 0.15711E-02 0.93036E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -16.931 27.192 5.6074 7.9997 v Velocity[Y] -18.652 20.113 -0.14313 -0.00067291 v Velocity[Z] -3.0509 2.98 3.0759e-06 -5.3863e-08 v ǁVelocityǁ 0.0009075 27.81 6.9041 8.0291 v Pressure -76821 2.4159e+05 79725 44568 v TurbVisc 3.5615e-21 0.0050999 0.00013356 1.0345e-05 v CourantNb 6.1392e-08 0.01178 0.00016694 4.8999e-06 v FourierNb 1.2425e-07 0.047013 0.00014561 2.0252e-07 v total_pressure 24504 3.4292e+05 1.8105e+05 1.4589e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0738 0.10055 0.0028945 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2185e-07 0.052251 0.00031255 5.1024e-06 INSTANT 0.875323000E-01 TIME STEP NUMBER 55521 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282853288E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.711549205E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11066E-01 0.21126E+01 Friction velocity uk : 0.11066E-01 0.21126E+01 Dimensionless distance yplus : 0.10726E-01 0.20744E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.539009802e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29434E+08 1 0.18517E-09 0.23735E+02 0.19130E+04 c Velocity[X] 0.12012E+02 c Velocity[Y] 0.11723E+02 c Velocity[Z] 0.24158E-05 c Pressure 0.10532E-03 9 0.53668E-04 0.15119E-02 0.68263E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -16.946 27.213 5.6075 7.9999 v Velocity[Y] -18.67 20.132 -0.14314 -0.00067234 v Velocity[Z] -3.0508 2.9799 3.075e-06 -5.3863e-08 v ǁVelocityǁ 0.001187 27.829 6.9057 8.0293 v Pressure -76413 2.4221e+05 80319 44863 v TurbVisc 3.5833e-21 0.005118 0.00013365 1.0364e-05 v CourantNb 6.0836e-08 0.01178 0.00016694 4.9e-06 v FourierNb 1.2425e-07 0.047018 0.00014561 2.0265e-07 v total_pressure 24912 3.4354e+05 1.8164e+05 1.4619e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0744 0.10052 0.0028946 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2186e-07 0.052257 0.00031255 5.1027e-06 INSTANT 0.875324000E-01 TIME STEP NUMBER 55522 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282860280E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.712137701E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13742E-01 0.21132E+01 Friction velocity uk : 0.13742E-01 0.21132E+01 Dimensionless distance yplus : 0.13320E-01 0.20750E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.628905798e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29435E+08 1 0.18514E-09 0.23754E+02 0.19136E+04 c Velocity[X] 0.12024E+02 c Velocity[Y] 0.11730E+02 c Velocity[Z] 0.24343E-05 c Pressure 0.10344E-03 134 0.98941E-04 0.14835E-02 0.76567E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -16.961 27.235 5.6077 8 v Velocity[Y] -18.687 20.151 -0.14315 -0.00067212 v Velocity[Z] -3.0508 2.9799 3.074e-06 -5.3863e-08 v ǁVelocityǁ 0.0014994 27.849 6.9074 8.0296 v Pressure -76022 2.4278e+05 80814 45199 v TurbVisc 3.4762e-21 0.0051362 0.00013374 1.0383e-05 v CourantNb 5.5724e-08 0.01178 0.00016695 4.9002e-06 v FourierNb 1.2425e-07 0.047023 0.00014561 2.0279e-07 v total_pressure 25303 3.441e+05 1.8214e+05 1.4652e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.075 0.10048 0.0028947 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2187e-07 0.052263 0.00031256 5.1029e-06 INSTANT 0.875325000E-01 TIME STEP NUMBER 55523 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282867333E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.712727256E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.16022E-01 0.21137E+01 Friction velocity uk : 0.16022E-01 0.21137E+01 Dimensionless distance yplus : 0.15480E-01 0.20755E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.690584159e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29436E+08 1 0.18511E-09 0.23773E+02 0.19144E+04 c Velocity[X] 0.12035E+02 c Velocity[Y] 0.11738E+02 c Velocity[Z] 0.24516E-05 c Pressure 0.10075E-03 32 0.82712E-04 0.14435E-02 0.58433E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -16.977 27.257 5.6079 8.0002 v Velocity[Y] -18.705 20.17 -0.14316 -0.00067238 v Velocity[Z] -3.0507 2.9799 3.0731e-06 -5.3863e-08 v ǁVelocityǁ 0.0017094 27.868 6.909 8.0298 v Pressure -75647 2.4329e+05 81320 45463 v TurbVisc 2.6905e-21 0.0051543 0.00013383 1.0403e-05 v CourantNb 1.5029e-08 0.01178 0.00016695 4.9003e-06 v FourierNb 1.2425e-07 0.047027 0.00014561 2.0292e-07 v total_pressure 25678 3.4461e+05 1.8265e+05 1.4679e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0755 0.10044 0.0028948 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2188e-07 0.052269 0.00031256 5.1032e-06 INSTANT 0.875326000E-01 TIME STEP NUMBER 55524 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282874424E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.713329934E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.14172E-01 0.21142E+01 Friction velocity uk : 0.14172E-01 0.21142E+01 Dimensionless distance yplus : 0.13671E-01 0.20760E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.752344864e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29436E+08 1 0.18509E-09 0.23795E+02 0.19152E+04 c Velocity[X] 0.12046E+02 c Velocity[Y] 0.11749E+02 c Velocity[Z] 0.24767E-05 c Pressure 0.98187E-04 15 0.52953E-04 0.14053E-02 0.51703E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -16.992 27.278 5.608 8.0003 v Velocity[Y] -18.722 20.188 -0.14318 -0.00067344 v Velocity[Z] -3.0506 2.9799 3.0721e-06 -5.3863e-08 v ǁVelocityǁ 0.0016061 27.886 6.9106 8.03 v Pressure -75284 2.4376e+05 81778 45677 v TurbVisc 2.4836e-21 0.0051725 0.00013392 1.0422e-05 v CourantNb 5.5517e-08 0.01178 0.00016696 4.9004e-06 v FourierNb 1.2425e-07 0.047031 0.00014561 2.0306e-07 v total_pressure 26041 3.4508e+05 1.831e+05 1.47e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.076 0.10039 0.0028949 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2189e-07 0.052274 0.00031257 5.1035e-06 INSTANT 0.875327000E-01 TIME STEP NUMBER 55525 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282881587E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.713930072E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.52117E-02 0.21147E+01 Friction velocity uk : 0.52117E-02 0.21147E+01 Dimensionless distance yplus : 0.50276E-02 0.20764E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.811778495e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29437E+08 1 0.18506E-09 0.23814E+02 0.19159E+04 c Velocity[X] 0.12059E+02 c Velocity[Y] 0.11755E+02 c Velocity[Z] 0.24898E-05 c Pressure 0.96991E-04 30 0.75551E-04 0.13868E-02 0.98662E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -17.007 27.3 5.6082 8.0004 v Velocity[Y] -18.74 20.207 -0.14319 -0.00067275 v Velocity[Z] -3.0505 2.9799 3.0712e-06 -5.3863e-08 v ǁVelocityǁ 0.0015125 27.905 6.9122 8.0302 v Pressure -74934 2.4418e+05 82180 46052 v TurbVisc 2.5772e-21 0.0051907 0.00013401 1.0441e-05 v CourantNb 7.1827e-08 0.01178 0.00016696 4.9006e-06 v FourierNb 1.2425e-07 0.047035 0.00014561 2.0319e-07 v total_pressure 26391 3.4551e+05 1.835e+05 1.4738e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0764 0.10035 0.0028951 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2191e-07 0.052279 0.00031257 5.1038e-06 INSTANT 0.875328000E-01 TIME STEP NUMBER 55526 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282888694E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.714532601E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10615E-01 0.21151E+01 Friction velocity uk : 0.10615E-01 0.21151E+01 Dimensionless distance yplus : 0.10256E-01 0.20769E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.844745732e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29438E+08 1 0.18504E-09 0.23834E+02 0.19166E+04 c Velocity[X] 0.12069E+02 c Velocity[Y] 0.11766E+02 c Velocity[Z] 0.25028E-05 c Pressure 0.95370E-04 377 0.79695E-04 0.13623E-02 0.64622E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -17.023 27.322 5.6083 8.0006 v Velocity[Y] -18.757 20.226 -0.1432 -0.00067379 v Velocity[Z] -3.0504 2.9799 3.0702e-06 -5.3863e-08 v ǁVelocityǁ 0.0014094 27.924 6.9139 8.0305 v Pressure -74595 2.4456e+05 82526 46173 v TurbVisc 1.6472e-21 0.0052088 0.0001341 1.0461e-05 v CourantNb 7.3668e-08 0.01178 0.00016697 4.9007e-06 v FourierNb 1.2425e-07 0.047039 0.00014561 2.0333e-07 v total_pressure 26730 3.4589e+05 1.8385e+05 1.475e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0769 0.10032 0.0028954 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2192e-07 0.052284 0.00031257 5.104e-06 INSTANT 0.875329000E-01 TIME STEP NUMBER 55527 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282895956E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.715144046E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12677E-01 0.21155E+01 Friction velocity uk : 0.12677E-01 0.21155E+01 Dimensionless distance yplus : 0.12328E-01 0.20773E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.877459257e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29438E+08 1 0.18501E-09 0.23854E+02 0.19173E+04 c Velocity[X] 0.12080E+02 c Velocity[Y] 0.11774E+02 c Velocity[Z] 0.25181E-05 c Pressure 0.94311E-04 92 0.92903E-04 0.13459E-02 0.81947E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -17.038 27.344 5.6085 8.0007 v Velocity[Y] -18.775 20.244 -0.14321 -0.00067289 v Velocity[Z] -3.0503 2.9799 3.0693e-06 -5.3863e-08 v ǁVelocityǁ 0.0013072 27.943 6.9155 8.0307 v Pressure -74269 2.449e+05 82838 46378 v TurbVisc 1.1369e-21 0.005227 0.00013419 1.048e-05 v CourantNb 5.4682e-08 0.01178 0.00016697 4.9008e-06 v FourierNb 1.2425e-07 0.047043 0.00014561 2.0346e-07 v total_pressure 27056 3.4623e+05 1.8416e+05 1.477e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0773 0.10028 0.0028956 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2193e-07 0.052288 0.00031258 5.1043e-06 INSTANT 0.875330000E-01 TIME STEP NUMBER 55528 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282903114E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.715756899E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.26535E-02 0.21159E+01 Friction velocity uk : 0.26535E-02 0.21159E+01 Dimensionless distance yplus : 0.25603E-02 0.20777E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.891764281e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29439E+08 1 0.18499E-09 0.23869E+02 0.19179E+04 c Velocity[X] 0.12090E+02 c Velocity[Y] 0.11780E+02 c Velocity[Z] 0.25299E-05 c Pressure 0.93553E-04 250 0.78530E-04 0.13337E-02 0.47164E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -17.053 27.366 5.6086 8.0009 v Velocity[Y] -18.792 20.263 -0.14322 -0.00067314 v Velocity[Z] -3.0502 2.9799 3.0683e-06 -5.3863e-08 v ǁVelocityǁ 0.0012096 27.962 6.9171 8.0309 v Pressure -73956 2.452e+05 83100 46498 v TurbVisc 7.8875e-22 0.0052452 0.00013428 1.05e-05 v CourantNb 1.8862e-08 0.01178 0.00016698 4.901e-06 v FourierNb 1.2425e-07 0.047046 0.0001456 2.036e-07 v total_pressure 27369 3.4653e+05 1.8443e+05 1.4782e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0777 0.10025 0.0028959 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2194e-07 0.052292 0.00031258 5.1046e-06 INSTANT 0.875331000E-01 TIME STEP NUMBER 55529 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282910378E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.716374760E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.96160E-02 0.21163E+01 Friction velocity uk : 0.96160E-02 0.21163E+01 Dimensionless distance yplus : 0.92900E-02 0.20780E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.892551419e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29440E+08 1 0.18496E-09 0.23890E+02 0.19186E+04 c Velocity[X] 0.12099E+02 c Velocity[Y] 0.11790E+02 c Velocity[Z] 0.25424E-05 c Pressure 0.91193E-04 7 0.53267E-04 0.12988E-02 0.28185E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -17.068 27.388 5.6088 8.001 v Velocity[Y] -18.81 20.282 -0.14323 -0.00067398 v Velocity[Z] -3.0501 2.9798 3.0674e-06 -5.3863e-08 v ǁVelocityǁ 0.0011119 27.981 6.9187 8.0312 v Pressure -73659 2.4546e+05 83284 46554 v TurbVisc 5.2121e-22 0.0052634 0.00013437 1.0519e-05 v CourantNb 1.8928e-08 0.01178 0.00016698 4.9011e-06 v FourierNb 1.2425e-07 0.04705 0.0001456 2.0374e-07 v total_pressure 27666 3.4678e+05 1.8461e+05 1.4788e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.078 0.10021 0.0028962 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2195e-07 0.052297 0.00031259 5.1048e-06 INSTANT 0.875332000E-01 TIME STEP NUMBER 55530 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282917686E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.716995528E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.14416E-01 0.21167E+01 Friction velocity uk : 0.14416E-01 0.21167E+01 Dimensionless distance yplus : 0.13927E-01 0.20784E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.878914538e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29440E+08 1 0.18494E-09 0.23906E+02 0.19192E+04 c Velocity[X] 0.12110E+02 c Velocity[Y] 0.11796E+02 c Velocity[Z] 0.25503E-05 c Pressure 0.91350E-04 91 0.99244E-04 0.12997E-02 0.47683E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -17.084 27.41 5.6089 8.0012 v Velocity[Y] -18.827 20.3 -0.14325 -0.00067423 v Velocity[Z] -3.0501 2.9798 3.0664e-06 -5.3863e-08 v ǁVelocityǁ 0.0010419 27.999 6.9204 8.0314 v Pressure -73382 2.4568e+05 83513 46763 v TurbVisc 2.7369e-22 0.0052816 0.00013446 1.0538e-05 v CourantNb 4.4185e-08 0.01178 0.00016699 4.9012e-06 v FourierNb 1.2425e-07 0.047053 0.0001456 2.0387e-07 v total_pressure 27943 3.47e+05 1.8484e+05 1.4809e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0784 0.10018 0.0028965 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2196e-07 0.052301 0.00031259 5.1051e-06 INSTANT 0.875333000E-01 TIME STEP NUMBER 55531 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282924984E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.717621991E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.90011E-02 0.21170E+01 Friction velocity uk : 0.90011E-02 0.21170E+01 Dimensionless distance yplus : 0.89084E-02 0.20787E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.850077437e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29441E+08 1 0.18492E-09 0.23923E+02 0.19198E+04 c Velocity[X] 0.12119E+02 c Velocity[Y] 0.11804E+02 c Velocity[Z] 0.25561E-05 c Pressure 0.90861E-04 113 0.83208E-04 0.12915E-02 0.17041E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -17.099 27.432 5.6091 8.0013 v Velocity[Y] -18.845 20.319 -0.14326 -0.0006742 v Velocity[Z] -3.05 2.9798 3.0655e-06 -5.3863e-08 v ǁVelocityǁ 0.00097477 28.018 6.922 8.0316 v Pressure -73127 2.4585e+05 83620 46800 v TurbVisc 3.5201e-22 0.0052998 0.00013455 1.0558e-05 v CourantNb 3.8437e-08 0.01178 0.00016699 4.9014e-06 v FourierNb 1.2425e-07 0.047056 0.0001456 2.0401e-07 v total_pressure 28198 3.4718e+05 1.8495e+05 1.4812e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0787 0.10014 0.0028967 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2198e-07 0.052304 0.00031259 5.1054e-06 INSTANT 0.875334000E-01 TIME STEP NUMBER 55532 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282932253E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.718244601E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.45511E-02 0.21174E+01 Friction velocity uk : 0.45511E-02 0.21174E+01 Dimensionless distance yplus : 0.45553E-02 0.20791E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.807498402e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29442E+08 1 0.18490E-09 0.23942E+02 0.19205E+04 c Velocity[X] 0.12128E+02 c Velocity[Y] 0.11814E+02 c Velocity[Z] 0.25649E-05 c Pressure 0.90419E-04 6 0.52467E-04 0.12839E-02 0.24329E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -17.114 27.455 5.6092 8.0015 v Velocity[Y] -18.862 20.337 -0.14327 -0.00067365 v Velocity[Z] -3.0499 2.9798 3.0646e-06 -5.3863e-08 v ǁVelocityǁ 0.00092752 28.037 6.9236 8.0319 v Pressure -72898 2.4599e+05 83654 46808 v TurbVisc 7.0351e-22 0.0053181 0.00013464 1.0578e-05 v CourantNb 3.6192e-08 0.01178 0.000167 4.9015e-06 v FourierNb 1.2425e-07 0.047059 0.0001456 2.0415e-07 v total_pressure 28427 3.4731e+05 1.8498e+05 1.4813e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0791 0.10009 0.0028968 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2199e-07 0.052308 0.0003126 5.1056e-06 INSTANT 0.875335000E-01 TIME STEP NUMBER 55533 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282939496E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.718871459E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.45384E-02 0.21177E+01 Friction velocity uk : 0.45384E-02 0.21177E+01 Dimensionless distance yplus : 0.45427E-02 0.20794E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.766908196e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29442E+08 1 0.18488E-09 0.23958E+02 0.19211E+04 c Velocity[X] 0.12137E+02 c Velocity[Y] 0.11822E+02 c Velocity[Z] 0.25657E-05 c Pressure 0.91469E-04 28 0.75494E-04 0.12976E-02 0.53220E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -17.129 27.477 5.6094 8.0016 v Velocity[Y] -18.88 20.356 -0.14328 -0.00067442 v Velocity[Z] -3.0498 2.9798 3.0636e-06 -5.3863e-08 v ǁVelocityǁ 0.00089212 28.056 6.9252 8.0321 v Pressure -72700 2.4608e+05 83753 46841 v TurbVisc 1.1757e-21 0.0053363 0.00013473 1.0597e-05 v CourantNb 8.1493e-08 0.01178 0.000167 4.9016e-06 v FourierNb 1.2425e-07 0.047062 0.0001456 2.0428e-07 v total_pressure 28625 3.4741e+05 1.8508e+05 1.4817e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0794 0.10004 0.0028968 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.22e-07 0.052312 0.0003126 5.1059e-06 INSTANT 0.875336000E-01 TIME STEP NUMBER 55534 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282946854E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.719506947E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.42826E-02 0.21180E+01 Friction velocity uk : 0.42826E-02 0.21180E+01 Dimensionless distance yplus : 0.42263E-02 0.20797E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.675899517e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29443E+08 1 0.18486E-09 0.23976E+02 0.19217E+04 c Velocity[X] 0.12146E+02 c Velocity[Y] 0.11830E+02 c Velocity[Z] 0.25657E-05 c Pressure 0.92135E-04 47 0.79646E-04 0.13057E-02 0.57028E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -17.144 27.499 5.6095 8.0018 v Velocity[Y] -18.897 20.375 -0.14329 -0.0006738 v Velocity[Z] -3.0497 2.9798 3.0627e-06 -5.3863e-08 v ǁVelocityǁ 0.0008767 28.075 6.9269 8.0323 v Pressure -72536 2.4613e+05 83715 46834 v TurbVisc 6.4437e-22 0.0053545 0.00013482 1.0617e-05 v CourantNb 7.0708e-08 0.01178 0.00016701 4.9018e-06 v FourierNb 1.2425e-07 0.047065 0.0001456 2.0442e-07 v total_pressure 28789 3.4746e+05 1.8504e+05 1.4816e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0797 0.099999 0.0028968 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2201e-07 0.052316 0.0003126 5.1062e-06 INSTANT 0.875337000E-01 TIME STEP NUMBER 55535 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282954076E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.720133478E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11542E-01 0.21184E+01 Friction velocity uk : 0.11542E-01 0.21184E+01 Dimensionless distance yplus : 0.11235E-01 0.20801E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.607107293e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29444E+08 1 0.18484E-09 0.23992E+02 0.19223E+04 c Velocity[X] 0.12153E+02 c Velocity[Y] 0.11839E+02 c Velocity[Z] 0.25656E-05 c Pressure 0.93289E-04 65 0.92584E-04 0.13208E-02 0.69175E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -17.16 27.522 5.6096 8.0019 v Velocity[Y] -18.915 20.393 -0.14329 -0.00067477 v Velocity[Z] -3.0496 2.9798 3.0617e-06 -5.3863e-08 v ǁVelocityǁ 0.00087942 28.094 6.9285 8.0325 v Pressure -72410 2.4614e+05 83650 46767 v TurbVisc 5.6574e-22 0.0053728 0.00013491 1.0637e-05 v CourantNb 9.8109e-08 0.011779 0.00016701 4.9019e-06 v FourierNb 1.2425e-07 0.047068 0.0001456 2.0456e-07 v total_pressure 28915 3.4747e+05 1.8497e+05 1.4809e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0801 0.099989 0.0028969 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2202e-07 0.05232 0.00031261 5.1065e-06 INSTANT 0.875338000E-01 TIME STEP NUMBER 55536 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282961437E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.720767047E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10429E-01 0.21187E+01 Friction velocity uk : 0.10429E-01 0.21187E+01 Dimensionless distance yplus : 0.10062E-01 0.20804E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.517829981e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29444E+08 1 0.18482E-09 0.24005E+02 0.19227E+04 c Velocity[X] 0.12161E+02 c Velocity[Y] 0.11844E+02 c Velocity[Z] 0.25656E-05 c Pressure 0.94684E-04 75 0.78030E-04 0.13392E-02 0.40679E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -17.175 27.544 5.6098 8.0021 v Velocity[Y] -18.932 20.412 -0.1433 -0.00067476 v Velocity[Z] -3.0495 2.9797 3.0608e-06 -5.3863e-08 v ǁVelocityǁ 0.00090144 28.113 6.9301 8.0328 v Pressure -72328 2.4611e+05 83541 46711 v TurbVisc 8.3931e-22 0.005391 0.00013501 1.0656e-05 v CourantNb 9.862e-08 0.011779 0.00016701 4.902e-06 v FourierNb 1.2425e-07 0.047071 0.0001456 2.047e-07 v total_pressure 28997 3.4743e+05 1.8487e+05 1.4804e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0804 0.099967 0.0028969 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2203e-07 0.052323 0.00031261 5.1067e-06 INSTANT 0.875339000E-01 TIME STEP NUMBER 55537 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282968693E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.721401478E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10769E-01 0.21191E+01 Friction velocity uk : 0.10769E-01 0.21191E+01 Dimensionless distance yplus : 0.10390E-01 0.20807E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.420885256e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29445E+08 1 0.18481E-09 0.24022E+02 0.19234E+04 c Velocity[X] 0.12169E+02 c Velocity[Y] 0.11853E+02 c Velocity[Z] 0.25633E-05 c Pressure 0.94456E-04 7 0.52676E-04 0.13346E-02 0.27162E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -17.19 27.566 5.6099 8.0022 v Velocity[Y] -18.95 20.431 -0.14331 -0.00067412 v Velocity[Z] -3.0494 2.9797 3.0598e-06 -5.3863e-08 v ǁVelocityǁ 0.00094585 28.132 6.9317 8.033 v Pressure -72296 2.4602e+05 83400 46665 v TurbVisc 5.711e-22 0.0054093 0.0001351 1.0676e-05 v CourantNb 9.2895e-08 0.011779 0.00016702 4.9022e-06 v FourierNb 1.2425e-07 0.047074 0.0001456 2.0483e-07 v total_pressure 29029 3.4735e+05 1.8473e+05 1.4799e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0807 0.09994 0.0028967 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2205e-07 0.052327 0.00031261 5.107e-06 INSTANT 0.875340000E-01 TIME STEP NUMBER 55538 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282975909E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.722037056E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12577E-01 0.21194E+01 Friction velocity uk : 0.12577E-01 0.21194E+01 Dimensionless distance yplus : 0.12135E-01 0.20811E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.305281881e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29446E+08 1 0.18479E-09 0.24035E+02 0.19238E+04 c Velocity[X] 0.12175E+02 c Velocity[Y] 0.11860E+02 c Velocity[Z] 0.25585E-05 c Pressure 0.96636E-04 15 0.98488E-04 0.13641E-02 0.55199E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -17.205 27.588 5.61 8.0024 v Velocity[Y] -18.967 20.45 -0.14331 -0.00067405 v Velocity[Z] -3.0493 2.9797 3.0589e-06 -5.3863e-08 v ǁVelocityǁ 0.00101 28.151 6.9333 8.0332 v Pressure -72320 2.4588e+05 83154 46423 v TurbVisc 2.6499e-22 0.0054276 0.00013519 1.0696e-05 v CourantNb 8.7992e-08 0.011779 0.00016702 4.9023e-06 v FourierNb 1.2425e-07 0.047077 0.0001456 2.0497e-07 v total_pressure 29005 3.4721e+05 1.8448e+05 1.4775e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0811 0.099912 0.0028964 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2206e-07 0.052331 0.00031262 5.1073e-06 INSTANT 0.875341000E-01 TIME STEP NUMBER 55539 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282983119E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.722675359E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.64413E-02 0.21198E+01 Friction velocity uk : 0.64413E-02 0.21198E+01 Dimensionless distance yplus : 0.64079E-02 0.20815E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.211623185e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29446E+08 1 0.18477E-09 0.24049E+02 0.19243E+04 c Velocity[X] 0.12182E+02 c Velocity[Y] 0.11867E+02 c Velocity[Z] 0.25498E-05 c Pressure 0.98125E-04 208 0.82663E-04 0.13837E-02 0.29112E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -17.22 27.611 5.6101 8.0025 v Velocity[Y] -18.984 20.469 -0.14332 -0.00067424 v Velocity[Z] -3.0493 2.9797 3.058e-06 -5.3863e-08 v ǁVelocityǁ 0.0010966 28.171 6.9349 8.0335 v Pressure -72405 2.457e+05 82942 46308 v TurbVisc 8.8727e-22 0.0054459 0.00013528 1.0716e-05 v CourantNb 8.4067e-08 0.011779 0.00016703 4.9024e-06 v FourierNb 1.2425e-07 0.047081 0.0001456 2.0511e-07 v total_pressure 28920 3.4702e+05 1.8427e+05 1.4763e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0815 0.099878 0.0028961 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2207e-07 0.052335 0.00031262 5.1075e-06 INSTANT 0.875342000E-01 TIME STEP NUMBER 55540 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282990349E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.723309824E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.80327E-02 0.21202E+01 Friction velocity uk : 0.80327E-02 0.21202E+01 Dimensionless distance yplus : 0.79910E-02 0.20818E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.090036435e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29447E+08 1 0.18476E-09 0.24066E+02 0.19249E+04 c Velocity[X] 0.12189E+02 c Velocity[Y] 0.11877E+02 c Velocity[Z] 0.25445E-05 c Pressure 0.99615E-04 12 0.52388E-04 0.14033E-02 0.41667E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -17.235 27.633 5.6102 8.0026 v Velocity[Y] -19.002 20.488 -0.14332 -0.00067502 v Velocity[Z] -3.0492 2.9797 3.057e-06 -5.3863e-08 v ǁVelocityǁ 0.0012093 28.19 6.9365 8.0337 v Pressure -72554 2.4546e+05 82621 46153 v TurbVisc 1.4428e-22 0.0054641 0.00013537 1.0736e-05 v CourantNb 8.0295e-08 0.011779 0.00016703 4.9026e-06 v FourierNb 1.2425e-07 0.047084 0.0001456 2.0525e-07 v total_pressure 28771 3.4679e+05 1.8395e+05 1.4748e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0818 0.099853 0.0028957 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2208e-07 0.052339 0.00031262 5.1078e-06 INSTANT 0.875343000E-01 TIME STEP NUMBER 55541 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282997564E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.723946788E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13741E-01 0.21205E+01 Friction velocity uk : 0.13741E-01 0.21205E+01 Dimensionless distance yplus : 0.13302E-01 0.20822E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 9.688055602e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29447E+08 1 0.18474E-09 0.24079E+02 0.19254E+04 c Velocity[X] 0.12195E+02 c Velocity[Y] 0.11884E+02 c Velocity[Z] 0.25405E-05 c Pressure 0.10246E-03 242 0.75216E-04 0.14420E-02 0.73152E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -17.25 27.655 5.6103 8.0028 v Velocity[Y] -19.019 20.507 -0.14333 -0.00067432 v Velocity[Z] -3.0491 2.9797 3.0561e-06 -5.3863e-08 v ǁVelocityǁ 0.0013338 28.21 6.9381 8.0339 v Pressure -72772 2.4517e+05 82302 45936 v TurbVisc 1.7784e-22 0.0054824 0.00013547 1.0755e-05 v CourantNb 8.4614e-08 0.011779 0.00016703 4.9027e-06 v FourierNb 1.2425e-07 0.047087 0.0001456 2.0539e-07 v total_pressure 28553 3.4649e+05 1.8363e+05 1.4726e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0822 0.099828 0.0028953 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2209e-07 0.052343 0.00031263 5.1081e-06 INSTANT 0.875344000E-01 TIME STEP NUMBER 55542 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283004676E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.724588362E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13951E-01 0.21209E+01 Friction velocity uk : 0.13951E-01 0.21209E+01 Dimensionless distance yplus : 0.13505E-01 0.20826E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 8.748408329e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29448E+08 1 0.18473E-09 0.24093E+02 0.19259E+04 c Velocity[X] 0.12201E+02 c Velocity[Y] 0.11893E+02 c Velocity[Z] 0.25350E-05 c Pressure 0.10483E-03 52 0.79426E-04 0.14739E-02 0.77150E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -17.266 27.677 5.6104 8.0029 v Velocity[Y] -19.036 20.526 -0.14333 -0.00067511 v Velocity[Z] -3.049 2.9797 3.0552e-06 -5.3863e-08 v ǁVelocityǁ 0.0014834 28.23 6.9398 8.0342 v Pressure -73062 2.4482e+05 81903 45709 v TurbVisc 3.8764e-22 0.0055007 0.00013556 1.0775e-05 v CourantNb 9.189e-08 0.011779 0.00016703 4.9028e-06 v FourierNb 1.2425e-07 0.047091 0.0001456 2.0553e-07 v total_pressure 28263 3.4614e+05 1.8323e+05 1.4703e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0826 0.0998 0.0028947 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2211e-07 0.052348 0.00031263 5.1083e-06 INSTANT 0.875345000E-01 TIME STEP NUMBER 55543 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283011866E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.725220645E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13348E-01 0.21213E+01 Friction velocity uk : 0.13348E-01 0.21213E+01 Dimensionless distance yplus : 0.12879E-01 0.20829E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 7.511883000e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29449E+08 1 0.18472E-09 0.24107E+02 0.19263E+04 c Velocity[X] 0.12207E+02 c Velocity[Y] 0.11900E+02 c Velocity[Z] 0.25277E-05 c Pressure 0.10765E-03 542 0.92655E-04 0.15121E-02 0.84911E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -17.281 27.7 5.6105 8.0031 v Velocity[Y] -19.054 20.545 -0.14333 -0.00067406 v Velocity[Z] -3.0489 2.9797 3.0542e-06 -5.3863e-08 v ǁVelocityǁ 0.0015623 28.25 6.9414 8.0344 v Pressure -73428 2.4441e+05 81466 45475 v TurbVisc 4.8318e-22 0.0055191 0.00013565 1.0795e-05 v CourantNb 8.7804e-08 0.011779 0.00016704 4.9029e-06 v FourierNb 1.2425e-07 0.047094 0.0001456 2.0567e-07 v total_pressure 27897 3.4573e+05 1.8279e+05 1.468e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0829 0.099774 0.0028941 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2212e-07 0.052352 0.00031263 5.1086e-06 INSTANT 0.875346000E-01 TIME STEP NUMBER 55544 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283018866E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.725857315E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.68126E-02 0.21217E+01 Friction velocity uk : 0.68126E-02 0.21217E+01 Dimensionless distance yplus : 0.65732E-02 0.20833E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 6.386299812e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29449E+08 1 0.18470E-09 0.24116E+02 0.19266E+04 c Velocity[X] 0.12211E+02 c Velocity[Y] 0.11905E+02 c Velocity[Z] 0.25216E-05 c Pressure 0.11066E-03 82 0.78337E-04 0.15527E-02 0.84789E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -17.296 27.722 5.6106 8.0032 v Velocity[Y] -19.071 20.564 -0.14333 -0.00067435 v Velocity[Z] -3.0488 2.9796 3.0533e-06 -5.3863e-08 v ǁVelocityǁ 0.0015307 28.27 6.943 8.0346 v Pressure -73872 2.4394e+05 80969 45137 v TurbVisc 3.2376e-22 0.0055374 0.00013574 1.0815e-05 v CourantNb 8.5413e-08 0.011779 0.00016704 4.9031e-06 v FourierNb 1.2425e-07 0.047098 0.0001456 2.0581e-07 v total_pressure 27453 3.4527e+05 1.8229e+05 1.4646e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0833 0.099749 0.0028934 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2213e-07 0.052356 0.00031264 5.1089e-06 INSTANT 0.875347000E-01 TIME STEP NUMBER 55545 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283025908E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.726491707E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12057E-01 0.21221E+01 Friction velocity uk : 0.12057E-01 0.21221E+01 Dimensionless distance yplus : 0.11644E-01 0.20837E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 5.361254424e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29450E+08 1 0.18469E-09 0.24130E+02 0.19271E+04 c Velocity[X] 0.12217E+02 c Velocity[Y] 0.11914E+02 c Velocity[Z] 0.25182E-05 c Pressure 0.11225E-03 9 0.53084E-04 0.15734E-02 0.59256E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -17.311 27.744 5.6106 8.0034 v Velocity[Y] -19.089 20.584 -0.14333 -0.00067506 v Velocity[Z] -3.0487 2.9796 3.0523e-06 -5.3863e-08 v ǁVelocityǁ 0.0015064 28.29 6.9445 8.0348 v Pressure -74396 2.4342e+05 80445 44893 v TurbVisc 7.4123e-22 0.0055557 0.00013584 1.0835e-05 v CourantNb 8.409e-08 0.011779 0.00016704 4.9032e-06 v FourierNb 1.2425e-07 0.047101 0.0001456 2.0594e-07 v total_pressure 26929 3.4474e+05 1.8177e+05 1.4622e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0837 0.099724 0.0028927 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2214e-07 0.05236 0.00031264 5.1091e-06 INSTANT 0.875348000E-01 TIME STEP NUMBER 55546 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283032912E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.727125225E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.82784E-02 0.21224E+01 Friction velocity uk : 0.82784E-02 0.21224E+01 Dimensionless distance yplus : 0.79946E-02 0.20841E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 4.225699225e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29451E+08 1 0.18468E-09 0.24140E+02 0.19275E+04 c Velocity[X] 0.12221E+02 c Velocity[Y] 0.11920E+02 c Velocity[Z] 0.25126E-05 c Pressure 0.11588E-03 133 0.98462E-04 0.16227E-02 0.83848E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -17.326 27.766 5.6107 8.0035 v Velocity[Y] -19.106 20.603 -0.14333 -0.00067538 v Velocity[Z] -3.0486 2.9796 3.0514e-06 -5.3864e-08 v ǁVelocityǁ 0.0014881 28.31 6.9461 8.0351 v Pressure -75024 2.4283e+05 79883 44527 v TurbVisc 7.0839e-22 0.005574 0.00013593 1.0855e-05 v CourantNb 8.4206e-08 0.011779 0.00016704 4.9033e-06 v FourierNb 1.2425e-07 0.047104 0.0001456 2.0608e-07 v total_pressure 26301 3.4416e+05 1.8121e+05 1.4585e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0841 0.0997 0.002892 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2215e-07 0.052364 0.00031264 5.1094e-06 INSTANT 0.875349000E-01 TIME STEP NUMBER 55547 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283039838E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.727758385E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.62438E-02 0.21228E+01 Friction velocity uk : 0.62438E-02 0.21228E+01 Dimensionless distance yplus : 0.61904E-02 0.20844E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 3.539412040e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29451E+08 1 0.18467E-09 0.24151E+02 0.19278E+04 c Velocity[X] 0.12225E+02 c Velocity[Y] 0.11926E+02 c Velocity[Z] 0.25096E-05 c Pressure 0.11881E-03 32 0.82332E-04 0.16621E-02 0.75408E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -17.342 27.788 5.6108 8.0036 v Velocity[Y] -19.124 20.623 -0.14332 -0.00067521 v Velocity[Z] -3.0485 2.9796 3.0505e-06 -5.3864e-08 v ǁVelocityǁ 0.0014736 28.331 6.9477 8.0353 v Pressure -75774 2.4219e+05 79252 44190 v TurbVisc 3.5097e-22 0.0055924 0.00013602 1.0875e-05 v CourantNb 8.4921e-08 0.011779 0.00016705 4.9034e-06 v FourierNb 1.2425e-07 0.047107 0.0001456 2.0622e-07 v total_pressure 25551 3.4352e+05 1.8058e+05 1.4552e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0844 0.099676 0.0028912 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2216e-07 0.052368 0.00031264 5.1097e-06 INSTANT 0.875350000E-01 TIME STEP NUMBER 55548 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283046710E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.728385563E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.56961E-02 0.21232E+01 Friction velocity uk : 0.56961E-02 0.21232E+01 Dimensionless distance yplus : 0.56374E-02 0.20848E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 2.712846986e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29452E+08 1 0.18466E-09 0.24164E+02 0.19283E+04 c Velocity[X] 0.12229E+02 c Velocity[Y] 0.11934E+02 c Velocity[Z] 0.25109E-05 c Pressure 0.12176E-03 9 0.52236E-04 0.17017E-02 0.79464E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -17.357 27.811 5.6108 8.0038 v Velocity[Y] -19.142 20.642 -0.14332 -0.00067423 v Velocity[Z] -3.0484 2.9796 3.0495e-06 -5.3864e-08 v ǁVelocityǁ 0.0014624 28.351 6.9493 8.0355 v Pressure -76592 2.4149e+05 78573 43845 v TurbVisc 1.3094e-21 0.0056107 0.00013612 1.0895e-05 v CourantNb 8.6409e-08 0.011779 0.00016705 4.9036e-06 v FourierNb 1.2425e-07 0.047111 0.0001456 2.0636e-07 v total_pressure 24733 3.4282e+05 1.799e+05 1.4517e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0848 0.099659 0.0028905 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2217e-07 0.052372 0.00031265 5.1099e-06 INSTANT 0.875351000E-01 TIME STEP NUMBER 55549 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283053476E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.729014394E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11065E-01 0.21235E+01 Friction velocity uk : 0.11065E-01 0.21235E+01 Dimensionless distance yplus : 0.10771E-01 0.20851E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.831083459e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29452E+08 1 0.18465E-09 0.24172E+02 0.19285E+04 c Velocity[X] 0.12232E+02 c Velocity[Y] 0.11941E+02 c Velocity[Z] 0.25109E-05 c Pressure 0.12573E-03 24 0.99243E-04 0.17554E-02 0.11593E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -17.373 27.833 5.6109 8.0039 v Velocity[Y] -19.159 20.662 -0.14332 -0.0006741 v Velocity[Z] -3.0483 2.9796 3.0486e-06 -5.3864e-08 v ǁVelocityǁ 0.0014535 28.372 6.9509 8.0357 v Pressure -77474 2.4073e+05 77857 43346 v TurbVisc 7.53e-22 0.0056291 0.00013621 1.0915e-05 v CourantNb 8.8794e-08 0.011779 0.00016705 4.9037e-06 v FourierNb 1.2425e-07 0.047114 0.0001456 2.065e-07 v total_pressure 23851 3.4206e+05 1.7918e+05 1.4467e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0851 0.099643 0.0028898 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2218e-07 0.052376 0.00031265 5.1102e-06 INSTANT 0.875352000E-01 TIME STEP NUMBER 55550 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283060231E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.729641027E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10170E-01 0.21238E+01 Friction velocity uk : 0.10170E-01 0.21238E+01 Dimensionless distance yplus : 0.10204E-01 0.20854E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.438825746e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29453E+08 1 0.18463E-09 0.24182E+02 0.19288E+04 c Velocity[X] 0.12235E+02 c Velocity[Y] 0.11947E+02 c Velocity[Z] 0.25109E-05 c Pressure 0.12906E-03 165 0.84212E-04 0.18000E-02 0.97040E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -17.388 27.855 5.611 8.004 v Velocity[Y] -19.177 20.681 -0.14331 -0.0006742 v Velocity[Z] -3.0482 2.9796 3.0477e-06 -5.3864e-08 v ǁVelocityǁ 0.0014464 28.392 6.9525 8.036 v Pressure -78420 2.3992e+05 77099 42915 v TurbVisc 9.1272e-22 0.0056475 0.0001363 1.0935e-05 v CourantNb 9.1718e-08 0.011779 0.00016705 4.9038e-06 v FourierNb 1.2425e-07 0.047116 0.0001456 2.0664e-07 v total_pressure 22905 3.4125e+05 1.7842e+05 1.4424e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0854 0.099625 0.002889 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.222e-07 0.05238 0.00031265 5.1105e-06 INSTANT 0.875353000E-01 TIME STEP NUMBER 55551 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283066919E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.730263743E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.76879E-02 0.21241E+01 Friction velocity uk : 0.76879E-02 0.21241E+01 Dimensionless distance yplus : 0.77133E-02 0.20857E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 8.853242024e-03 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29454E+08 1 0.18462E-09 0.24193E+02 0.19292E+04 c Velocity[X] 0.12238E+02 c Velocity[Y] 0.11956E+02 c Velocity[Z] 0.25161E-05 c Pressure 0.13225E-03 9 0.54826E-04 0.18427E-02 0.99651E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -17.403 27.877 5.611 8.0042 v Velocity[Y] -19.195 20.701 -0.14331 -0.0006748 v Velocity[Z] -3.0481 2.9795 3.0467e-06 -5.3864e-08 v ǁVelocityǁ 0.001441 28.413 6.9541 8.0362 v Pressure -79430 2.3905e+05 76287 42492 v TurbVisc 1.9843e-22 0.0056658 0.0001364 1.0955e-05 v CourantNb 9.4953e-08 0.011779 0.00016705 4.9039e-06 v FourierNb 1.2425e-07 0.047119 0.0001456 2.0678e-07 v total_pressure 21895 3.4038e+05 1.7761e+05 1.4382e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0857 0.099609 0.0028883 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2221e-07 0.052383 0.00031265 5.1107e-06 INSTANT 0.875354000E-01 TIME STEP NUMBER 55552 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283073547E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.730884039E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12388E-01 0.21244E+01 Friction velocity uk : 0.12388E-01 0.21244E+01 Dimensionless distance yplus : 0.12430E-01 0.20860E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 3.676010262e-03 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29454E+08 1 0.18462E-09 0.24202E+02 0.19295E+04 c Velocity[X] 0.12240E+02 c Velocity[Y] 0.11962E+02 c Velocity[Z] 0.25175E-05 c Pressure 0.13633E-03 152 0.76945E-04 0.18977E-02 0.13018E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -17.419 27.899 5.6111 8.0043 v Velocity[Y] -19.213 20.721 -0.1433 -0.00067405 v Velocity[Z] -3.0481 2.9795 3.0458e-06 -5.3864e-08 v ǁVelocityǁ 0.0014364 28.434 6.9557 8.0364 v Pressure -80498 2.3814e+05 75443 42005 v TurbVisc 2.4154e-22 0.0056842 0.00013649 1.0975e-05 v CourantNb 9.5151e-08 0.011779 0.00016706 4.9041e-06 v FourierNb 1.2425e-07 0.047122 0.0001456 2.0692e-07 v total_pressure 20827 3.3946e+05 1.7677e+05 1.4333e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.086 0.099596 0.0028875 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2222e-07 0.052386 0.00031266 5.111e-06 INSTANT 0.875355000E-01 TIME STEP NUMBER 55553 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283080060E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.731499087E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15134E-01 0.21246E+01 Friction velocity uk : 0.15134E-01 0.21246E+01 Dimensionless distance yplus : 0.14582E-01 0.20862E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 2.664466544e-03 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29455E+08 1 0.18460E-09 0.24211E+02 0.19298E+04 c Velocity[X] 0.12242E+02 c Velocity[Y] 0.11970E+02 c Velocity[Z] 0.25224E-05 c Pressure 0.14005E-03 51 0.81369E-04 0.19475E-02 0.13752E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -17.435 27.921 5.6111 8.0044 v Velocity[Y] -19.231 20.74 -0.14329 -0.00067473 v Velocity[Z] -3.048 2.9795 3.0449e-06 -5.3864e-08 v ǁVelocityǁ 0.0014312 28.454 6.9573 8.0366 v Pressure -81623 2.3717e+05 74547 41489 v TurbVisc 1.7444e-22 0.0057026 0.00013658 1.0996e-05 v CourantNb 9.8205e-08 0.011779 0.00016706 4.9042e-06 v FourierNb 1.2425e-07 0.047124 0.0001456 2.0706e-07 v total_pressure 19702 3.3849e+05 1.7587e+05 1.4281e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0862 0.099582 0.0028868 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2223e-07 0.052389 0.00031266 5.1112e-06 INSTANT 0.875356000E-01 TIME STEP NUMBER 55554 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283086590E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.732114123E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12976E-01 0.21249E+01 Friction velocity uk : 0.12976E-01 0.21249E+01 Dimensionless distance yplus : 0.12826E-01 0.20864E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 4.298013700e-04 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29455E+08 1 0.18460E-09 0.24220E+02 0.19301E+04 c Velocity[X] 0.12244E+02 c Velocity[Y] 0.11976E+02 c Velocity[Z] 0.25288E-05 c Pressure 0.14385E-03 303 0.94678E-04 0.19983E-02 0.14090E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -17.45 27.944 5.6111 8.0046 v Velocity[Y] -19.249 20.76 -0.14329 -0.00067373 v Velocity[Z] -3.0479 2.9795 3.0439e-06 -5.3864e-08 v ǁVelocityǁ 0.0014258 28.475 6.9589 8.0368 v Pressure -82803 2.3615e+05 73608 40974 v TurbVisc 1.624e-22 0.005721 0.00013668 1.1016e-05 v CourantNb 8.3278e-08 0.011779 0.00016706 4.9043e-06 v FourierNb 1.2425e-07 0.047126 0.0001456 2.072e-07 v total_pressure 18522 3.3748e+05 1.7493e+05 1.423e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0864 0.099566 0.0028862 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2224e-07 0.052392 0.00031266 5.1115e-06 INSTANT 0.875357000E-01 TIME STEP NUMBER 55555 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283092870E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.732723223E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.57429E-02 0.21251E+01 Friction velocity uk : 0.57429E-02 0.21251E+01 Dimensionless distance yplus : 0.56767E-02 0.20866E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.961253145e-04 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29456E+08 1 0.18459E-09 0.24224E+02 0.19302E+04 c Velocity[X] 0.12245E+02 c Velocity[Y] 0.11979E+02 c Velocity[Z] 0.25365E-05 c Pressure 0.14765E-03 100 0.80031E-04 0.20490E-02 0.14245E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -17.466 27.966 5.6112 8.0047 v Velocity[Y] -19.267 20.78 -0.14328 -0.00067376 v Velocity[Z] -3.0478 2.9795 3.043e-06 -5.3864e-08 v ǁVelocityǁ 0.0014196 28.496 6.9605 8.0371 v Pressure -84035 2.3509e+05 72635 40406 v TurbVisc 2.5927e-22 0.0057394 0.00013677 1.1036e-05 v CourantNb 7.0895e-08 0.011779 0.00016706 4.9044e-06 v FourierNb 1.2425e-07 0.047128 0.0001456 2.0735e-07 v total_pressure 17290 3.3641e+05 1.7396e+05 1.4173e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0866 0.099551 0.0028855 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2225e-07 0.052394 0.00031267 5.1118e-06 INSTANT 0.875358000E-01 TIME STEP NUMBER 55556 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283099169E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.733328178E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.78721E-02 0.21252E+01 Friction velocity uk : 0.78721E-02 0.21252E+01 Dimensionless distance yplus : 0.77813E-02 0.20868E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.749806100e-04 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29457E+08 1 0.18458E-09 0.24233E+02 0.19305E+04 c Velocity[X] 0.12246E+02 c Velocity[Y] 0.11987E+02 c Velocity[Z] 0.25559E-05 c Pressure 0.15010E-03 9 0.56473E-04 0.20810E-02 0.12353E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -17.482 27.988 5.6112 8.0048 v Velocity[Y] -19.285 20.799 -0.14327 -0.00067436 v Velocity[Z] -3.0477 2.9795 3.0421e-06 -5.3864e-08 v ǁVelocityǁ 0.0014107 28.516 6.9621 8.0373 v Pressure -85314 2.3399e+05 71642 39901 v TurbVisc 1.4762e-22 0.0057578 0.00013686 1.1056e-05 v CourantNb 6.2329e-08 0.011779 0.00016706 4.9045e-06 v FourierNb 1.2425e-07 0.04713 0.0001456 2.0749e-07 v total_pressure 16011 3.3531e+05 1.7297e+05 1.4123e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0868 0.099539 0.0028849 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2226e-07 0.052396 0.00031267 5.112e-06 INSTANT 0.875359000E-01 TIME STEP NUMBER 55557 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283105356E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.733927831E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.52494E-02 0.21253E+01 Friction velocity uk : 0.52494E-02 0.21253E+01 Dimensionless distance yplus : 0.50651E-02 0.20869E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 8.765058586e-04 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29457E+08 1 0.18457E-09 0.24240E+02 0.19307E+04 c Velocity[X] 0.12247E+02 c Velocity[Y] 0.11993E+02 c Velocity[Z] 0.25594E-05 c Pressure 0.15392E-03 136 0.75499E-04 0.21318E-02 0.17282E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -17.498 28.01 5.6113 8.0049 v Velocity[Y] -19.303 20.819 -0.14326 -0.00067357 v Velocity[Z] -3.0476 2.9794 3.0412e-06 -5.3864e-08 v ǁVelocityǁ 0.0014047 28.537 6.9636 8.0375 v Pressure -86634 2.3285e+05 70557 39259 v TurbVisc 1.2172e-21 0.0057762 0.00013696 1.1076e-05 v CourantNb 6.5227e-08 0.011779 0.00016707 4.9047e-06 v FourierNb 1.2425e-07 0.047131 0.00014561 2.0763e-07 v total_pressure 14691 3.3418e+05 1.7188e+05 1.4058e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0869 0.099529 0.0028845 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2227e-07 0.052398 0.00031267 5.1123e-06 INSTANT 0.875360000E-01 TIME STEP NUMBER 55558 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283111444E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.734518542E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.79405E-02 0.21254E+01 Friction velocity uk : 0.79405E-02 0.21254E+01 Dimensionless distance yplus : 0.78489E-02 0.20870E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 3.597606164e-03 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29458E+08 1 0.18456E-09 0.24247E+02 0.19309E+04 c Velocity[X] 0.12247E+02 c Velocity[Y] 0.12001E+02 c Velocity[Z] 0.25659E-05 c Pressure 0.15754E-03 55 0.80674E-04 0.21798E-02 0.17527E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -17.514 28.033 5.6113 8.0051 v Velocity[Y] -19.322 20.838 -0.14325 -0.00067427 v Velocity[Z] -3.0475 2.9794 3.0402e-06 -5.3864e-08 v ǁVelocityǁ 0.0013967 28.557 6.9652 8.0377 v Pressure -88056 2.3168e+05 69454 38613 v TurbVisc 2.3844e-22 0.0057946 0.00013705 1.1097e-05 v CourantNb 6.9785e-08 0.01178 0.00016707 4.9048e-06 v FourierNb 1.2425e-07 0.047132 0.00014561 2.0777e-07 v total_pressure 13269 3.3301e+05 1.7078e+05 1.3994e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.087 0.099522 0.002884 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2228e-07 0.0524 0.00031268 5.1125e-06 INSTANT 0.875361000E-01 TIME STEP NUMBER 55559 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283117517E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.735113711E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.84532E-02 0.21255E+01 Friction velocity uk : 0.84532E-02 0.21255E+01 Dimensionless distance yplus : 0.83557E-02 0.20871E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 6.347262002e-03 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29458E+08 1 0.18455E-09 0.24254E+02 0.19311E+04 c Velocity[X] 0.12248E+02 c Velocity[Y] 0.12006E+02 c Velocity[Z] 0.25775E-05 c Pressure 0.16109E-03 320 0.93345E-04 0.22266E-02 0.17289E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -17.53 28.055 5.6113 8.0052 v Velocity[Y] -19.34 20.857 -0.14324 -0.00067321 v Velocity[Z] -3.0474 2.9794 3.0393e-06 -5.3864e-08 v ǁVelocityǁ 0.001388 28.578 6.9668 8.0379 v Pressure -89522 2.3048e+05 68316 37995 v TurbVisc 1.8187e-22 0.005813 0.00013714 1.1117e-05 v CourantNb 6.995e-08 0.01178 0.00016707 4.9049e-06 v FourierNb 1.2425e-07 0.047134 0.00014561 2.0791e-07 v total_pressure 11803 3.318e+05 1.6964e+05 1.3932e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0871 0.099515 0.0028837 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2229e-07 0.052401 0.00031268 5.1128e-06 INSTANT 0.875362000E-01 TIME STEP NUMBER 55560 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283123326E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.735699690E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.54831E-02 0.21256E+01 Friction velocity uk : 0.54831E-02 0.21256E+01 Dimensionless distance yplus : 0.52906E-02 0.20871E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 9.835211295e-03 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29459E+08 1 0.18454E-09 0.24256E+02 0.19311E+04 c Velocity[X] 0.12247E+02 c Velocity[Y] 0.12009E+02 c Velocity[Z] 0.25866E-05 c Pressure 0.16459E-03 82 0.79390E-04 0.22729E-02 0.18198E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -17.546 28.078 5.6114 8.0053 v Velocity[Y] -19.358 20.877 -0.14323 -0.00067323 v Velocity[Z] -3.0473 2.9794 3.0384e-06 -5.3864e-08 v ǁVelocityǁ 0.0013793 28.598 6.9684 8.0381 v Pressure -91027 2.2924e+05 67143 37307 v TurbVisc 1.3623e-22 0.0058315 0.00013724 1.1137e-05 v CourantNb 7.0224e-08 0.01178 0.00016707 4.905e-06 v FourierNb 1.2425e-07 0.047134 0.00014561 2.0805e-07 v total_pressure 10298 3.3056e+05 1.6847e+05 1.3863e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0871 0.099509 0.0028834 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.223e-07 0.052402 0.00031268 5.1131e-06 INSTANT 0.875363000E-01 TIME STEP NUMBER 55561 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283129133E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.736279594E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.45903E-02 0.21256E+01 Friction velocity uk : 0.45903E-02 0.21256E+01 Dimensionless distance yplus : 0.44291E-02 0.20872E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.377859184e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29459E+08 1 0.18453E-09 0.24264E+02 0.19314E+04 c Velocity[X] 0.12247E+02 c Velocity[Y] 0.12017E+02 c Velocity[Z] 0.26021E-05 c Pressure 0.16688E-03 10 0.57210E-04 0.23021E-02 0.15897E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -17.562 28.1 5.6114 8.0054 v Velocity[Y] -19.377 20.896 -0.14323 -0.00067383 v Velocity[Z] -3.0472 2.9794 3.0374e-06 -5.3864e-08 v ǁVelocityǁ 0.0013686 28.618 6.9701 8.0383 v Pressure -92566 2.2798e+05 65954 36695 v TurbVisc 1.423e-22 0.0058499 0.00013733 1.1157e-05 v CourantNb 7.0676e-08 0.01178 0.00016708 4.9051e-06 v FourierNb 1.2425e-07 0.047135 0.00014561 2.0819e-07 v total_pressure 8758.9 3.293e+05 1.6728e+05 1.3802e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0872 0.099503 0.0028832 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2231e-07 0.052403 0.00031269 5.1133e-06 INSTANT 0.875364000E-01 TIME STEP NUMBER 55562 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283134799E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.736852139E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.51055E-02 0.21256E+01 Friction velocity uk : 0.51055E-02 0.21256E+01 Dimensionless distance yplus : 0.49107E-02 0.20872E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.811466514e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29460E+08 1 0.18453E-09 0.24269E+02 0.19315E+04 c Velocity[X] 0.12246E+02 c Velocity[Y] 0.12022E+02 c Velocity[Z] 0.26092E-05 c Pressure 0.17033E-03 345 0.75096E-04 0.23474E-02 0.21403E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -17.578 28.123 5.6114 8.0055 v Velocity[Y] -19.395 20.915 -0.14322 -0.00067303 v Velocity[Z] -3.0471 2.9794 3.0365e-06 -5.3864e-08 v ǁVelocityǁ 0.0013639 28.638 6.9717 8.0385 v Pressure -94129 2.2669e+05 64684 35947 v TurbVisc 2.0307e-22 0.0058684 0.00013742 1.1177e-05 v CourantNb 7.161e-08 0.01178 0.00016708 4.9052e-06 v FourierNb 1.2425e-07 0.047136 0.00014561 2.0833e-07 v total_pressure 7195.9 3.2802e+05 1.6601e+05 1.3727e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0872 0.099497 0.002883 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2232e-07 0.052404 0.00031269 5.1136e-06 INSTANT 0.875365000E-01 TIME STEP NUMBER 55563 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283140370E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.737413232E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.34364E-02 0.21256E+01 Friction velocity uk : 0.34364E-02 0.21256E+01 Dimensionless distance yplus : 0.33157E-02 0.20872E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 2.188019656e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29460E+08 1 0.18452E-09 0.24274E+02 0.19317E+04 c Velocity[X] 0.12245E+02 c Velocity[Y] 0.12029E+02 c Velocity[Z] 0.26191E-05 c Pressure 0.17366E-03 76 0.80584E-04 0.23909E-02 0.21833E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -17.594 28.145 5.6115 8.0056 v Velocity[Y] -19.413 20.934 -0.14321 -0.00067375 v Velocity[Z] -3.047 2.9793 3.0356e-06 -5.3864e-08 v ǁVelocityǁ 0.0013603 28.659 6.9733 8.0387 v Pressure -95717 2.2539e+05 63392 35185 v TurbVisc 1.3644e-22 0.0058868 0.00013752 1.1198e-05 v CourantNb 7.1844e-08 0.01178 0.00016708 4.9053e-06 v FourierNb 1.2425e-07 0.047136 0.00014561 2.0848e-07 v total_pressure 5608.3 3.2672e+05 1.6472e+05 1.3651e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0872 0.099494 0.0028829 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2233e-07 0.052404 0.00031269 5.1138e-06 INSTANT 0.875366000E-01 TIME STEP NUMBER 55564 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283145901E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.737978878E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.39808E-02 0.21256E+01 Friction velocity uk : 0.39808E-02 0.21256E+01 Dimensionless distance yplus : 0.38289E-02 0.20872E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 2.711398388e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29461E+08 1 0.18451E-09 0.24279E+02 0.19318E+04 c Velocity[X] 0.12245E+02 c Velocity[Y] 0.12034E+02 c Velocity[Z] 0.26244E-05 c Pressure 0.17688E-03 463 0.93083E-04 0.24329E-02 0.21061E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -17.61 28.168 5.6115 8.0057 v Velocity[Y] -19.432 20.953 -0.1432 -0.00067271 v Velocity[Z] -3.0469 2.9793 3.0347e-06 -5.3864e-08 v ǁVelocityǁ 0.0013599 28.678 6.9749 8.0389 v Pressure -97328 2.2406e+05 62074 34475 v TurbVisc 1.5454e-22 0.0059053 0.00013761 1.1218e-05 v CourantNb 4.4473e-08 0.01178 0.00016709 4.9055e-06 v FourierNb 1.2425e-07 0.047137 0.00014561 2.0862e-07 v total_pressure 3996.9 3.2539e+05 1.634e+05 1.358e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0872 0.099492 0.0028828 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2233e-07 0.052405 0.0003127 5.1141e-06 INSTANT 0.875367000E-01 TIME STEP NUMBER 55565 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283151146E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.738533494E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.39373E-02 0.21256E+01 Friction velocity uk : 0.39373E-02 0.21256E+01 Dimensionless distance yplus : 0.37871E-02 0.20872E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 3.206808844e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29461E+08 1 0.18450E-09 0.24279E+02 0.19317E+04 c Velocity[X] 0.12243E+02 c Velocity[Y] 0.12036E+02 c Velocity[Z] 0.26331E-05 c Pressure 0.18007E-03 487 0.79416E-04 0.24743E-02 0.23104E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -17.626 28.19 5.6116 8.0058 v Velocity[Y] -19.45 20.972 -0.14319 -0.00067258 v Velocity[Z] -3.0468 2.9793 3.0337e-06 -5.3864e-08 v ǁVelocityǁ 0.0013634 28.698 6.9765 8.0391 v Pressure -98960 2.2272e+05 60720 33668 v TurbVisc 8.7209e-22 0.0059237 0.0001377 1.1238e-05 v CourantNb 7.3587e-09 0.01178 0.00016709 4.9056e-06 v FourierNb 1.2425e-07 0.047137 0.00014561 2.0876e-07 v total_pressure 2364.5 3.2404e+05 1.6204e+05 1.3499e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0872 0.099489 0.0028828 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2234e-07 0.052406 0.0003127 5.1143e-06 INSTANT 0.875368000E-01 TIME STEP NUMBER 55566 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283156382E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.739080480E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.59140E-02 0.21256E+01 Friction velocity uk : 0.59140E-02 0.21256E+01 Dimensionless distance yplus : 0.56884E-02 0.20871E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 3.657912373e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29462E+08 1 0.18449E-09 0.24285E+02 0.19319E+04 c Velocity[X] 0.12242E+02 c Velocity[Y] 0.12043E+02 c Velocity[Z] 0.26450E-05 c Pressure 0.18215E-03 10 0.58888E-04 0.25004E-02 0.20530E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -17.642 28.213 5.6116 8.0059 v Velocity[Y] -19.468 20.99 -0.14319 -0.00067337 v Velocity[Z] -3.0467 2.9793 3.0328e-06 -5.3864e-08 v ǁVelocityǁ 0.0013727 28.718 6.9781 8.0393 v Pressure -1.0061e+05 2.2135e+05 59345 32941 v TurbVisc 2.0284e-22 0.0059422 0.00013779 1.1259e-05 v CourantNb 4.8945e-08 0.01178 0.00016709 4.9057e-06 v FourierNb 1.2425e-07 0.047138 0.00014561 2.089e-07 v total_pressure 714.64 3.2268e+05 1.6067e+05 1.3427e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0871 0.099484 0.0028827 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2235e-07 0.052406 0.0003127 5.1146e-06 INSTANT 0.875369000E-01 TIME STEP NUMBER 55567 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283161430E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.739618896E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.65899E-02 0.21256E+01 Friction velocity uk : 0.65899E-02 0.21256E+01 Dimensionless distance yplus : 0.63585E-02 0.20872E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 4.164522910e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29462E+08 1 0.18449E-09 0.24288E+02 0.19320E+04 c Velocity[X] 0.12240E+02 c Velocity[Y] 0.12048E+02 c Velocity[Z] 0.26450E-05 c Pressure 0.18535E-03 281 0.75569E-04 0.25418E-02 0.26054E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -17.658 28.235 5.6116 8.0061 v Velocity[Y] -19.487 21.009 -0.14318 -0.00067259 v Velocity[Z] -3.0466 2.9793 3.0319e-06 -5.3864e-08 v ǁVelocityǁ 0.0013877 28.738 6.9797 8.0395 v Pressure -1.0227e+05 2.1997e+05 57927 32110 v TurbVisc 1.94e-22 0.0059607 0.00013789 1.1279e-05 v CourantNb 5.6741e-08 0.01178 0.00016709 4.9058e-06 v FourierNb 1.2425e-07 0.047138 0.00014561 2.0904e-07 v total_pressure -944.99 3.213e+05 1.5925e+05 1.3343e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0872 0.099477 0.0028827 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2236e-07 0.052407 0.00031271 5.1148e-06 INSTANT 0.875370000E-01 TIME STEP NUMBER 55568 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283166408E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.740146559E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.60707E-02 0.21256E+01 Friction velocity uk : 0.60707E-02 0.21256E+01 Dimensionless distance yplus : 0.58391E-02 0.20871E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 4.452998536e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29463E+08 1 0.18448E-09 0.24292E+02 0.19321E+04 c Velocity[X] 0.12238E+02 c Velocity[Y] 0.12054E+02 c Velocity[Z] 0.26449E-05 c Pressure 0.18834E-03 29 0.81570E-04 0.25802E-02 0.27874E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -17.674 28.258 5.6117 8.0061 v Velocity[Y] -19.505 21.028 -0.14317 -0.00067348 v Velocity[Z] -3.0465 2.9793 3.031e-06 -5.3864e-08 v ǁVelocityǁ 0.0014103 28.757 6.9814 8.0397 v Pressure -1.0394e+05 2.1858e+05 56452 31211 v TurbVisc 1.771e-25 0.0059792 0.00013798 1.1299e-05 v CourantNb 5.6717e-08 0.01178 0.0001671 4.9059e-06 v FourierNb 1.2425e-07 0.047139 0.00014561 2.0918e-07 v total_pressure -2617.6 3.199e+05 1.5778e+05 1.3254e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0871 0.099469 0.0028827 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2237e-07 0.052408 0.00031271 5.1151e-06 INSTANT 0.875371000E-01 TIME STEP NUMBER 55569 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283171291E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.740673727E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.43614E-02 0.21256E+01 Friction velocity uk : 0.43614E-02 0.21256E+01 Dimensionless distance yplus : 0.41950E-02 0.20872E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 4.965784484e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29463E+08 1 0.18447E-09 0.24295E+02 0.19321E+04 c Velocity[X] 0.12237E+02 c Velocity[Y] 0.12058E+02 c Velocity[Z] 0.26441E-05 c Pressure 0.19131E-03 348 0.94036E-04 0.26183E-02 0.24825E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -17.691 28.281 5.6117 8.0062 v Velocity[Y] -19.523 21.046 -0.14317 -0.00067234 v Velocity[Z] -3.0464 2.9792 3.03e-06 -5.3864e-08 v ǁVelocityǁ 0.0014394 28.777 6.983 8.0399 v Pressure -1.0563e+05 2.1717e+05 54988 30462 v TurbVisc 3.0382e-22 0.0059977 0.00013807 1.132e-05 v CourantNb 5.7654e-08 0.01178 0.0001671 4.906e-06 v FourierNb 1.2425e-07 0.04714 0.00014561 2.0933e-07 v total_pressure -4304.6 3.1849e+05 1.5631e+05 1.3179e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0872 0.099456 0.0028827 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2238e-07 0.052409 0.00031272 5.1153e-06 INSTANT 0.875372000E-01 TIME STEP NUMBER 55570 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283175917E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.741191614E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.40785E-02 0.21256E+01 Friction velocity uk : 0.40785E-02 0.21256E+01 Dimensionless distance yplus : 0.39687E-02 0.20872E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 5.357428995e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29463E+08 1 0.18446E-09 0.24294E+02 0.19320E+04 c Velocity[X] 0.12234E+02 c Velocity[Y] 0.12060E+02 c Velocity[Z] 0.26438E-05 c Pressure 0.19419E-03 97 0.80111E-04 0.26552E-02 0.29582E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -17.707 28.303 5.6118 8.0063 v Velocity[Y] -19.541 21.065 -0.14317 -0.00067243 v Velocity[Z] -3.0463 2.9792 3.0291e-06 -5.3864e-08 v ǁVelocityǁ 0.0014768 28.796 6.9846 8.04 v Pressure -1.0733e+05 2.1573e+05 53468 29526 v TurbVisc 1.0715e-23 0.0060162 0.00013816 1.134e-05 v CourantNb 3.2749e-08 0.01178 0.00016711 4.9061e-06 v FourierNb 1.2425e-07 0.04714 0.00014561 2.0947e-07 v total_pressure -6006.6 3.1706e+05 1.5479e+05 1.3085e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0872 0.099448 0.0028827 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2238e-07 0.05241 0.00031272 5.1156e-06 INSTANT 0.875373000E-01 TIME STEP NUMBER 55571 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283180486E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.741699412E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.63672E-02 0.21257E+01 Friction velocity uk : 0.63672E-02 0.21257E+01 Dimensionless distance yplus : 0.61243E-02 0.20872E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 5.682866126e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29464E+08 1 0.18445E-09 0.24299E+02 0.19321E+04 c Velocity[X] 0.12233E+02 c Velocity[Y] 0.12065E+02 c Velocity[Z] 0.26476E-05 c Pressure 0.19602E-03 10 0.60438E-04 0.26776E-02 0.25072E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -17.723 28.326 5.6119 8.0064 v Velocity[Y] -19.559 21.083 -0.14316 -0.00067311 v Velocity[Z] -3.0462 2.9792 3.0282e-06 -5.3864e-08 v ǁVelocityǁ 0.0015196 28.815 6.9862 8.0402 v Pressure -1.0905e+05 2.1429e+05 51935 28732 v TurbVisc 5.0023e-22 0.0060347 0.00013826 1.1361e-05 v CourantNb 6.4213e-08 0.011781 0.00016711 4.9062e-06 v FourierNb 1.2425e-07 0.047141 0.00014562 2.0961e-07 v total_pressure -7722 3.1561e+05 1.5326e+05 1.3006e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0872 0.099449 0.0028829 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2239e-07 0.052411 0.00031272 5.1158e-06 INSTANT 0.875374000E-01 TIME STEP NUMBER 55572 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283184865E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.742197608E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.22315E-02 0.21258E+01 Friction velocity uk : 0.22315E-02 0.21258E+01 Dimensionless distance yplus : 0.21853E-02 0.20874E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 6.084590521e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29464E+08 1 0.18445E-09 0.24300E+02 0.19321E+04 c Velocity[X] 0.12230E+02 c Velocity[Y] 0.12069E+02 c Velocity[Z] 0.26389E-05 c Pressure 0.19896E-03 141 0.76174E-04 0.27151E-02 0.32769E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -17.739 28.348 5.6119 8.0065 v Velocity[Y] -19.578 21.102 -0.14316 -0.0006724 v Velocity[Z] -3.0461 2.9792 3.0273e-06 -5.3864e-08 v ǁVelocityǁ 0.0015687 28.834 6.9879 8.0404 v Pressure -1.1077e+05 2.1282e+05 50386 27793 v TurbVisc 4.0758e-22 0.0060532 0.00013835 1.1381e-05 v CourantNb 7.6167e-08 0.011781 0.00016711 4.9063e-06 v FourierNb 1.2425e-07 0.047143 0.00014562 2.0975e-07 v total_pressure -9445.6 3.1414e+05 1.5171e+05 1.2912e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0874 0.099443 0.002883 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.224e-07 0.052413 0.00031273 5.1161e-06 INSTANT 0.875375000E-01 TIME STEP NUMBER 55573 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283189160E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.742686242E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.22637E-02 0.21259E+01 Friction velocity uk : 0.22637E-02 0.21259E+01 Dimensionless distance yplus : 0.22264E-02 0.20875E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 6.146678598e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29465E+08 1 0.18444E-09 0.24302E+02 0.19322E+04 c Velocity[X] 0.12228E+02 c Velocity[Y] 0.12074E+02 c Velocity[Z] 0.26284E-05 c Pressure 0.20153E-03 30 0.82316E-04 0.27475E-02 0.34644E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -17.755 28.371 5.612 8.0066 v Velocity[Y] -19.596 21.12 -0.14316 -0.00067335 v Velocity[Z] -3.046 2.9792 3.0263e-06 -5.3864e-08 v ǁVelocityǁ 0.0016244 28.854 6.9895 8.0406 v Pressure -1.1251e+05 2.1134e+05 48754 26798 v TurbVisc 6.6115e-22 0.0060717 0.00013844 1.1401e-05 v CourantNb 8.989e-08 0.011781 0.00016712 4.9064e-06 v FourierNb 1.2425e-07 0.047144 0.00014562 2.099e-07 v total_pressure -11183 3.1266e+05 1.5008e+05 1.2812e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0875 0.099441 0.0028831 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.224e-07 0.052414 0.00031273 5.1163e-06 INSTANT 0.875376000E-01 TIME STEP NUMBER 55574 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283193348E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.743168090E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.48071E-02 0.21261E+01 Friction velocity uk : 0.48071E-02 0.21261E+01 Dimensionless distance yplus : 0.47723E-02 0.20876E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 6.510926399e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29465E+08 1 0.18443E-09 0.24304E+02 0.19322E+04 c Velocity[X] 0.12226E+02 c Velocity[Y] 0.12078E+02 c Velocity[Z] 0.26184E-05 c Pressure 0.20420E-03 224 0.95325E-04 0.27811E-02 0.30650E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -17.771 28.393 5.612 8.0067 v Velocity[Y] -19.614 21.139 -0.14316 -0.00067225 v Velocity[Z] -3.0459 2.9792 3.0254e-06 -5.3864e-08 v ǁVelocityǁ 0.0016848 28.873 6.9911 8.0407 v Pressure -1.1426e+05 2.0983e+05 47152 25974 v TurbVisc 6.8055e-22 0.0060902 0.00013853 1.1422e-05 v CourantNb 1.0225e-07 0.011781 0.00016712 4.9065e-06 v FourierNb 1.2425e-07 0.047146 0.00014562 2.1004e-07 v total_pressure -12937 3.1115e+05 1.4848e+05 1.273e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0876 0.099442 0.0028832 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2241e-07 0.052417 0.00031273 5.1166e-06 INSTANT 0.875377000E-01 TIME STEP NUMBER 55575 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283197256E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.743643792E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.44314E-02 0.21263E+01 Friction velocity uk : 0.44314E-02 0.21263E+01 Dimensionless distance yplus : 0.42982E-02 0.20878E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 6.729102671e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29465E+08 1 0.18442E-09 0.24301E+02 0.19320E+04 c Velocity[X] 0.12223E+02 c Velocity[Y] 0.12078E+02 c Velocity[Z] 0.26088E-05 c Pressure 0.20673E-03 100 0.81015E-04 0.28129E-02 0.36771E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -17.787 28.415 5.6121 8.0068 v Velocity[Y] -19.632 21.157 -0.14316 -0.00067241 v Velocity[Z] -3.0458 2.9791 3.0245e-06 -5.3864e-08 v ǁVelocityǁ 0.0017494 28.892 6.9928 8.0409 v Pressure -1.1604e+05 2.0829e+05 45494 24954 v TurbVisc 8.4529e-22 0.0061088 0.00013862 1.1442e-05 v CourantNb 1.0895e-07 0.011781 0.00016712 4.9066e-06 v FourierNb 1.2425e-07 0.047148 0.00014562 2.1018e-07 v total_pressure -14710 3.0962e+05 1.4682e+05 1.2628e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0878 0.099446 0.0028834 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2242e-07 0.052419 0.00031274 5.1168e-06 INSTANT 0.875378000E-01 TIME STEP NUMBER 55576 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283201102E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.744107512E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.60617E-02 0.21265E+01 Friction velocity uk : 0.60617E-02 0.21265E+01 Dimensionless distance yplus : 0.58894E-02 0.20880E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 6.900883938e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29466E+08 1 0.18441E-09 0.24305E+02 0.19321E+04 c Velocity[X] 0.12222E+02 c Velocity[Y] 0.12083E+02 c Velocity[Z] 0.26054E-05 c Pressure 0.20822E-03 10 0.62107E-04 0.28304E-02 0.31378E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -17.803 28.438 5.6122 8.0068 v Velocity[Y] -19.65 21.175 -0.14316 -0.00067316 v Velocity[Z] -3.0457 2.9791 3.0236e-06 -5.3864e-08 v ǁVelocityǁ 0.0018144 28.911 6.9944 8.0411 v Pressure -1.1783e+05 2.0674e+05 43823 24087 v TurbVisc 1.0437e-21 0.0061273 0.00013871 1.1463e-05 v CourantNb 9.9772e-08 0.011781 0.00016713 4.9067e-06 v FourierNb 1.2425e-07 0.04715 0.00014562 2.1032e-07 v total_pressure -16502 3.0806e+05 1.4515e+05 1.2541e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.088 0.09945 0.0028835 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2242e-07 0.052422 0.00031274 5.1171e-06 INSTANT 0.875379000E-01 TIME STEP NUMBER 55577 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283204737E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.744560896E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.88026E-02 0.21268E+01 Friction velocity uk : 0.88026E-02 0.21268E+01 Dimensionless distance yplus : 0.86973E-02 0.20883E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 7.138233294e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29466E+08 1 0.18441E-09 0.24305E+02 0.19321E+04 c Velocity[X] 0.12219E+02 c Velocity[Y] 0.12086E+02 c Velocity[Z] 0.25891E-05 c Pressure 0.21080E-03 203 0.77205E-04 0.28627E-02 0.41058E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -17.819 28.46 5.6123 8.0069 v Velocity[Y] -19.668 21.194 -0.14316 -0.00067251 v Velocity[Z] -3.0456 2.9791 3.0227e-06 -5.3864e-08 v ǁVelocityǁ 0.0018845 28.93 6.9961 8.0412 v Pressure -1.1963e+05 2.0516e+05 42157 23064 v TurbVisc 9.9813e-22 0.0061458 0.0001388 1.1483e-05 v CourantNb 6.7368e-08 0.011781 0.00016713 4.9068e-06 v FourierNb 1.2425e-07 0.047153 0.00014562 2.1047e-07 v total_pressure -18309 3.0648e+05 1.4348e+05 1.2439e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0883 0.099452 0.0028836 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2243e-07 0.052425 0.00031274 5.1173e-06 INSTANT 0.875380000E-01 TIME STEP NUMBER 55578 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283208290E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.745005204E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.39463E-02 0.21270E+01 Friction velocity uk : 0.39463E-02 0.21270E+01 Dimensionless distance yplus : 0.38991E-02 0.20886E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 7.029293660e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29466E+08 1 0.18440E-09 0.24307E+02 0.19321E+04 c Velocity[X] 0.12217E+02 c Velocity[Y] 0.12090E+02 c Velocity[Z] 0.25719E-05 c Pressure 0.21293E-03 30 0.83277E-04 0.28888E-02 0.42968E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -17.835 28.482 5.6123 8.007 v Velocity[Y] -19.686 21.212 -0.14316 -0.00067355 v Velocity[Z] -3.0455 2.9791 3.0217e-06 -5.3864e-08 v ǁVelocityǁ 0.0018805 28.949 6.9977 8.0414 v Pressure -1.2146e+05 2.0355e+05 40395 21997 v TurbVisc 1.1281e-21 0.0061644 0.00013889 1.1503e-05 v CourantNb 6.3394e-08 0.011781 0.00016713 4.907e-06 v FourierNb 1.2425e-07 0.047155 0.00014562 2.1061e-07 v total_pressure -20136 3.0488e+05 1.4172e+05 1.2332e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0886 0.099455 0.0028836 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2244e-07 0.052428 0.00031275 5.1176e-06 INSTANT 0.875381000E-01 TIME STEP NUMBER 55579 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283211720E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.745439253E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.45067E-02 0.21274E+01 Friction velocity uk : 0.45067E-02 0.21274E+01 Dimensionless distance yplus : 0.44528E-02 0.20889E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 7.276398168e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29467E+08 1 0.18439E-09 0.24308E+02 0.19320E+04 c Velocity[X] 0.12215E+02 c Velocity[Y] 0.12093E+02 c Velocity[Z] 0.25551E-05 c Pressure 0.21520E-03 222 0.96145E-04 0.29168E-02 0.38278E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -17.851 28.504 5.6124 8.007 v Velocity[Y] -19.704 21.23 -0.14317 -0.00067251 v Velocity[Z] -3.0454 2.9791 3.0208e-06 -5.3864e-08 v ǁVelocityǁ 0.0018584 28.968 6.9994 8.0416 v Pressure -1.2331e+05 2.0191e+05 38673 21107 v TurbVisc 1.0035e-21 0.0061829 0.00013899 1.1524e-05 v CourantNb 6.1606e-08 0.011781 0.00016714 4.9071e-06 v FourierNb 1.2425e-07 0.047158 0.00014562 2.1075e-07 v total_pressure -21989 3.0324e+05 1.4e+05 1.2243e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0889 0.099456 0.0028836 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2244e-07 0.052432 0.00031275 5.1178e-06 INSTANT 0.875382000E-01 TIME STEP NUMBER 55580 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283214857E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.745868640E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.70836E-02 0.21277E+01 Friction velocity uk : 0.70836E-02 0.21277E+01 Dimensionless distance yplus : 0.70033E-02 0.20892E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 7.376033545e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29467E+08 1 0.18438E-09 0.24304E+02 0.19318E+04 c Velocity[X] 0.12212E+02 c Velocity[Y] 0.12092E+02 c Velocity[Z] 0.25414E-05 c Pressure 0.21731E-03 128 0.82005E-04 0.29426E-02 0.45978E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -17.867 28.525 5.6125 8.0071 v Velocity[Y] -19.722 21.249 -0.14317 -0.00067274 v Velocity[Z] -3.0453 2.9791 3.0199e-06 -5.3864e-08 v ǁVelocityǁ 0.0018343 28.987 7.001 8.0417 v Pressure -1.2519e+05 2.0023e+05 36899 20018 v TurbVisc 1.1172e-21 0.0062015 0.00013908 1.1544e-05 v CourantNb 3.8656e-08 0.011781 0.00016714 4.9072e-06 v FourierNb 1.2425e-07 0.047162 0.00014562 2.1089e-07 v total_pressure -23868 3.0156e+05 1.3822e+05 1.2134e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0892 0.099451 0.0028834 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2245e-07 0.052436 0.00031276 5.118e-06 INSTANT 0.875383000E-01 TIME STEP NUMBER 55581 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283217924E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.746285087E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.89639E-02 0.21281E+01 Friction velocity uk : 0.89639E-02 0.21281E+01 Dimensionless distance yplus : 0.88623E-02 0.20896E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 7.444078821e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29467E+08 1 0.18437E-09 0.24307E+02 0.19319E+04 c Velocity[X] 0.12211E+02 c Velocity[Y] 0.12096E+02 c Velocity[Z] 0.25353E-05 c Pressure 0.21840E-03 10 0.63479E-04 0.29544E-02 0.39517E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -17.883 28.547 5.6126 8.0072 v Velocity[Y] -19.74 21.267 -0.14318 -0.00067357 v Velocity[Z] -3.0452 2.979 3.019e-06 -5.3864e-08 v ǁVelocityǁ 0.0018104 29.006 7.0026 8.0419 v Pressure -1.271e+05 1.9852e+05 35118 19091 v TurbVisc 9.2299e-22 0.0062201 0.00013917 1.1565e-05 v CourantNb 1.6845e-08 0.011781 0.00016714 4.9073e-06 v FourierNb 1.2425e-07 0.047165 0.00014561 2.1104e-07 v total_pressure -25773 2.9985e+05 1.3644e+05 1.2042e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0896 0.099447 0.0028833 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2245e-07 0.052441 0.00031276 5.1183e-06 INSTANT 0.875384000E-01 TIME STEP NUMBER 55582 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283220765E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.746690555E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.30809E-02 0.21285E+01 Friction velocity uk : 0.30809E-02 0.21285E+01 Dimensionless distance yplus : 0.30351E-02 0.20900E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 7.578079218e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29467E+08 1 0.18436E-09 0.24307E+02 0.19319E+04 c Velocity[X] 0.12209E+02 c Velocity[Y] 0.12098E+02 c Velocity[Z] 0.25157E-05 c Pressure 0.22054E-03 280 0.78182E-04 0.29806E-02 0.51559E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -17.899 28.569 5.6127 8.0072 v Velocity[Y] -19.758 21.285 -0.14318 -0.00067298 v Velocity[Z] -3.0451 2.979 3.0181e-06 -5.3864e-08 v ǁVelocityǁ 0.0017861 29.025 7.0043 8.042 v Pressure -1.2902e+05 1.9678e+05 33341 18006 v TurbVisc 7.9238e-22 0.0062387 0.00013926 1.1585e-05 v CourantNb 1.0676e-08 0.011781 0.00016715 4.9073e-06 v FourierNb 1.2425e-07 0.047169 0.00014561 2.1118e-07 v total_pressure -27699 2.981e+05 1.3467e+05 1.1933e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.09 0.099438 0.002883 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2246e-07 0.052446 0.00031276 5.1185e-06 INSTANT 0.875385000E-01 TIME STEP NUMBER 55583 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283223526E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.747085980E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12008E-01 0.21290E+01 Friction velocity uk : 0.12008E-01 0.21290E+01 Dimensionless distance yplus : 0.11829E-01 0.20905E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 7.445193540e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29468E+08 1 0.18435E-09 0.24308E+02 0.19318E+04 c Velocity[X] 0.12207E+02 c Velocity[Y] 0.12101E+02 c Velocity[Z] 0.24966E-05 c Pressure 0.22228E-03 30 0.84342E-04 0.30012E-02 0.53893E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -17.915 28.59 5.6127 8.0073 v Velocity[Y] -19.776 21.304 -0.14319 -0.0006741 v Velocity[Z] -3.045 2.979 3.0172e-06 -5.3864e-08 v ǁVelocityǁ 0.0017322 29.044 7.0059 8.0422 v Pressure -1.3098e+05 1.95e+05 31476 16880 v TurbVisc 2.9394e-22 0.0062572 0.00013935 1.1606e-05 v CourantNb 2.8698e-08 0.011781 0.00016715 4.9074e-06 v FourierNb 1.2425e-07 0.047173 0.00014561 2.1132e-07 v total_pressure -29651 2.9633e+05 1.328e+05 1.182e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0905 0.099433 0.0028828 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2246e-07 0.05245 0.00031276 5.1188e-06 INSTANT 0.875386000E-01 TIME STEP NUMBER 55584 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283226152E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.747472323E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.79303E-02 0.21294E+01 Friction velocity uk : 0.79303E-02 0.21294E+01 Dimensionless distance yplus : 0.79637E-02 0.20909E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 7.641470356e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29468E+08 1 0.18434E-09 0.24309E+02 0.19318E+04 c Velocity[X] 0.12206E+02 c Velocity[Y] 0.12103E+02 c Velocity[Z] 0.24805E-05 c Pressure 0.22411E-03 221 0.97318E-04 0.30231E-02 0.48098E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -17.931 28.611 5.6128 8.0073 v Velocity[Y] -19.794 21.322 -0.1432 -0.00067311 v Velocity[Z] -3.0449 2.979 3.0162e-06 -5.3864e-08 v ǁVelocityǁ 0.001648 29.063 7.0076 8.0423 v Pressure -1.3296e+05 1.9318e+05 29657 15942 v TurbVisc 6.3999e-22 0.0062758 0.00013943 1.1626e-05 v CourantNb 1.7784e-08 0.011781 0.00016715 4.9075e-06 v FourierNb 1.2425e-07 0.047177 0.00014561 2.1146e-07 v total_pressure -31632 2.9451e+05 1.3098e+05 1.1727e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0909 0.099418 0.0028824 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2247e-07 0.052455 0.00031277 5.119e-06 INSTANT 0.875387000E-01 TIME STEP NUMBER 55585 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283228474E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.747853110E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.29192E-02 0.21299E+01 Friction velocity uk : 0.29192E-02 0.21299E+01 Dimensionless distance yplus : 0.28627E-02 0.20914E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 7.706701669e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29468E+08 1 0.18433E-09 0.24304E+02 0.19316E+04 c Velocity[X] 0.12204E+02 c Velocity[Y] 0.12101E+02 c Velocity[Z] 0.24682E-05 c Pressure 0.22580E-03 512 0.83004E-04 0.30430E-02 0.57396E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -17.947 28.633 5.6129 8.0074 v Velocity[Y] -19.812 21.34 -0.14321 -0.00067322 v Velocity[Z] -3.0448 2.979 3.0153e-06 -5.3865e-08 v ǁVelocityǁ 0.0015609 29.082 7.0092 8.0424 v Pressure -1.3497e+05 1.9132e+05 27793 14811 v TurbVisc 6.9914e-22 0.0062944 0.00013952 1.1647e-05 v CourantNb 8.3488e-09 0.01178 0.00016716 4.9076e-06 v FourierNb 1.2425e-07 0.047181 0.00014561 2.1161e-07 v total_pressure -33642 2.9265e+05 1.2912e+05 1.1614e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0914 0.099404 0.002882 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2247e-07 0.05246 0.00031277 5.1192e-06 INSTANT 0.875388000E-01 TIME STEP NUMBER 55586 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283230729E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.748220808E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.34377E-02 0.21303E+01 Friction velocity uk : 0.34377E-02 0.21303E+01 Dimensionless distance yplus : 0.33856E-02 0.20918E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 7.754816186e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29468E+08 1 0.18431E-09 0.24307E+02 0.19317E+04 c Velocity[X] 0.12203E+02 c Velocity[Y] 0.12104E+02 c Velocity[Z] 0.24648E-05 c Pressure 0.22644E-03 10 0.64990E-04 0.30487E-02 0.50871E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -17.962 28.654 5.613 8.0074 v Velocity[Y] -19.83 21.359 -0.14322 -0.00067431 v Velocity[Z] -3.0447 2.9789 3.0144e-06 -5.3865e-08 v ǁVelocityǁ 0.0014757 29.101 7.0109 8.0426 v Pressure -1.37e+05 1.8943e+05 25925 13819 v TurbVisc 5.2114e-22 0.006313 0.00013961 1.1667e-05 v CourantNb 6.7928e-09 0.01178 0.00016716 4.9077e-06 v FourierNb 1.2425e-07 0.047185 0.00014561 2.1175e-07 v total_pressure -35679 2.9075e+05 1.2725e+05 1.1514e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0918 0.099409 0.0028817 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2247e-07 0.052465 0.00031277 5.1195e-06 INSTANT 0.875389000E-01 TIME STEP NUMBER 55587 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283232729E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.748577177E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10199E-01 0.21309E+01 Friction velocity uk : 0.10199E-01 0.21309E+01 Dimensionless distance yplus : 0.98270E-02 0.20923E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 7.832774620e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29468E+08 1 0.18431E-09 0.24307E+02 0.19316E+04 c Velocity[X] 0.12201E+02 c Velocity[Y] 0.12105E+02 c Velocity[Z] 0.24471E-05 c Pressure 0.22808E-03 208 0.79212E-04 0.30679E-02 0.64537E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -17.978 28.675 5.6131 8.0075 v Velocity[Y] -19.848 21.377 -0.14323 -0.00067374 v Velocity[Z] -3.0446 2.9789 3.0135e-06 -5.3865e-08 v ǁVelocityǁ 0.0013831 29.12 7.0125 8.0427 v Pressure -1.3906e+05 1.875e+05 24050 12701 v TurbVisc 4.8837e-22 0.0063316 0.0001397 1.1688e-05 v CourantNb 1.8641e-08 0.01178 0.00016716 4.9078e-06 v FourierNb 1.2425e-07 0.047189 0.00014561 2.1189e-07 v total_pressure -37735 2.8882e+05 1.2538e+05 1.1403e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0923 0.099421 0.0028814 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2248e-07 0.05247 0.00031278 5.1197e-06 INSTANT 0.875390000E-01 TIME STEP NUMBER 55588 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283234667E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.748921403E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.66723E-02 0.21313E+01 Friction velocity uk : 0.66723E-02 0.21313E+01 Dimensionless distance yplus : 0.64291E-02 0.20927E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 7.779494706e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29469E+08 1 0.18429E-09 0.24307E+02 0.19316E+04 c Velocity[X] 0.12200E+02 c Velocity[Y] 0.12107E+02 c Velocity[Z] 0.24316E-05 c Pressure 0.22946E-03 51 0.85345E-04 0.30835E-02 0.67703E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -17.994 28.696 5.6131 8.0075 v Velocity[Y] -19.866 21.395 -0.14324 -0.00067494 v Velocity[Z] -3.0445 2.9789 3.0126e-06 -5.3865e-08 v ǁVelocityǁ 0.0013004 29.139 7.0142 8.0428 v Pressure -1.4114e+05 1.8553e+05 22117 11531 v TurbVisc 5.384e-22 0.0063502 0.00013979 1.1708e-05 v CourantNb 1.3448e-08 0.01178 0.00016717 4.9079e-06 v FourierNb 1.2425e-07 0.047193 0.00014561 2.1204e-07 v total_pressure -39813 2.8686e+05 1.2344e+05 1.1286e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0927 0.099424 0.002881 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2248e-07 0.052475 0.00031278 5.1199e-06 INSTANT 0.875391000E-01 TIME STEP NUMBER 55589 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283236454E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.749261842E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.48753E-02 0.21318E+01 Friction velocity uk : 0.48753E-02 0.21318E+01 Dimensionless distance yplus : 0.46976E-02 0.20932E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 7.904482692e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29469E+08 1 0.18428E-09 0.24307E+02 0.19315E+04 c Velocity[X] 0.12199E+02 c Velocity[Y] 0.12108E+02 c Velocity[Z] 0.24214E-05 c Pressure 0.23079E-03 220 0.98651E-04 0.30984E-02 0.60281E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -18.01 28.717 5.6132 8.0075 v Velocity[Y] -19.884 21.414 -0.14325 -0.00067397 v Velocity[Z] -3.0444 2.9789 3.0117e-06 -5.3865e-08 v ǁVelocityǁ 0.0012239 29.158 7.0158 8.043 v Pressure -1.4324e+05 1.8353e+05 20223 10561 v TurbVisc 2.2366e-22 0.0063688 0.00013988 1.1729e-05 v CourantNb 7.5035e-09 0.01178 0.00016717 4.908e-06 v FourierNb 1.2425e-07 0.047197 0.00014561 2.1218e-07 v total_pressure -41915 2.8486e+05 1.2155e+05 1.1189e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0932 0.099424 0.0028806 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2248e-07 0.05248 0.00031278 5.1202e-06 INSTANT 0.875392000E-01 TIME STEP NUMBER 55590 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283237933E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.749593248E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.34410E-02 0.21322E+01 Friction velocity uk : 0.34410E-02 0.21322E+01 Dimensionless distance yplus : 0.33155E-02 0.20936E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 7.961563483e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29469E+08 1 0.18427E-09 0.24303E+02 0.19313E+04 c Velocity[X] 0.12197E+02 c Velocity[Y] 0.12105E+02 c Velocity[Z] 0.24134E-05 c Pressure 0.23197E-03 580 0.84067E-04 0.31113E-02 0.72317E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -18.026 28.737 5.6133 8.0076 v Velocity[Y] -19.902 21.432 -0.14326 -0.00067411 v Velocity[Z] -3.0443 2.9789 3.0108e-06 -5.3865e-08 v ǁVelocityǁ 0.0011554 29.177 7.0175 8.0431 v Pressure -1.4536e+05 1.8149e+05 18287 9384.7 v TurbVisc 2.5958e-22 0.0063875 0.00013997 1.1749e-05 v CourantNb 1.4488e-08 0.01178 0.00016717 4.9081e-06 v FourierNb 1.2425e-07 0.0472 0.00014561 2.1232e-07 v total_pressure -44039 2.8281e+05 1.1961e+05 1.1071e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0936 0.09942 0.0028802 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2249e-07 0.052485 0.00031279 5.1204e-06 INSTANT 0.875393000E-01 TIME STEP NUMBER 55591 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283239339E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.749911945E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.41212E-02 0.21326E+01 Friction velocity uk : 0.41212E-02 0.21326E+01 Dimensionless distance yplus : 0.39710E-02 0.20940E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 7.976976757e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29469E+08 1 0.18425E-09 0.24305E+02 0.19313E+04 c Velocity[X] 0.12197E+02 c Velocity[Y] 0.12108E+02 c Velocity[Z] 0.24157E-05 c Pressure 0.23207E-03 10 0.65685E-04 0.31098E-02 0.62317E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -18.041 28.758 5.6134 8.0076 v Velocity[Y] -19.92 21.45 -0.14327 -0.00067526 v Velocity[Z] -3.0442 2.9788 3.0099e-06 -5.3865e-08 v ǁVelocityǁ 0.0010986 29.196 7.0191 8.0432 v Pressure -1.475e+05 1.7942e+05 16373 8380.9 v TurbVisc 1.304e-22 0.0064061 0.00014005 1.177e-05 v CourantNb 2.4926e-08 0.01178 0.00016718 4.9082e-06 v FourierNb 1.2425e-07 0.047204 0.00014561 2.1247e-07 v total_pressure -46180 2.8074e+05 1.177e+05 1.0971e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.094 0.099414 0.0028798 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2249e-07 0.052489 0.00031279 5.1206e-06 INSTANT 0.875394000E-01 TIME STEP NUMBER 55592 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283240494E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.750219587E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.66341E-02 0.21330E+01 Friction velocity uk : 0.66341E-02 0.21330E+01 Dimensionless distance yplus : 0.63923E-02 0.20945E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 7.930333239e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29469E+08 1 0.18424E-09 0.24304E+02 0.19312E+04 c Velocity[X] 0.12196E+02 c Velocity[Y] 0.12108E+02 c Velocity[Z] 0.24030E-05 c Pressure 0.23307E-03 197 0.80080E-04 0.31202E-02 0.79737E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -18.057 28.779 5.6134 8.0076 v Velocity[Y] -19.938 21.468 -0.14328 -0.00067471 v Velocity[Z] -3.0441 2.9788 3.0089e-06 -5.3865e-08 v ǁVelocityǁ 0.0010436 29.214 7.0208 8.0433 v Pressure -1.4965e+05 1.7732e+05 14421 7229.4 v TurbVisc 3.1379e-22 0.0064247 0.00014014 1.179e-05 v CourantNb 2.3129e-08 0.01178 0.00016718 4.9082e-06 v FourierNb 1.2425e-07 0.047208 0.00014561 2.1261e-07 v total_pressure -48327 2.7864e+05 1.1575e+05 1.0855e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0945 0.09941 0.0028795 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2249e-07 0.052494 0.00031279 5.1209e-06 INSTANT 0.875395000E-01 TIME STEP NUMBER 55593 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283241576E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.750512280E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.28336E-02 0.21334E+01 Friction velocity uk : 0.28336E-02 0.21334E+01 Dimensionless distance yplus : 0.27490E-02 0.20948E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 7.929540463e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29469E+08 1 0.18423E-09 0.24304E+02 0.19312E+04 c Velocity[X] 0.12195E+02 c Velocity[Y] 0.12109E+02 c Velocity[Z] 0.23925E-05 c Pressure 0.23396E-03 53 0.86376E-04 0.31292E-02 0.82498E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -18.073 28.799 5.6135 8.0076 v Velocity[Y] -19.956 21.486 -0.14329 -0.00067594 v Velocity[Z] -3.044 2.9788 3.008e-06 -5.3865e-08 v ǁVelocityǁ 0.0010037 29.233 7.0224 8.0434 v Pressure -1.5181e+05 1.752e+05 12444 6032 v TurbVisc 2.7097e-22 0.0064434 0.00014023 1.1811e-05 v CourantNb 2.0143e-08 0.01178 0.00016718 4.9083e-06 v FourierNb 1.2425e-07 0.047211 0.00014561 2.1275e-07 v total_pressure -50483 2.7652e+05 1.1377e+05 1.0736e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0948 0.099409 0.0028792 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2249e-07 0.052498 0.0003128 5.1211e-06 INSTANT 0.875396000E-01 TIME STEP NUMBER 55594 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283242509E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.750806735E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.35659E-02 0.21337E+01 Friction velocity uk : 0.35659E-02 0.21337E+01 Dimensionless distance yplus : 0.34594E-02 0.20951E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 7.887764137e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29469E+08 1 0.18421E-09 0.24304E+02 0.19312E+04 c Velocity[X] 0.12195E+02 c Velocity[Y] 0.12109E+02 c Velocity[Z] 0.23886E-05 c Pressure 0.23464E-03 145 0.99640E-04 0.31354E-02 0.72449E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -18.089 28.82 5.6136 8.0076 v Velocity[Y] -19.974 21.504 -0.14331 -0.00067499 v Velocity[Z] -3.0439 2.9788 3.0071e-06 -5.3865e-08 v ǁVelocityǁ 0.00097409 29.251 7.024 8.0435 v Pressure -1.5397e+05 1.7305e+05 10511 5042.3 v TurbVisc 9.7114e-23 0.006462 0.00014031 1.1831e-05 v CourantNb 1.1569e-08 0.01178 0.00016718 4.9084e-06 v FourierNb 1.2425e-07 0.047214 0.00014561 2.1289e-07 v total_pressure -52650 2.7437e+05 1.1184e+05 1.0637e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0951 0.099407 0.0028789 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2249e-07 0.052502 0.0003128 5.1213e-06 INSTANT 0.875397000E-01 TIME STEP NUMBER 55595 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283243125E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.751088796E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.64259E-02 0.21340E+01 Friction velocity uk : 0.64259E-02 0.21340E+01 Dimensionless distance yplus : 0.62341E-02 0.20954E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 7.801344265e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29469E+08 1 0.18419E-09 0.24299E+02 0.19309E+04 c Velocity[X] 0.12194E+02 c Velocity[Y] 0.12105E+02 c Velocity[Z] 0.23847E-05 c Pressure 0.23515E-03 388 0.84835E-04 0.31392E-02 0.84684E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -18.105 28.84 5.6136 8.0077 v Velocity[Y] -19.992 21.521 -0.14332 -0.00067517 v Velocity[Z] -3.0438 2.9788 3.0062e-06 -5.3865e-08 v ǁVelocityǁ 0.00095374 29.27 7.0257 8.0436 v Pressure -1.5615e+05 1.7087e+05 8529.8 3855.2 v TurbVisc 7.0309e-23 0.0064807 0.0001404 1.1852e-05 v CourantNb 2.8896e-09 0.01178 0.00016719 4.9085e-06 v FourierNb 1.2425e-07 0.047217 0.00014561 2.1304e-07 v total_pressure -54822 2.722e+05 1.0985e+05 1.0518e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0954 0.099407 0.0028787 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2249e-07 0.052505 0.0003128 5.1215e-06 INSTANT 0.875398000E-01 TIME STEP NUMBER 55596 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283243677E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.751357857E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.84795E-02 0.21343E+01 Friction velocity uk : 0.84795E-02 0.21343E+01 Dimensionless distance yplus : 0.81815E-02 0.20957E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 7.681995216e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29469E+08 1 0.18418E-09 0.24301E+02 0.19310E+04 c Velocity[X] 0.12194E+02 c Velocity[Y] 0.12107E+02 c Velocity[Z] 0.23843E-05 c Pressure 0.23456E-03 11 0.66295E-04 0.31286E-02 0.73445E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -18.12 28.86 5.6137 8.0077 v Velocity[Y] -20.01 21.539 -0.14333 -0.00067629 v Velocity[Z] -3.0437 2.9787 3.0053e-06 -5.3865e-08 v ǁVelocityǁ 0.00094483 29.288 7.0273 8.0437 v Pressure -1.5832e+05 1.6868e+05 6590.6 2817.1 v TurbVisc 6.8333e-23 0.0064993 0.00014049 1.1872e-05 v CourantNb 5.2881e-09 0.01178 0.00016719 4.9086e-06 v FourierNb 1.2425e-07 0.047219 0.00014561 2.1318e-07 v total_pressure -56995 2.7001e+05 1.0792e+05 1.0414e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0957 0.099406 0.0028785 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.225e-07 0.052508 0.00031281 5.1217e-06 INSTANT 0.875399000E-01 TIME STEP NUMBER 55597 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283243961E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.751616560E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.60521E-02 0.21345E+01 Friction velocity uk : 0.60521E-02 0.21345E+01 Dimensionless distance yplus : 0.58394E-02 0.20959E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 7.359030318e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29469E+08 1 0.18416E-09 0.24301E+02 0.19309E+04 c Velocity[X] 0.12194E+02 c Velocity[Y] 0.12107E+02 c Velocity[Z] 0.23822E-05 c Pressure 0.23485E-03 209 0.81097E-04 0.31295E-02 0.89114E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -18.136 28.881 5.6137 8.0077 v Velocity[Y] -20.028 21.557 -0.14334 -0.00067573 v Velocity[Z] -3.0436 2.9787 3.0044e-06 -5.3865e-08 v ǁVelocityǁ 0.00093637 29.306 7.0289 8.0438 v Pressure -1.6048e+05 1.6648e+05 4599.1 1666.8 v TurbVisc 2.3946e-22 0.006518 0.00014057 1.1893e-05 v CourantNb 1.4164e-08 0.01178 0.00016719 4.9086e-06 v FourierNb 1.2425e-07 0.047221 0.00014562 2.1332e-07 v total_pressure -59156 2.678e+05 1.0592e+05 1.0299e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0959 0.099404 0.0028784 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.225e-07 0.052511 0.00031281 5.122e-06 INSTANT 0.875400000E-01 TIME STEP NUMBER 55598 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283244187E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.751858696E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11004E-01 0.21347E+01 Friction velocity uk : 0.11004E-01 0.21347E+01 Dimensionless distance yplus : 0.10618E-01 0.20961E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 7.223728460e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29469E+08 1 0.18415E-09 0.24301E+02 0.19309E+04 c Velocity[X] 0.12194E+02 c Velocity[Y] 0.12107E+02 c Velocity[Z] 0.23763E-05 c Pressure 0.23506E-03 30 0.87689E-04 0.31294E-02 0.90375E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -18.152 28.901 5.6138 8.0077 v Velocity[Y] -20.046 21.574 -0.14335 -0.00067697 v Velocity[Z] -3.0435 2.9787 3.0035e-06 -5.3865e-08 v ǁVelocityǁ 0.00094043 29.324 7.0306 8.0439 v Pressure -1.6263e+05 1.6427e+05 2610.1 455.91 v TurbVisc 1.7009e-23 0.0065366 0.00014066 1.1913e-05 v CourantNb 2.176e-08 0.01178 0.0001672 4.9087e-06 v FourierNb 1.2425e-07 0.047223 0.00014562 2.1347e-07 v total_pressure -61308 2.656e+05 1.0394e+05 1.0178e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0961 0.099401 0.0028782 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.225e-07 0.052513 0.00031281 5.1222e-06 INSTANT 0.875401000E-01 TIME STEP NUMBER 55599 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283244256E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.752104852E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.62666E-02 0.21348E+01 Friction velocity uk : 0.62666E-02 0.21348E+01 Dimensionless distance yplus : 0.61295E-02 0.20962E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 6.883932944e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29469E+08 1 0.18413E-09 0.24296E+02 0.19306E+04 c Velocity[X] 0.12194E+02 c Velocity[Y] 0.12102E+02 c Velocity[Z] 0.23747E-05 c Pressure 0.23500E-03 160 0.75730E-04 0.31258E-02 0.75251E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -18.168 28.921 5.6138 8.0077 v Velocity[Y] -20.064 21.591 -0.14336 -0.00067693 v Velocity[Z] -3.0434 2.9787 3.0026e-06 -5.3865e-08 v ǁVelocityǁ 0.00095281 29.342 7.0322 8.044 v Pressure -1.6477e+05 1.6206e+05 659.03 -557.44 v TurbVisc 7.9886e-23 0.0065553 0.00014074 1.1934e-05 v CourantNb 2.7611e-08 0.01178 0.0001672 4.9088e-06 v FourierNb 1.2425e-07 0.047224 0.00014562 2.1361e-07 v total_pressure -63449 2.6338e+05 1.0198e+05 1.0077e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0962 0.099399 0.0028781 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.225e-07 0.052515 0.00031282 5.1224e-06 INSTANT 0.875402000E-01 TIME STEP NUMBER 55600 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283244091E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.752336242E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.29634E-02 0.21349E+01 Friction velocity uk : 0.29634E-02 0.21349E+01 Dimensionless distance yplus : 0.28986E-02 0.20962E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 6.492475513e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29469E+08 1 0.18411E-09 0.24298E+02 0.19307E+04 c Velocity[X] 0.12194E+02 c Velocity[Y] 0.12103E+02 c Velocity[Z] 0.23845E-05 c Pressure 0.23396E-03 10 0.62758E-04 0.31090E-02 0.72587E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -18.183 28.942 5.6138 8.0077 v Velocity[Y] -20.082 21.609 -0.14337 -0.00067632 v Velocity[Z] -3.0433 2.9787 3.0017e-06 -5.3865e-08 v ǁVelocityǁ 0.00097471 29.36 7.0338 8.0441 v Pressure -1.669e+05 1.5984e+05 -1288.7 -1590.9 v TurbVisc 4.7126e-23 0.006574 0.00014082 1.1954e-05 v CourantNb 2.6022e-08 0.01178 0.0001672 4.9089e-06 v FourierNb 1.2425e-07 0.047226 0.00014562 2.1375e-07 v total_pressure -65576 2.6116e+05 1.0004e+05 99734 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0962 0.099396 0.002878 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.225e-07 0.052516 0.00031282 5.1226e-06 INSTANT 0.875403000E-01 TIME STEP NUMBER 55601 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283243592E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.752554780E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.50337E-02 0.21349E+01 Friction velocity uk : 0.50337E-02 0.21349E+01 Dimensionless distance yplus : 0.50205E-02 0.20963E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 5.860746059e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29469E+08 1 0.18409E-09 0.24295E+02 0.19305E+04 c Velocity[X] 0.12195E+02 c Velocity[Y] 0.12101E+02 c Velocity[Z] 0.23759E-05 c Pressure 0.23357E-03 23 0.96552E-04 0.31011E-02 0.88062E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -18.199 28.962 5.6139 8.0077 v Velocity[Y] -20.1 21.626 -0.14338 -0.00067631 v Velocity[Z] -3.0432 2.9786 3.0008e-06 -5.3865e-08 v ǁVelocityǁ 0.0010005 29.378 7.0355 8.0442 v Pressure -1.69e+05 1.5762e+05 -3264.2 -2798.9 v TurbVisc 5.4697e-22 0.0065927 0.00014091 1.1975e-05 v CourantNb 2.4984e-08 0.01178 0.00016721 4.9089e-06 v FourierNb 1.2425e-07 0.047227 0.00014562 2.1389e-07 v total_pressure -67679 2.5894e+05 98061 98526 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0963 0.099397 0.002878 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.225e-07 0.052518 0.00031282 5.1228e-06 INSTANT 0.875404000E-01 TIME STEP NUMBER 55602 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283243115E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.752755326E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.82092E-02 0.21349E+01 Friction velocity uk : 0.82092E-02 0.21349E+01 Dimensionless distance yplus : 0.81877E-02 0.20963E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 5.490123782e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29469E+08 1 0.18407E-09 0.24294E+02 0.19305E+04 c Velocity[X] 0.12195E+02 c Velocity[Y] 0.12099E+02 c Velocity[Z] 0.23663E-05 c Pressure 0.23296E-03 67 0.81432E-04 0.30901E-02 0.82578E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -18.215 28.982 5.6139 8.0076 v Velocity[Y] -20.118 21.643 -0.14339 -0.00067673 v Velocity[Z] -3.0431 2.9786 2.9999e-06 -5.3865e-08 v ǁVelocityǁ 0.0010367 29.395 7.0371 8.0443 v Pressure -1.7109e+05 1.554e+05 -5266.5 -3994.9 v TurbVisc 1.0796e-22 0.0066114 0.00014099 1.1995e-05 v CourantNb 2.5206e-08 0.01178 0.00016721 4.909e-06 v FourierNb 1.2425e-07 0.047227 0.00014562 2.1404e-07 v total_pressure -69762 2.5673e+05 96059 97330 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0963 0.099407 0.0028781 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.225e-07 0.052518 0.00031283 5.123e-06 INSTANT 0.875405000E-01 TIME STEP NUMBER 55603 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283242438E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.752955689E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13381E-01 0.21348E+01 Friction velocity uk : 0.13381E-01 0.21348E+01 Dimensionless distance yplus : 0.13013E-01 0.20962E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 4.906912966e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29469E+08 1 0.18405E-09 0.24296E+02 0.19305E+04 c Velocity[X] 0.12196E+02 c Velocity[Y] 0.12100E+02 c Velocity[Z] 0.23730E-05 c Pressure 0.23202E-03 10 0.60569E-04 0.30750E-02 0.72066E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -18.23 29.002 5.6139 8.0076 v Velocity[Y] -20.136 21.659 -0.14339 -0.00067757 v Velocity[Z] -3.043 2.9786 2.999e-06 -5.3865e-08 v ǁVelocityǁ 0.0010833 29.413 7.0387 8.0444 v Pressure -1.7315e+05 1.532e+05 -7227.8 -5063.6 v TurbVisc 1.4899e-22 0.0066301 0.00014107 1.2016e-05 v CourantNb 3.0952e-08 0.01178 0.00016721 4.9091e-06 v FourierNb 1.2425e-07 0.047227 0.00014562 2.1418e-07 v total_pressure -71823 2.5452e+05 94097 96261 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0962 0.099418 0.0028782 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2249e-07 0.052518 0.00031283 5.1232e-06 INSTANT 0.875406000E-01 TIME STEP NUMBER 55604 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283241573E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.753144674E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13621E-01 0.21348E+01 Friction velocity uk : 0.13621E-01 0.21348E+01 Dimensionless distance yplus : 0.13246E-01 0.20962E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 3.837380802e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29469E+08 1 0.18403E-09 0.24294E+02 0.19304E+04 c Velocity[X] 0.12197E+02 c Velocity[Y] 0.12097E+02 c Velocity[Z] 0.23654E-05 c Pressure 0.23140E-03 116 0.99848E-04 0.30639E-02 0.76087E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -18.246 29.023 5.6139 8.0076 v Velocity[Y] -20.154 21.676 -0.1434 -0.00067817 v Velocity[Z] -3.0428 2.9786 2.9981e-06 -5.3865e-08 v ǁVelocityǁ 0.0011304 29.43 7.0403 8.0444 v Pressure -1.7518e+05 1.5111e+05 -9154.7 -6180.7 v TurbVisc 2.8669e-22 0.0066488 0.00014115 1.2036e-05 v CourantNb 3.4983e-08 0.01178 0.00016722 4.9091e-06 v FourierNb 1.2425e-07 0.047227 0.00014562 2.1432e-07 v total_pressure -73854 2.5243e+05 92170 95144 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0962 0.099425 0.0028783 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2249e-07 0.052518 0.00031284 5.1234e-06 INSTANT 0.875407000E-01 TIME STEP NUMBER 55605 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283240582E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.753317224E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13765E-01 0.21346E+01 Friction velocity uk : 0.13765E-01 0.21346E+01 Dimensionless distance yplus : 0.13386E-01 0.20960E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 3.362681938e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29469E+08 1 0.18401E-09 0.24292E+02 0.19303E+04 c Velocity[X] 0.12198E+02 c Velocity[Y] 0.12094E+02 c Velocity[Z] 0.23551E-05 c Pressure 0.23037E-03 36 0.83577E-04 0.30475E-02 0.67980E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -18.261 29.043 5.6139 8.0076 v Velocity[Y] -20.172 21.693 -0.14341 -0.00067816 v Velocity[Z] -3.0427 2.9786 2.9972e-06 -5.3865e-08 v ǁVelocityǁ 0.001188 29.447 7.0419 8.0445 v Pressure -1.7718e+05 1.4908e+05 -11109 -7252 v TurbVisc 1.7213e-22 0.0066675 0.00014124 1.2057e-05 v CourantNb 4.3175e-08 0.01178 0.00016722 4.9092e-06 v FourierNb 1.2425e-07 0.047227 0.00014562 2.1446e-07 v total_pressure -75858 2.5041e+05 90216 94073 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.096 0.099434 0.0028784 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2249e-07 0.052518 0.00031284 5.1236e-06 INSTANT 0.875408000E-01 TIME STEP NUMBER 55606 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283239397E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.753484822E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.14311E-01 0.21345E+01 Friction velocity uk : 0.14311E-01 0.21345E+01 Dimensionless distance yplus : 0.13917E-01 0.20959E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 2.446713191e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29469E+08 1 0.18399E-09 0.24294E+02 0.19303E+04 c Velocity[X] 0.12199E+02 c Velocity[Y] 0.12095E+02 c Velocity[Z] 0.23514E-05 c Pressure 0.22899E-03 11 0.61683E-04 0.30266E-02 0.63957E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -18.277 29.063 5.6139 8.0076 v Velocity[Y] -20.19 21.709 -0.14341 -0.00067726 v Velocity[Z] -3.0426 2.9785 2.9962e-06 -5.3865e-08 v ǁVelocityǁ 0.0012494 29.464 7.0435 8.0446 v Pressure -1.7935e+05 1.4707e+05 -13060 -8301.8 v TurbVisc 1.2491e-22 0.0066862 0.00014132 1.2077e-05 v CourantNb 3.9425e-08 0.01178 0.00016722 4.9092e-06 v FourierNb 1.2425e-07 0.047226 0.00014562 2.1461e-07 v total_pressure -78022 2.484e+05 88265 93023 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0959 0.09944 0.0028784 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2249e-07 0.052517 0.00031284 5.1238e-06 INSTANT 0.875409000E-01 TIME STEP NUMBER 55607 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283237949E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.753639410E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.14379E-01 0.21343E+01 Friction velocity uk : 0.14379E-01 0.21343E+01 Dimensionless distance yplus : 0.13983E-01 0.20957E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.257999234e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29469E+08 1 0.18396E-09 0.24293E+02 0.19302E+04 c Velocity[X] 0.12201E+02 c Velocity[Y] 0.12093E+02 c Velocity[Z] 0.23472E-05 c Pressure 0.22810E-03 105 0.75829E-04 0.30122E-02 0.80140E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -18.292 29.083 5.6138 8.0075 v Velocity[Y] -20.207 21.725 -0.14341 -0.00067842 v Velocity[Z] -3.0425 2.9785 2.9953e-06 -5.3865e-08 v ǁVelocityǁ 0.0013097 29.481 7.0451 8.0446 v Pressure -1.8156e+05 1.4508e+05 -15001 -9593.9 v TurbVisc 1.6816e-22 0.0067049 0.0001414 1.2098e-05 v CourantNb 3.7031e-08 0.01178 0.00016722 4.9093e-06 v FourierNb 1.2425e-07 0.047226 0.00014562 2.1475e-07 v total_pressure -80237 2.464e+05 86324 91731 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0957 0.099445 0.0028785 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2249e-07 0.052516 0.00031285 5.124e-06 INSTANT 0.875410000E-01 TIME STEP NUMBER 55608 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283236538E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.753779796E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.14210E-01 0.21341E+01 Friction velocity uk : 0.14210E-01 0.21341E+01 Dimensionless distance yplus : 0.13832E-01 0.20955E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 5.351351314e-03 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29469E+08 1 0.18394E-09 0.24293E+02 0.19302E+04 c Velocity[X] 0.12202E+02 c Velocity[Y] 0.12092E+02 c Velocity[Z] 0.23382E-05 c Pressure 0.22694E-03 399 0.79917E-04 0.29942E-02 0.56961E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -18.308 29.103 5.6138 8.0075 v Velocity[Y] -20.225 21.742 -0.14342 -0.00067744 v Velocity[Z] -3.0424 2.9785 2.9944e-06 -5.3865e-08 v ǁVelocityǁ 0.0013734 29.498 7.0467 8.0447 v Pressure -1.8375e+05 1.4311e+05 -16907 -10545 v TurbVisc 7.012e-23 0.0067236 0.00014148 1.2118e-05 v CourantNb 3.5377e-08 0.01178 0.00016723 4.9093e-06 v FourierNb 1.2425e-07 0.047225 0.00014563 2.1489e-07 v total_pressure -82425 2.4443e+05 84418 90780 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0955 0.099447 0.0028785 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2249e-07 0.052515 0.00031285 5.1242e-06 INSTANT 0.875411000E-01 TIME STEP NUMBER 55609 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283234805E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.753915274E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.14059E-01 0.21339E+01 Friction velocity uk : 0.14059E-01 0.21339E+01 Dimensionless distance yplus : 0.13684E-01 0.20953E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -6.131678123e-03 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29469E+08 1 0.18392E-09 0.24293E+02 0.19302E+04 c Velocity[X] 0.12204E+02 c Velocity[Y] 0.12090E+02 c Velocity[Z] 0.23293E-05 c Pressure 0.22564E-03 45 0.93460E-04 0.29744E-02 0.66234E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -18.323 29.123 5.6138 8.0075 v Velocity[Y] -20.242 21.758 -0.14342 -0.00067881 v Velocity[Z] -3.0423 2.9785 2.9935e-06 -5.3865e-08 v ǁVelocityǁ 0.0014358 29.514 7.0483 8.0448 v Pressure -1.8591e+05 1.4118e+05 -18816 -11706 v TurbVisc 1.8205e-22 0.0067424 0.00014156 1.2139e-05 v CourantNb 3.1071e-08 0.01178 0.00016723 4.9094e-06 v FourierNb 1.2425e-07 0.047223 0.00014563 2.1503e-07 v total_pressure -84586 2.425e+05 82509 89619 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0953 0.099447 0.0028784 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2248e-07 0.052514 0.00031286 5.1244e-06 INSTANT 0.875412000E-01 TIME STEP NUMBER 55610 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283232968E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.754036834E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.14218E-01 0.21336E+01 Friction velocity uk : 0.14218E-01 0.21336E+01 Dimensionless distance yplus : 0.13840E-01 0.20950E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.767482568e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29468E+08 1 0.18389E-09 0.24289E+02 0.19300E+04 c Velocity[X] 0.12205E+02 c Velocity[Y] 0.12084E+02 c Velocity[Z] 0.23173E-05 c Pressure 0.22426E-03 160 0.78715E-04 0.29536E-02 0.54628E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -18.338 29.143 5.6137 8.0074 v Velocity[Y] -20.26 21.774 -0.14342 -0.00067866 v Velocity[Z] -3.0422 2.9785 2.9926e-06 -5.3865e-08 v ǁVelocityǁ 0.0014943 29.531 7.0499 8.0448 v Pressure -1.8804e+05 1.3935e+05 -20699 -12705 v TurbVisc 1.2254e-22 0.0067611 0.00014164 1.2159e-05 v CourantNb 2.6006e-08 0.01178 0.00016723 4.9094e-06 v FourierNb 1.2425e-07 0.047222 0.00014563 2.1518e-07 v total_pressure -86719 2.4067e+05 80626 88620 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.095 0.099444 0.0028783 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2248e-07 0.052512 0.00031286 5.1246e-06 INSTANT 0.875413000E-01 TIME STEP NUMBER 55611 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283230934E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.754144084E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.14071E-01 0.21333E+01 Friction velocity uk : 0.14071E-01 0.21333E+01 Dimensionless distance yplus : 0.13814E-01 0.20947E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -2.901418709e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29468E+08 1 0.18386E-09 0.24291E+02 0.19300E+04 c Velocity[X] 0.12206E+02 c Velocity[Y] 0.12084E+02 c Velocity[Z] 0.23150E-05 c Pressure 0.22187E-03 10 0.62210E-04 0.29195E-02 0.49481E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -18.354 29.163 5.6137 8.0074 v Velocity[Y] -20.277 21.79 -0.14342 -0.00067793 v Velocity[Z] -3.0421 2.9784 2.9917e-06 -5.3865e-08 v ǁVelocityǁ 0.0015488 29.547 7.0515 8.0449 v Pressure -1.9015e+05 1.3754e+05 -22578 -13697 v TurbVisc 6.5644e-23 0.0067798 0.00014172 1.218e-05 v CourantNb 3.646e-08 0.01178 0.00016723 4.9095e-06 v FourierNb 1.2425e-07 0.047221 0.00014563 2.1532e-07 v total_pressure -88820 2.3887e+05 78747 87628 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0947 0.099437 0.0028781 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2248e-07 0.05251 0.00031286 5.1248e-06 INSTANT 0.875414000E-01 TIME STEP NUMBER 55612 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283228585E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.754239484E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.49273E-02 0.21331E+01 Friction velocity uk : 0.49273E-02 0.21331E+01 Dimensionless distance yplus : 0.48376E-02 0.20945E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -4.272973764e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29468E+08 1 0.18384E-09 0.24288E+02 0.19299E+04 c Velocity[X] 0.12208E+02 c Velocity[Y] 0.12079E+02 c Velocity[Z] 0.22965E-05 c Pressure 0.22047E-03 23 0.98647E-04 0.28986E-02 0.58524E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -18.369 29.183 5.6136 8.0073 v Velocity[Y] -20.295 21.806 -0.14342 -0.00067781 v Velocity[Z] -3.042 2.9784 2.9908e-06 -5.3865e-08 v ǁVelocityǁ 0.0015889 29.564 7.053 8.0449 v Pressure -1.9221e+05 1.3577e+05 -24421 -14861 v TurbVisc 3.1085e-22 0.0067986 0.00014179 1.22e-05 v CourantNb 3.9404e-08 0.01178 0.00016724 4.9095e-06 v FourierNb 1.2425e-07 0.047219 0.00014563 2.1546e-07 v total_pressure -90881 2.3709e+05 76904 86464 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0945 0.099426 0.0028779 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2247e-07 0.052509 0.00031287 5.125e-06 INSTANT 0.875415000E-01 TIME STEP NUMBER 55613 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283226249E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.754323305E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.93877E-02 0.21328E+01 Friction velocity uk : 0.93877E-02 0.21328E+01 Dimensionless distance yplus : 0.92167E-02 0.20942E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -5.231085357e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29468E+08 1 0.18381E-09 0.24286E+02 0.19298E+04 c Velocity[X] 0.12210E+02 c Velocity[Y] 0.12076E+02 c Velocity[Z] 0.22773E-05 c Pressure 0.21852E-03 82 0.83386E-04 0.28704E-02 0.52863E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -18.384 29.203 5.6136 8.0073 v Velocity[Y] -20.312 21.821 -0.14341 -0.00067813 v Velocity[Z] -3.0419 2.9784 2.9899e-06 -5.3865e-08 v ǁVelocityǁ 0.0016234 29.58 7.0546 8.045 v Pressure -1.9423e+05 1.3402e+05 -26309 -15993 v TurbVisc 5.7248e-23 0.0068173 0.00014187 1.2221e-05 v CourantNb 4.3335e-08 0.011781 0.00016724 4.9096e-06 v FourierNb 1.2425e-07 0.047218 0.00014563 2.156e-07 v total_pressure -92909 2.3534e+05 75016 85332 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0942 0.099416 0.0028776 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2247e-07 0.052507 0.00031287 5.1252e-06 INSTANT 0.875416000E-01 TIME STEP NUMBER 55614 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283223729E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.754396712E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13844E-01 0.21324E+01 Friction velocity uk : 0.13844E-01 0.21324E+01 Dimensionless distance yplus : 0.13463E-01 0.20939E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -6.443600056e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29468E+08 1 0.18378E-09 0.24288E+02 0.19298E+04 c Velocity[X] 0.12213E+02 c Velocity[Y] 0.12076E+02 c Velocity[Z] 0.22695E-05 c Pressure 0.21646E-03 10 0.60857E-04 0.28409E-02 0.45722E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -18.399 29.223 5.6135 8.0072 v Velocity[Y] -20.329 21.837 -0.14341 -0.00067891 v Velocity[Z] -3.0418 2.9784 2.989e-06 -5.3865e-08 v ǁVelocityǁ 0.0016493 29.596 7.0562 8.045 v Pressure -1.9623e+05 1.3229e+05 -28176 -17006 v TurbVisc 1.9881e-21 0.0068361 0.00014195 1.2241e-05 v CourantNb 4.8982e-08 0.011781 0.00016724 4.9096e-06 v FourierNb 1.2425e-07 0.047216 0.00014564 2.1574e-07 v total_pressure -94906 2.3361e+05 73149 84319 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0939 0.099403 0.0028772 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2247e-07 0.052504 0.00031288 5.1254e-06 INSTANT 0.875417000E-01 TIME STEP NUMBER 55615 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283221027E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.754464653E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15778E-01 0.21322E+01 Friction velocity uk : 0.15778E-01 0.21322E+01 Dimensionless distance yplus : 0.15343E-01 0.20936E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -7.733842358e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29467E+08 1 0.18376E-09 0.24287E+02 0.19297E+04 c Velocity[X] 0.12215E+02 c Velocity[Y] 0.12072E+02 c Velocity[Z] 0.22503E-05 c Pressure 0.21494E-03 101 0.76332E-04 0.28186E-02 0.47995E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -18.415 29.243 5.6134 8.0072 v Velocity[Y] -20.347 21.853 -0.14341 -0.00067829 v Velocity[Z] -3.0417 2.9783 2.9881e-06 -5.3865e-08 v ǁVelocityǁ 0.0016562 29.612 7.0577 8.045 v Pressure -1.9819e+05 1.3058e+05 -29933 -18029 v TurbVisc 1.133e-22 0.0068548 0.00014203 1.2261e-05 v CourantNb 5.5665e-08 0.011781 0.00016724 4.9097e-06 v FourierNb 1.2425e-07 0.047215 0.00014564 2.1589e-07 v total_pressure -96869 2.319e+05 71392 83296 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0936 0.099385 0.0028767 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2246e-07 0.052503 0.00031288 5.1255e-06 INSTANT 0.875418000E-01 TIME STEP NUMBER 55616 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283218223E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.754521122E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.76688E-02 0.21318E+01 Friction velocity uk : 0.76688E-02 0.21318E+01 Dimensionless distance yplus : 0.73993E-02 0.20933E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -8.672351404e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29467E+08 1 0.18373E-09 0.24287E+02 0.19297E+04 c Velocity[X] 0.12217E+02 c Velocity[Y] 0.12069E+02 c Velocity[Z] 0.22289E-05 c Pressure 0.21289E-03 30 0.81465E-04 0.27893E-02 0.48170E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -18.43 29.262 5.6133 8.0071 v Velocity[Y] -20.364 21.868 -0.1434 -0.00067929 v Velocity[Z] -3.0415 2.9783 2.9872e-06 -5.3865e-08 v ǁVelocityǁ 0.0016552 29.629 7.0593 8.0451 v Pressure -2.0013e+05 1.2889e+05 -31775 -19144 v TurbVisc 4.6922e-23 0.0068736 0.0001421 1.2282e-05 v CourantNb 4.9705e-08 0.011781 0.00016724 4.9097e-06 v FourierNb 1.2425e-07 0.047213 0.00014564 2.1603e-07 v total_pressure -98805 2.3021e+05 69550 82181 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0933 0.099359 0.0028761 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2246e-07 0.0525 0.00031288 5.1257e-06 INSTANT 0.875419000E-01 TIME STEP NUMBER 55617 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283215277E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.754563085E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.83852E-02 0.21315E+01 Friction velocity uk : 0.83852E-02 0.21315E+01 Dimensionless distance yplus : 0.84204E-02 0.20930E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -9.797544257e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29467E+08 1 0.18370E-09 0.24286E+02 0.19297E+04 c Velocity[X] 0.12219E+02 c Velocity[Y] 0.12067E+02 c Velocity[Z] 0.22090E-05 c Pressure 0.21096E-03 236 0.94261E-04 0.27617E-02 0.38874E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -18.445 29.282 5.6132 8.007 v Velocity[Y] -20.381 21.884 -0.14339 -0.00067824 v Velocity[Z] -3.0414 2.9783 2.9863e-06 -5.3865e-08 v ǁVelocityǁ 0.0016417 29.645 7.0608 8.0451 v Pressure -2.0204e+05 1.2721e+05 -33525 -20034 v TurbVisc 7.3845e-23 0.0068924 0.00014218 1.2302e-05 v CourantNb 3.8043e-08 0.011781 0.00016724 4.9097e-06 v FourierNb 1.2425e-07 0.047211 0.00014564 2.1617e-07 v total_pressure -1.0072e+05 2.2853e+05 67800 81291 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.093 0.099327 0.0028754 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2245e-07 0.052498 0.00031289 5.1259e-06 INSTANT 0.875420000E-01 TIME STEP NUMBER 55618 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283212031E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.754596706E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15694E-02 0.21312E+01 Friction velocity uk : 0.15694E-02 0.21312E+01 Dimensionless distance yplus : 0.15351E-02 0.20926E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.084741867e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29466E+08 1 0.18367E-09 0.24281E+02 0.19294E+04 c Velocity[X] 0.12221E+02 c Velocity[Y] 0.12060E+02 c Velocity[Z] 0.21918E-05 c Pressure 0.20889E-03 364 0.80029E-04 0.27321E-02 0.42901E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -18.46 29.302 5.6132 8.007 v Velocity[Y] -20.398 21.899 -0.14339 -0.00067825 v Velocity[Z] -3.0413 2.9783 2.9854e-06 -5.3865e-08 v ǁVelocityǁ 0.0016154 29.661 7.0624 8.0451 v Pressure -2.0393e+05 1.2554e+05 -35290 -21107 v TurbVisc 4.7828e-23 0.0069112 0.00014226 1.2323e-05 v CourantNb 2.4803e-08 0.011781 0.00016724 4.9098e-06 v FourierNb 1.2425e-07 0.047209 0.00014564 2.1631e-07 v total_pressure -1.026e+05 2.2687e+05 66035 80218 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0926 0.099291 0.0028745 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2245e-07 0.052496 0.00031289 5.1261e-06 INSTANT 0.875421000E-01 TIME STEP NUMBER 55619 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283208731E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.754615744E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.32674E-02 0.21309E+01 Friction velocity uk : 0.32674E-02 0.21309E+01 Dimensionless distance yplus : 0.32178E-02 0.20923E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.178431334e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29466E+08 1 0.18364E-09 0.24283E+02 0.19295E+04 c Velocity[X] 0.12224E+02 c Velocity[Y] 0.12059E+02 c Velocity[Z] 0.21816E-05 c Pressure 0.20571E-03 10 0.61563E-04 0.26883E-02 0.34995E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -18.475 29.321 5.6131 8.0069 v Velocity[Y] -20.415 21.915 -0.14338 -0.00067918 v Velocity[Z] -3.0412 2.9782 2.9845e-06 -5.3865e-08 v ǁVelocityǁ 0.0015785 29.677 7.0639 8.0452 v Pressure -2.0579e+05 1.239e+05 -37031 -22031 v TurbVisc 6.1425e-23 0.00693 0.00014233 1.2343e-05 v CourantNb 1.0025e-08 0.011781 0.00016725 4.9098e-06 v FourierNb 1.2425e-07 0.047208 0.00014565 2.1645e-07 v total_pressure -1.0447e+05 2.2523e+05 64294 79294 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0923 0.099274 0.0028738 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2244e-07 0.052494 0.00031289 5.1263e-06 INSTANT 0.875422000E-01 TIME STEP NUMBER 55620 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283205199E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.754623412E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.65174E-02 0.21306E+01 Friction velocity uk : 0.65174E-02 0.21306E+01 Dimensionless distance yplus : 0.64186E-02 0.20921E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.272873280e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29466E+08 1 0.18361E-09 0.24281E+02 0.19294E+04 c Velocity[X] 0.12227E+02 c Velocity[Y] 0.12055E+02 c Velocity[Z] 0.21596E-05 c Pressure 0.20373E-03 81 0.76289E-04 0.26602E-02 0.40177E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -18.489 29.34 5.613 8.0068 v Velocity[Y] -20.432 21.93 -0.14337 -0.0006785 v Velocity[Z] -3.0411 2.9782 2.9836e-06 -5.3865e-08 v ǁVelocityǁ 0.0015232 29.693 7.0654 8.0452 v Pressure -2.0766e+05 1.2229e+05 -38712 -23042 v TurbVisc 2.8305e-22 0.0069487 0.00014241 1.2364e-05 v CourantNb 5.8148e-09 0.011781 0.00016725 4.9098e-06 v FourierNb 1.2425e-07 0.047206 0.00014565 2.166e-07 v total_pressure -1.0634e+05 2.2362e+05 62613 78283 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0921 0.099259 0.002873 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2244e-07 0.052493 0.00031289 5.1264e-06 INSTANT 0.875423000E-01 TIME STEP NUMBER 55621 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283201610E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.754621945E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.43655E-02 0.21303E+01 Friction velocity uk : 0.43655E-02 0.21303E+01 Dimensionless distance yplus : 0.42352E-02 0.20918E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.338694603e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29466E+08 1 0.18357E-09 0.24281E+02 0.19294E+04 c Velocity[X] 0.12230E+02 c Velocity[Y] 0.12051E+02 c Velocity[Z] 0.21368E-05 c Pressure 0.20132E-03 30 0.82166E-04 0.26265E-02 0.39402E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -18.504 29.36 5.6129 8.0068 v Velocity[Y] -20.448 21.945 -0.14337 -0.00067951 v Velocity[Z] -3.041 2.9782 2.9828e-06 -5.3866e-08 v ǁVelocityǁ 0.0014628 29.709 7.067 8.0452 v Pressure -2.0949e+05 1.2071e+05 -40451 -24109 v TurbVisc 4.0907e-23 0.0069675 0.00014248 1.2384e-05 v CourantNb 2.3149e-08 0.011781 0.00016725 4.9099e-06 v FourierNb 1.2425e-07 0.047205 0.00014565 2.1674e-07 v total_pressure -1.0817e+05 2.2203e+05 60874 77216 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0918 0.099247 0.0028721 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2243e-07 0.05249 0.0003129 5.1266e-06 INSTANT 0.875424000E-01 TIME STEP NUMBER 55622 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283197895E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.754611386E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.97579E-02 0.21300E+01 Friction velocity uk : 0.97579E-02 0.21300E+01 Dimensionless distance yplus : 0.94666E-02 0.20915E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.399253299e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29465E+08 1 0.18354E-09 0.24280E+02 0.19293E+04 c Velocity[X] 0.12231E+02 c Velocity[Y] 0.12049E+02 c Velocity[Z] 0.21154E-05 c Pressure 0.19905E-03 231 0.94899E-04 0.25947E-02 0.31618E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -18.519 29.379 5.6127 8.0067 v Velocity[Y] -20.465 21.961 -0.14336 -0.0006784 v Velocity[Z] -3.0409 2.9782 2.9819e-06 -5.3866e-08 v ǁVelocityǁ 0.0013945 29.725 7.0685 8.0452 v Pressure -2.113e+05 1.1913e+05 -42095 -24945 v TurbVisc 6.7578e-23 0.0069863 0.00014255 1.2404e-05 v CourantNb 2.1222e-08 0.011781 0.00016725 4.9099e-06 v FourierNb 1.2425e-07 0.047203 0.00014565 2.1688e-07 v total_pressure -1.0998e+05 2.2045e+05 59230 76380 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0915 0.099235 0.0028713 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2243e-07 0.052488 0.0003129 5.1268e-06 INSTANT 0.875425000E-01 TIME STEP NUMBER 55623 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283193898E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.754596492E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11833E-01 0.21297E+01 Friction velocity uk : 0.11833E-01 0.21297E+01 Dimensionless distance yplus : 0.11470E-01 0.20912E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.451020464e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29465E+08 1 0.18351E-09 0.24274E+02 0.19291E+04 c Velocity[X] 0.12234E+02 c Velocity[Y] 0.12040E+02 c Velocity[Z] 0.20978E-05 c Pressure 0.19665E-03 126 0.80648E-04 0.25613E-02 0.34949E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -18.534 29.398 5.6126 8.0066 v Velocity[Y] -20.482 21.976 -0.14335 -0.00067857 v Velocity[Z] -3.0408 2.9782 2.981e-06 -5.3866e-08 v ǁVelocityǁ 0.0013202 29.741 7.07 8.0452 v Pressure -2.1309e+05 1.1755e+05 -43748 -25962 v TurbVisc 1.7624e-22 0.0070051 0.00014263 1.2425e-05 v CourantNb 1.3199e-08 0.011781 0.00016725 4.9099e-06 v FourierNb 1.2425e-07 0.047201 0.00014566 2.1702e-07 v total_pressure -1.1176e+05 2.1888e+05 57577 75363 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0912 0.09922 0.0028705 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2242e-07 0.052486 0.0003129 5.1269e-06 INSTANT 0.875426000E-01 TIME STEP NUMBER 55624 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283189847E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.754568536E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15851E-01 0.21294E+01 Friction velocity uk : 0.15851E-01 0.21294E+01 Dimensionless distance yplus : 0.15544E-01 0.20909E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.489119903e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29464E+08 1 0.18347E-09 0.24275E+02 0.19291E+04 c Velocity[X] 0.12237E+02 c Velocity[Y] 0.12039E+02 c Velocity[Z] 0.20872E-05 c Pressure 0.19305E-03 10 0.60636E-04 0.25123E-02 0.27438E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -18.549 29.417 5.6125 8.0065 v Velocity[Y] -20.499 21.991 -0.14334 -0.00067934 v Velocity[Z] -3.0407 2.9781 2.9801e-06 -5.3866e-08 v ǁVelocityǁ 0.0012436 29.758 7.0715 8.0452 v Pressure -2.1484e+05 1.16e+05 -45356 -26798 v TurbVisc 1.2315e-22 0.007024 0.0001427 1.2445e-05 v CourantNb 3.1721e-09 0.011781 0.00016725 4.91e-06 v FourierNb 1.2425e-07 0.0472 0.00014566 2.1716e-07 v total_pressure -1.1351e+05 2.1732e+05 55969 74527 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0909 0.099197 0.0028695 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2241e-07 0.052484 0.00031291 5.1271e-06 INSTANT 0.875427000E-01 TIME STEP NUMBER 55625 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283185600E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.754529640E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.84544E-02 0.21291E+01 Friction velocity uk : 0.84544E-02 0.21291E+01 Dimensionless distance yplus : 0.82906E-02 0.20906E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.516142999e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29464E+08 1 0.18344E-09 0.24273E+02 0.19290E+04 c Velocity[X] 0.12240E+02 c Velocity[Y] 0.12034E+02 c Velocity[Z] 0.20664E-05 c Pressure 0.19070E-03 203 0.76510E-04 0.24796E-02 0.32784E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -18.563 29.436 5.6124 8.0064 v Velocity[Y] -20.515 22.006 -0.14333 -0.00067864 v Velocity[Z] -3.0406 2.9781 2.9792e-06 -5.3866e-08 v ǁVelocityǁ 0.0011595 29.774 7.0731 8.0452 v Pressure -2.1657e+05 1.1444e+05 -46930 -27750 v TurbVisc 4.6942e-22 0.0070428 0.00014277 1.2466e-05 v CourantNb 2.098e-08 0.011782 0.00016725 4.91e-06 v FourierNb 1.2425e-07 0.047198 0.00014566 2.173e-07 v total_pressure -1.1524e+05 2.1576e+05 54395 73575 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0906 0.099165 0.0028685 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2241e-07 0.052483 0.00031291 5.1273e-06 INSTANT 0.875428000E-01 TIME STEP NUMBER 55626 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283181271E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.754479803E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.36822E-02 0.21288E+01 Friction velocity uk : 0.36822E-02 0.21288E+01 Dimensionless distance yplus : 0.36405E-02 0.20903E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.532159142e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29464E+08 1 0.18340E-09 0.24272E+02 0.19289E+04 c Velocity[X] 0.12243E+02 c Velocity[Y] 0.12029E+02 c Velocity[Z] 0.20458E-05 c Pressure 0.18800E-03 29 0.82573E-04 0.24425E-02 0.31503E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -18.578 29.454 5.6123 8.0063 v Velocity[Y] -20.532 22.021 -0.14332 -0.00067966 v Velocity[Z] -3.0404 2.9781 2.9783e-06 -5.3866e-08 v ǁVelocityǁ 0.0010811 29.79 7.0746 8.0452 v Pressure -2.1826e+05 1.129e+05 -48528 -28718 v TurbVisc 2.7053e-22 0.0070616 0.00014284 1.2486e-05 v CourantNb 3.4363e-08 0.011782 0.00016725 4.91e-06 v FourierNb 1.2425e-07 0.047197 0.00014566 2.1745e-07 v total_pressure -1.1694e+05 2.1422e+05 52797 72607 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0903 0.099139 0.0028674 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.224e-07 0.05248 0.00031291 5.1274e-06 INSTANT 0.875429000E-01 TIME STEP NUMBER 55627 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283176848E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.754424235E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.39601E-02 0.21285E+01 Friction velocity uk : 0.39601E-02 0.21285E+01 Dimensionless distance yplus : 0.39128E-02 0.20900E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.524781174e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29463E+08 1 0.18337E-09 0.24270E+02 0.19288E+04 c Velocity[X] 0.12244E+02 c Velocity[Y] 0.12026E+02 c Velocity[Z] 0.20287E-05 c Pressure 0.18538E-03 237 0.95011E-04 0.24065E-02 0.25879E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -18.593 29.473 5.6122 8.0062 v Velocity[Y] -20.549 22.036 -0.14331 -0.00067856 v Velocity[Z] -3.0403 2.9781 2.9774e-06 -5.3866e-08 v ǁVelocityǁ 0.0010078 29.806 7.0761 8.0452 v Pressure -2.1993e+05 1.1137e+05 -50043 -29487 v TurbVisc 1.9321e-22 0.0070804 0.00014291 1.2507e-05 v CourantNb 5.1119e-08 0.011782 0.00016725 4.91e-06 v FourierNb 1.2425e-07 0.047195 0.00014567 2.1759e-07 v total_pressure -1.186e+05 2.1269e+05 51282 71838 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.09 0.099126 0.0028665 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2239e-07 0.052478 0.00031291 5.1276e-06 INSTANT 0.875430000E-01 TIME STEP NUMBER 55628 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283172150E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.754362530E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.45220E-02 0.21281E+01 Friction velocity uk : 0.45220E-02 0.21281E+01 Dimensionless distance yplus : 0.44679E-02 0.20896E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.509991077e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29463E+08 1 0.18333E-09 0.24264E+02 0.19285E+04 c Velocity[X] 0.12247E+02 c Velocity[Y] 0.12017E+02 c Velocity[Z] 0.20150E-05 c Pressure 0.18267E-03 110 0.80931E-04 0.23694E-02 0.28398E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -18.608 29.492 5.6121 8.0061 v Velocity[Y] -20.566 22.051 -0.1433 -0.00067874 v Velocity[Z] -3.0402 2.978 2.9765e-06 -5.3866e-08 v ǁVelocityǁ 0.00094225 29.822 7.0776 8.0452 v Pressure -2.2157e+05 1.0984e+05 -51558 -30423 v TurbVisc 4.0188e-22 0.0070993 0.00014299 1.2527e-05 v CourantNb 8.3509e-08 0.011782 0.00016725 4.91e-06 v FourierNb 1.2425e-07 0.047193 0.00014567 2.1773e-07 v total_pressure -1.2025e+05 2.1116e+05 49767 70902 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0896 0.099099 0.0028654 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2238e-07 0.052476 0.00031292 5.1278e-06 INSTANT 0.875431000E-01 TIME STEP NUMBER 55629 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283167410E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.754289752E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.61323E-02 0.21278E+01 Friction velocity uk : 0.61323E-02 0.21278E+01 Dimensionless distance yplus : 0.60879E-02 0.20893E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.483752900e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29462E+08 1 0.18329E-09 0.24264E+02 0.19285E+04 c Velocity[X] 0.12249E+02 c Velocity[Y] 0.12014E+02 c Velocity[Z] 0.20077E-05 c Pressure 0.17867E-03 10 0.59553E-04 0.23156E-02 0.22021E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -18.622 29.51 5.6119 8.006 v Velocity[Y] -20.582 22.066 -0.1433 -0.00067954 v Velocity[Z] -3.0401 2.978 2.9756e-06 -5.3866e-08 v ǁVelocityǁ 0.00088825 29.838 7.0791 8.0452 v Pressure -2.2318e+05 1.0833e+05 -53018 -31179 v TurbVisc 2.5317e-22 0.0071181 0.00014306 1.2548e-05 v CourantNb 9.4418e-08 0.011782 0.00016725 4.9101e-06 v FourierNb 1.2425e-07 0.047192 0.00014567 2.1787e-07 v total_pressure -1.2185e+05 2.0966e+05 48307 70146 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0893 0.099078 0.0028644 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2238e-07 0.052474 0.00031292 5.1279e-06 INSTANT 0.875432000E-01 TIME STEP NUMBER 55630 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283162497E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.754207687E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.40031E-02 0.21275E+01 Friction velocity uk : 0.40031E-02 0.21275E+01 Dimensionless distance yplus : 0.38893E-02 0.20890E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.439837844e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29462E+08 1 0.18326E-09 0.24260E+02 0.19284E+04 c Velocity[X] 0.12252E+02 c Velocity[Y] 0.12009E+02 c Velocity[Z] 0.19914E-05 c Pressure 0.17599E-03 160 0.76411E-04 0.22791E-02 0.26394E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -18.637 29.528 5.6118 8.0059 v Velocity[Y] -20.599 22.081 -0.14329 -0.00067886 v Velocity[Z] -3.04 2.978 2.9747e-06 -5.3866e-08 v ǁVelocityǁ 0.00084269 29.853 7.0806 8.0452 v Pressure -2.2476e+05 1.0683e+05 -54459 -32033 v TurbVisc 7.8655e-22 0.0071369 0.00014313 1.2568e-05 v CourantNb 8.3136e-08 0.011782 0.00016725 4.9101e-06 v FourierNb 1.2425e-07 0.04719 0.00014567 2.1801e-07 v total_pressure -1.2343e+05 2.0815e+05 46866 69292 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.089 0.099064 0.0028634 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2237e-07 0.052472 0.00031292 5.1281e-06 INSTANT 0.875433000E-01 TIME STEP NUMBER 55631 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283157498E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.754114272E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.23456E-02 0.21272E+01 Friction velocity uk : 0.23456E-02 0.21272E+01 Dimensionless distance yplus : 0.22971E-02 0.20887E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.403929801e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29462E+08 1 0.18322E-09 0.24258E+02 0.19283E+04 c Velocity[X] 0.12255E+02 c Velocity[Y] 0.12003E+02 c Velocity[Z] 0.19763E-05 c Pressure 0.17305E-03 59 0.82324E-04 0.22391E-02 0.25915E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -18.651 29.547 5.6117 8.0058 v Velocity[Y] -20.615 22.095 -0.14328 -0.00067991 v Velocity[Z] -3.0399 2.978 2.9738e-06 -5.3866e-08 v ǁVelocityǁ 0.00081268 29.869 7.0822 8.0452 v Pressure -2.2629e+05 1.0535e+05 -55900 -32916 v TurbVisc 4.9226e-22 0.0071558 0.00014319 1.2589e-05 v CourantNb 3.6899e-08 0.011782 0.00016725 4.9101e-06 v FourierNb 1.2425e-07 0.047188 0.00014568 2.1816e-07 v total_pressure -1.2497e+05 2.0667e+05 45425 68409 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0887 0.099051 0.0028624 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2236e-07 0.05247 0.00031293 5.1283e-06 INSTANT 0.875434000E-01 TIME STEP NUMBER 55632 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283152427E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.754020118E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.80818E-02 0.21268E+01 Friction velocity uk : 0.80818E-02 0.21268E+01 Dimensionless distance yplus : 0.77996E-02 0.20883E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.334782982e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29461E+08 1 0.18318E-09 0.24255E+02 0.19281E+04 c Velocity[X] 0.12256E+02 c Velocity[Y] 0.12000E+02 c Velocity[Z] 0.19639E-05 c Pressure 0.17012E-03 198 0.94937E-04 0.21995E-02 0.20962E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -18.666 29.565 5.6116 8.0057 v Velocity[Y] -20.632 22.11 -0.14327 -0.00067883 v Velocity[Z] -3.0398 2.978 2.9729e-06 -5.3866e-08 v ǁVelocityǁ 0.00079513 29.885 7.0837 8.0452 v Pressure -2.278e+05 1.0388e+05 -57259 -33592 v TurbVisc 5.7131e-22 0.0071746 0.00014326 1.2609e-05 v CourantNb 6.0996e-08 0.011782 0.00016725 4.9101e-06 v FourierNb 1.2425e-07 0.047186 0.00014568 2.183e-07 v total_pressure -1.2647e+05 2.0521e+05 44066 67733 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0883 0.099049 0.0028617 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2235e-07 0.052467 0.00031293 5.1284e-06 INSTANT 0.875435000E-01 TIME STEP NUMBER 55633 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283147095E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.753917976E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.35900E-02 0.21264E+01 Friction velocity uk : 0.35900E-02 0.21264E+01 Dimensionless distance yplus : 0.34933E-02 0.20880E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.264006634e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29461E+08 1 0.18314E-09 0.24247E+02 0.19278E+04 c Velocity[X] 0.12258E+02 c Velocity[Y] 0.11989E+02 c Velocity[Z] 0.19545E-05 c Pressure 0.16711E-03 300 0.80742E-04 0.21587E-02 0.23047E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -18.681 29.583 5.6115 8.0056 v Velocity[Y] -20.648 22.124 -0.14327 -0.000679 v Velocity[Z] -3.0397 2.9779 2.972e-06 -5.3866e-08 v ǁVelocityǁ 0.00078796 29.901 7.0852 8.0452 v Pressure -2.2927e+05 1.0243e+05 -58615 -34429 v TurbVisc 3.2967e-22 0.0071935 0.00014333 1.2629e-05 v CourantNb 6.5487e-08 0.011782 0.00016725 4.9101e-06 v FourierNb 1.2425e-07 0.047184 0.00014568 2.1844e-07 v total_pressure -1.2795e+05 2.0376e+05 42710 66896 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.088 0.099035 0.0028608 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2235e-07 0.052465 0.00031293 5.1286e-06 INSTANT 0.875436000E-01 TIME STEP NUMBER 55634 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283141740E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.753805968E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.78902E-02 0.21261E+01 Friction velocity uk : 0.78902E-02 0.21261E+01 Dimensionless distance yplus : 0.76921E-02 0.20876E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.189792277e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29460E+08 1 0.18310E-09 0.24246E+02 0.19277E+04 c Velocity[X] 0.12260E+02 c Velocity[Y] 0.11986E+02 c Velocity[Z] 0.19500E-05 c Pressure 0.16268E-03 10 0.58438E-04 0.20998E-02 0.17648E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -18.695 29.602 5.6114 8.0055 v Velocity[Y] -20.665 22.139 -0.14326 -0.00067988 v Velocity[Z] -3.0395 2.9779 2.9711e-06 -5.3866e-08 v ǁVelocityǁ 0.00078749 29.916 7.0867 8.0452 v Pressure -2.307e+05 1.0101e+05 -59907 -35098 v TurbVisc 3.7436e-22 0.0072124 0.0001434 1.265e-05 v CourantNb 6.6521e-08 0.011782 0.00016725 4.9101e-06 v FourierNb 1.2425e-07 0.047182 0.00014568 2.1858e-07 v total_pressure -1.2938e+05 2.0233e+05 41418 66227 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0876 0.099041 0.0028603 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2234e-07 0.052462 0.00031293 5.1287e-06 INSTANT 0.875437000E-01 TIME STEP NUMBER 55635 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283136227E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.753685284E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.89417E-02 0.21257E+01 Friction velocity uk : 0.89417E-02 0.21257E+01 Dimensionless distance yplus : 0.88386E-02 0.20873E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.097762408e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29460E+08 1 0.18306E-09 0.24242E+02 0.19275E+04 c Velocity[X] 0.12262E+02 c Velocity[Y] 0.11980E+02 c Velocity[Z] 0.19391E-05 c Pressure 0.15970E-03 374 0.76330E-04 0.20597E-02 0.21592E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -18.71 29.62 5.6113 8.0054 v Velocity[Y] -20.681 22.153 -0.14325 -0.00067927 v Velocity[Z] -3.0394 2.9779 2.9702e-06 -5.3866e-08 v ǁVelocityǁ 0.00078818 29.932 7.0882 8.0452 v Pressure -2.321e+05 99603 -61192 -35856 v TurbVisc 7.7803e-23 0.0072312 0.00014347 1.267e-05 v CourantNb 6.5035e-08 0.011782 0.00016725 4.9102e-06 v FourierNb 1.2425e-07 0.04718 0.00014569 2.1872e-07 v total_pressure -1.3077e+05 2.0093e+05 40133 65469 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0873 0.09905 0.0028598 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2233e-07 0.05246 0.00031294 5.1289e-06 INSTANT 0.875438000E-01 TIME STEP NUMBER 55636 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283130628E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.753552514E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.50113E-02 0.21253E+01 Friction velocity uk : 0.50113E-02 0.21253E+01 Dimensionless distance yplus : 0.49684E-02 0.20869E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.034807858e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29459E+08 1 0.18302E-09 0.24238E+02 0.19274E+04 c Velocity[X] 0.12264E+02 c Velocity[Y] 0.11974E+02 c Velocity[Z] 0.19290E-05 c Pressure 0.15648E-03 92 0.81923E-04 0.20166E-02 0.21029E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -18.724 29.638 5.6112 8.0053 v Velocity[Y] -20.698 22.167 -0.14325 -0.00068035 v Velocity[Z] -3.0393 2.9779 2.9693e-06 -5.3866e-08 v ǁVelocityǁ 0.00079161 29.947 7.0898 8.0452 v Pressure -2.3344e+05 98233 -62453 -36628 v TurbVisc 9.4732e-23 0.0072501 0.00014353 1.2691e-05 v CourantNb 6.2969e-08 0.011782 0.00016725 4.9102e-06 v FourierNb 1.2425e-07 0.047178 0.00014569 2.1887e-07 v total_pressure -1.3211e+05 1.9956e+05 38872 64697 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0869 0.099069 0.0028595 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2232e-07 0.052457 0.00031294 5.129e-06 INSTANT 0.875439000E-01 TIME STEP NUMBER 55637 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283124981E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.753422092E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11276E-01 0.21249E+01 Friction velocity uk : 0.11276E-01 0.21249E+01 Dimensionless distance yplus : 0.10887E-01 0.20865E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -9.346976897e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29459E+08 1 0.18298E-09 0.24234E+02 0.19272E+04 c Velocity[X] 0.12265E+02 c Velocity[Y] 0.11970E+02 c Velocity[Z] 0.19201E-05 c Pressure 0.15325E-03 191 0.94677E-04 0.19734E-02 0.17105E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -18.739 29.656 5.6111 8.0052 v Velocity[Y] -20.714 22.181 -0.14324 -0.00067934 v Velocity[Z] -3.0392 2.9778 2.9685e-06 -5.3866e-08 v ǁVelocityǁ 0.00079552 29.962 7.0913 8.0451 v Pressure -2.3474e+05 96888 -63636 -37208 v TurbVisc 1.5044e-21 0.007269 0.0001436 1.2711e-05 v CourantNb 6.7593e-08 0.011782 0.00016725 4.9102e-06 v FourierNb 1.2425e-07 0.047175 0.00014569 2.1901e-07 v total_pressure -1.3341e+05 1.9821e+05 37689 64117 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0865 0.099091 0.0028592 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2231e-07 0.052454 0.00031294 5.1292e-06 INSTANT 0.875440000E-01 TIME STEP NUMBER 55638 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283119091E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.753281910E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.96704E-02 0.21245E+01 Friction velocity uk : 0.96704E-02 0.21245E+01 Dimensionless distance yplus : 0.93280E-02 0.20861E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -8.423962182e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29458E+08 1 0.18294E-09 0.24225E+02 0.19268E+04 c Velocity[X] 0.12266E+02 c Velocity[Y] 0.11959E+02 c Velocity[Z] 0.19133E-05 c Pressure 0.14998E-03 126 0.80267E-04 0.19298E-02 0.18734E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -18.753 29.674 5.611 8.0051 v Velocity[Y] -20.731 22.195 -0.14324 -0.00067962 v Velocity[Z] -3.0391 2.9778 2.9676e-06 -5.3866e-08 v ǁVelocityǁ 0.00079826 29.977 7.0928 8.0451 v Pressure -2.36e+05 95574 -64812 -37942 v TurbVisc 2.8595e-22 0.0072879 0.00014367 1.2732e-05 v CourantNb 5.4253e-08 0.011782 0.00016725 4.9102e-06 v FourierNb 1.2425e-07 0.047173 0.00014569 2.1915e-07 v total_pressure -1.3467e+05 1.969e+05 36513 63383 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0861 0.099112 0.002859 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.223e-07 0.052451 0.00031295 5.1293e-06 INSTANT 0.875441000E-01 TIME STEP NUMBER 55639 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283113189E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.753132754E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.26939E-02 0.21241E+01 Friction velocity uk : 0.26939E-02 0.21241E+01 Dimensionless distance yplus : 0.26584E-02 0.20857E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -7.558314109e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29458E+08 1 0.18290E-09 0.24222E+02 0.19267E+04 c Velocity[X] 0.12267E+02 c Velocity[Y] 0.11955E+02 c Velocity[Z] 0.19188E-05 c Pressure 0.14516E-03 9 0.56874E-04 0.18663E-02 0.13646E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -18.768 29.692 5.6109 8.0049 v Velocity[Y] -20.747 22.209 -0.14324 -0.00068053 v Velocity[Z] -3.039 2.9778 2.9667e-06 -5.3866e-08 v ǁVelocityǁ 0.00079867 29.992 7.0943 8.0451 v Pressure -2.372e+05 94303 -65914 -38496 v TurbVisc 6.1741e-22 0.0073068 0.00014373 1.2752e-05 v CourantNb 5.137e-08 0.011782 0.00016725 4.9102e-06 v FourierNb 1.2425e-07 0.047171 0.0001457 2.1929e-07 v total_pressure -1.3588e+05 1.9563e+05 35411 62829 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0857 0.099129 0.0028588 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2229e-07 0.052448 0.00031295 5.1295e-06 INSTANT 0.875442000E-01 TIME STEP NUMBER 55640 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283107168E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.752975323E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12689E-01 0.21237E+01 Friction velocity uk : 0.12689E-01 0.21237E+01 Dimensionless distance yplus : 0.12240E-01 0.20853E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -6.598946638e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29457E+08 1 0.18286E-09 0.24216E+02 0.19265E+04 c Velocity[X] 0.12268E+02 c Velocity[Y] 0.11948E+02 c Velocity[Z] 0.19073E-05 c Pressure 0.14202E-03 169 0.75536E-04 0.18245E-02 0.17682E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -18.782 29.709 5.6108 8.0048 v Velocity[Y] -20.763 22.222 -0.14323 -0.00067994 v Velocity[Z] -3.0389 2.9778 2.9658e-06 -5.3866e-08 v ǁVelocityǁ 0.00079794 30.007 7.0959 8.0451 v Pressure -2.3836e+05 93063 -67017 -39159 v TurbVisc 8.8142e-22 0.0073257 0.00014379 1.2773e-05 v CourantNb 7.8688e-09 0.011782 0.00016725 4.9102e-06 v FourierNb 1.2425e-07 0.047168 0.0001457 2.1943e-07 v total_pressure -1.3704e+05 1.9439e+05 34308 62166 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0853 0.099152 0.0028587 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2228e-07 0.052445 0.00031295 5.1297e-06 INSTANT 0.875443000E-01 TIME STEP NUMBER 55641 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283101043E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.752806881E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11847E-01 0.21232E+01 Friction velocity uk : 0.11847E-01 0.21232E+01 Dimensionless distance yplus : 0.11446E-01 0.20848E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -5.978875412e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29456E+08 1 0.18281E-09 0.24211E+02 0.19262E+04 c Velocity[X] 0.12269E+02 c Velocity[Y] 0.11942E+02 c Velocity[Z] 0.18960E-05 c Pressure 0.13857E-03 62 0.80807E-04 0.17789E-02 0.16408E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -18.796 29.727 5.6107 8.0047 v Velocity[Y] -20.779 22.235 -0.14323 -0.00068097 v Velocity[Z] -3.0387 2.9777 2.9649e-06 -5.3866e-08 v ǁVelocityǁ 0.00079489 30.021 7.0974 8.045 v Pressure -2.3946e+05 91875 -68071 -39779 v TurbVisc 2.074e-22 0.0073446 0.00014386 1.2793e-05 v CourantNb 2.5373e-08 0.011782 0.00016726 4.9102e-06 v FourierNb 1.2425e-07 0.047166 0.0001457 2.1957e-07 v total_pressure -1.3813e+05 1.932e+05 33254 61546 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0848 0.099173 0.0028586 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2227e-07 0.052442 0.00031296 5.1298e-06 INSTANT 0.875444000E-01 TIME STEP NUMBER 55642 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283094925E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.752638906E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.93693E-02 0.21228E+01 Friction velocity uk : 0.93693E-02 0.21228E+01 Dimensionless distance yplus : 0.90376E-02 0.20844E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -5.110240006e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29456E+08 1 0.18277E-09 0.24206E+02 0.19260E+04 c Velocity[X] 0.12269E+02 c Velocity[Y] 0.11937E+02 c Velocity[Z] 0.18867E-05 c Pressure 0.13522E-03 300 0.93346E-04 0.17345E-02 0.14976E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -18.811 29.745 5.6106 8.0046 v Velocity[Y] -20.795 22.249 -0.14323 -0.00068015 v Velocity[Z] -3.0386 2.9777 2.964e-06 -5.3866e-08 v ǁVelocityǁ 0.00079115 30.036 7.0989 8.045 v Pressure -2.4051e+05 90723 -69079 -40327 v TurbVisc 5.6172e-22 0.0073635 0.00014392 1.2814e-05 v CourantNb 5.0821e-08 0.011782 0.00016726 4.9102e-06 v FourierNb 1.2425e-07 0.047163 0.0001457 2.1972e-07 v total_pressure -1.3919e+05 1.9205e+05 32246 60998 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0844 0.099192 0.0028586 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2226e-07 0.052439 0.00031296 5.13e-06 INSTANT 0.875445000E-01 TIME STEP NUMBER 55643 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283088534E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.752461004E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.84658E-02 0.21224E+01 Friction velocity uk : 0.84658E-02 0.21224E+01 Dimensionless distance yplus : 0.84219E-02 0.20840E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -4.367550863e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29455E+08 1 0.18273E-09 0.24195E+02 0.19256E+04 c Velocity[X] 0.12269E+02 c Velocity[Y] 0.11925E+02 c Velocity[Z] 0.18807E-05 c Pressure 0.13192E-03 83 0.79173E-04 0.16909E-02 0.13967E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -18.825 29.763 5.6105 8.0044 v Velocity[Y] -20.812 22.262 -0.14323 -0.00068051 v Velocity[Z] -3.0385 2.9777 2.9631e-06 -5.3866e-08 v ǁVelocityǁ 0.00078829 30.05 7.1004 8.045 v Pressure -2.4151e+05 89622 -70040 -40896 v TurbVisc 4.2711e-22 0.0073824 0.00014399 1.2834e-05 v CourantNb 4.9666e-08 0.011782 0.00016726 4.9103e-06 v FourierNb 1.2425e-07 0.047161 0.0001457 2.1986e-07 v total_pressure -1.4019e+05 1.9095e+05 31285 60429 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.084 0.099208 0.0028585 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2225e-07 0.052436 0.00031296 5.1301e-06 INSTANT 0.875446000E-01 TIME STEP NUMBER 55644 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283082177E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.752275543E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.22984E-02 0.21220E+01 Friction velocity uk : 0.22984E-02 0.21220E+01 Dimensionless distance yplus : 0.22865E-02 0.20836E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -3.754555162e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29455E+08 1 0.18268E-09 0.24190E+02 0.19254E+04 c Velocity[X] 0.12269E+02 c Velocity[Y] 0.11921E+02 c Velocity[Z] 0.18791E-05 c Pressure 0.12692E-03 9 0.54924E-04 0.16256E-02 0.10618E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -18.839 29.78 5.6104 8.0043 v Velocity[Y] -20.827 22.275 -0.14323 -0.00068148 v Velocity[Z] -3.0384 2.9777 2.9622e-06 -5.3866e-08 v ǁVelocityǁ 0.00078774 30.064 7.102 8.0449 v Pressure -2.4245e+05 88575 -70946 -41347 v TurbVisc 1.1906e-21 0.0074013 0.00014405 1.2855e-05 v CourantNb 4.9934e-08 0.011782 0.00016726 4.9103e-06 v FourierNb 1.2425e-07 0.047158 0.00014571 2.2e-07 v total_pressure -1.4113e+05 1.899e+05 30379 59978 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0836 0.099225 0.0028585 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2224e-07 0.052433 0.00031297 5.1303e-06 INSTANT 0.875447000E-01 TIME STEP NUMBER 55645 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283075731E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.752081439E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11798E-01 0.21216E+01 Friction velocity uk : 0.11798E-01 0.21216E+01 Dimensionless distance yplus : 0.11419E-01 0.20832E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -3.129934822e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29454E+08 1 0.18264E-09 0.24181E+02 0.19250E+04 c Velocity[X] 0.12269E+02 c Velocity[Y] 0.11912E+02 c Velocity[Z] 0.18685E-05 c Pressure 0.12393E-03 362 0.99751E-04 0.15860E-02 0.13040E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -18.853 29.798 5.6103 8.0042 v Velocity[Y] -20.843 22.288 -0.14323 -0.00068214 v Velocity[Z] -3.0383 2.9776 2.9614e-06 -5.3866e-08 v ǁVelocityǁ 0.00078802 30.079 7.1035 8.0449 v Pressure -2.4334e+05 87574 -71829 -41908 v TurbVisc 2.1939e-21 0.0074202 0.00014411 1.2875e-05 v CourantNb 4.9326e-08 0.011782 0.00016726 4.9103e-06 v FourierNb 1.2425e-07 0.047156 0.00014571 2.2014e-07 v total_pressure -1.4202e+05 1.889e+05 29496 59417 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0832 0.099247 0.0028586 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2223e-07 0.05243 0.00031297 5.1304e-06 INSTANT 0.875448000E-01 TIME STEP NUMBER 55646 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283069194E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.751877717E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13735E-01 0.21212E+01 Friction velocity uk : 0.13735E-01 0.21212E+01 Dimensionless distance yplus : 0.13294E-01 0.20828E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -2.788405151e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29454E+08 1 0.18260E-09 0.24172E+02 0.19247E+04 c Velocity[X] 0.12268E+02 c Velocity[Y] 0.11905E+02 c Velocity[Z] 0.18568E-05 c Pressure 0.12020E-03 144 0.83275E-04 0.15372E-02 0.10298E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -18.868 29.815 5.6103 8.004 v Velocity[Y] -20.859 22.301 -0.14324 -0.00068223 v Velocity[Z] -3.0382 2.9776 2.9605e-06 -5.3866e-08 v ǁVelocityǁ 0.00079253 30.092 7.105 8.0449 v Pressure -2.4417e+05 86632 -72675 -42363 v TurbVisc 2.2381e-21 0.0074392 0.00014417 1.2896e-05 v CourantNb 3.323e-08 0.011782 0.00016726 4.9103e-06 v FourierNb 1.2425e-07 0.047154 0.00014571 2.2028e-07 v total_pressure -1.4285e+05 1.8796e+05 28650 58962 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0828 0.099267 0.0028586 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2222e-07 0.052427 0.00031297 5.1306e-06 INSTANT 0.875449000E-01 TIME STEP NUMBER 55647 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283062587E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.751670392E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.16030E-01 0.21208E+01 Friction velocity uk : 0.16030E-01 0.21208E+01 Dimensionless distance yplus : 0.15574E-01 0.20824E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -2.414014209e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29453E+08 1 0.18255E-09 0.24167E+02 0.19244E+04 c Velocity[X] 0.12266E+02 c Velocity[Y] 0.11901E+02 c Velocity[Z] 0.18505E-05 c Pressure 0.11631E-03 9 0.52955E-04 0.14862E-02 0.87544E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -18.882 29.833 5.6102 8.0039 v Velocity[Y] -20.875 22.313 -0.14324 -0.00068143 v Velocity[Z] -3.038 2.9776 2.9596e-06 -5.3866e-08 v ǁVelocityǁ 0.00080251 30.106 7.1066 8.0448 v Pressure -2.4494e+05 85746 -73466 -42744 v TurbVisc 5.2846e-22 0.0074581 0.00014423 1.2916e-05 v CourantNb 4.2486e-08 0.011782 0.00016727 4.9103e-06 v FourierNb 1.2425e-07 0.047151 0.00014571 2.2043e-07 v total_pressure -1.4362e+05 1.8707e+05 27859 58581 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0824 0.099284 0.0028587 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2221e-07 0.052424 0.00031298 5.1307e-06 INSTANT 0.875450000E-01 TIME STEP NUMBER 55648 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283055865E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.751456346E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10055E-01 0.21204E+01 Friction velocity uk : 0.10055E-01 0.21204E+01 Dimensionless distance yplus : 0.97687E-02 0.20821E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -2.133308715e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29452E+08 1 0.18251E-09 0.24158E+02 0.19240E+04 c Velocity[X] 0.12266E+02 c Velocity[Y] 0.11891E+02 c Velocity[Z] 0.18402E-05 c Pressure 0.11367E-03 78 0.75463E-04 0.14514E-02 0.14802E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -18.896 29.85 5.6101 8.0038 v Velocity[Y] -20.89 22.326 -0.14324 -0.00068262 v Velocity[Z] -3.0379 2.9776 2.9587e-06 -5.3866e-08 v ǁVelocityǁ 0.00082079 30.12 7.1081 8.0448 v Pressure -2.4567e+05 84911 -74224 -43331 v TurbVisc 4.4445e-22 0.007477 0.00014429 1.2937e-05 v CourantNb 2.4434e-08 0.011782 0.00016727 4.9103e-06 v FourierNb 1.2425e-07 0.047149 0.00014571 2.2057e-07 v total_pressure -1.4435e+05 1.8624e+05 27101 57994 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0821 0.099297 0.0028587 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.222e-07 0.052422 0.00031298 5.1309e-06 INSTANT 0.875451000E-01 TIME STEP NUMBER 55649 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283049218E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.751234053E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.74692E-02 0.21201E+01 Friction velocity uk : 0.74692E-02 0.21201E+01 Dimensionless distance yplus : 0.72568E-02 0.20817E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -2.022369469e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29452E+08 1 0.18247E-09 0.24150E+02 0.19237E+04 c Velocity[X] 0.12264E+02 c Velocity[Y] 0.11886E+02 c Velocity[Z] 0.18298E-05 c Pressure 0.11054E-03 61 0.79377E-04 0.14104E-02 0.99081E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -18.91 29.868 5.61 8.0036 v Velocity[Y] -20.906 22.338 -0.14325 -0.00068203 v Velocity[Z] -3.0378 2.9775 2.9578e-06 -5.3866e-08 v ǁVelocityǁ 0.0008452 30.133 7.1096 8.0448 v Pressure -2.4634e+05 84139 -74929 -43672 v TurbVisc 3.2215e-21 0.007496 0.00014435 1.2957e-05 v CourantNb 8.3091e-09 0.011782 0.00016727 4.9103e-06 v FourierNb 1.2425e-07 0.047147 0.00014571 2.2071e-07 v total_pressure -1.4501e+05 1.8546e+05 26396 57653 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0817 0.099308 0.0028587 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2219e-07 0.052419 0.00031298 5.131e-06 INSTANT 0.875452000E-01 TIME STEP NUMBER 55650 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283042339E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.751005814E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.53498E-02 0.21198E+01 Friction velocity uk : 0.53498E-02 0.21198E+01 Dimensionless distance yplus : 0.53393E-02 0.20814E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.930133885e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29451E+08 1 0.18242E-09 0.24141E+02 0.19234E+04 c Velocity[X] 0.12263E+02 c Velocity[Y] 0.11878E+02 c Velocity[Z] 0.18173E-05 c Pressure 0.10779E-03 101 0.92699E-04 0.13743E-02 0.12072E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -18.924 29.885 5.61 8.0035 v Velocity[Y] -20.921 22.351 -0.14325 -0.00068345 v Velocity[Z] -3.0377 2.9775 2.9569e-06 -5.3866e-08 v ǁVelocityǁ 0.00087541 30.147 7.1112 8.0447 v Pressure -2.4695e+05 83426 -75591 -44091 v TurbVisc 2.3499e-21 0.0075149 0.00014441 1.2978e-05 v CourantNb 1.426e-08 0.011782 0.00016727 4.9103e-06 v FourierNb 1.2425e-07 0.047146 0.00014571 2.2085e-07 v total_pressure -1.4563e+05 1.8475e+05 25734 57234 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0814 0.099318 0.0028587 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2218e-07 0.052417 0.00031299 5.1312e-06 INSTANT 0.875453000E-01 TIME STEP NUMBER 55651 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283035539E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.750770583E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.69935E-02 0.21195E+01 Friction velocity uk : 0.69935E-02 0.21195E+01 Dimensionless distance yplus : 0.69798E-02 0.20811E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.950991765e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29451E+08 1 0.18238E-09 0.24127E+02 0.19228E+04 c Velocity[X] 0.12259E+02 c Velocity[Y] 0.11868E+02 c Velocity[Z] 0.18056E-05 c Pressure 0.10521E-03 272 0.78388E-04 0.13404E-02 0.76167E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -18.937 29.902 5.6099 8.0033 v Velocity[Y] -20.937 22.364 -0.14326 -0.0006835 v Velocity[Z] -3.0376 2.9775 2.956e-06 -5.3866e-08 v ǁVelocityǁ 0.00090989 30.16 7.1127 8.0447 v Pressure -2.4752e+05 82794 -76192 -44366 v TurbVisc 1.9771e-21 0.0075339 0.00014447 1.2998e-05 v CourantNb 2.9025e-08 0.011782 0.00016727 4.9103e-06 v FourierNb 1.2425e-07 0.047144 0.00014572 2.2099e-07 v total_pressure -1.4619e+05 1.8412e+05 25133 56959 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0811 0.099331 0.0028587 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2217e-07 0.052415 0.00031299 5.1313e-06 INSTANT 0.875454000E-01 TIME STEP NUMBER 55652 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283028620E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.750527757E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15646E-01 0.21192E+01 Friction velocity uk : 0.15646E-01 0.21192E+01 Dimensionless distance yplus : 0.15615E-01 0.20809E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -2.086883515e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29450E+08 1 0.18233E-09 0.24119E+02 0.19225E+04 c Velocity[X] 0.12256E+02 c Velocity[Y] 0.11863E+02 c Velocity[Z] 0.18091E-05 c Pressure 0.10065E-03 15 0.54366E-04 0.12813E-02 0.58593E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -18.951 29.919 5.6099 8.0032 v Velocity[Y] -20.952 22.376 -0.14326 -0.000683 v Velocity[Z] -3.0375 2.9775 2.9552e-06 -5.3866e-08 v ǁVelocityǁ 0.00094243 30.173 7.1142 8.0446 v Pressure -2.4803e+05 82232 -76752 -44618 v TurbVisc 2.1178e-21 0.0075528 0.00014453 1.3019e-05 v CourantNb 3.0924e-08 0.011782 0.00016728 4.9103e-06 v FourierNb 1.2425e-07 0.047143 0.00014572 2.2114e-07 v total_pressure -1.467e+05 1.8356e+05 24573 56707 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0809 0.099349 0.0028588 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2216e-07 0.052413 0.00031299 5.1315e-06 INSTANT 0.875455000E-01 TIME STEP NUMBER 55653 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283021598E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.750277877E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.18246E-01 0.21189E+01 Friction velocity uk : 0.18246E-01 0.21189E+01 Dimensionless distance yplus : 0.17567E-01 0.20806E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -2.328450228e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29449E+08 1 0.18229E-09 0.24107E+02 0.19220E+04 c Velocity[X] 0.12254E+02 c Velocity[Y] 0.11853E+02 c Velocity[Z] 0.17868E-05 c Pressure 0.98792E-04 15 0.99094E-04 0.12568E-02 0.10002E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -18.965 29.936 5.6098 8.0031 v Velocity[Y] -20.967 22.388 -0.14327 -0.00068326 v Velocity[Z] -3.0373 2.9774 2.9543e-06 -5.3866e-08 v ǁVelocityǁ 0.00098408 30.186 7.1158 8.0446 v Pressure -2.485e+05 81717 -77300 -45078 v TurbVisc 2.0402e-21 0.0075718 0.00014459 1.3039e-05 v CourantNb 3.3014e-08 0.011782 0.00016728 4.9103e-06 v FourierNb 1.2425e-07 0.047141 0.00014572 2.2128e-07 v total_pressure -1.4717e+05 1.8304e+05 24025 56247 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0806 0.099364 0.0028587 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2215e-07 0.052412 0.000313 5.1316e-06 INSTANT 0.875456000E-01 TIME STEP NUMBER 55654 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283014556E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.750022492E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.16496E-01 0.21187E+01 Friction velocity uk : 0.16496E-01 0.21187E+01 Dimensionless distance yplus : 0.15882E-01 0.20804E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -2.567075381e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29449E+08 1 0.18225E-09 0.24095E+02 0.19215E+04 c Velocity[X] 0.12250E+02 c Velocity[Y] 0.11845E+02 c Velocity[Z] 0.17650E-05 c Pressure 0.96002E-04 242 0.83192E-04 0.12204E-02 0.55110E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -18.978 29.953 5.6097 8.0029 v Velocity[Y] -20.982 22.401 -0.14328 -0.00068376 v Velocity[Z] -3.0372 2.9774 2.9534e-06 -5.3866e-08 v ǁVelocityǁ 0.001021 30.199 7.1173 8.0445 v Pressure -2.4891e+05 81274 -77758 -45327 v TurbVisc 2.3417e-21 0.0075908 0.00014465 1.306e-05 v CourantNb 3.359e-08 0.011782 0.00016728 4.9103e-06 v FourierNb 1.2425e-07 0.04714 0.00014572 2.2142e-07 v total_pressure -1.4759e+05 1.826e+05 23567 55998 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0804 0.099373 0.0028587 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2214e-07 0.052411 0.000313 5.1318e-06 INSTANT 0.875457000E-01 TIME STEP NUMBER 55655 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283007526E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.749761261E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.14426E-01 0.21185E+01 Friction velocity uk : 0.14426E-01 0.21185E+01 Dimensionless distance yplus : 0.13889E-01 0.20802E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -3.009876684e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29448E+08 1 0.18220E-09 0.24086E+02 0.19211E+04 c Velocity[X] 0.12247E+02 c Velocity[Y] 0.11840E+02 c Velocity[Z] 0.17605E-05 c Pressure 0.93150E-04 15 0.52849E-04 0.11833E-02 0.53732E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -18.992 29.97 5.6097 8.0028 v Velocity[Y] -20.997 22.413 -0.14328 -0.0006849 v Velocity[Z] -3.0371 2.9774 2.9525e-06 -5.3866e-08 v ǁVelocityǁ 0.0010505 30.212 7.1188 8.0445 v Pressure -2.4928e+05 80890 -78211 -45548 v TurbVisc 1.3158e-21 0.0076097 0.00014471 1.3081e-05 v CourantNb 3.3737e-08 0.011782 0.00016728 4.9103e-06 v FourierNb 1.2425e-07 0.04714 0.00014572 2.2156e-07 v total_pressure -1.4796e+05 1.8222e+05 23114 55777 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0802 0.099382 0.0028586 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2213e-07 0.05241 0.000313 5.1319e-06 INSTANT 0.875458000E-01 TIME STEP NUMBER 55656 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283000471E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.749495718E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10743E-01 0.21184E+01 Friction velocity uk : 0.10743E-01 0.21184E+01 Dimensionless distance yplus : 0.10379E-01 0.20800E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -3.386686776e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29448E+08 1 0.18216E-09 0.24074E+02 0.19206E+04 c Velocity[X] 0.12242E+02 c Velocity[Y] 0.11831E+02 c Velocity[Z] 0.17423E-05 c Pressure 0.92044E-04 154 0.75901E-04 0.11684E-02 0.78500E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -19.005 29.986 5.6096 8.0026 v Velocity[Y] -21.012 22.426 -0.14329 -0.00068447 v Velocity[Z] -3.037 2.9774 2.9516e-06 -5.3867e-08 v ǁVelocityǁ 0.0010866 30.225 7.1204 8.0444 v Pressure -2.4961e+05 80579 -78576 -45783 v TurbVisc 3.1631e-23 0.0076287 0.00014476 1.3101e-05 v CourantNb 3.4522e-08 0.011782 0.00016728 4.9103e-06 v FourierNb 1.2425e-07 0.047139 0.00014572 2.217e-07 v total_pressure -1.4829e+05 1.819e+05 22749 55542 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.08 0.099389 0.0028584 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2212e-07 0.052409 0.000313 5.1321e-06 INSTANT 0.875459000E-01 TIME STEP NUMBER 55657 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282993307E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.749227283E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10598E-01 0.21182E+01 Friction velocity uk : 0.10598E-01 0.21182E+01 Dimensionless distance yplus : 0.10239E-01 0.20799E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -3.795254239e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29447E+08 1 0.18211E-09 0.24063E+02 0.19202E+04 c Velocity[X] 0.12238E+02 c Velocity[Y] 0.11824E+02 c Velocity[Z] 0.17231E-05 c Pressure 0.90325E-04 43 0.80411E-04 0.11457E-02 0.77688E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -19.019 30.003 5.6096 8.0025 v Velocity[Y] -21.027 22.438 -0.1433 -0.00068569 v Velocity[Z] -3.0369 2.9773 2.9507e-06 -5.3867e-08 v ǁVelocityǁ 0.0011135 30.238 7.1219 8.0444 v Pressure -2.499e+05 80358 -78922 -45989 v TurbVisc 1.2749e-21 0.0076477 0.00014482 1.3122e-05 v CourantNb 4.1134e-08 0.011782 0.00016729 4.9104e-06 v FourierNb 1.2425e-07 0.047138 0.00014572 2.2185e-07 v total_pressure -1.4857e+05 1.8168e+05 22403 55336 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0799 0.099392 0.0028582 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.221e-07 0.052408 0.00031301 5.1322e-06 INSTANT 0.875460000E-01 TIME STEP NUMBER 55658 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282986237E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.748949334E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11711E-01 0.21181E+01 Friction velocity uk : 0.11711E-01 0.21181E+01 Dimensionless distance yplus : 0.11275E-01 0.20798E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -4.314085781e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29446E+08 1 0.18207E-09 0.24051E+02 0.19197E+04 c Velocity[X] 0.12233E+02 c Velocity[Y] 0.11818E+02 c Velocity[Z] 0.17067E-05 c Pressure 0.89224E-04 458 0.93572E-04 0.11309E-02 0.81125E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -19.032 30.02 5.6095 8.0023 v Velocity[Y] -21.042 22.45 -0.14331 -0.00068504 v Velocity[Z] -3.0367 2.9773 2.9499e-06 -5.3867e-08 v ǁVelocityǁ 0.0011352 30.25 7.1234 8.0444 v Pressure -2.5014e+05 80179 -79216 -46148 v TurbVisc 1.4579e-21 0.0076667 0.00014488 1.3143e-05 v CourantNb 4.1601e-08 0.011782 0.00016729 4.9104e-06 v FourierNb 1.2425e-07 0.047138 0.00014572 2.2199e-07 v total_pressure -1.4882e+05 1.815e+05 22109 55177 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0798 0.099395 0.002858 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2209e-07 0.052408 0.00031301 5.1323e-06 INSTANT 0.875461000E-01 TIME STEP NUMBER 55659 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282978970E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.748668878E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11934E-01 0.21180E+01 Friction velocity uk : 0.11934E-01 0.21180E+01 Dimensionless distance yplus : 0.11553E-01 0.20797E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -4.846671887e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29446E+08 1 0.18202E-09 0.24034E+02 0.19190E+04 c Velocity[X] 0.12228E+02 c Velocity[Y] 0.11806E+02 c Velocity[Z] 0.16941E-05 c Pressure 0.88424E-04 456 0.79294E-04 0.11200E-02 0.52482E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -19.045 30.036 5.6094 8.0022 v Velocity[Y] -21.056 22.462 -0.14332 -0.00068541 v Velocity[Z] -3.0366 2.9773 2.949e-06 -5.3867e-08 v ǁVelocityǁ 0.0011514 30.263 7.1249 8.0443 v Pressure -2.5035e+05 80045 -79457 -46290 v TurbVisc 1.5931e-21 0.0076857 0.00014493 1.3163e-05 v CourantNb 4.2014e-08 0.011782 0.00016729 4.9104e-06 v FourierNb 1.2425e-07 0.047138 0.00014572 2.2213e-07 v total_pressure -1.4903e+05 1.8137e+05 21868 55035 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0797 0.099396 0.0028577 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2208e-07 0.052408 0.00031301 5.1325e-06 INSTANT 0.875462000E-01 TIME STEP NUMBER 55660 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282971802E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.748383756E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12071E-01 0.21179E+01 Friction velocity uk : 0.12071E-01 0.21179E+01 Dimensionless distance yplus : 0.11686E-01 0.20796E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -5.369741399e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29445E+08 1 0.18198E-09 0.24023E+02 0.19186E+04 c Velocity[X] 0.12222E+02 c Velocity[Y] 0.11800E+02 c Velocity[Z] 0.16837E-05 c Pressure 0.85310E-04 7 0.54049E-04 0.10798E-02 0.38011E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -19.058 30.052 5.6094 8.0021 v Velocity[Y] -21.071 22.475 -0.14333 -0.00068683 v Velocity[Z] -3.0365 2.9772 2.9481e-06 -5.3867e-08 v ǁVelocityǁ 0.0011571 30.275 7.1265 8.0443 v Pressure -2.5056e+05 79956 -79649 -46397 v TurbVisc 1.6758e-21 0.0077047 0.00014499 1.3184e-05 v CourantNb 4.7335e-08 0.011782 0.00016729 4.9104e-06 v FourierNb 1.2425e-07 0.047138 0.00014572 2.2228e-07 v total_pressure -1.4924e+05 1.8128e+05 21676 54928 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0796 0.099397 0.0028574 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2207e-07 0.052408 0.00031302 5.1326e-06 INSTANT 0.875463000E-01 TIME STEP NUMBER 55661 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282964630E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.748094190E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15203E-01 0.21178E+01 Friction velocity uk : 0.15203E-01 0.21178E+01 Dimensionless distance yplus : 0.14718E-01 0.20795E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -5.956322226e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29444E+08 1 0.18194E-09 0.24008E+02 0.19180E+04 c Velocity[X] 0.12216E+02 c Velocity[Y] 0.11792E+02 c Velocity[Z] 0.16675E-05 c Pressure 0.85567E-04 48 0.75663E-04 0.10822E-02 0.65907E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -19.071 30.068 5.6093 8.0019 v Velocity[Y] -21.086 22.487 -0.14334 -0.00068641 v Velocity[Z] -3.0364 2.9772 2.9472e-06 -5.3867e-08 v ǁVelocityǁ 0.001167 30.288 7.128 8.0442 v Pressure -2.5074e+05 79899 -79813 -46503 v TurbVisc 2.1835e-21 0.0077237 0.00014504 1.3204e-05 v CourantNb 4.9502e-08 0.011782 0.00016729 4.9104e-06 v FourierNb 1.2425e-07 0.047138 0.00014572 2.2242e-07 v total_pressure -1.4942e+05 1.8122e+05 21512 54822 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0795 0.099398 0.0028571 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2206e-07 0.052408 0.00031302 5.1328e-06 INSTANT 0.875464000E-01 TIME STEP NUMBER 55662 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282957342E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.747802407E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15921E-01 0.21178E+01 Friction velocity uk : 0.15921E-01 0.21178E+01 Dimensionless distance yplus : 0.15341E-01 0.20795E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -6.381392909e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29444E+08 1 0.18189E-09 0.23995E+02 0.19175E+04 c Velocity[X] 0.12211E+02 c Velocity[Y] 0.11785E+02 c Velocity[Z] 0.16506E-05 c Pressure 0.85333E-04 46 0.80751E-04 0.10785E-02 0.68262E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -19.084 30.084 5.6093 8.0018 v Velocity[Y] -21.1 22.499 -0.14335 -0.00068769 v Velocity[Z] -3.0363 2.9772 2.9463e-06 -5.3867e-08 v ǁVelocityǁ 0.0011672 30.301 7.1295 8.0442 v Pressure -2.5088e+05 79886 -79917 -46585 v TurbVisc 2.5905e-21 0.0077427 0.0001451 1.3225e-05 v CourantNb 4.2944e-08 0.011782 0.0001673 4.9104e-06 v FourierNb 1.2425e-07 0.047138 0.00014572 2.2256e-07 v total_pressure -1.4955e+05 1.8121e+05 21408 54740 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0795 0.099395 0.0028567 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2205e-07 0.052408 0.00031302 5.1329e-06 INSTANT 0.875465000E-01 TIME STEP NUMBER 55663 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282950191E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.747506547E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12797E-01 0.21177E+01 Friction velocity uk : 0.12797E-01 0.21177E+01 Dimensionless distance yplus : 0.12331E-01 0.20794E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -6.904191847e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29443E+08 1 0.18185E-09 0.23982E+02 0.19169E+04 c Velocity[X] 0.12203E+02 c Velocity[Y] 0.11778E+02 c Velocity[Z] 0.16367E-05 c Pressure 0.85713E-04 65 0.93745E-04 0.10825E-02 0.76181E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -19.097 30.1 5.6092 8.0016 v Velocity[Y] -21.115 22.511 -0.14335 -0.00068709 v Velocity[Z] -3.0361 2.9772 2.9455e-06 -5.3867e-08 v ǁVelocityǁ 0.001163 30.313 7.131 8.0441 v Pressure -2.5098e+05 79915 -79979 -46604 v TurbVisc 2.7078e-21 0.0077617 0.00014515 1.3246e-05 v CourantNb 3.7486e-08 0.011782 0.0001673 4.9104e-06 v FourierNb 1.2425e-07 0.047138 0.00014573 2.227e-07 v total_pressure -1.4966e+05 1.8124e+05 21346 54721 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0794 0.099394 0.0028563 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2204e-07 0.052408 0.00031302 5.1331e-06 INSTANT 0.875466000E-01 TIME STEP NUMBER 55664 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282942867E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.747210748E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.96468E-02 0.21177E+01 Friction velocity uk : 0.96468E-02 0.21177E+01 Dimensionless distance yplus : 0.92954E-02 0.20794E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -7.381391352e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29442E+08 1 0.18180E-09 0.23962E+02 0.19161E+04 c Velocity[X] 0.12196E+02 c Velocity[Y] 0.11766E+02 c Velocity[Z] 0.16233E-05 c Pressure 0.86437E-04 80 0.79215E-04 0.10909E-02 0.44739E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -19.11 30.116 5.6091 8.0015 v Velocity[Y] -21.129 22.524 -0.14336 -0.00068763 v Velocity[Z] -3.036 2.9771 2.9446e-06 -5.3867e-08 v ǁVelocityǁ 0.001155 30.326 7.1325 8.0441 v Pressure -2.5105e+05 79980 -79992 -46639 v TurbVisc 2.6776e-21 0.0077807 0.00014521 1.3267e-05 v CourantNb 3.0094e-08 0.011782 0.0001673 4.9104e-06 v FourierNb 1.2425e-07 0.047138 0.00014573 2.2285e-07 v total_pressure -1.4972e+05 1.813e+05 21333 54686 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0794 0.099393 0.0028558 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2203e-07 0.052408 0.00031302 5.1332e-06 INSTANT 0.875467000E-01 TIME STEP NUMBER 55665 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282935654E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.746912830E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10087E-01 0.21176E+01 Friction velocity uk : 0.10087E-01 0.21176E+01 Dimensionless distance yplus : 0.97192E-02 0.20793E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -7.807755575e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29442E+08 1 0.18176E-09 0.23949E+02 0.19156E+04 c Velocity[X] 0.12189E+02 c Velocity[Y] 0.11760E+02 c Velocity[Z] 0.16127E-05 c Pressure 0.84813E-04 6 0.53611E-04 0.10697E-02 0.28064E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -19.123 30.132 5.6091 8.0013 v Velocity[Y] -21.143 22.536 -0.14337 -0.00068877 v Velocity[Z] -3.0359 2.9771 2.9437e-06 -5.3867e-08 v ǁVelocityǁ 0.0011439 30.338 7.134 8.044 v Pressure -2.5108e+05 80082 -79974 -46632 v TurbVisc 2.7602e-21 0.0077998 0.00014526 1.3288e-05 v CourantNb 2.2532e-08 0.011782 0.0001673 4.9104e-06 v FourierNb 1.2425e-07 0.047138 0.00014573 2.2299e-07 v total_pressure -1.4975e+05 1.8141e+05 21351 54693 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0793 0.099393 0.0028554 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2201e-07 0.052408 0.00031303 5.1334e-06 INSTANT 0.875468000E-01 TIME STEP NUMBER 55666 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282928475E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.746613095E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10898E-01 0.21176E+01 Friction velocity uk : 0.10898E-01 0.21176E+01 Dimensionless distance yplus : 0.10501E-01 0.20793E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -8.078974125e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29441E+08 1 0.18172E-09 0.23931E+02 0.19149E+04 c Velocity[X] 0.12181E+02 c Velocity[Y] 0.11750E+02 c Velocity[Z] 0.15994E-05 c Pressure 0.86612E-04 87 0.99962E-04 0.10916E-02 0.27510E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -19.136 30.148 5.609 8.0012 v Velocity[Y] -21.158 22.548 -0.14338 -0.00068942 v Velocity[Z] -3.0358 2.9771 2.9428e-06 -5.3867e-08 v ǁVelocityǁ 0.0011306 30.35 7.1355 8.044 v Pressure -2.5107e+05 80264 -79854 -46541 v TurbVisc 3.6386e-21 0.0078188 0.00014532 1.3308e-05 v CourantNb 1.9618e-08 0.011782 0.0001673 4.9104e-06 v FourierNb 1.2425e-07 0.047138 0.00014573 2.2313e-07 v total_pressure -1.4975e+05 1.8159e+05 21471 54784 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0793 0.099392 0.0028549 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.22e-07 0.052408 0.00031303 5.1335e-06 INSTANT 0.875469000E-01 TIME STEP NUMBER 55667 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282921272E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.746314107E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.73508E-02 0.21175E+01 Friction velocity uk : 0.73508E-02 0.21175E+01 Dimensionless distance yplus : 0.70830E-02 0.20792E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -8.678053280e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29440E+08 1 0.18168E-09 0.23915E+02 0.19142E+04 c Velocity[X] 0.12173E+02 c Velocity[Y] 0.11742E+02 c Velocity[Z] 0.15888E-05 c Pressure 0.87414E-04 121 0.83870E-04 0.11009E-02 0.20616E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -19.148 30.164 5.6089 8.001 v Velocity[Y] -21.172 22.56 -0.14339 -0.00068972 v Velocity[Z] -3.0357 2.9771 2.9419e-06 -5.3867e-08 v ǁVelocityǁ 0.0011173 30.363 7.137 8.0439 v Pressure -2.5104e+05 80511 -79744 -46484 v TurbVisc 2.1491e-22 0.0078378 0.00014537 1.3329e-05 v CourantNb 2.1395e-08 0.011782 0.0001673 4.9104e-06 v FourierNb 1.2425e-07 0.047138 0.00014573 2.2328e-07 v total_pressure -1.4971e+05 1.8184e+05 21581 54841 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0792 0.099395 0.0028545 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2199e-07 0.052408 0.00031303 5.1337e-06 INSTANT 0.875470000E-01 TIME STEP NUMBER 55668 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282914054E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.746010123E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11955E-01 0.21174E+01 Friction velocity uk : 0.11955E-01 0.21174E+01 Dimensionless distance yplus : 0.11520E-01 0.20791E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -8.811129359e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29440E+08 1 0.18163E-09 0.23901E+02 0.19136E+04 c Velocity[X] 0.12165E+02 c Velocity[Y] 0.11736E+02 c Velocity[Z] 0.15812E-05 c Pressure 0.88198E-04 7 0.52665E-04 0.11100E-02 0.33426E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -19.161 30.179 5.6088 8.0009 v Velocity[Y] -21.186 22.572 -0.1434 -0.00068935 v Velocity[Z] -3.0355 2.977 2.9411e-06 -5.3867e-08 v ǁVelocityǁ 0.0011058 30.375 7.1385 8.0439 v Pressure -2.5096e+05 80808 -79591 -46399 v TurbVisc 3.9698e-21 0.0078569 0.00014542 1.335e-05 v CourantNb 3.4269e-08 0.011782 0.0001673 4.9104e-06 v FourierNb 1.2425e-07 0.047138 0.00014573 2.2342e-07 v total_pressure -1.4964e+05 1.8213e+05 21734 54926 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0791 0.099397 0.002854 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2198e-07 0.052408 0.00031303 5.1338e-06 INSTANT 0.875471000E-01 TIME STEP NUMBER 55669 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282906828E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.745708739E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.86057E-02 0.21173E+01 Friction velocity uk : 0.86057E-02 0.21173E+01 Dimensionless distance yplus : 0.82922E-02 0.20790E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -9.122445965e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29439E+08 1 0.18159E-09 0.23884E+02 0.19129E+04 c Velocity[X] 0.12156E+02 c Velocity[Y] 0.11727E+02 c Velocity[Z] 0.15683E-05 c Pressure 0.90841E-04 50 0.76533E-04 0.11425E-02 0.67008E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -19.173 30.195 5.6088 8.0007 v Velocity[Y] -21.201 22.584 -0.1434 -0.00069059 v Velocity[Z] -3.0354 2.977 2.9402e-06 -5.3867e-08 v ǁVelocityǁ 0.0010871 30.387 7.14 8.0438 v Pressure -2.5085e+05 81162 -79343 -46269 v TurbVisc 1.5623e-21 0.0078759 0.00014547 1.3371e-05 v CourantNb 3.8444e-08 0.011782 0.00016731 4.9104e-06 v FourierNb 1.2425e-07 0.047138 0.00014573 2.2356e-07 v total_pressure -1.4952e+05 1.8249e+05 21982 55056 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.079 0.0994 0.0028535 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2197e-07 0.052408 0.00031304 5.134e-06 INSTANT 0.875472000E-01 TIME STEP NUMBER 55670 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282899725E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.745409023E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.76927E-02 0.21171E+01 Friction velocity uk : 0.76927E-02 0.21171E+01 Dimensionless distance yplus : 0.74124E-02 0.20788E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -9.220402148e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29439E+08 1 0.18155E-09 0.23868E+02 0.19123E+04 c Velocity[X] 0.12147E+02 c Velocity[Y] 0.11721E+02 c Velocity[Z] 0.15600E-05 c Pressure 0.92885E-04 42 0.80971E-04 0.11674E-02 0.76162E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -19.186 30.21 5.6087 8.0006 v Velocity[Y] -21.215 22.596 -0.14341 -0.00069016 v Velocity[Z] -3.0353 2.977 2.9393e-06 -5.3867e-08 v ǁVelocityǁ 0.0010735 30.4 7.1415 8.0438 v Pressure -2.507e+05 81555 -79084 -46096 v TurbVisc 3.3239e-21 0.007895 0.00014553 1.3391e-05 v CourantNb 2.9643e-08 0.011782 0.00016731 4.9104e-06 v FourierNb 1.2425e-07 0.047137 0.00014573 2.2371e-07 v total_pressure -1.4938e+05 1.8288e+05 22241 55229 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0788 0.099408 0.0028531 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2196e-07 0.052407 0.00031304 5.1341e-06 INSTANT 0.875473000E-01 TIME STEP NUMBER 55671 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282892513E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.745108405E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11006E-01 0.21170E+01 Friction velocity uk : 0.11006E-01 0.21170E+01 Dimensionless distance yplus : 0.10606E-01 0.20787E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -9.407741145e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29438E+08 1 0.18151E-09 0.23851E+02 0.19116E+04 c Velocity[X] 0.12139E+02 c Velocity[Y] 0.11712E+02 c Velocity[Z] 0.15520E-05 c Pressure 0.95446E-04 540 0.94357E-04 0.11987E-02 0.83040E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -19.198 30.226 5.6086 8.0005 v Velocity[Y] -21.229 22.608 -0.14342 -0.00069176 v Velocity[Z] -3.0352 2.9769 2.9384e-06 -5.3867e-08 v ǁVelocityǁ 0.0010613 30.412 7.143 8.0437 v Pressure -2.5051e+05 82003 -78773 -45946 v TurbVisc 3.4936e-21 0.007914 0.00014558 1.3412e-05 v CourantNb 3.074e-08 0.011782 0.00016731 4.9104e-06 v FourierNb 1.2425e-07 0.047137 0.00014573 2.2385e-07 v total_pressure -1.4919e+05 1.8333e+05 22552 55379 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0787 0.099416 0.0028527 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2195e-07 0.052406 0.00031304 5.1343e-06 INSTANT 0.875474000E-01 TIME STEP NUMBER 55672 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282885492E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.744809384E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10993E-01 0.21168E+01 Friction velocity uk : 0.10993E-01 0.21168E+01 Dimensionless distance yplus : 0.10621E-01 0.20785E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -9.507822972e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29437E+08 1 0.18146E-09 0.23829E+02 0.19107E+04 c Velocity[X] 0.12128E+02 c Velocity[Y] 0.11701E+02 c Velocity[Z] 0.15441E-05 c Pressure 0.98214E-04 77 0.79968E-04 0.12327E-02 0.68084E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -19.211 30.241 5.6085 8.0003 v Velocity[Y] -21.243 22.62 -0.14342 -0.00069193 v Velocity[Z] -3.035 2.9769 2.9376e-06 -5.3867e-08 v ǁVelocityǁ 0.0010513 30.424 7.1445 8.0437 v Pressure -2.5028e+05 82491 -78413 -45708 v TurbVisc 2.2437e-21 0.0079331 0.00014563 1.3433e-05 v CourantNb 4.0589e-08 0.011782 0.00016731 4.9104e-06 v FourierNb 1.2425e-07 0.047136 0.00014573 2.24e-07 v total_pressure -1.4896e+05 1.8382e+05 22912 55617 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0785 0.099427 0.0028524 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2194e-07 0.052405 0.00031304 5.1344e-06 INSTANT 0.875475000E-01 TIME STEP NUMBER 55673 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282878415E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.744511925E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.16424E-01 0.21165E+01 Friction velocity uk : 0.16424E-01 0.21165E+01 Dimensionless distance yplus : 0.15868E-01 0.20782E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -9.557623424e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29437E+08 1 0.18142E-09 0.23814E+02 0.19101E+04 c Velocity[X] 0.12119E+02 c Velocity[Y] 0.11695E+02 c Velocity[Z] 0.15465E-05 c Pressure 0.98795E-04 12 0.54929E-04 0.12391E-02 0.47482E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -19.223 30.257 5.6084 8.0002 v Velocity[Y] -21.258 22.632 -0.14343 -0.00069153 v Velocity[Z] -3.0349 2.9769 2.9367e-06 -5.3867e-08 v ǁVelocityǁ 0.0010494 30.436 7.146 8.0436 v Pressure -2.5002e+05 83023 -78018 -45530 v TurbVisc 3.5972e-21 0.0079522 0.00014568 1.3454e-05 v CourantNb 3.8509e-08 0.011782 0.00016731 4.9104e-06 v FourierNb 1.2425e-07 0.047134 0.00014574 2.2414e-07 v total_pressure -1.4869e+05 1.8435e+05 23307 55795 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0782 0.099441 0.002852 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2193e-07 0.052403 0.00031305 5.1345e-06 INSTANT 0.875476000E-01 TIME STEP NUMBER 55674 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282871356E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.744217011E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.14484E-01 0.21163E+01 Friction velocity uk : 0.14484E-01 0.21163E+01 Dimensionless distance yplus : 0.14061E-01 0.20780E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -9.617018846e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29436E+08 1 0.18138E-09 0.23795E+02 0.19093E+04 c Velocity[X] 0.12109E+02 c Velocity[Y] 0.11686E+02 c Velocity[Z] 0.15346E-05 c Pressure 0.10234E-03 255 0.76048E-04 0.12827E-02 0.88603E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -19.235 30.272 5.6083 8 v Velocity[Y] -21.272 22.644 -0.14343 -0.00069279 v Velocity[Z] -3.0348 2.9769 2.9358e-06 -5.3867e-08 v ǁVelocityǁ 0.0010394 30.448 7.1475 8.0436 v Pressure -2.4969e+05 83611 -77567 -45236 v TurbVisc 4.5325e-21 0.0079712 0.00014573 1.3475e-05 v CourantNb 3.5569e-08 0.011782 0.00016731 4.9104e-06 v FourierNb 1.2425e-07 0.047133 0.00014574 2.2429e-07 v total_pressure -1.4837e+05 1.8494e+05 23758 56089 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.078 0.099455 0.0028517 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2192e-07 0.052401 0.00031305 5.1347e-06 INSTANT 0.875477000E-01 TIME STEP NUMBER 55675 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282864421E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.743923586E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11193E-01 0.21160E+01 Friction velocity uk : 0.11193E-01 0.21160E+01 Dimensionless distance yplus : 0.10866E-01 0.20777E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -9.529788291e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29435E+08 1 0.18134E-09 0.23778E+02 0.19086E+04 c Velocity[X] 0.12098E+02 c Velocity[Y] 0.11679E+02 c Velocity[Z] 0.15271E-05 c Pressure 0.10524E-03 71 0.81536E-04 0.13182E-02 0.90391E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -19.247 30.288 5.6082 7.9999 v Velocity[Y] -21.286 22.656 -0.14343 -0.00069233 v Velocity[Z] -3.0347 2.9768 2.9349e-06 -5.3867e-08 v ǁVelocityǁ 0.0010374 30.46 7.149 8.0436 v Pressure -2.4934e+05 84233 -77074 -44961 v TurbVisc 4.3822e-21 0.0079903 0.00014578 1.3496e-05 v CourantNb 2.9907e-08 0.011782 0.00016731 4.9104e-06 v FourierNb 1.2425e-07 0.047131 0.00014574 2.2443e-07 v total_pressure -1.4801e+05 1.8556e+05 24251 56364 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0777 0.099473 0.0028514 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.219e-07 0.052399 0.00031305 5.1348e-06 INSTANT 0.875478000E-01 TIME STEP NUMBER 55676 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282857400E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.743634994E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12193E-01 0.21156E+01 Friction velocity uk : 0.12193E-01 0.21156E+01 Dimensionless distance yplus : 0.11836E-01 0.20773E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -9.540278647e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29435E+08 1 0.18130E-09 0.23760E+02 0.19079E+04 c Velocity[X] 0.12088E+02 c Velocity[Y] 0.11672E+02 c Velocity[Z] 0.15216E-05 c Pressure 0.10855E-03 227 0.94823E-04 0.13587E-02 0.10228E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -19.259 30.303 5.6081 7.9997 v Velocity[Y] -21.3 22.667 -0.14344 -0.00069382 v Velocity[Z] -3.0345 2.9768 2.9341e-06 -5.3867e-08 v ǁVelocityǁ 0.0010385 30.472 7.1504 8.0435 v Pressure -2.4892e+05 84914 -76525 -44647 v TurbVisc 4.3352e-21 0.0080094 0.00014583 1.3517e-05 v CourantNb 2.4295e-08 0.011782 0.00016731 4.9104e-06 v FourierNb 1.2425e-07 0.047129 0.00014574 2.2458e-07 v total_pressure -1.476e+05 1.8624e+05 24800 56678 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0773 0.099493 0.0028512 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2189e-07 0.052396 0.00031305 5.135e-06 INSTANT 0.875479000E-01 TIME STEP NUMBER 55677 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282850614E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.743347682E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15344E-01 0.21152E+01 Friction velocity uk : 0.15344E-01 0.21152E+01 Dimensionless distance yplus : 0.14896E-01 0.20770E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -9.495380626e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29434E+08 1 0.18126E-09 0.23737E+02 0.19070E+04 c Velocity[X] 0.12077E+02 c Velocity[Y] 0.11660E+02 c Velocity[Z] 0.15184E-05 c Pressure 0.11200E-03 78 0.80458E-04 0.14009E-02 0.88781E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -19.272 30.318 5.608 7.9996 v Velocity[Y] -21.314 22.679 -0.14344 -0.0006941 v Velocity[Z] -3.0344 2.9768 2.9332e-06 -5.3867e-08 v ǁVelocityǁ 0.00098956 30.484 7.1519 8.0435 v Pressure -2.4847e+05 85630 -75942 -44295 v TurbVisc 4.6265e-21 0.0080285 0.00014588 1.3538e-05 v CourantNb 3.6865e-08 0.011782 0.00016731 4.9104e-06 v FourierNb 1.2425e-07 0.047126 0.00014574 2.2472e-07 v total_pressure -1.4714e+05 1.8695e+05 25383 57030 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.077 0.099514 0.0028509 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2188e-07 0.052393 0.00031306 5.1351e-06 INSTANT 0.875480000E-01 TIME STEP NUMBER 55678 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282843764E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.743063668E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.14329E-01 0.21148E+01 Friction velocity uk : 0.14329E-01 0.21148E+01 Dimensionless distance yplus : 0.13791E-01 0.20766E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -9.445401229e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29434E+08 1 0.18122E-09 0.23720E+02 0.19063E+04 c Velocity[X] 0.12067E+02 c Velocity[Y] 0.11654E+02 c Velocity[Z] 0.15180E-05 c Pressure 0.11343E-03 9 0.54930E-04 0.14178E-02 0.71520E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -19.284 30.334 5.6079 7.9995 v Velocity[Y] -21.328 22.69 -0.14344 -0.0006937 v Velocity[Z] -3.0343 2.9768 2.9323e-06 -5.3867e-08 v ǁVelocityǁ 0.00084032 30.496 7.1534 8.0434 v Pressure -2.4796e+05 86388 -75314 -43992 v TurbVisc 4.9184e-21 0.0080476 0.00014593 1.3559e-05 v CourantNb 3.2081e-08 0.011782 0.00016732 4.9104e-06 v FourierNb 1.2425e-07 0.047124 0.00014574 2.2486e-07 v total_pressure -1.4664e+05 1.8771e+05 26011 57333 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0766 0.099537 0.0028507 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2187e-07 0.05239 0.00031306 5.1353e-06 INSTANT 0.875481000E-01 TIME STEP NUMBER 55679 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282836973E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.742783740E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13752E-01 0.21144E+01 Friction velocity uk : 0.13752E-01 0.21144E+01 Dimensionless distance yplus : 0.13236E-01 0.20761E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -9.411646231e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29433E+08 1 0.18118E-09 0.23701E+02 0.19055E+04 c Velocity[X] 0.12056E+02 c Velocity[Y] 0.11645E+02 c Velocity[Z] 0.15142E-05 c Pressure 0.11745E-03 155 0.76447E-04 0.14671E-02 0.11312E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -19.296 30.349 5.6078 7.9993 v Velocity[Y] -21.342 22.702 -0.14344 -0.00069493 v Velocity[Z] -3.0342 2.9767 2.9315e-06 -5.3867e-08 v ǁVelocityǁ 0.00071407 30.508 7.1549 8.0434 v Pressure -2.4739e+05 87204 -74655 -43572 v TurbVisc 5.6981e-21 0.0080667 0.00014598 1.358e-05 v CourantNb 3.6153e-08 0.011782 0.00016732 4.9104e-06 v FourierNb 1.2425e-07 0.047121 0.00014575 2.2501e-07 v total_pressure -1.4607e+05 1.8853e+05 26670 57753 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0761 0.099561 0.0028506 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2186e-07 0.052386 0.00031306 5.1354e-06 INSTANT 0.875482000E-01 TIME STEP NUMBER 55680 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282830310E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.742506177E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11347E-01 0.21139E+01 Friction velocity uk : 0.11347E-01 0.21139E+01 Dimensionless distance yplus : 0.10921E-01 0.20756E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -9.303771713e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29432E+08 1 0.18114E-09 0.23683E+02 0.19048E+04 c Velocity[X] 0.12044E+02 c Velocity[Y] 0.11639E+02 c Velocity[Z] 0.15095E-05 c Pressure 0.12080E-03 256 0.81752E-04 0.15079E-02 0.12616E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -19.307 30.365 5.6077 7.9992 v Velocity[Y] -21.356 22.713 -0.14344 -0.00069427 v Velocity[Z] -3.0341 2.9767 2.9306e-06 -5.3867e-08 v ǁVelocityǁ 0.00060883 30.52 7.1563 8.0434 v Pressure -2.4678e+05 88057 -73910 -43103 v TurbVisc 5.6869e-21 0.0080858 0.00014603 1.3601e-05 v CourantNb 4.2132e-08 0.011782 0.00016732 4.9104e-06 v FourierNb 1.2425e-07 0.047117 0.00014575 2.2515e-07 v total_pressure -1.4545e+05 1.8938e+05 27415 58222 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0756 0.099587 0.0028504 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2185e-07 0.052382 0.00031306 5.1356e-06 INSTANT 0.875483000E-01 TIME STEP NUMBER 55681 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282823601E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.742235845E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12305E-01 0.21133E+01 Friction velocity uk : 0.12305E-01 0.21133E+01 Dimensionless distance yplus : 0.11843E-01 0.20751E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -9.319030413e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29432E+08 1 0.18110E-09 0.23664E+02 0.19040E+04 c Velocity[X] 0.12034E+02 c Velocity[Y] 0.11631E+02 c Velocity[Z] 0.15070E-05 c Pressure 0.12455E-03 294 0.95193E-04 0.15536E-02 0.11330E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -19.319 30.38 5.6075 7.9991 v Velocity[Y] -21.369 22.724 -0.14344 -0.00069606 v Velocity[Z] -3.0339 2.9767 2.9297e-06 -5.3867e-08 v ǁVelocityǁ 0.00055473 30.532 7.1578 8.0433 v Pressure -2.4611e+05 88951 -73167 -42764 v TurbVisc 6.2917e-21 0.0081049 0.00014608 1.3622e-05 v CourantNb 4.7731e-08 0.011782 0.00016732 4.9104e-06 v FourierNb 1.2425e-07 0.047114 0.00014575 2.253e-07 v total_pressure -1.4478e+05 1.9028e+05 28158 58561 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0751 0.099614 0.0028503 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2184e-07 0.052378 0.00031307 5.1357e-06 INSTANT 0.875484000E-01 TIME STEP NUMBER 55682 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282817111E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.741965549E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12097E-01 0.21128E+01 Friction velocity uk : 0.12097E-01 0.21128E+01 Dimensionless distance yplus : 0.11643E-01 0.20746E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -9.288354221e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29431E+08 1 0.18106E-09 0.23640E+02 0.19030E+04 c Velocity[X] 0.12021E+02 c Velocity[Y] 0.11619E+02 c Velocity[Z] 0.15039E-05 c Pressure 0.12831E-03 90 0.80735E-04 0.15995E-02 0.12897E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -19.331 30.396 5.6074 7.9989 v Velocity[Y] -21.383 22.735 -0.14344 -0.00069621 v Velocity[Z] -3.0338 2.9766 2.9288e-06 -5.3867e-08 v ǁVelocityǁ 0.00056736 30.543 7.1592 8.0433 v Pressure -2.4537e+05 89894 -72349 -42231 v TurbVisc 6.8936e-21 0.008124 0.00014613 1.3643e-05 v CourantNb 4.6183e-08 0.011782 0.00016732 4.9104e-06 v FourierNb 1.2425e-07 0.04711 0.00014575 2.2545e-07 v total_pressure -1.4405e+05 1.9122e+05 28976 59094 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0746 0.099642 0.0028502 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2183e-07 0.052373 0.00031307 5.1359e-06 INSTANT 0.875485000E-01 TIME STEP NUMBER 55683 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282810612E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.741701328E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.14661E-01 0.21122E+01 Friction velocity uk : 0.14661E-01 0.21122E+01 Dimensionless distance yplus : 0.14221E-01 0.20740E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -9.316348489e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29431E+08 1 0.18103E-09 0.23623E+02 0.19024E+04 c Velocity[X] 0.12010E+02 c Velocity[Y] 0.11613E+02 c Velocity[Z] 0.15041E-05 c Pressure 0.13027E-03 9 0.55936E-04 0.16228E-02 0.96842E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -19.343 30.412 5.6073 7.9988 v Velocity[Y] -21.397 22.746 -0.14343 -0.00069583 v Velocity[Z] -3.0337 2.9766 2.928e-06 -5.3867e-08 v ǁVelocityǁ 0.00057906 30.555 7.1607 8.0432 v Pressure -2.4459e+05 90870 -71507 -41822 v TurbVisc 7.554e-21 0.0081431 0.00014618 1.3665e-05 v CourantNb 5.7499e-08 0.011782 0.00016732 4.9104e-06 v FourierNb 1.2425e-07 0.047106 0.00014575 2.2559e-07 v total_pressure -1.4326e+05 1.922e+05 29818 59503 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.074 0.099669 0.0028501 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2182e-07 0.052368 0.00031307 5.136e-06 INSTANT 0.875486000E-01 TIME STEP NUMBER 55684 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282804185E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.741441693E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10941E-01 0.21116E+01 Friction velocity uk : 0.10941E-01 0.21116E+01 Dimensionless distance yplus : 0.10530E-01 0.20734E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -9.373355765e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29430E+08 1 0.18099E-09 0.23603E+02 0.19015E+04 c Velocity[X] 0.11998E+02 c Velocity[Y] 0.11605E+02 c Velocity[Z] 0.15012E-05 c Pressure 0.13447E-03 254 0.76739E-04 0.16740E-02 0.14450E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -19.355 30.427 5.6072 7.9987 v Velocity[Y] -21.411 22.757 -0.14343 -0.00069703 v Velocity[Z] -3.0336 2.9766 2.9271e-06 -5.3867e-08 v ǁVelocityǁ 0.00055063 30.567 7.1622 8.0432 v Pressure -2.4373e+05 91903 -70627 -41272 v TurbVisc 2.6942e-21 0.0081622 0.00014623 1.3686e-05 v CourantNb 5.8022e-08 0.011782 0.00016732 4.9104e-06 v FourierNb 1.2425e-07 0.047102 0.00014576 2.2574e-07 v total_pressure -1.4241e+05 1.9323e+05 30698 60053 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0734 0.099697 0.00285 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2181e-07 0.052363 0.00031308 5.1362e-06 INSTANT 0.875487000E-01 TIME STEP NUMBER 55685 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282797888E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.741186062E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.95904E-02 0.21110E+01 Friction velocity uk : 0.95904E-02 0.21110E+01 Dimensionless distance yplus : 0.92304E-02 0.20728E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -9.374366717e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29430E+08 1 0.18095E-09 0.23585E+02 0.19008E+04 c Velocity[X] 0.11986E+02 c Velocity[Y] 0.11599E+02 c Velocity[Z] 0.14953E-05 c Pressure 0.13808E-03 653 0.82221E-04 0.17178E-02 0.16023E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -19.367 30.443 5.607 7.9985 v Velocity[Y] -21.424 22.768 -0.14343 -0.0006963 v Velocity[Z] -3.0334 2.9765 2.9262e-06 -5.3867e-08 v ǁVelocityǁ 0.00054339 30.579 7.1636 8.0432 v Pressure -2.4282e+05 92968 -69661 -40662 v TurbVisc 6.3446e-21 0.0081813 0.00014628 1.3707e-05 v CourantNb 6.1365e-08 0.011782 0.00016732 4.9104e-06 v FourierNb 1.2425e-07 0.047097 0.00014576 2.2588e-07 v total_pressure -1.415e+05 1.9429e+05 31664 60663 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0728 0.099723 0.0028499 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.218e-07 0.052358 0.00031308 5.1363e-06 INSTANT 0.875488000E-01 TIME STEP NUMBER 55686 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282791580E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.740935646E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.68827E-02 0.21103E+01 Friction velocity uk : 0.68827E-02 0.21103E+01 Dimensionless distance yplus : 0.66243E-02 0.20722E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -9.537269405e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29429E+08 1 0.18092E-09 0.23566E+02 0.19000E+04 c Velocity[X] 0.11975E+02 c Velocity[Y] 0.11591E+02 c Velocity[Z] 0.14929E-05 c Pressure 0.14197E-03 246 0.95572E-04 0.17651E-02 0.13232E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -19.378 30.458 5.6069 7.9984 v Velocity[Y] -21.438 22.779 -0.14342 -0.00069805 v Velocity[Z] -3.0333 2.9765 2.9254e-06 -5.3867e-08 v ǁVelocityǁ 0.00054055 30.59 7.1651 8.0432 v Pressure -2.4186e+05 94069 -68717 -40247 v TurbVisc 4.3107e-21 0.0082005 0.00014632 1.3728e-05 v CourantNb 5.5255e-08 0.011782 0.00016732 4.9104e-06 v FourierNb 1.2425e-07 0.047093 0.00014576 2.2603e-07 v total_pressure -1.4054e+05 1.9539e+05 32608 61078 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0722 0.09975 0.0028497 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2179e-07 0.052352 0.00031308 5.1365e-06 INSTANT 0.875489000E-01 TIME STEP NUMBER 55687 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282785500E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.740686696E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.89189E-02 0.21097E+01 Friction velocity uk : 0.89189E-02 0.21097E+01 Dimensionless distance yplus : 0.85840E-02 0.20715E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -9.665680581e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29428E+08 1 0.18088E-09 0.23542E+02 0.18990E+04 c Velocity[X] 0.11962E+02 c Velocity[Y] 0.11580E+02 c Velocity[Z] 0.14883E-05 c Pressure 0.14581E-03 96 0.81155E-04 0.18117E-02 0.16659E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -19.39 30.474 5.6068 7.9983 v Velocity[Y] -21.451 22.79 -0.14342 -0.00069829 v Velocity[Z] -3.0332 2.9765 2.9245e-06 -5.3867e-08 v ǁVelocityǁ 0.00055185 30.602 7.1665 8.0431 v Pressure -2.4083e+05 95218 -67683 -39575 v TurbVisc 3.756e-21 0.0082196 0.00014637 1.375e-05 v CourantNb 3.7498e-08 0.011782 0.00016732 4.9104e-06 v FourierNb 1.2425e-07 0.047088 0.00014576 2.2618e-07 v total_pressure -1.395e+05 1.9654e+05 33642 61750 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0715 0.099777 0.0028497 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2179e-07 0.052347 0.00031309 5.1366e-06 INSTANT 0.875490000E-01 TIME STEP NUMBER 55688 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282779423E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.740444855E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.26532E-02 0.21090E+01 Friction velocity uk : 0.26532E-02 0.21090E+01 Dimensionless distance yplus : 0.26284E-02 0.20709E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -9.845686374e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29428E+08 1 0.18084E-09 0.23525E+02 0.18983E+04 c Velocity[X] 0.11951E+02 c Velocity[Y] 0.11574E+02 c Velocity[Z] 0.14906E-05 c Pressure 0.14802E-03 9 0.57158E-04 0.18379E-02 0.12636E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -19.401 30.49 5.6066 7.9982 v Velocity[Y] -21.464 22.801 -0.14341 -0.0006979 v Velocity[Z] -3.033 2.9765 2.9236e-06 -5.3867e-08 v ǁVelocityǁ 0.00057162 30.614 7.168 8.0431 v Pressure -2.3974e+05 96393 -66640 -39058 v TurbVisc 4.7034e-21 0.0082387 0.00014642 1.3771e-05 v CourantNb 1.9305e-08 0.011782 0.00016732 4.9104e-06 v FourierNb 1.2425e-07 0.047084 0.00014577 2.2632e-07 v total_pressure -1.3842e+05 1.9772e+05 34685 62267 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0709 0.099804 0.0028496 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2178e-07 0.052341 0.00031309 5.1368e-06 INSTANT 0.875491000E-01 TIME STEP NUMBER 55689 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282773454E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.740207769E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.52530E-02 0.21084E+01 Friction velocity uk : 0.52530E-02 0.21084E+01 Dimensionless distance yplus : 0.50559E-02 0.20702E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.005218295e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29427E+08 1 0.18081E-09 0.23505E+02 0.18975E+04 c Velocity[X] 0.11938E+02 c Velocity[Y] 0.11567E+02 c Velocity[Z] 0.14849E-05 c Pressure 0.15214E-03 174 0.76752E-04 0.18878E-02 0.18017E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -19.413 30.506 5.6065 7.998 v Velocity[Y] -21.478 22.811 -0.1434 -0.00069911 v Velocity[Z] -3.0329 2.9764 2.9228e-06 -5.3868e-08 v ǁVelocityǁ 0.00069332 30.625 7.1695 8.0431 v Pressure -2.3859e+05 97619 -65546 -38392 v TurbVisc 6.859e-22 0.0082579 0.00014647 1.3792e-05 v CourantNb 2.7165e-08 0.011782 0.00016732 4.9104e-06 v FourierNb 1.2425e-07 0.047079 0.00014577 2.2647e-07 v total_pressure -1.3726e+05 1.9894e+05 35779 62933 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0702 0.099843 0.0028496 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2177e-07 0.052336 0.00031309 5.1369e-06 INSTANT 0.875492000E-01 TIME STEP NUMBER 55690 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282767608E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.739976382E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.70070E-02 0.21077E+01 Friction velocity uk : 0.70070E-02 0.21077E+01 Dimensionless distance yplus : 0.67541E-02 0.20696E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.020886866e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29427E+08 1 0.18077E-09 0.23487E+02 0.18967E+04 c Velocity[X] 0.11926E+02 c Velocity[Y] 0.11561E+02 c Velocity[Z] 0.14749E-05 c Pressure 0.15576E-03 410 0.82543E-04 0.19315E-02 0.19585E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -19.425 30.521 5.6064 7.9979 v Velocity[Y] -21.491 22.822 -0.1434 -0.00069839 v Velocity[Z] -3.0328 2.9764 2.9219e-06 -5.3868e-08 v ǁVelocityǁ 0.00086307 30.637 7.1709 8.0431 v Pressure -2.3738e+05 98873 -64379 -37667 v TurbVisc 2.3464e-21 0.008277 0.00014652 1.3813e-05 v CourantNb 4.6961e-08 0.011782 0.00016732 4.9104e-06 v FourierNb 1.2425e-07 0.047075 0.00014577 2.2662e-07 v total_pressure -1.3606e+05 2.002e+05 36946 63658 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0696 0.099877 0.0028496 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2176e-07 0.05233 0.00031309 5.1371e-06 INSTANT 0.875493000E-01 TIME STEP NUMBER 55691 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282761777E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.739747281E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.62214E-02 0.21071E+01 Friction velocity uk : 0.62214E-02 0.21071E+01 Dimensionless distance yplus : 0.59840E-02 0.20690E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.050278909e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29426E+08 1 0.18074E-09 0.23468E+02 0.18960E+04 c Velocity[X] 0.11915E+02 c Velocity[Y] 0.11553E+02 c Velocity[Z] 0.14700E-05 c Pressure 0.15956E-03 229 0.95727E-04 0.19772E-02 0.16464E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -19.436 30.537 5.6062 7.9978 v Velocity[Y] -21.504 22.833 -0.14339 -0.00070012 v Velocity[Z] -3.0327 2.9764 2.921e-06 -5.3868e-08 v ǁVelocityǁ 0.0010676 30.648 7.1724 8.0431 v Pressure -2.3613e+05 1.0016e+05 -63236 -37127 v TurbVisc 3.4722e-21 0.0082962 0.00014656 1.3835e-05 v CourantNb 6.7459e-08 0.011782 0.00016732 4.9105e-06 v FourierNb 1.2425e-07 0.04707 0.00014577 2.2677e-07 v total_pressure -1.348e+05 2.0148e+05 38089 64198 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.069 0.09991 0.0028496 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2175e-07 0.052325 0.0003131 5.1372e-06 INSTANT 0.875494000E-01 TIME STEP NUMBER 55692 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282756201E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.739521334E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.46454E-02 0.21065E+01 Friction velocity uk : 0.46454E-02 0.21065E+01 Dimensionless distance yplus : 0.44681E-02 0.20684E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.075134434e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29426E+08 1 0.18071E-09 0.23444E+02 0.18950E+04 c Velocity[X] 0.11902E+02 c Velocity[Y] 0.11542E+02 c Velocity[Z] 0.14631E-05 c Pressure 0.16324E-03 416 0.81272E-04 0.20215E-02 0.20227E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -19.448 30.553 5.6061 7.9977 v Velocity[Y] -21.517 22.843 -0.14338 -0.0007004 v Velocity[Z] -3.0325 2.9763 2.9201e-06 -5.3868e-08 v ǁVelocityǁ 0.0012199 30.66 7.1738 8.043 v Pressure -2.3481e+05 1.0148e+05 -62005 -36357 v TurbVisc 2.0403e-21 0.0083153 0.00014661 1.3856e-05 v CourantNb 8.7811e-08 0.011782 0.00016733 4.9105e-06 v FourierNb 1.2425e-07 0.047066 0.00014577 2.2691e-07 v total_pressure -1.3348e+05 2.028e+05 39320 64968 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0684 0.099941 0.0028495 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2174e-07 0.052319 0.0003131 5.1374e-06 INSTANT 0.875495000E-01 TIME STEP NUMBER 55693 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282750635E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.739302834E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.71818E-02 0.21059E+01 Friction velocity uk : 0.71818E-02 0.21059E+01 Dimensionless distance yplus : 0.69078E-02 0.20678E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.101814024e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29425E+08 1 0.18067E-09 0.23428E+02 0.18943E+04 c Velocity[X] 0.11890E+02 c Velocity[Y] 0.11537E+02 c Velocity[Z] 0.14667E-05 c Pressure 0.16541E-03 9 0.58134E-04 0.20470E-02 0.15360E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -19.459 30.569 5.606 7.9976 v Velocity[Y] -21.53 22.854 -0.14338 -0.00070002 v Velocity[Z] -3.0324 2.9763 2.9193e-06 -5.3868e-08 v ǁVelocityǁ 0.001214 30.672 7.1753 8.043 v Pressure -2.3345e+05 1.0282e+05 -60786 -35766 v TurbVisc 2.8944e-21 0.0083345 0.00014666 1.3878e-05 v CourantNb 7.421e-08 0.011782 0.00016733 4.9105e-06 v FourierNb 1.2425e-07 0.047062 0.00014578 2.2706e-07 v total_pressure -1.3212e+05 2.0414e+05 40539 65559 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0678 0.099971 0.0028495 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2173e-07 0.052314 0.0003131 5.1375e-06 INSTANT 0.875496000E-01 TIME STEP NUMBER 55694 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282745198E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.739088826E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.39710E-02 0.21053E+01 Friction velocity uk : 0.39710E-02 0.21053E+01 Dimensionless distance yplus : 0.38195E-02 0.20672E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.125844047e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29425E+08 1 0.18064E-09 0.23408E+02 0.18935E+04 c Velocity[X] 0.11878E+02 c Velocity[Y] 0.11530E+02 c Velocity[Z] 0.14585E-05 c Pressure 0.16919E-03 353 0.76837E-04 0.20924E-02 0.22720E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -19.47 30.584 5.6059 7.9975 v Velocity[Y] -21.543 22.865 -0.14337 -0.00070124 v Velocity[Z] -3.0323 2.9763 2.9184e-06 -5.3868e-08 v ǁVelocityǁ 0.0011997 30.683 7.1767 8.043 v Pressure -2.3201e+05 1.0421e+05 -59490 -34969 v TurbVisc 3.3313e-22 0.0083536 0.0001467 1.3899e-05 v CourantNb 5.8775e-08 0.011782 0.00016733 4.9105e-06 v FourierNb 1.2425e-07 0.047058 0.00014578 2.2721e-07 v total_pressure -1.3069e+05 2.0553e+05 41835 66356 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0672 0.099999 0.0028495 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2173e-07 0.052309 0.0003131 5.1377e-06 INSTANT 0.875497000E-01 TIME STEP NUMBER 55695 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282739891E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.738883015E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.39651E-02 0.21047E+01 Friction velocity uk : 0.39651E-02 0.21047E+01 Dimensionless distance yplus : 0.38138E-02 0.20667E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.146366668e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29424E+08 1 0.18061E-09 0.23390E+02 0.18928E+04 c Velocity[X] 0.11866E+02 c Velocity[Y] 0.11525E+02 c Velocity[Z] 0.14462E-05 c Pressure 0.17259E-03 70 0.82510E-04 0.21332E-02 0.23197E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -19.482 30.6 5.6057 7.9974 v Velocity[Y] -21.556 22.875 -0.14336 -0.00070064 v Velocity[Z] -3.0322 2.9763 2.9175e-06 -5.3868e-08 v ǁVelocityǁ 0.0011816 30.695 7.1782 8.043 v Pressure -2.3055e+05 1.0561e+05 -58148 -34160 v TurbVisc 2.5073e-21 0.0083728 0.00014675 1.3921e-05 v CourantNb 4.1672e-08 0.011782 0.00016733 4.9105e-06 v FourierNb 1.2425e-07 0.047054 0.00014578 2.2736e-07 v total_pressure -1.2922e+05 2.0694e+05 43177 67165 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0667 0.10002 0.0028494 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2172e-07 0.052304 0.00031311 5.1379e-06 INSTANT 0.875498000E-01 TIME STEP NUMBER 55696 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282734621E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.738676800E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.14946E-02 0.21042E+01 Friction velocity uk : 0.14946E-02 0.21042E+01 Dimensionless distance yplus : 0.14441E-02 0.20661E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.171201590e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29424E+08 1 0.18058E-09 0.23373E+02 0.18921E+04 c Velocity[X] 0.11855E+02 c Velocity[Y] 0.11518E+02 c Velocity[Z] 0.14376E-05 c Pressure 0.17603E-03 310 0.95549E-04 0.21742E-02 0.21034E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -19.493 30.616 5.6056 7.9973 v Velocity[Y] -21.569 22.886 -0.14335 -0.00070232 v Velocity[Z] -3.032 2.9762 2.9167e-06 -5.3868e-08 v ǁVelocityǁ 0.0011585 30.707 7.1796 8.043 v Pressure -2.2903e+05 1.0705e+05 -56808 -33482 v TurbVisc 2.9221e-21 0.008392 0.0001468 1.3943e-05 v CourantNb 2.2334e-08 0.011782 0.00016733 4.9105e-06 v FourierNb 1.2425e-07 0.04705 0.00014578 2.2751e-07 v total_pressure -1.2771e+05 2.0838e+05 44517 67843 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0661 0.10004 0.0028492 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2171e-07 0.0523 0.00031311 5.138e-06 INSTANT 0.875499000E-01 TIME STEP NUMBER 55697 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282729614E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.738475960E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.70967E-02 0.21037E+01 Friction velocity uk : 0.70967E-02 0.21037E+01 Dimensionless distance yplus : 0.68259E-02 0.20657E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.191828471e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29424E+08 1 0.18055E-09 0.23350E+02 0.18911E+04 c Velocity[X] 0.11842E+02 c Velocity[Y] 0.11507E+02 c Velocity[Z] 0.14301E-05 c Pressure 0.17938E-03 124 0.81455E-04 0.22142E-02 0.23758E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -19.505 30.632 5.6055 7.9972 v Velocity[Y] -21.581 22.897 -0.14334 -0.00070261 v Velocity[Z] -3.0319 2.9762 2.9158e-06 -5.3868e-08 v ǁVelocityǁ 0.0011311 30.719 7.1811 8.043 v Pressure -2.2747e+05 1.0852e+05 -55418 -32646 v TurbVisc 4.6477e-21 0.0084111 0.00014685 1.3964e-05 v CourantNb 5.3491e-08 0.011782 0.00016733 4.9105e-06 v FourierNb 1.2425e-07 0.047047 0.00014578 2.2766e-07 v total_pressure -1.2614e+05 2.0985e+05 45907 68679 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0657 0.10007 0.0028492 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.217e-07 0.052296 0.00031311 5.1382e-06 INSTANT 0.875500000E-01 TIME STEP NUMBER 55698 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282724637E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.738281561E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.80665E-02 0.21032E+01 Friction velocity uk : 0.80665E-02 0.21032E+01 Dimensionless distance yplus : 0.77587E-02 0.20652E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.204912239e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29423E+08 1 0.18051E-09 0.23334E+02 0.18905E+04 c Velocity[X] 0.11831E+02 c Velocity[Y] 0.11503E+02 c Velocity[Z] 0.14238E-05 c Pressure 0.18126E-03 10 0.59034E-04 0.22360E-02 0.20444E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -19.516 30.647 5.6054 7.9971 v Velocity[Y] -21.594 22.908 -0.14334 -0.00070228 v Velocity[Z] -3.0318 2.9762 2.9149e-06 -5.3868e-08 v ǁVelocityǁ 0.0010987 30.73 7.1825 8.043 v Pressure -2.2587e+05 1.1001e+05 -54015 -31920 v TurbVisc 3.5762e-21 0.0084303 0.00014689 1.3986e-05 v CourantNb 6.4411e-08 0.011782 0.00016733 4.9105e-06 v FourierNb 1.2425e-07 0.047044 0.00014578 2.2781e-07 v total_pressure -1.2455e+05 2.1133e+05 47310 69405 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0652 0.10009 0.0028491 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.217e-07 0.052292 0.00031311 5.1383e-06 INSTANT 0.875501000E-01 TIME STEP NUMBER 55699 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282719827E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.738093620E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.37594E-02 0.21028E+01 Friction velocity uk : 0.37594E-02 0.21028E+01 Dimensionless distance yplus : 0.37590E-02 0.20648E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.209127725e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29423E+08 1 0.18048E-09 0.23316E+02 0.18897E+04 c Velocity[X] 0.11819E+02 c Velocity[Y] 0.11497E+02 c Velocity[Z] 0.14183E-05 c Pressure 0.18460E-03 223 0.77297E-04 0.22756E-02 0.26966E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -19.527 30.663 5.6053 7.997 v Velocity[Y] -21.607 22.918 -0.14333 -0.00070355 v Velocity[Z] -3.0316 2.9761 2.9141e-06 -5.3868e-08 v ǁVelocityǁ 0.0010689 30.742 7.184 8.043 v Pressure -2.2421e+05 1.1154e+05 -52557 -31058 v TurbVisc 5.4262e-21 0.0084495 0.00014694 1.4008e-05 v CourantNb 7.6392e-08 0.011782 0.00016733 4.9106e-06 v FourierNb 1.2425e-07 0.04704 0.00014579 2.2795e-07 v total_pressure -1.2289e+05 2.1287e+05 48768 70267 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0648 0.10011 0.0028489 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2169e-07 0.052288 0.00031311 5.1385e-06 INSTANT 0.875502000E-01 TIME STEP NUMBER 55700 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282715115E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.737914608E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.98537E-02 0.21024E+01 Friction velocity uk : 0.98537E-02 0.21024E+01 Dimensionless distance yplus : 0.94777E-02 0.20644E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.215299128e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29422E+08 1 0.18045E-09 0.23300E+02 0.18890E+04 c Velocity[X] 0.11808E+02 c Velocity[Y] 0.11492E+02 c Velocity[Z] 0.14104E-05 c Pressure 0.18765E-03 42 0.83141E-04 0.23118E-02 0.28362E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -19.538 30.679 5.6052 7.9969 v Velocity[Y] -21.619 22.929 -0.14332 -0.00070297 v Velocity[Z] -3.0315 2.9761 2.9132e-06 -5.3868e-08 v ǁVelocityǁ 0.0010344 30.754 7.1854 8.043 v Pressure -2.2254e+05 1.1308e+05 -51051 -30146 v TurbVisc 2.3918e-21 0.0084687 0.00014699 1.403e-05 v CourantNb 6.7864e-08 0.011782 0.00016733 4.9106e-06 v FourierNb 1.2425e-07 0.047038 0.00014579 2.2811e-07 v total_pressure -1.2121e+05 2.144e+05 50274 71179 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0644 0.10013 0.0028487 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2168e-07 0.052285 0.00031312 5.1387e-06 INSTANT 0.875503000E-01 TIME STEP NUMBER 55701 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282710476E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.737733367E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.63011E-02 0.21021E+01 Friction velocity uk : 0.63011E-02 0.21021E+01 Dimensionless distance yplus : 0.62695E-02 0.20640E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.213299688e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29422E+08 1 0.18042E-09 0.23284E+02 0.18883E+04 c Velocity[X] 0.11798E+02 c Velocity[Y] 0.11486E+02 c Velocity[Z] 0.14036E-05 c Pressure 0.19065E-03 237 0.96227E-04 0.23471E-02 0.25301E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -19.55 30.694 5.6051 7.9968 v Velocity[Y] -21.632 22.94 -0.14331 -0.00070471 v Velocity[Z] -3.0314 2.9761 2.9124e-06 -5.3868e-08 v ǁVelocityǁ 0.00099881 30.766 7.1869 8.043 v Pressure -2.2083e+05 1.1464e+05 -49556 -29393 v TurbVisc 3.2509e-21 0.0084879 0.00014703 1.4051e-05 v CourantNb 5.906e-08 0.011782 0.00016733 4.9106e-06 v FourierNb 1.2425e-07 0.047036 0.00014579 2.2826e-07 v total_pressure -1.195e+05 2.1597e+05 51769 71932 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.064 0.10015 0.0028484 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2168e-07 0.052282 0.00031312 5.1388e-06 INSTANT 0.875504000E-01 TIME STEP NUMBER 55702 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282706116E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.737559318E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10527E-01 0.21017E+01 Friction velocity uk : 0.10527E-01 0.21017E+01 Dimensionless distance yplus : 0.10125E-01 0.20637E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.202912127e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29421E+08 1 0.18040E-09 0.23262E+02 0.18874E+04 c Velocity[X] 0.11786E+02 c Velocity[Y] 0.11476E+02 c Velocity[Z] 0.13986E-05 c Pressure 0.19354E-03 111 0.81915E-04 0.23812E-02 0.29775E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -19.561 30.71 5.605 7.9967 v Velocity[Y] -21.644 22.951 -0.14331 -0.00070508 v Velocity[Z] -3.0312 2.976 2.9115e-06 -5.3868e-08 v ǁVelocityǁ 0.00096396 30.778 7.1883 8.043 v Pressure -2.1912e+05 1.1622e+05 -48005 -28444 v TurbVisc 6.1793e-21 0.0085071 0.00014708 1.4073e-05 v CourantNb 4.9717e-08 0.011782 0.00016733 4.9106e-06 v FourierNb 1.2425e-07 0.047034 0.00014579 2.2841e-07 v total_pressure -1.1779e+05 2.1755e+05 53320 72881 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0637 0.10017 0.0028481 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2167e-07 0.05228 0.00031312 5.139e-06 INSTANT 0.875505000E-01 TIME STEP NUMBER 55703 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282701797E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.737392911E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10524E-01 0.21015E+01 Friction velocity uk : 0.10524E-01 0.21015E+01 Dimensionless distance yplus : 0.10122E-01 0.20635E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.182992412e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29421E+08 1 0.18037E-09 0.23249E+02 0.18869E+04 c Velocity[X] 0.11776E+02 c Velocity[Y] 0.11473E+02 c Velocity[Z] 0.13939E-05 c Pressure 0.19506E-03 10 0.60305E-04 0.23983E-02 0.25142E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -19.572 30.726 5.6049 7.9966 v Velocity[Y] -21.657 22.962 -0.1433 -0.00070479 v Velocity[Z] -3.0311 2.976 2.9106e-06 -5.3868e-08 v ǁVelocityǁ 0.00092968 30.79 7.1898 8.043 v Pressure -2.174e+05 1.1781e+05 -46452 -27640 v TurbVisc 4.6105e-21 0.0085263 0.00014713 1.4095e-05 v CourantNb 4.0118e-08 0.011782 0.00016733 4.9106e-06 v FourierNb 1.2425e-07 0.047032 0.00014579 2.2856e-07 v total_pressure -1.1608e+05 2.1913e+05 54873 73685 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0635 0.10019 0.0028479 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2166e-07 0.052278 0.00031312 5.1392e-06 INSTANT 0.875506000E-01 TIME STEP NUMBER 55704 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282697669E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.737233764E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10283E-01 0.21012E+01 Friction velocity uk : 0.10283E-01 0.21012E+01 Dimensionless distance yplus : 0.98909E-02 0.20632E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.146997483e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29421E+08 1 0.18034E-09 0.23232E+02 0.18862E+04 c Velocity[X] 0.11765E+02 c Velocity[Y] 0.11467E+02 c Velocity[Z] 0.13896E-05 c Pressure 0.19795E-03 141 0.77974E-04 0.24323E-02 0.32642E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -19.583 30.741 5.6048 7.9965 v Velocity[Y] -21.669 22.973 -0.1433 -0.00070614 v Velocity[Z] -3.031 2.976 2.9098e-06 -5.3868e-08 v ǁVelocityǁ 0.00090215 30.802 7.1913 8.043 v Pressure -2.1562e+05 1.1944e+05 -44859 -26702 v TurbVisc 6.2416e-21 0.0085455 0.00014717 1.4117e-05 v CourantNb 3.3742e-08 0.011782 0.00016733 4.9107e-06 v FourierNb 1.2425e-07 0.04703 0.00014579 2.2871e-07 v total_pressure -1.143e+05 2.2077e+05 56466 74623 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0632 0.10021 0.0028475 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2166e-07 0.052276 0.00031312 5.1394e-06 INSTANT 0.875507000E-01 TIME STEP NUMBER 55705 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282693630E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.737083863E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.99509E-02 0.21010E+01 Friction velocity uk : 0.99509E-02 0.21010E+01 Dimensionless distance yplus : 0.95712E-02 0.20630E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.117805905e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29420E+08 1 0.18031E-09 0.23218E+02 0.18856E+04 c Velocity[X] 0.11755E+02 c Velocity[Y] 0.11463E+02 c Velocity[Z] 0.13832E-05 c Pressure 0.20052E-03 35 0.84043E-04 0.24623E-02 0.34775E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -19.594 30.757 5.6047 7.9964 v Velocity[Y] -21.682 22.984 -0.14329 -0.00070562 v Velocity[Z] -3.0309 2.9759 2.9089e-06 -5.3868e-08 v ǁVelocityǁ 0.00087563 30.817 7.1927 8.0431 v Pressure -2.1384e+05 1.2108e+05 -43205 -25697 v TurbVisc 7.5189e-21 0.0085647 0.00014722 1.4139e-05 v CourantNb 3.3863e-08 0.011782 0.00016733 4.9107e-06 v FourierNb 1.2425e-07 0.047029 0.00014579 2.2886e-07 v total_pressure -1.1252e+05 2.224e+05 58120 75628 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.063 0.10022 0.0028472 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2165e-07 0.052274 0.00031312 5.1395e-06 INSTANT 0.875508000E-01 TIME STEP NUMBER 55706 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282689685E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.736934494E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.93063E-02 0.21008E+01 Friction velocity uk : 0.93063E-02 0.21008E+01 Dimensionless distance yplus : 0.89512E-02 0.20628E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.072851266e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29420E+08 1 0.18029E-09 0.23204E+02 0.18850E+04 c Velocity[X] 0.11746E+02 c Velocity[Y] 0.11459E+02 c Velocity[Z] 0.13777E-05 c Pressure 0.20308E-03 238 0.97016E-04 0.24921E-02 0.30722E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -19.606 30.772 5.6047 7.9964 v Velocity[Y] -21.694 22.995 -0.14329 -0.00070745 v Velocity[Z] -3.0307 2.9759 2.908e-06 -5.3868e-08 v ǁVelocityǁ 0.00085279 30.833 7.1942 8.0431 v Pressure -2.1204e+05 1.2273e+05 -41578 -24872 v TurbVisc 7.9732e-21 0.0085839 0.00014727 1.4161e-05 v CourantNb 3.3731e-08 0.011782 0.00016733 4.9107e-06 v FourierNb 1.2425e-07 0.047028 0.00014579 2.2901e-07 v total_pressure -1.1071e+05 2.2406e+05 59747 76453 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0628 0.10023 0.0028468 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2165e-07 0.052273 0.00031313 5.1397e-06 INSTANT 0.875509000E-01 TIME STEP NUMBER 55707 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282686035E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.736791805E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.79525E-02 0.21007E+01 Friction velocity uk : 0.79525E-02 0.21007E+01 Dimensionless distance yplus : 0.77054E-02 0.20627E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.018300079e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29420E+08 1 0.18026E-09 0.23185E+02 0.18842E+04 c Velocity[X] 0.11735E+02 c Velocity[Y] 0.11449E+02 c Velocity[Z] 0.13750E-05 c Pressure 0.20552E-03 556 0.82800E-04 0.25204E-02 0.36063E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -19.617 30.788 5.6046 7.9963 v Velocity[Y] -21.707 23.006 -0.14328 -0.00070809 v Velocity[Z] -3.0306 2.9759 2.9072e-06 -5.3868e-08 v ǁVelocityǁ 0.00083417 30.849 7.1957 8.0431 v Pressure -2.102e+05 1.2441e+05 -39899 -23855 v TurbVisc 8.4593e-21 0.0086031 0.00014731 1.4183e-05 v CourantNb 3.3604e-08 0.011782 0.00016733 4.9107e-06 v FourierNb 1.2425e-07 0.047027 0.00014579 2.2916e-07 v total_pressure -1.0888e+05 2.2573e+05 61426 77470 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0627 0.10024 0.0028464 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2164e-07 0.052272 0.00031313 5.1399e-06 INSTANT 0.875510000E-01 TIME STEP NUMBER 55708 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282682428E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.736658507E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.76357E-02 0.21005E+01 Friction velocity uk : 0.76357E-02 0.21005E+01 Dimensionless distance yplus : 0.73443E-02 0.20625E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -9.549087437e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29419E+08 1 0.18023E-09 0.23174E+02 0.18837E+04 c Velocity[X] 0.11727E+02 c Velocity[Y] 0.11447E+02 c Velocity[Z] 0.13743E-05 c Pressure 0.20661E-03 10 0.62015E-04 0.25322E-02 0.31748E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -19.628 30.803 5.6045 7.9962 v Velocity[Y] -21.719 23.017 -0.14328 -0.00070768 v Velocity[Z] -3.0305 2.9759 2.9063e-06 -5.3868e-08 v ǁVelocityǁ 0.000819 30.864 7.1972 8.0431 v Pressure -2.0836e+05 1.2609e+05 -38207 -22956 v TurbVisc 8.6819e-21 0.0086224 0.00014736 1.4206e-05 v CourantNb 4.0381e-08 0.011782 0.00016733 4.9108e-06 v FourierNb 1.2425e-07 0.047026 0.00014579 2.2932e-07 v total_pressure -1.0703e+05 2.2741e+05 63118 78369 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0625 0.10024 0.002846 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2164e-07 0.052272 0.00031313 5.1401e-06 INSTANT 0.875511000E-01 TIME STEP NUMBER 55709 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282679047E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.736533921E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.69605E-02 0.21004E+01 Friction velocity uk : 0.69605E-02 0.21004E+01 Dimensionless distance yplus : 0.66949E-02 0.20624E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -8.708732753e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29419E+08 1 0.18021E-09 0.23159E+02 0.18831E+04 c Velocity[X] 0.11717E+02 c Velocity[Y] 0.11442E+02 c Velocity[Z] 0.13729E-05 c Pressure 0.20909E-03 193 0.78972E-04 0.25609E-02 0.39685E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -19.639 30.819 5.6045 7.9961 v Velocity[Y] -21.731 23.028 -0.14328 -0.00070914 v Velocity[Z] -3.0303 2.9758 2.9055e-06 -5.3868e-08 v ǁVelocityǁ 0.00081003 30.88 7.1986 8.0432 v Pressure -2.0647e+05 1.2781e+05 -36505 -21957 v TurbVisc 9.9474e-21 0.0086416 0.00014741 1.4228e-05 v CourantNb 4.8652e-08 0.011782 0.00016734 4.9108e-06 v FourierNb 1.2425e-07 0.047026 0.00014579 2.2947e-07 v total_pressure -1.0514e+05 2.2914e+05 64820 79368 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0624 0.10025 0.0028456 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2163e-07 0.052271 0.00031313 5.1403e-06 INSTANT 0.875512000E-01 TIME STEP NUMBER 55710 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282675737E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.736418328E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.55233E-02 0.21003E+01 Friction velocity uk : 0.55233E-02 0.21003E+01 Dimensionless distance yplus : 0.53125E-02 0.20623E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -8.054776956e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29419E+08 1 0.18018E-09 0.23148E+02 0.18826E+04 c Velocity[X] 0.11709E+02 c Velocity[Y] 0.11439E+02 c Velocity[Z] 0.13683E-05 c Pressure 0.21116E-03 30 0.85219E-04 0.25846E-02 0.42453E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -19.65 30.834 5.6044 7.9961 v Velocity[Y] -21.744 23.04 -0.14327 -0.00070869 v Velocity[Z] -3.0302 2.9758 2.9046e-06 -5.3868e-08 v ǁVelocityǁ 0.00080259 30.896 7.2001 8.0432 v Pressure -2.0458e+05 1.2954e+05 -34733 -20876 v TurbVisc 7.2632e-21 0.0086608 0.00014746 1.425e-05 v CourantNb 5.6195e-08 0.011782 0.00016734 4.9108e-06 v FourierNb 1.2425e-07 0.047026 0.00014579 2.2962e-07 v total_pressure -1.0326e+05 2.3086e+05 66592 80449 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0623 0.10025 0.0028453 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2163e-07 0.052271 0.00031313 5.1404e-06 INSTANT 0.875513000E-01 TIME STEP NUMBER 55711 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282672548E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.736306764E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.31590E-02 0.21003E+01 Friction velocity uk : 0.31590E-02 0.21003E+01 Dimensionless distance yplus : 0.30385E-02 0.20623E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -7.172415677e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29419E+08 1 0.18016E-09 0.23137E+02 0.18821E+04 c Velocity[X] 0.11701E+02 c Velocity[Y] 0.11435E+02 c Velocity[Z] 0.13678E-05 c Pressure 0.21326E-03 227 0.98607E-04 0.26086E-02 0.37428E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -19.661 30.85 5.6044 7.996 v Velocity[Y] -21.756 23.051 -0.14327 -0.00071063 v Velocity[Z] -3.0301 2.9758 2.9037e-06 -5.3868e-08 v ǁVelocityǁ 0.00079772 30.911 7.2016 8.0432 v Pressure -2.0268e+05 1.3128e+05 -32993 -19993 v TurbVisc 3.3044e-21 0.00868 0.0001475 1.4272e-05 v CourantNb 6.3315e-08 0.011782 0.00016734 4.9109e-06 v FourierNb 1.2425e-07 0.047026 0.0001458 2.2978e-07 v total_pressure -1.0136e+05 2.3261e+05 68332 81332 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0623 0.10025 0.0028449 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2162e-07 0.052271 0.00031313 5.1406e-06 INSTANT 0.875514000E-01 TIME STEP NUMBER 55712 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282669660E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.736202055E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.28707E-02 0.21002E+01 Friction velocity uk : 0.28707E-02 0.21002E+01 Dimensionless distance yplus : 0.27612E-02 0.20622E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -6.234170909e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29418E+08 1 0.18013E-09 0.23120E+02 0.18814E+04 c Velocity[X] 0.11693E+02 c Velocity[Y] 0.11427E+02 c Velocity[Z] 0.13689E-05 c Pressure 0.21524E-03 387 0.83978E-04 0.26311E-02 0.44160E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -19.672 30.865 5.6044 7.996 v Velocity[Y] -21.769 23.062 -0.14327 -0.00071135 v Velocity[Z] -3.0299 2.9757 2.9029e-06 -5.3868e-08 v ǁVelocityǁ 0.00079494 30.927 7.2031 8.0433 v Pressure -2.0076e+05 1.3305e+05 -31207 -18908 v TurbVisc 1.8608e-21 0.0086993 0.00014755 1.4295e-05 v CourantNb 6.743e-08 0.011782 0.00016734 4.9109e-06 v FourierNb 1.2425e-07 0.047026 0.0001458 2.2993e-07 v total_pressure -99433 2.3438e+05 70118 82417 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0622 0.10024 0.0028445 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2162e-07 0.052271 0.00031314 5.1408e-06 INSTANT 0.875515000E-01 TIME STEP NUMBER 55713 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282666824E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.736108235E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.36322E-02 0.21002E+01 Friction velocity uk : 0.36322E-02 0.21002E+01 Dimensionless distance yplus : 0.34936E-02 0.20622E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -5.256428405e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29418E+08 1 0.18011E-09 0.23112E+02 0.18811E+04 c Velocity[X] 0.11686E+02 c Velocity[Y] 0.11426E+02 c Velocity[Z] 0.13715E-05 c Pressure 0.21587E-03 10 0.63439E-04 0.26372E-02 0.38752E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -19.683 30.881 5.6043 7.9959 v Velocity[Y] -21.781 23.073 -0.14327 -0.00071105 v Velocity[Z] -3.0298 2.9757 2.902e-06 -5.3868e-08 v ǁVelocityǁ 0.00079349 30.942 7.2046 8.0433 v Pressure -1.9883e+05 1.3493e+05 -29409 -17956 v TurbVisc 2.0606e-21 0.0087185 0.0001476 1.4317e-05 v CourantNb 6.7619e-08 0.011782 0.00016734 4.9109e-06 v FourierNb 1.2425e-07 0.047026 0.0001458 2.3008e-07 v total_pressure -97510 2.3625e+05 71916 83369 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0622 0.10024 0.0028442 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2162e-07 0.052271 0.00031314 5.141e-06 INSTANT 0.875516000E-01 TIME STEP NUMBER 55714 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282664229E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.736024450E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.61587E-02 0.21002E+01 Friction velocity uk : 0.61587E-02 0.21002E+01 Dimensionless distance yplus : 0.59237E-02 0.20622E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -4.077333542e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29418E+08 1 0.18008E-09 0.23101E+02 0.18806E+04 c Velocity[X] 0.11679E+02 c Velocity[Y] 0.11422E+02 c Velocity[Z] 0.13744E-05 c Pressure 0.21790E-03 143 0.80102E-04 0.26602E-02 0.48635E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -19.694 30.896 5.6043 7.9959 v Velocity[Y] -21.793 23.085 -0.14328 -0.00071261 v Velocity[Z] -3.0297 2.9757 2.9012e-06 -5.3868e-08 v ǁVelocityǁ 0.00079531 30.958 7.2061 8.0434 v Pressure -1.9686e+05 1.3687e+05 -27620 -16893 v TurbVisc 2.5764e-21 0.0087378 0.00014765 1.4339e-05 v CourantNb 6.7957e-08 0.011782 0.00016734 4.911e-06 v FourierNb 1.2425e-07 0.047026 0.0001458 2.3024e-07 v total_pressure -95539 2.3819e+05 73705 84432 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0622 0.10023 0.002844 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2161e-07 0.052271 0.00031314 5.1412e-06 INSTANT 0.875517000E-01 TIME STEP NUMBER 55715 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282661708E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.735950210E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.71269E-02 0.21002E+01 Friction velocity uk : 0.71269E-02 0.21002E+01 Dimensionless distance yplus : 0.68550E-02 0.20622E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -3.204080848e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29418E+08 1 0.18006E-09 0.23092E+02 0.18802E+04 c Velocity[X] 0.11672E+02 c Velocity[Y] 0.11420E+02 c Velocity[Z] 0.13733E-05 c Pressure 0.21945E-03 35 0.86354E-04 0.26774E-02 0.51500E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -19.705 30.912 5.6043 7.9958 v Velocity[Y] -21.806 23.096 -0.14328 -0.00071226 v Velocity[Z] -3.0295 2.9756 2.9003e-06 -5.3868e-08 v ǁVelocityǁ 0.000798 30.974 7.2076 8.0434 v Pressure -1.9499e+05 1.3879e+05 -25748 -15759 v TurbVisc 5.5388e-21 0.008757 0.00014769 1.4362e-05 v CourantNb 6.7939e-08 0.011781 0.00016735 4.911e-06 v FourierNb 1.2425e-07 0.047026 0.0001458 2.3039e-07 v total_pressure -93667 2.4012e+05 75577 85566 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0622 0.10022 0.0028437 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2161e-07 0.052271 0.00031314 5.1414e-06 INSTANT 0.875518000E-01 TIME STEP NUMBER 55716 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282659309E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.735883252E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.53636E-02 0.21002E+01 Friction velocity uk : 0.53636E-02 0.21002E+01 Dimensionless distance yplus : 0.51590E-02 0.20622E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -2.108575025e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29417E+08 1 0.18004E-09 0.23084E+02 0.18798E+04 c Velocity[X] 0.11667E+02 c Velocity[Y] 0.11417E+02 c Velocity[Z] 0.13747E-05 c Pressure 0.22109E-03 146 0.99851E-04 0.26957E-02 0.45570E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -19.716 30.927 5.6043 7.9958 v Velocity[Y] -21.818 23.107 -0.14328 -0.00071431 v Velocity[Z] -3.0294 2.9756 2.8994e-06 -5.3868e-08 v ǁVelocityǁ 0.00080286 30.989 7.2091 8.0435 v Pressure -1.9324e+05 1.4074e+05 -23926 -14825 v TurbVisc 5.4061e-21 0.0087763 0.00014774 1.4385e-05 v CourantNb 6.8153e-08 0.011781 0.00016735 4.9111e-06 v FourierNb 1.2425e-07 0.047026 0.0001458 2.3055e-07 v total_pressure -91912 2.4206e+05 77399 86500 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0622 0.10021 0.0028435 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2161e-07 0.052272 0.00031314 5.1416e-06 INSTANT 0.875519000E-01 TIME STEP NUMBER 55717 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282657234E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.735822193E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.40503E-02 0.21002E+01 Friction velocity uk : 0.40503E-02 0.21002E+01 Dimensionless distance yplus : 0.38958E-02 0.20622E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -9.970249965e-03 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29417E+08 1 0.18002E-09 0.23070E+02 0.18793E+04 c Velocity[X] 0.11661E+02 c Velocity[Y] 0.11409E+02 c Velocity[Z] 0.13776E-05 c Pressure 0.22257E-03 382 0.85026E-04 0.27120E-02 0.53439E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -19.727 30.943 5.6043 7.9957 v Velocity[Y] -21.831 23.119 -0.14329 -0.00071515 v Velocity[Z] -3.0293 2.9756 2.8986e-06 -5.3868e-08 v ǁVelocityǁ 0.00081068 31.005 7.2106 8.0435 v Pressure -1.9146e+05 1.4271e+05 -22051 -13694 v TurbVisc 5.1814e-21 0.0087955 0.00014779 1.4407e-05 v CourantNb 6.8326e-08 0.011781 0.00016735 4.9111e-06 v FourierNb 1.2425e-07 0.047027 0.0001458 2.3071e-07 v total_pressure -90132 2.4403e+05 79274 87631 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0622 0.1002 0.0028433 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2161e-07 0.052272 0.00031315 5.1418e-06 INSTANT 0.875520000E-01 TIME STEP NUMBER 55718 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282655206E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.735774344E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.56517E-02 0.21002E+01 Friction velocity uk : 0.56517E-02 0.21002E+01 Dimensionless distance yplus : 0.54361E-02 0.20622E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 3.936172964e-04 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29417E+08 1 0.18000E-09 0.23066E+02 0.18790E+04 c Velocity[X] 0.11656E+02 c Velocity[Y] 0.11409E+02 c Velocity[Z] 0.13830E-05 c Pressure 0.22273E-03 10 0.64647E-04 0.27121E-02 0.46982E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -19.738 30.958 5.6043 7.9957 v Velocity[Y] -21.843 23.13 -0.14329 -0.00071494 v Velocity[Z] -3.0291 2.9755 2.8977e-06 -5.3868e-08 v ǁVelocityǁ 0.00082127 31.021 7.2122 8.0436 v Pressure -1.8967e+05 1.4466e+05 -20179 -12700 v TurbVisc 4.9341e-21 0.0088148 0.00014784 1.443e-05 v CourantNb 6.8471e-08 0.011781 0.00016735 4.9111e-06 v FourierNb 1.2425e-07 0.047027 0.0001458 2.3086e-07 v total_pressure -88343 2.4599e+05 81146 88625 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0622 0.10019 0.0028432 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.216e-07 0.052273 0.00031315 5.142e-06 INSTANT 0.875521000E-01 TIME STEP NUMBER 55719 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282653436E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.735736877E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.73876E-02 0.21002E+01 Friction velocity uk : 0.73876E-02 0.21002E+01 Dimensionless distance yplus : 0.71057E-02 0.20622E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.257554525e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29417E+08 1 0.17997E-09 0.23058E+02 0.18787E+04 c Velocity[X] 0.11652E+02 c Velocity[Y] 0.11406E+02 c Velocity[Z] 0.13871E-05 c Pressure 0.22426E-03 162 0.81113E-04 0.27291E-02 0.58725E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -19.748 30.974 5.6043 7.9956 v Velocity[Y] -21.855 23.141 -0.1433 -0.00071662 v Velocity[Z] -3.029 2.9755 2.8969e-06 -5.3868e-08 v ǁVelocityǁ 0.00083988 31.037 7.2137 8.0437 v Pressure -1.8783e+05 1.4668e+05 -18318 -11592 v TurbVisc 5.295e-21 0.008834 0.00014789 1.4453e-05 v CourantNb 6.8791e-08 0.011781 0.00016736 4.9112e-06 v FourierNb 1.2425e-07 0.047027 0.0001458 2.3102e-07 v total_pressure -86504 2.48e+05 83007 89733 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0622 0.10018 0.0028431 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.216e-07 0.052273 0.00031315 5.1422e-06 INSTANT 0.875522000E-01 TIME STEP NUMBER 55720 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282651738E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.735710599E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.74848E-02 0.21003E+01 Friction velocity uk : 0.74848E-02 0.21003E+01 Dimensionless distance yplus : 0.71992E-02 0.20623E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 2.097061153e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29417E+08 1 0.17995E-09 0.23053E+02 0.18784E+04 c Velocity[X] 0.11648E+02 c Velocity[Y] 0.11406E+02 c Velocity[Z] 0.13870E-05 c Pressure 0.22532E-03 30 0.87465E-04 0.27401E-02 0.61621E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -19.759 30.99 5.6043 7.9956 v Velocity[Y] -21.868 23.152 -0.1433 -0.00071635 v Velocity[Z] -3.0289 2.9755 2.896e-06 -5.3868e-08 v ǁVelocityǁ 0.00086178 31.052 7.2152 8.0437 v Pressure -1.8599e+05 1.4876e+05 -16376 -10418 v TurbVisc 4.5275e-21 0.0088533 0.00014793 1.4476e-05 v CourantNb 6.8755e-08 0.011781 0.00016736 4.9112e-06 v FourierNb 1.2425e-07 0.047028 0.0001458 2.3118e-07 v total_pressure -84665 2.5008e+05 84949 90907 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0623 0.10016 0.002843 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.216e-07 0.052274 0.00031315 5.1424e-06 INSTANT 0.875523000E-01 TIME STEP NUMBER 55721 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282650171E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.735692087E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.77812E-02 0.21003E+01 Friction velocity uk : 0.77812E-02 0.21003E+01 Dimensionless distance yplus : 0.74843E-02 0.20623E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 3.082747812e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29417E+08 1 0.17993E-09 0.23043E+02 0.18780E+04 c Velocity[X] 0.11644E+02 c Velocity[Y] 0.11399E+02 c Velocity[Z] 0.13904E-05 c Pressure 0.22646E-03 161 0.75708E-04 0.27522E-02 0.52211E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -19.77 31.005 5.6043 7.9956 v Velocity[Y] -21.88 23.164 -0.14331 -0.0007175 v Velocity[Z] -3.0287 2.9754 2.8952e-06 -5.3869e-08 v ǁVelocityǁ 0.00088892 31.068 7.2167 8.0438 v Pressure -1.8413e+05 1.5085e+05 -14492 -9437.8 v TurbVisc 4.0144e-21 0.0088726 0.00014798 1.4498e-05 v CourantNb 6.894e-08 0.011781 0.00016736 4.9113e-06 v FourierNb 1.2425e-07 0.047029 0.0001458 2.3133e-07 v total_pressure -82804 2.5218e+05 86833 91887 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0623 0.10014 0.002843 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.216e-07 0.052275 0.00031316 5.1426e-06 INSTANT 0.875524000E-01 TIME STEP NUMBER 55722 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282648845E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.735680335E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.29840E-02 0.21003E+01 Friction velocity uk : 0.29840E-02 0.21003E+01 Dimensionless distance yplus : 0.29690E-02 0.20623E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 4.009973326e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29417E+08 1 0.17991E-09 0.23041E+02 0.18779E+04 c Velocity[X] 0.11642E+02 c Velocity[Y] 0.11399E+02 c Velocity[Z] 0.13971E-05 c Pressure 0.22639E-03 10 0.60860E-04 0.27496E-02 0.51836E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -19.781 31.021 5.6044 7.9956 v Velocity[Y] -21.892 23.175 -0.14332 -0.0007193 v Velocity[Z] -3.0286 2.9754 2.8943e-06 -5.3869e-08 v ǁVelocityǁ 0.00091946 31.084 7.2183 8.0439 v Pressure -1.8225e+05 1.5294e+05 -12579 -8434.6 v TurbVisc 3.9848e-21 0.0088918 0.00014803 1.4521e-05 v CourantNb 6.9079e-08 0.011781 0.00016736 4.9114e-06 v FourierNb 1.2425e-07 0.047029 0.0001458 2.3149e-07 v total_pressure -80929 2.5427e+05 88746 92890 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0623 0.10012 0.002843 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.216e-07 0.052275 0.00031316 5.1428e-06 INSTANT 0.875525000E-01 TIME STEP NUMBER 55723 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282647849E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.735682659E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.69768E-02 0.21003E+01 Friction velocity uk : 0.69768E-02 0.21003E+01 Dimensionless distance yplus : 0.67106E-02 0.20624E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 4.983452855e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29417E+08 1 0.17989E-09 0.23034E+02 0.18776E+04 c Velocity[X] 0.11639E+02 c Velocity[Y] 0.11396E+02 c Velocity[Z] 0.14025E-05 c Pressure 0.22737E-03 23 0.96672E-04 0.27597E-02 0.66958E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -19.791 31.037 5.6044 7.9955 v Velocity[Y] -21.905 23.186 -0.14333 -0.00072043 v Velocity[Z] -3.0285 2.9754 2.8935e-06 -5.3869e-08 v ǁVelocityǁ 0.00096127 31.1 7.2198 8.044 v Pressure -1.8034e+05 1.5508e+05 -10672 -7235.9 v TurbVisc 4.05e-21 0.0089111 0.00014808 1.4544e-05 v CourantNb 6.9384e-08 0.011781 0.00016737 4.9114e-06 v FourierNb 1.2425e-07 0.047029 0.0001458 2.3165e-07 v total_pressure -79010 2.5641e+05 90653 94089 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0624 0.10011 0.002843 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.216e-07 0.052276 0.00031316 5.1431e-06 INSTANT 0.875526000E-01 TIME STEP NUMBER 55724 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282646836E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.735698635E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.42496E-02 0.21004E+01 Friction velocity uk : 0.42496E-02 0.21004E+01 Dimensionless distance yplus : 0.42491E-02 0.20624E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 5.613585070e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29416E+08 1 0.17987E-09 0.23031E+02 0.18774E+04 c Velocity[X] 0.11637E+02 c Velocity[Y] 0.11394E+02 c Velocity[Z] 0.14018E-05 c Pressure 0.22777E-03 119 0.81391E-04 0.27627E-02 0.64856E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -19.802 31.053 5.6044 7.9955 v Velocity[Y] -21.917 23.198 -0.14333 -0.00072111 v Velocity[Z] -3.0283 2.9753 2.8926e-06 -5.3869e-08 v ǁVelocityǁ 0.0010043 31.116 7.2213 8.044 v Pressure -1.784e+05 1.572e+05 -8701.1 -6061.3 v TurbVisc 2.0172e-21 0.0089304 0.00014813 1.4567e-05 v CourantNb 6.9301e-08 0.011781 0.00016737 4.9115e-06 v FourierNb 1.2425e-07 0.04703 0.0001458 2.3181e-07 v total_pressure -77077 2.5853e+05 92624 95264 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0624 0.10009 0.0028431 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.216e-07 0.052277 0.00031317 5.1433e-06 INSTANT 0.875527000E-01 TIME STEP NUMBER 55725 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282646018E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.735723788E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.52202E-02 0.21005E+01 Friction velocity uk : 0.52202E-02 0.21005E+01 Dimensionless distance yplus : 0.50210E-02 0.20625E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 6.279705596e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29416E+08 1 0.17985E-09 0.23031E+02 0.18773E+04 c Velocity[X] 0.11636E+02 c Velocity[Y] 0.11395E+02 c Velocity[Z] 0.14089E-05 c Pressure 0.22801E-03 10 0.58776E-04 0.27639E-02 0.59537E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -19.813 31.068 5.6044 7.9955 v Velocity[Y] -21.929 23.209 -0.14334 -0.00072135 v Velocity[Z] -3.0282 2.9753 2.8918e-06 -5.3869e-08 v ǁVelocityǁ 0.0010487 31.132 7.2229 8.0441 v Pressure -1.7646e+05 1.5931e+05 -6735 -5002.9 v TurbVisc 6.877e-21 0.0089497 0.00014818 1.459e-05 v CourantNb 6.8445e-08 0.011781 0.00016737 4.9115e-06 v FourierNb 1.2425e-07 0.047031 0.0001458 2.3197e-07 v total_pressure -75138 2.6064e+05 94590 96322 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0625 0.10009 0.0028432 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.216e-07 0.052278 0.00031317 5.1435e-06 INSTANT 0.875528000E-01 TIME STEP NUMBER 55726 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282645387E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.735755291E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.70208E-02 0.21005E+01 Friction velocity uk : 0.70208E-02 0.21005E+01 Dimensionless distance yplus : 0.67530E-02 0.20625E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 6.998705284e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29416E+08 1 0.17983E-09 0.23026E+02 0.18771E+04 c Velocity[X] 0.11635E+02 c Velocity[Y] 0.11391E+02 c Velocity[Z] 0.14147E-05 c Pressure 0.22878E-03 90 0.99675E-04 0.27714E-02 0.65352E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -19.823 31.084 5.6045 7.9955 v Velocity[Y] -21.941 23.22 -0.14335 -0.00072185 v Velocity[Z] -3.0281 2.9753 2.8909e-06 -5.3869e-08 v ǁVelocityǁ 0.0011016 31.148 7.2244 8.0442 v Pressure -1.745e+05 1.6146e+05 -4847.9 -3899.4 v TurbVisc 1.9655e-21 0.0089689 0.00014823 1.4613e-05 v CourantNb 6.3463e-08 0.011781 0.00016738 4.9116e-06 v FourierNb 1.2425e-07 0.047031 0.0001458 2.3212e-07 v total_pressure -73173 2.6278e+05 96477 97426 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0625 0.10008 0.0028434 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.216e-07 0.052278 0.00031317 5.1437e-06 INSTANT 0.875529000E-01 TIME STEP NUMBER 55727 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282644883E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.735799730E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.91260E-02 0.21006E+01 Friction velocity uk : 0.91260E-02 0.21006E+01 Dimensionless distance yplus : 0.88424E-02 0.20626E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 7.354136721e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29416E+08 1 0.17981E-09 0.23025E+02 0.18770E+04 c Velocity[X] 0.11635E+02 c Velocity[Y] 0.11390E+02 c Velocity[Z] 0.14132E-05 c Pressure 0.22883E-03 38 0.83738E-04 0.27703E-02 0.62448E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -19.834 31.1 5.6045 7.9955 v Velocity[Y] -21.954 23.232 -0.14336 -0.00072302 v Velocity[Z] -3.0279 2.9752 2.8901e-06 -5.3869e-08 v ǁVelocityǁ 0.0011501 31.164 7.226 8.0443 v Pressure -1.7252e+05 1.6358e+05 -2874.8 -2815.8 v TurbVisc 9.8372e-22 0.0089882 0.00014828 1.4637e-05 v CourantNb 5.7977e-08 0.01178 0.00016738 4.9116e-06 v FourierNb 1.2425e-07 0.047032 0.0001458 2.3229e-07 v total_pressure -71192 2.6491e+05 98450 98509 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0626 0.10007 0.0028435 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.216e-07 0.052279 0.00031318 5.1439e-06 INSTANT 0.875530000E-01 TIME STEP NUMBER 55728 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282644584E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.735855711E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.80721E-02 0.21006E+01 Friction velocity uk : 0.80721E-02 0.21006E+01 Dimensionless distance yplus : 0.78213E-02 0.20626E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 7.735078304e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29416E+08 1 0.17980E-09 0.23027E+02 0.18771E+04 c Velocity[X] 0.11635E+02 c Velocity[Y] 0.11392E+02 c Velocity[Z] 0.14188E-05 c Pressure 0.22869E-03 10 0.60456E-04 0.27667E-02 0.59485E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -19.845 31.116 5.6046 7.9955 v Velocity[Y] -21.966 23.243 -0.14337 -0.00072518 v Velocity[Z] -3.0278 2.9752 2.8892e-06 -5.3869e-08 v ǁVelocityǁ 0.0011964 31.18 7.2275 8.0444 v Pressure -1.7052e+05 1.6569e+05 -910.14 -1781.3 v TurbVisc 1.6168e-21 0.0090075 0.00014833 1.466e-05 v CourantNb 5.2525e-08 0.01178 0.00016738 4.9117e-06 v FourierNb 1.2425e-07 0.047033 0.0001458 2.3244e-07 v total_pressure -69194 2.6702e+05 1.0041e+05 99544 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0626 0.10006 0.0028436 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.216e-07 0.05228 0.00031318 5.1442e-06 INSTANT 0.875531000E-01 TIME STEP NUMBER 55729 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282644545E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.735919939E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10422E-01 0.21007E+01 Friction velocity uk : 0.10422E-01 0.21007E+01 Dimensionless distance yplus : 0.10098E-01 0.20627E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 8.145144738e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29416E+08 1 0.17978E-09 0.23026E+02 0.18770E+04 c Velocity[X] 0.11636E+02 c Velocity[Y] 0.11390E+02 c Velocity[Z] 0.14221E-05 c Pressure 0.22908E-03 104 0.75763E-04 0.27696E-02 0.81659E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -19.855 31.132 5.6046 7.9955 v Velocity[Y] -21.978 23.254 -0.14338 -0.00072508 v Velocity[Z] -3.0277 2.9752 2.8884e-06 -5.3869e-08 v ǁVelocityǁ 0.0012491 31.196 7.2291 8.0445 v Pressure -1.6849e+05 1.6787e+05 1050.3 -451.62 v TurbVisc 2.6762e-21 0.0090268 0.00014838 1.4683e-05 v CourantNb 4.6694e-08 0.01178 0.00016739 4.9118e-06 v FourierNb 1.2425e-07 0.047033 0.0001458 2.326e-07 v total_pressure -67169 2.6919e+05 1.0238e+05 1.0087e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0627 0.10005 0.0028437 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.216e-07 0.052281 0.00031318 5.1444e-06 INSTANT 0.875532000E-01 TIME STEP NUMBER 55730 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282644475E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.735998615E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12583E-01 0.21008E+01 Friction velocity uk : 0.12583E-01 0.21008E+01 Dimensionless distance yplus : 0.12192E-01 0.20628E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 8.225870948e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29416E+08 1 0.17976E-09 0.23029E+02 0.18771E+04 c Velocity[X] 0.11637E+02 c Velocity[Y] 0.11391E+02 c Velocity[Z] 0.14198E-05 c Pressure 0.22914E-03 455 0.79905E-04 0.27686E-02 0.58472E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -19.866 31.148 5.6047 7.9955 v Velocity[Y] -21.99 23.266 -0.1434 -0.00072733 v Velocity[Z] -3.0275 2.9751 2.8875e-06 -5.3869e-08 v ǁVelocityǁ 0.0012925 31.212 7.2306 8.0446 v Pressure -1.6648e+05 1.6997e+05 2992.8 496.7 v TurbVisc 2.596e-21 0.0090461 0.00014843 1.4707e-05 v CourantNb 4.0907e-08 0.01178 0.00016739 4.9118e-06 v FourierNb 1.2425e-07 0.047034 0.0001458 2.3277e-07 v total_pressure -65159 2.7129e+05 1.0432e+05 1.0182e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0628 0.10003 0.0028438 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.216e-07 0.052282 0.00031319 5.1446e-06 INSTANT 0.875533000E-01 TIME STEP NUMBER 55731 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282644736E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.736081599E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11284E-01 0.21009E+01 Friction velocity uk : 0.11284E-01 0.21009E+01 Dimensionless distance yplus : 0.10892E-01 0.20629E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 8.283245031e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29416E+08 1 0.17974E-09 0.23032E+02 0.18771E+04 c Velocity[X] 0.11640E+02 c Velocity[Y] 0.11392E+02 c Velocity[Z] 0.14212E-05 c Pressure 0.22905E-03 30 0.93811E-04 0.27657E-02 0.71749E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -19.876 31.164 5.6047 7.9955 v Velocity[Y] -22.002 23.277 -0.14341 -0.00072701 v Velocity[Z] -3.0274 2.9751 2.8867e-06 -5.3869e-08 v ǁVelocityǁ 0.0013307 31.229 7.2322 8.0447 v Pressure -1.6445e+05 1.721e+05 4947.2 1680.9 v TurbVisc 1.4142e-21 0.0090654 0.00014848 1.473e-05 v CourantNb 1.9469e-08 0.01178 0.00016739 4.9119e-06 v FourierNb 1.2425e-07 0.047035 0.0001458 2.3293e-07 v total_pressure -63127 2.7343e+05 1.0627e+05 1.0301e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0629 0.10002 0.0028438 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.216e-07 0.052283 0.00031319 5.1448e-06 INSTANT 0.875534000E-01 TIME STEP NUMBER 55732 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282645100E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.736177738E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12169E-01 0.21010E+01 Friction velocity uk : 0.12169E-01 0.21010E+01 Dimensionless distance yplus : 0.11746E-01 0.20630E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 8.271173224e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29416E+08 1 0.17973E-09 0.23030E+02 0.18770E+04 c Velocity[X] 0.11642E+02 c Velocity[Y] 0.11388E+02 c Velocity[Z] 0.14220E-05 c Pressure 0.22885E-03 160 0.78915E-04 0.27615E-02 0.60478E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -19.887 31.18 5.6048 7.9955 v Velocity[Y] -22.014 23.289 -0.14342 -0.00072836 v Velocity[Z] -3.0272 2.9751 2.8858e-06 -5.3869e-08 v ǁVelocityǁ 0.0013628 31.245 7.2337 8.0448 v Pressure -1.6241e+05 1.7422e+05 6887.9 2698.1 v TurbVisc 2.4871e-21 0.0090847 0.00014853 1.4754e-05 v CourantNb 2.7108e-08 0.01178 0.00016739 4.912e-06 v FourierNb 1.2425e-07 0.047036 0.0001458 2.3309e-07 v total_pressure -61083 2.7554e+05 1.0821e+05 1.0402e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.063 0.10001 0.0028439 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2161e-07 0.052284 0.00031319 5.1451e-06 INSTANT 0.875535000E-01 TIME STEP NUMBER 55733 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282645671E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.736287481E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.17986E-01 0.21011E+01 Friction velocity uk : 0.17986E-01 0.21011E+01 Dimensionless distance yplus : 0.17300E-01 0.20631E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 8.133532377e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29416E+08 1 0.17971E-09 0.23036E+02 0.18772E+04 c Velocity[X] 0.11645E+02 c Velocity[Y] 0.11391E+02 c Velocity[Z] 0.14263E-05 c Pressure 0.22745E-03 10 0.61062E-04 0.27427E-02 0.56031E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -19.897 31.196 5.6048 7.9955 v Velocity[Y] -22.026 23.3 -0.14343 -0.00073036 v Velocity[Z] -3.0271 2.975 2.885e-06 -5.3869e-08 v ǁVelocityǁ 0.0013842 31.261 7.2353 8.0449 v Pressure -1.6037e+05 1.7631e+05 8819.9 3710.3 v TurbVisc 2.5904e-21 0.009104 0.00014858 1.4777e-05 v CourantNb 3.3486e-08 0.01178 0.0001674 4.9121e-06 v FourierNb 1.2425e-07 0.047037 0.0001458 2.3325e-07 v total_pressure -59048 2.7764e+05 1.1014e+05 1.0504e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0631 0.09999 0.0028439 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2161e-07 0.052285 0.00031319 5.1453e-06 INSTANT 0.875536000E-01 TIME STEP NUMBER 55734 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282646574E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.736408164E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.14032E-01 0.21012E+01 Friction velocity uk : 0.14032E-01 0.21012E+01 Dimensionless distance yplus : 0.13557E-01 0.20631E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 7.927134159e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29417E+08 1 0.17969E-09 0.23037E+02 0.18772E+04 c Velocity[X] 0.11648E+02 c Velocity[Y] 0.11389E+02 c Velocity[Z] 0.14291E-05 c Pressure 0.22710E-03 23 0.98904E-04 0.27368E-02 0.68993E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -19.907 31.213 5.6049 7.9955 v Velocity[Y] -22.039 23.312 -0.14344 -0.00073168 v Velocity[Z] -3.027 2.975 2.8841e-06 -5.3869e-08 v ǁVelocityǁ 0.0014086 31.278 7.2368 8.0451 v Pressure -1.5832e+05 1.7844e+05 10761 4917.1 v TurbVisc 2.6118e-21 0.0091233 0.00014863 1.48e-05 v CourantNb 3.3262e-08 0.01178 0.0001674 4.9121e-06 v FourierNb 1.2425e-07 0.047037 0.0001458 2.3341e-07 v total_pressure -56992 2.7977e+05 1.1209e+05 1.0624e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0631 0.099977 0.0028439 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2161e-07 0.052286 0.0003132 5.1455e-06 INSTANT 0.875537000E-01 TIME STEP NUMBER 55735 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282647462E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.736543174E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15721E-01 0.21013E+01 Friction velocity uk : 0.15721E-01 0.21013E+01 Dimensionless distance yplus : 0.15189E-01 0.20633E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 7.650167276e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29417E+08 1 0.17968E-09 0.23042E+02 0.18773E+04 c Velocity[X] 0.11652E+02 c Velocity[Y] 0.11389E+02 c Velocity[Z] 0.14263E-05 c Pressure 0.22629E-03 258 0.83525E-04 0.27252E-02 0.63602E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -19.918 31.229 5.6049 7.9955 v Velocity[Y] -22.051 23.324 -0.14345 -0.00073255 v Velocity[Z] -3.0268 2.975 2.8833e-06 -5.3869e-08 v ǁVelocityǁ 0.0014198 31.294 7.2384 8.0452 v Pressure -1.5627e+05 1.8054e+05 12739 6090.6 v TurbVisc 1.8709e-21 0.0091426 0.00014869 1.4824e-05 v CourantNb 3.3511e-08 0.011779 0.0001674 4.9122e-06 v FourierNb 1.2425e-07 0.047038 0.0001458 2.3358e-07 v total_pressure -54943 2.8186e+05 1.1406e+05 1.0742e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0633 0.099961 0.0028439 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2162e-07 0.052288 0.0003132 5.1458e-06 INSTANT 0.875538000E-01 TIME STEP NUMBER 55736 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282648546E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.736680601E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.17677E-01 0.21014E+01 Friction velocity uk : 0.17677E-01 0.21014E+01 Dimensionless distance yplus : 0.17148E-01 0.20634E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 7.276474737e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29417E+08 1 0.17966E-09 0.23050E+02 0.18776E+04 c Velocity[X] 0.11657E+02 c Velocity[Y] 0.11393E+02 c Velocity[Z] 0.14301E-05 c Pressure 0.22519E-03 10 0.60025E-04 0.27102E-02 0.55608E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -19.928 31.245 5.605 7.9956 v Velocity[Y] -22.063 23.336 -0.14346 -0.00073287 v Velocity[Z] -3.0267 2.9749 2.8824e-06 -5.3869e-08 v ǁVelocityǁ 0.0014195 31.31 7.2399 8.0453 v Pressure -1.5423e+05 1.8261e+05 14676 7138.7 v TurbVisc 2.4869e-21 0.0091619 0.00014874 1.4848e-05 v CourantNb 3.3483e-08 0.011779 0.00016741 4.9123e-06 v FourierNb 1.2425e-07 0.04704 0.0001458 2.3374e-07 v total_pressure -52905 2.8393e+05 1.16e+05 1.0846e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0634 0.099945 0.0028439 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2162e-07 0.052289 0.0003132 5.146e-06 INSTANT 0.875539000E-01 TIME STEP NUMBER 55737 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282649821E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.736826983E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.18015E-01 0.21015E+01 Friction velocity uk : 0.18015E-01 0.21015E+01 Dimensionless distance yplus : 0.17476E-01 0.20635E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 6.775727815e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29417E+08 1 0.17965E-09 0.23056E+02 0.18778E+04 c Velocity[X] 0.11662E+02 c Velocity[Y] 0.11393E+02 c Velocity[Z] 0.14336E-05 c Pressure 0.22457E-03 145 0.76391E-04 0.27009E-02 0.60561E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -19.939 31.261 5.605 7.9956 v Velocity[Y] -22.075 23.347 -0.14347 -0.00073473 v Velocity[Z] -3.0266 2.9749 2.8816e-06 -5.3869e-08 v ǁVelocityǁ 0.001421 31.327 7.2415 8.0454 v Pressure -1.5218e+05 1.847e+05 16577 8222.4 v TurbVisc 2.6929e-21 0.0091812 0.00014879 1.4871e-05 v CourantNb 3.3229e-08 0.011779 0.00016741 4.9124e-06 v FourierNb 1.2425e-07 0.047041 0.0001458 2.339e-07 v total_pressure -50859 2.8603e+05 1.179e+05 1.0955e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0635 0.09993 0.0028438 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2162e-07 0.05229 0.00031321 5.1463e-06 INSTANT 0.875540000E-01 TIME STEP NUMBER 55738 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282651215E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.736989556E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.14855E-01 0.21017E+01 Friction velocity uk : 0.14855E-01 0.21017E+01 Dimensionless distance yplus : 0.14716E-01 0.20637E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 6.406978302e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29417E+08 1 0.17963E-09 0.23065E+02 0.18781E+04 c Velocity[X] 0.11669E+02 c Velocity[Y] 0.11396E+02 c Velocity[Z] 0.14305E-05 c Pressure 0.22361E-03 30 0.81577E-04 0.26877E-02 0.60316E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -19.949 31.278 5.6051 7.9956 v Velocity[Y] -22.087 23.359 -0.14348 -0.00073482 v Velocity[Z] -3.0264 2.9749 2.8807e-06 -5.3869e-08 v ǁVelocityǁ 0.0014094 31.343 7.243 8.0456 v Pressure -1.5016e+05 1.8675e+05 18520 9379.6 v TurbVisc 2.5326e-21 0.0092006 0.00014884 1.4895e-05 v CourantNb 3.3415e-08 0.011779 0.00016741 4.9124e-06 v FourierNb 1.2425e-07 0.047042 0.00014579 2.3406e-07 v total_pressure -48832 2.8807e+05 1.1985e+05 1.107e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0637 0.09991 0.0028437 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2163e-07 0.052292 0.00031321 5.1465e-06 INSTANT 0.875541000E-01 TIME STEP NUMBER 55739 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282652749E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.737155600E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.50254E-02 0.21019E+01 Friction velocity uk : 0.50254E-02 0.21019E+01 Dimensionless distance yplus : 0.49784E-02 0.20638E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 5.787273210e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29417E+08 1 0.17962E-09 0.23074E+02 0.18784E+04 c Velocity[X] 0.11675E+02 c Velocity[Y] 0.11399E+02 c Velocity[Z] 0.14294E-05 c Pressure 0.22255E-03 224 0.94473E-04 0.26731E-02 0.50208E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -19.959 31.294 5.6051 7.9957 v Velocity[Y] -22.099 23.371 -0.14348 -0.00073717 v Velocity[Z] -3.0263 2.9749 2.8799e-06 -5.3869e-08 v ǁVelocityǁ 0.0013899 31.359 7.2446 8.0457 v Pressure -1.4814e+05 1.8878e+05 20397 10328 v TurbVisc 2.5627e-21 0.0092199 0.0001489 1.4919e-05 v CourantNb 3.3319e-08 0.011779 0.00016741 4.9125e-06 v FourierNb 1.2425e-07 0.047043 0.00014579 2.3423e-07 v total_pressure -46817 2.9011e+05 1.2172e+05 1.1165e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0638 0.099891 0.0028435 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2163e-07 0.052294 0.00031321 5.1467e-06 INSTANT 0.875542000E-01 TIME STEP NUMBER 55740 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282654613E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.737335670E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.60082E-02 0.21020E+01 Friction velocity uk : 0.60082E-02 0.21020E+01 Dimensionless distance yplus : 0.59520E-02 0.20640E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 5.213345437e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29417E+08 1 0.17960E-09 0.23077E+02 0.18785E+04 c Velocity[X] 0.11681E+02 c Velocity[Y] 0.11396E+02 c Velocity[Z] 0.14313E-05 c Pressure 0.22134E-03 82 0.80273E-04 0.26568E-02 0.56055E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -19.97 31.31 5.6051 7.9957 v Velocity[Y] -22.111 23.384 -0.14349 -0.00073817 v Velocity[Z] -3.0261 2.9752 2.879e-06 -5.3869e-08 v ǁVelocityǁ 0.0013649 31.376 7.2461 8.0458 v Pressure -1.4617e+05 1.9082e+05 22303 11482 v TurbVisc 8.9349e-22 0.0092392 0.00014895 1.4943e-05 v CourantNb 3.3207e-08 0.011779 0.00016742 4.9126e-06 v FourierNb 1.2425e-07 0.047044 0.00014579 2.3439e-07 v total_pressure -44843 2.9214e+05 1.2363e+05 1.1281e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.064 0.099877 0.0028434 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2163e-07 0.052295 0.00031321 5.147e-06 INSTANT 0.875543000E-01 TIME STEP NUMBER 55741 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282656543E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.737529110E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15244E-01 0.21022E+01 Friction velocity uk : 0.15244E-01 0.21022E+01 Dimensionless distance yplus : 0.15102E-01 0.20641E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 4.646190835e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29418E+08 1 0.17959E-09 0.23089E+02 0.18790E+04 c Velocity[X] 0.11688E+02 c Velocity[Y] 0.11401E+02 c Velocity[Z] 0.14352E-05 c Pressure 0.21888E-03 10 0.61009E-04 0.26255E-02 0.44527E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -19.98 31.327 5.6052 7.9957 v Velocity[Y] -22.123 23.396 -0.1435 -0.00073855 v Velocity[Z] -3.026 2.9754 2.8782e-06 -5.3869e-08 v ǁVelocityǁ 0.0013316 31.392 7.2477 8.046 v Pressure -1.4423e+05 1.928e+05 24163 12442 v TurbVisc 3.2311e-21 0.0092585 0.000149 1.4967e-05 v CourantNb 3.3099e-08 0.011779 0.00016742 4.9127e-06 v FourierNb 1.2425e-07 0.047046 0.00014579 2.3456e-07 v total_pressure -42906 2.9412e+05 1.2549e+05 1.1377e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0641 0.099864 0.0028432 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2164e-07 0.052297 0.00031321 5.1472e-06 INSTANT 0.875544000E-01 TIME STEP NUMBER 55742 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282658704E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.737733720E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.18557E-01 0.21023E+01 Friction velocity uk : 0.18557E-01 0.21023E+01 Dimensionless distance yplus : 0.18001E-01 0.20643E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 3.988653998e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29418E+08 1 0.17957E-09 0.23099E+02 0.18793E+04 c Velocity[X] 0.11696E+02 c Velocity[Y] 0.11403E+02 c Velocity[Z] 0.14380E-05 c Pressure 0.21760E-03 101 0.76297E-04 0.26085E-02 0.53464E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -19.99 31.343 5.6052 7.9958 v Velocity[Y] -22.135 23.408 -0.1435 -0.00074047 v Velocity[Z] -3.0259 2.9756 2.8774e-06 -5.3869e-08 v ǁVelocityǁ 0.0013029 31.409 7.2492 8.0461 v Pressure -1.4227e+05 1.9482e+05 26029 13550 v TurbVisc 3.0448e-21 0.0092778 0.00014906 1.4991e-05 v CourantNb 3.2732e-08 0.011779 0.00016742 4.9128e-06 v FourierNb 1.2425e-07 0.047047 0.00014579 2.3472e-07 v total_pressure -40948 2.9614e+05 1.2735e+05 1.1487e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0643 0.099853 0.002843 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2164e-07 0.052298 0.00031322 5.1475e-06 INSTANT 0.875545000E-01 TIME STEP NUMBER 55743 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282660949E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.737951778E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.18289E-01 0.21025E+01 Friction velocity uk : 0.18289E-01 0.21025E+01 Dimensionless distance yplus : 0.17741E-01 0.20644E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 3.590677308e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29418E+08 1 0.17956E-09 0.23111E+02 0.18798E+04 c Velocity[X] 0.11705E+02 c Velocity[Y] 0.11406E+02 c Velocity[Z] 0.14370E-05 c Pressure 0.21607E-03 30 0.82221E-04 0.25884E-02 0.52090E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -20.001 31.359 5.6053 7.9958 v Velocity[Y] -22.147 23.42 -0.14351 -0.00074057 v Velocity[Z] -3.0257 2.9758 2.8765e-06 -5.3869e-08 v ǁVelocityǁ 0.0012654 31.426 7.2508 8.0463 v Pressure -1.4036e+05 1.9677e+05 27921 14702 v TurbVisc 2.4499e-21 0.0092972 0.00014911 1.5016e-05 v CourantNb 3.2858e-08 0.011778 0.00016742 4.9128e-06 v FourierNb 1.2425e-07 0.047048 0.00014579 2.3489e-07 v total_pressure -39030 2.981e+05 1.2925e+05 1.1603e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0644 0.099838 0.0028428 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2165e-07 0.0523 0.00031322 5.1477e-06 INSTANT 0.875546000E-01 TIME STEP NUMBER 55744 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282663327E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.738170972E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.18053E-01 0.21026E+01 Friction velocity uk : 0.18053E-01 0.21026E+01 Dimensionless distance yplus : 0.17512E-01 0.20646E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 2.884889778e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29418E+08 1 0.17955E-09 0.23124E+02 0.18802E+04 c Velocity[X] 0.11713E+02 c Velocity[Y] 0.11411E+02 c Velocity[Z] 0.14373E-05 c Pressure 0.21448E-03 231 0.95027E-04 0.25677E-02 0.42112E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -20.011 31.376 5.6053 7.9959 v Velocity[Y] -22.159 23.433 -0.14351 -0.00074298 v Velocity[Z] -3.0256 2.9761 2.8757e-06 -5.3869e-08 v ǁVelocityǁ 0.0012248 31.442 7.2523 8.0464 v Pressure -1.3846e+05 1.9871e+05 29732 15613 v TurbVisc 2.689e-21 0.0093165 0.00014917 1.504e-05 v CourantNb 3.2691e-08 0.011778 0.00016743 4.9129e-06 v FourierNb 1.2425e-07 0.047049 0.00014579 2.3506e-07 v total_pressure -37135 3.0003e+05 1.3106e+05 1.1694e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0646 0.099824 0.0028425 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2166e-07 0.052302 0.00031322 5.148e-06 INSTANT 0.875547000E-01 TIME STEP NUMBER 55745 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282666018E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.738400356E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.17801E-01 0.21028E+01 Friction velocity uk : 0.17801E-01 0.21028E+01 Dimensionless distance yplus : 0.17268E-01 0.20648E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 2.295820227e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29418E+08 1 0.17954E-09 0.23131E+02 0.18804E+04 c Velocity[X] 0.11722E+02 c Velocity[Y] 0.11409E+02 c Velocity[Z] 0.14404E-05 c Pressure 0.21275E-03 142 0.80837E-04 0.25453E-02 0.46763E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -20.021 31.392 5.6053 7.9959 v Velocity[Y] -22.171 23.445 -0.14352 -0.000744 v Velocity[Z] -3.0254 2.9763 2.8748e-06 -5.3869e-08 v ǁVelocityǁ 0.0011831 31.459 7.2538 8.0466 v Pressure -1.3658e+05 2.0064e+05 31562 16729 v TurbVisc 6.3057e-22 0.0093358 0.00014922 1.5064e-05 v CourantNb 3.2528e-08 0.011778 0.00016743 4.913e-06 v FourierNb 1.2425e-07 0.04705 0.00014579 2.3523e-07 v total_pressure -35257 3.0196e+05 1.3289e+05 1.1805e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0648 0.09981 0.0028422 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2166e-07 0.052303 0.00031322 5.1482e-06 INSTANT 0.875548000E-01 TIME STEP NUMBER 55746 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282668770E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.738642840E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.17627E-01 0.21029E+01 Friction velocity uk : 0.17627E-01 0.21029E+01 Dimensionless distance yplus : 0.17099E-01 0.20649E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.784474257e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29419E+08 1 0.17953E-09 0.23147E+02 0.18810E+04 c Velocity[X] 0.11732E+02 c Velocity[Y] 0.11415E+02 c Velocity[Z] 0.14464E-05 c Pressure 0.20969E-03 10 0.60857E-04 0.25070E-02 0.36798E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -20.032 31.409 5.6054 7.996 v Velocity[Y] -22.183 23.458 -0.14352 -0.00074439 v Velocity[Z] -3.0253 2.9765 2.874e-06 -5.3869e-08 v ǁVelocityǁ 0.0011393 31.476 7.2554 8.0467 v Pressure -1.3475e+05 2.0251e+05 33349 17650 v TurbVisc 2.5822e-21 0.0093552 0.00014928 1.5089e-05 v CourantNb 3.236e-08 0.011778 0.00016743 4.9131e-06 v FourierNb 1.2425e-07 0.047051 0.00014579 2.354e-07 v total_pressure -33423 3.0384e+05 1.3467e+05 1.1898e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0649 0.099797 0.0028419 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2167e-07 0.052305 0.00031322 5.1485e-06 INSTANT 0.875549000E-01 TIME STEP NUMBER 55747 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282671744E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.738897357E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.17737E-01 0.21031E+01 Friction velocity uk : 0.17737E-01 0.21031E+01 Dimensionless distance yplus : 0.17205E-01 0.20650E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.213545500e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29419E+08 1 0.17951E-09 0.23159E+02 0.18815E+04 c Velocity[X] 0.11742E+02 c Velocity[Y] 0.11418E+02 c Velocity[Z] 0.14522E-05 c Pressure 0.20795E-03 183 0.77011E-04 0.24844E-02 0.44038E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -20.042 31.426 5.6054 7.9961 v Velocity[Y] -22.195 23.471 -0.14352 -0.00074636 v Velocity[Z] -3.0252 2.9767 2.8732e-06 -5.3869e-08 v ǁVelocityǁ 0.0011046 31.492 7.2569 8.0469 v Pressure -1.329e+05 2.0442e+05 35122 18705 v TurbVisc 2.9982e-21 0.0093745 0.00014933 1.5113e-05 v CourantNb 2.93e-08 0.011778 0.00016743 4.9132e-06 v FourierNb 1.2425e-07 0.047052 0.00014579 2.3556e-07 v total_pressure -31575 3.0574e+05 1.3645e+05 1.2003e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.065 0.099785 0.0028417 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2167e-07 0.052306 0.00031323 5.1488e-06 INSTANT 0.875550000E-01 TIME STEP NUMBER 55748 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282674805E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.739165191E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.17775E-01 0.21032E+01 Friction velocity uk : 0.17775E-01 0.21032E+01 Dimensionless distance yplus : 0.17242E-01 0.20652E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 9.967048120e-03 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29419E+08 1 0.17950E-09 0.23175E+02 0.18821E+04 c Velocity[X] 0.11753E+02 c Velocity[Y] 0.11422E+02 c Velocity[Z] 0.14540E-05 c Pressure 0.20585E-03 29 0.83024E-04 0.24578E-02 0.43204E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -20.052 31.442 5.6054 7.9961 v Velocity[Y] -22.207 23.484 -0.14352 -0.00074647 v Velocity[Z] -3.025 2.9769 2.8723e-06 -5.3869e-08 v ǁVelocityǁ 0.0010672 31.509 7.2585 8.0471 v Pressure -1.311e+05 2.0627e+05 36924 19807 v TurbVisc 3.691e-24 0.0093938 0.00014939 1.5138e-05 v CourantNb 2.6172e-08 0.011778 0.00016744 4.9133e-06 v FourierNb 1.2425e-07 0.047053 0.00014579 2.3573e-07 v total_pressure -29778 3.0759e+05 1.3825e+05 1.2113e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0652 0.099771 0.0028414 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2168e-07 0.052307 0.00031323 5.149e-06 INSTANT 0.875551000E-01 TIME STEP NUMBER 55749 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282677987E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.739437160E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.16591E-01 0.21033E+01 Friction velocity uk : 0.16591E-01 0.21033E+01 Dimensionless distance yplus : 0.16029E-01 0.20653E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 4.643383135e-03 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29420E+08 1 0.17949E-09 0.23191E+02 0.18826E+04 c Velocity[X] 0.11763E+02 c Velocity[Y] 0.11428E+02 c Velocity[Z] 0.14588E-05 c Pressure 0.20379E-03 238 0.95648E-04 0.24315E-02 0.34856E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -20.063 31.459 5.6055 7.9962 v Velocity[Y] -22.219 23.497 -0.14352 -0.00074893 v Velocity[Z] -3.0249 2.9772 2.8715e-06 -5.3869e-08 v ǁVelocityǁ 0.0010323 31.526 7.26 8.0472 v Pressure -1.2933e+05 2.0809e+05 38642 20670 v TurbVisc 3.2376e-22 0.0094132 0.00014944 1.5163e-05 v CourantNb 2.3381e-08 0.011778 0.00016744 4.9134e-06 v FourierNb 1.2425e-07 0.047054 0.00014579 2.3591e-07 v total_pressure -28007 3.0941e+05 1.3997e+05 1.2199e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0653 0.09976 0.0028411 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2169e-07 0.052309 0.00031323 5.1493e-06 INSTANT 0.875552000E-01 TIME STEP NUMBER 55750 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282681470E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.739718494E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13353E-01 0.21035E+01 Friction velocity uk : 0.13353E-01 0.21035E+01 Dimensionless distance yplus : 0.12901E-01 0.20654E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.230675775e-03 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29420E+08 1 0.17948E-09 0.23201E+02 0.18830E+04 c Velocity[X] 0.11774E+02 c Velocity[Y] 0.11427E+02 c Velocity[Z] 0.14641E-05 c Pressure 0.20161E-03 274 0.81461E-04 0.24039E-02 0.38435E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -20.073 31.476 5.6055 7.9963 v Velocity[Y] -22.232 23.509 -0.14352 -0.00075002 v Velocity[Z] -3.0247 2.9774 2.8706e-06 -5.3869e-08 v ǁVelocityǁ 0.001001 31.543 7.2616 8.0474 v Pressure -1.2759e+05 2.0989e+05 40370 21725 v TurbVisc 7.0151e-22 0.0094325 0.0001495 1.5187e-05 v CourantNb 2.3081e-08 0.011778 0.00016744 4.9135e-06 v FourierNb 1.2425e-07 0.047055 0.00014579 2.3608e-07 v total_pressure -26263 3.1122e+05 1.417e+05 1.2305e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0654 0.099749 0.0028408 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.217e-07 0.05231 0.00031323 5.1495e-06 INSTANT 0.875553000E-01 TIME STEP NUMBER 55751 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282685003E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.740012472E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10322E-01 0.21036E+01 Friction velocity uk : 0.10322E-01 0.21036E+01 Dimensionless distance yplus : 0.99725E-02 0.20655E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.334273976e-03 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29420E+08 1 0.17947E-09 0.23220E+02 0.18837E+04 c Velocity[X] 0.11785E+02 c Velocity[Y] 0.11434E+02 c Velocity[Z] 0.14726E-05 c Pressure 0.19801E-03 10 0.60778E-04 0.23594E-02 0.30445E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -20.084 31.493 5.6055 7.9963 v Velocity[Y] -22.244 23.522 -0.14352 -0.00075039 v Velocity[Z] -3.0246 2.9776 2.8698e-06 -5.3869e-08 v ǁVelocityǁ 0.00097188 31.56 7.2631 8.0476 v Pressure -1.2589e+05 2.1166e+05 42061 22604 v TurbVisc 1.6996e-21 0.0094519 0.00014956 1.5212e-05 v CourantNb 2.3256e-08 0.011778 0.00016744 4.9135e-06 v FourierNb 1.2425e-07 0.047055 0.00014579 2.3625e-07 v total_pressure -24567 3.1298e+05 1.4339e+05 1.2393e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0655 0.099738 0.0028405 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.217e-07 0.052311 0.00031324 5.1498e-06 INSTANT 0.875554000E-01 TIME STEP NUMBER 55752 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282688756E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.740317814E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11154E-01 0.21036E+01 Friction velocity uk : 0.11154E-01 0.21036E+01 Dimensionless distance yplus : 0.10776E-01 0.20656E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -4.070989369e-03 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29421E+08 1 0.17946E-09 0.23235E+02 0.18843E+04 c Velocity[X] 0.11797E+02 c Velocity[Y] 0.11438E+02 c Velocity[Z] 0.14816E-05 c Pressure 0.19592E-03 185 0.77165E-04 0.23329E-02 0.36381E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -20.094 31.51 5.6056 7.9964 v Velocity[Y] -22.256 23.536 -0.14352 -0.00075239 v Velocity[Z] -3.0244 2.9778 2.869e-06 -5.3869e-08 v ǁVelocityǁ 0.00095281 31.577 7.2647 8.0478 v Pressure -1.2419e+05 2.1344e+05 43714 23594 v TurbVisc 2.1857e-21 0.0094712 0.00014962 1.5237e-05 v CourantNb 2.3025e-08 0.011777 0.00016744 4.9136e-06 v FourierNb 1.2425e-07 0.047056 0.00014579 2.3642e-07 v total_pressure -22865 3.1477e+05 1.4504e+05 1.2492e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0656 0.099731 0.0028403 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2171e-07 0.052311 0.00031324 5.1501e-06 INSTANT 0.875555000E-01 TIME STEP NUMBER 55753 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282692587E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.740634577E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.14439E-01 0.21037E+01 Friction velocity uk : 0.14439E-01 0.21037E+01 Dimensionless distance yplus : 0.13950E-01 0.20657E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -3.708076718e-03 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29421E+08 1 0.17945E-09 0.23254E+02 0.18850E+04 c Velocity[X] 0.11810E+02 c Velocity[Y] 0.11443E+02 c Velocity[Z] 0.14876E-05 c Pressure 0.19336E-03 29 0.83332E-04 0.23008E-02 0.35259E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -20.105 31.527 5.6056 7.9965 v Velocity[Y] -22.268 23.549 -0.14352 -0.00075253 v Velocity[Z] -3.0243 2.9781 2.8681e-06 -5.387e-08 v ǁVelocityǁ 0.00093413 31.595 7.2662 8.048 v Pressure -1.2254e+05 2.1516e+05 45400 24616 v TurbVisc 2.0541e-21 0.0094905 0.00014967 1.5262e-05 v CourantNb 2.5166e-08 0.011777 0.00016745 4.9137e-06 v FourierNb 1.2425e-07 0.047056 0.00014579 2.3659e-07 v total_pressure -21219 3.1649e+05 1.4673e+05 1.2594e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0657 0.099722 0.0028401 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2172e-07 0.052312 0.00031324 5.1503e-06 INSTANT 0.875556000E-01 TIME STEP NUMBER 55754 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282696518E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.740957844E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.17879E-01 0.21038E+01 Friction velocity uk : 0.17879E-01 0.21038E+01 Dimensionless distance yplus : 0.17274E-01 0.20657E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -5.635375404e-03 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29421E+08 1 0.17944E-09 0.23272E+02 0.18856E+04 c Velocity[X] 0.11822E+02 c Velocity[Y] 0.11450E+02 c Velocity[Z] 0.14937E-05 c Pressure 0.19092E-03 229 0.96079E-04 0.22703E-02 0.28956E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -20.115 31.544 5.6056 7.9966 v Velocity[Y] -22.281 23.562 -0.14351 -0.00075502 v Velocity[Z] -3.0242 2.9783 2.8673e-06 -5.387e-08 v ǁVelocityǁ 0.00091906 31.612 7.2678 8.0481 v Pressure -1.2093e+05 2.1687e+05 47000 25422 v TurbVisc 2.2793e-21 0.0095099 0.00014973 1.5287e-05 v CourantNb 2.7998e-08 0.011777 0.00016745 4.9138e-06 v FourierNb 1.2425e-07 0.047057 0.00014579 2.3676e-07 v total_pressure -19605 3.1819e+05 1.4833e+05 1.2675e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0657 0.099715 0.0028399 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2173e-07 0.052312 0.00031324 5.1506e-06 INSTANT 0.875557000E-01 TIME STEP NUMBER 55755 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282700749E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.741288526E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.20995E-01 0.21038E+01 Friction velocity uk : 0.20995E-01 0.21038E+01 Dimensionless distance yplus : 0.20284E-01 0.20658E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -5.887451139e-03 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29422E+08 1 0.17943E-09 0.23285E+02 0.18861E+04 c Velocity[X] 0.11835E+02 c Velocity[Y] 0.11450E+02 c Velocity[Z] 0.15023E-05 c Pressure 0.18837E-03 435 0.81436E-04 0.22384E-02 0.32530E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -20.126 31.561 5.6056 7.9966 v Velocity[Y] -22.293 23.575 -0.14351 -0.00075612 v Velocity[Z] -3.024 2.9785 2.8664e-06 -5.387e-08 v ǁVelocityǁ 0.00090791 31.629 7.2693 8.0483 v Pressure -1.1934e+05 2.1856e+05 48615 26435 v TurbVisc 6.8576e-22 0.0095292 0.00014979 1.5312e-05 v CourantNb 3.0923e-08 0.011777 0.00016745 4.9139e-06 v FourierNb 1.2425e-07 0.047057 0.00014579 2.3694e-07 v total_pressure -18016 3.1989e+05 1.4994e+05 1.2776e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0658 0.099709 0.0028397 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2174e-07 0.052313 0.00031325 5.1509e-06 INSTANT 0.875558000E-01 TIME STEP NUMBER 55756 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282705024E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.741631767E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.22621E-01 0.21039E+01 Friction velocity uk : 0.22621E-01 0.21039E+01 Dimensionless distance yplus : 0.21943E-01 0.20658E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -5.409308713e-03 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29422E+08 1 0.17942E-09 0.23306E+02 0.18869E+04 c Velocity[X] 0.11847E+02 c Velocity[Y] 0.11459E+02 c Velocity[Z] 0.15124E-05 c Pressure 0.18433E-03 10 0.59616E-04 0.21889E-02 0.23270E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -20.136 31.579 5.6057 7.9967 v Velocity[Y] -22.305 23.588 -0.1435 -0.00075656 v Velocity[Z] -3.0239 2.9787 2.8656e-06 -5.387e-08 v ǁVelocityǁ 0.0008994 31.647 7.2709 8.0485 v Pressure -1.1781e+05 2.2019e+05 50162 27189 v TurbVisc 3.2622e-21 0.0095486 0.00014985 1.5337e-05 v CourantNb 3.4117e-08 0.011777 0.00016745 4.914e-06 v FourierNb 1.2425e-07 0.047057 0.00014579 2.3711e-07 v total_pressure -16489 3.2152e+05 1.5149e+05 1.2851e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0658 0.099704 0.0028396 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2175e-07 0.052313 0.00031325 5.1511e-06 INSTANT 0.875559000E-01 TIME STEP NUMBER 55757 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282709469E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.741985196E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.22187E-01 0.21039E+01 Friction velocity uk : 0.22187E-01 0.21039E+01 Dimensionless distance yplus : 0.21522E-01 0.20658E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -4.274196980e-03 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29422E+08 1 0.17941E-09 0.23324E+02 0.18876E+04 c Velocity[X] 0.11861E+02 c Velocity[Y] 0.11463E+02 c Velocity[Z] 0.15231E-05 c Pressure 0.18190E-03 256 0.77342E-04 0.21586E-02 0.30564E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -20.147 31.596 5.6057 7.9968 v Velocity[Y] -22.318 23.602 -0.1435 -0.00075862 v Velocity[Z] -3.0237 2.9789 2.8648e-06 -5.387e-08 v ǁVelocityǁ 0.000898 31.664 7.2724 8.0487 v Pressure -1.1627e+05 2.2186e+05 51684 28129 v TurbVisc 2.3508e-21 0.0095679 0.00014991 1.5363e-05 v CourantNb 3.7528e-08 0.011777 0.00016746 4.9141e-06 v FourierNb 1.2425e-07 0.047057 0.0001458 2.3728e-07 v total_pressure -14949 3.2319e+05 1.5301e+05 1.2945e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0658 0.099701 0.0028395 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2176e-07 0.052313 0.00031325 5.1514e-06 INSTANT 0.875560000E-01 TIME STEP NUMBER 55758 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282714029E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.742349865E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.21776E-01 0.21039E+01 Friction velocity uk : 0.21776E-01 0.21039E+01 Dimensionless distance yplus : 0.21124E-01 0.20659E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.910263676e-03 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29423E+08 1 0.17940E-09 0.23345E+02 0.18883E+04 c Velocity[X] 0.11875E+02 c Velocity[Y] 0.11470E+02 c Velocity[Z] 0.15300E-05 c Pressure 0.17898E-03 35 0.82990E-04 0.21224E-02 0.29234E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -20.157 31.614 5.6057 7.9969 v Velocity[Y] -22.33 23.615 -0.14349 -0.00075881 v Velocity[Z] -3.0236 2.9792 2.8639e-06 -5.387e-08 v ǁVelocityǁ 0.00089714 31.682 7.274 8.0489 v Pressure -1.1479e+05 2.2347e+05 53234 29070 v TurbVisc 1.5635e-22 0.0095873 0.00014997 1.5388e-05 v CourantNb 4.1666e-08 0.011777 0.00016746 4.9142e-06 v FourierNb 1.2425e-07 0.047057 0.0001458 2.3746e-07 v total_pressure -13470 3.248e+05 1.5456e+05 1.304e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0659 0.099697 0.0028394 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2177e-07 0.052313 0.00031325 5.1517e-06 INSTANT 0.875561000E-01 TIME STEP NUMBER 55759 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282718657E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.742721816E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.21525E-01 0.21039E+01 Friction velocity uk : 0.21525E-01 0.21039E+01 Dimensionless distance yplus : 0.20880E-01 0.20659E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -4.526595539e-04 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29423E+08 1 0.17940E-09 0.23366E+02 0.18891E+04 c Velocity[X] 0.11888E+02 c Velocity[Y] 0.11477E+02 c Velocity[Z] 0.15397E-05 c Pressure 0.17622E-03 233 0.95717E-04 0.20884E-02 0.23945E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -20.168 31.631 5.6057 7.997 v Velocity[Y] -22.343 23.628 -0.14349 -0.00076137 v Velocity[Z] -3.0234 2.9794 2.8631e-06 -5.387e-08 v ǁVelocityǁ 0.00089889 31.699 7.2755 8.0491 v Pressure -1.1335e+05 2.2506e+05 54695 29800 v TurbVisc 1.4446e-21 0.0096066 0.00015003 1.5413e-05 v CourantNb 4.5746e-08 0.011777 0.00016746 4.9143e-06 v FourierNb 1.2425e-07 0.047056 0.0001458 2.3763e-07 v total_pressure -12021 3.2638e+05 1.5602e+05 1.3113e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0659 0.099694 0.0028393 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2178e-07 0.052313 0.00031326 5.152e-06 INSTANT 0.875562000E-01 TIME STEP NUMBER 55760 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282723569E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.743099944E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.21378E-01 0.21039E+01 Friction velocity uk : 0.21378E-01 0.21039E+01 Dimensionless distance yplus : 0.20737E-01 0.20659E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 2.206066086e-03 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29424E+08 1 0.17939E-09 0.23380E+02 0.18896E+04 c Velocity[X] 0.11902E+02 c Velocity[Y] 0.11478E+02 c Velocity[Z] 0.15495E-05 c Pressure 0.17339E-03 443 0.81411E-04 0.20534E-02 0.25814E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -20.179 31.649 5.6058 7.9971 v Velocity[Y] -22.355 23.642 -0.14348 -0.00076271 v Velocity[Z] -3.0233 2.9796 2.8623e-06 -5.387e-08 v ǁVelocityǁ 0.0009031 31.717 7.2771 8.0493 v Pressure -1.1193e+05 2.2663e+05 56150 30689 v TurbVisc 7.857e-22 0.009626 0.00015009 1.5439e-05 v CourantNb 5.0111e-08 0.011777 0.00016746 4.9144e-06 v FourierNb 1.2425e-07 0.047056 0.0001458 2.3781e-07 v total_pressure -10608 3.2795e+05 1.5747e+05 1.3201e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0659 0.099692 0.0028393 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2179e-07 0.052313 0.00031326 5.1522e-06 INSTANT 0.875563000E-01 TIME STEP NUMBER 55761 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282728500E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.743489579E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.21347E-01 0.21039E+01 Friction velocity uk : 0.21347E-01 0.21039E+01 Dimensionless distance yplus : 0.20708E-01 0.20659E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 5.378365906e-03 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29424E+08 1 0.17938E-09 0.23404E+02 0.18905E+04 c Velocity[X] 0.11916E+02 c Velocity[Y] 0.11487E+02 c Velocity[Z] 0.15603E-05 c Pressure 0.16892E-03 10 0.58928E-04 0.19991E-02 0.20640E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -20.19 31.667 5.6058 7.9972 v Velocity[Y] -22.368 23.655 -0.14348 -0.00076301 v Velocity[Z] -3.0232 2.9798 2.8614e-06 -5.387e-08 v ǁVelocityǁ 0.00090852 31.735 7.2787 8.0495 v Pressure -1.1057e+05 2.2816e+05 57570 31433 v TurbVisc 1.7635e-21 0.0096454 0.00015015 1.5464e-05 v CourantNb 5.1296e-08 0.011777 0.00016746 4.9145e-06 v FourierNb 1.2425e-07 0.047056 0.0001458 2.3798e-07 v total_pressure -9241.7 3.2949e+05 1.5889e+05 1.3276e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0659 0.09969 0.0028392 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.218e-07 0.052313 0.00031326 5.1525e-06 INSTANT 0.875564000E-01 TIME STEP NUMBER 55762 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282733611E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.743889397E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.21561E-01 0.21039E+01 Friction velocity uk : 0.21561E-01 0.21039E+01 Dimensionless distance yplus : 0.20914E-01 0.20658E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 9.166394755e-03 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29425E+08 1 0.17937E-09 0.23423E+02 0.18912E+04 c Velocity[X] 0.11931E+02 c Velocity[Y] 0.11492E+02 c Velocity[Z] 0.15716E-05 c Pressure 0.16629E-03 156 0.77089E-04 0.19666E-02 0.24595E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -20.2 31.684 5.6058 7.9973 v Velocity[Y] -22.38 23.669 -0.14347 -0.00076517 v Velocity[Z] -3.023 2.98 2.8606e-06 -5.387e-08 v ǁVelocityǁ 0.00091996 31.753 7.2802 8.0497 v Pressure -1.092e+05 2.297e+05 58932 32251 v TurbVisc 2.224e-21 0.0096647 0.00015021 1.549e-05 v CourantNb 5.0273e-08 0.011777 0.00016747 4.9146e-06 v FourierNb 1.2425e-07 0.047055 0.0001458 2.3816e-07 v total_pressure -7879.4 3.3103e+05 1.6026e+05 1.3358e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0658 0.099689 0.0028393 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2181e-07 0.052313 0.00031326 5.1528e-06 INSTANT 0.875565000E-01 TIME STEP NUMBER 55763 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282738813E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.744298662E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.21740E-01 0.21039E+01 Friction velocity uk : 0.21740E-01 0.21039E+01 Dimensionless distance yplus : 0.21088E-01 0.20658E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.314493508e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29425E+08 1 0.17937E-09 0.23446E+02 0.18921E+04 c Velocity[X] 0.11946E+02 c Velocity[Y] 0.11500E+02 c Velocity[Z] 0.15805E-05 c Pressure 0.16313E-03 70 0.82678E-04 0.19279E-02 0.24043E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -20.211 31.702 5.6059 7.9974 v Velocity[Y] -22.393 23.682 -0.14346 -0.00076543 v Velocity[Z] -3.0229 2.9803 2.8598e-06 -5.387e-08 v ǁVelocityǁ 0.00093043 31.771 7.2818 8.0499 v Pressure -1.079e+05 2.3119e+05 60319 33091 v TurbVisc 1.0512e-21 0.0096841 0.00015027 1.5516e-05 v CourantNb 4.9568e-08 0.011777 0.00016747 4.9147e-06 v FourierNb 1.2425e-07 0.047055 0.0001458 2.3834e-07 v total_pressure -6577 3.3252e+05 1.6164e+05 1.3442e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0658 0.099685 0.0028393 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2182e-07 0.052312 0.00031327 5.1531e-06 INSTANT 0.875566000E-01 TIME STEP NUMBER 55764 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282744066E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.744714235E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.22101E-01 0.21039E+01 Friction velocity uk : 0.22101E-01 0.21039E+01 Dimensionless distance yplus : 0.21439E-01 0.20658E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.689646340e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29426E+08 1 0.17936E-09 0.23468E+02 0.18929E+04 c Velocity[X] 0.11960E+02 c Velocity[Y] 0.11508E+02 c Velocity[Z] 0.15881E-05 c Pressure 0.16016E-03 192 0.95403E-04 0.18914E-02 0.19743E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -20.222 31.72 5.6059 7.9975 v Velocity[Y] -22.406 23.696 -0.14346 -0.00076807 v Velocity[Z] -3.0227 2.9805 2.8589e-06 -5.387e-08 v ǁVelocityǁ 0.00094182 31.789 7.2834 8.0501 v Pressure -1.0663e+05 2.3266e+05 61618 33730 v TurbVisc 1.6464e-21 0.0097034 0.00015033 1.5542e-05 v CourantNb 4.806e-08 0.011777 0.00016747 4.9149e-06 v FourierNb 1.2425e-07 0.047055 0.0001458 2.3852e-07 v total_pressure -5305.2 3.3398e+05 1.6294e+05 1.3505e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0658 0.099683 0.0028393 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2183e-07 0.052312 0.00031327 5.1534e-06 INSTANT 0.875567000E-01 TIME STEP NUMBER 55765 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282749586E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.745135643E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.22563E-01 0.21039E+01 Friction velocity uk : 0.22563E-01 0.21039E+01 Dimensionless distance yplus : 0.21887E-01 0.20658E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 2.128230240e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29426E+08 1 0.17936E-09 0.23484E+02 0.18935E+04 c Velocity[X] 0.11975E+02 c Velocity[Y] 0.11509E+02 c Velocity[Z] 0.15969E-05 c Pressure 0.15713E-03 131 0.81058E-04 0.18544E-02 0.21616E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -20.233 31.738 5.6059 7.9976 v Velocity[Y] -22.418 23.709 -0.14345 -0.00076931 v Velocity[Z] -3.0226 2.9807 2.8581e-06 -5.387e-08 v ǁVelocityǁ 0.00095375 31.808 7.2849 8.0504 v Pressure -1.0539e+05 2.3411e+05 62914 34540 v TurbVisc 7.971e-22 0.0097228 0.00015039 1.5567e-05 v CourantNb 4.6257e-08 0.011777 0.00016747 4.915e-06 v FourierNb 1.2425e-07 0.047055 0.0001458 2.3869e-07 v total_pressure -4069.9 3.3543e+05 1.6424e+05 1.3586e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0658 0.09968 0.0028393 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2184e-07 0.052312 0.00031327 5.1537e-06 INSTANT 0.875568000E-01 TIME STEP NUMBER 55766 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282755120E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.745567603E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.23121E-01 0.21039E+01 Friction velocity uk : 0.23121E-01 0.21039E+01 Dimensionless distance yplus : 0.22428E-01 0.20658E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 2.591926041e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29427E+08 1 0.17935E-09 0.23508E+02 0.18944E+04 c Velocity[X] 0.11989E+02 c Velocity[Y] 0.11519E+02 c Velocity[Z] 0.16164E-05 c Pressure 0.15233E-03 9 0.57621E-04 0.17965E-02 0.15834E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -20.244 31.756 5.606 7.9977 v Velocity[Y] -22.431 23.723 -0.14344 -0.00076989 v Velocity[Z] -3.0224 2.9809 2.8573e-06 -5.387e-08 v ǁVelocityǁ 0.00096788 31.826 7.2865 8.0506 v Pressure -1.0422e+05 2.3551e+05 64149 35154 v TurbVisc 1.4491e-21 0.0097422 0.00015045 1.5593e-05 v CourantNb 4.4131e-08 0.011776 0.00016748 4.9151e-06 v FourierNb 1.2425e-07 0.047054 0.0001458 2.3887e-07 v total_pressure -2892.6 3.3683e+05 1.6547e+05 1.3648e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0658 0.099675 0.0028394 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2185e-07 0.052312 0.00031328 5.1539e-06 INSTANT 0.875569000E-01 TIME STEP NUMBER 55767 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282760783E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.746008329E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.22749E-01 0.21039E+01 Friction velocity uk : 0.22749E-01 0.21039E+01 Dimensionless distance yplus : 0.22067E-01 0.20659E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 3.170254211e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29427E+08 1 0.17934E-09 0.23529E+02 0.18951E+04 c Velocity[X] 0.12004E+02 c Velocity[Y] 0.11525E+02 c Velocity[Z] 0.16214E-05 c Pressure 0.14955E-03 174 0.76332E-04 0.17625E-02 0.20528E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -20.255 31.775 5.606 7.9979 v Velocity[Y] -22.444 23.737 -0.14344 -0.00077215 v Velocity[Z] -3.0223 2.9811 2.8565e-06 -5.387e-08 v ǁVelocityǁ 0.00097861 31.844 7.2881 8.0508 v Pressure -1.0304e+05 2.3692e+05 65355 35891 v TurbVisc 1.157e-21 0.0097615 0.00015052 1.5619e-05 v CourantNb 4.1084e-08 0.011776 0.00016748 4.9152e-06 v FourierNb 1.2425e-07 0.047054 0.0001458 2.3905e-07 v total_pressure -1710.6 3.3825e+05 1.6668e+05 1.3722e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0659 0.099671 0.0028394 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2186e-07 0.052312 0.00031328 5.1542e-06 INSTANT 0.875570000E-01 TIME STEP NUMBER 55768 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282766566E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.746457688E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.22075E-01 0.21039E+01 Friction velocity uk : 0.22075E-01 0.21039E+01 Dimensionless distance yplus : 0.21414E-01 0.20659E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 3.546083638e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29428E+08 1 0.17934E-09 0.23552E+02 0.18960E+04 c Velocity[X] 0.12020E+02 c Velocity[Y] 0.11533E+02 c Velocity[Z] 0.16228E-05 c Pressure 0.14622E-03 396 0.81841E-04 0.17221E-02 0.20299E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -20.265 31.793 5.6061 7.998 v Velocity[Y] -22.456 23.75 -0.14343 -0.00077244 v Velocity[Z] -3.0221 2.9814 2.8556e-06 -5.387e-08 v ǁVelocityǁ 0.00098902 31.863 7.2897 8.051 v Pressure -1.0192e+05 2.3828e+05 66567 36643 v TurbVisc 3.6433e-21 0.0097809 0.00015058 1.5645e-05 v CourantNb 3.8625e-08 0.011776 0.00016748 4.9153e-06 v FourierNb 1.2425e-07 0.047054 0.0001458 2.3923e-07 v total_pressure -592.39 3.3961e+05 1.6789e+05 1.3797e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0659 0.099663 0.0028394 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2187e-07 0.052312 0.00031328 5.1545e-06 INSTANT 0.875571000E-01 TIME STEP NUMBER 55769 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282772361E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.746912493E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.21319E-01 0.21040E+01 Friction velocity uk : 0.21319E-01 0.21040E+01 Dimensionless distance yplus : 0.20680E-01 0.20659E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 4.064060522e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29428E+08 1 0.17934E-09 0.23575E+02 0.18969E+04 c Velocity[X] 0.12034E+02 c Velocity[Y] 0.11542E+02 c Velocity[Z] 0.16296E-05 c Pressure 0.14315E-03 230 0.94768E-04 0.16847E-02 0.15767E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -20.276 31.811 5.6061 7.9981 v Velocity[Y] -22.469 23.764 -0.14343 -0.00077528 v Velocity[Z] -3.022 2.9816 2.8548e-06 -5.387e-08 v ǁVelocityǁ 0.0009972 31.881 7.2913 8.0512 v Pressure -1.0085e+05 2.396e+05 67673 37154 v TurbVisc 1.7619e-21 0.0098002 0.00015064 1.5672e-05 v CourantNb 3.5587e-08 0.011776 0.00016749 4.9154e-06 v FourierNb 1.2425e-07 0.047054 0.0001458 2.3941e-07 v total_pressure 478.5 3.4093e+05 1.69e+05 1.3848e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0659 0.099655 0.0028395 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2189e-07 0.052313 0.00031329 5.1548e-06 INSTANT 0.875572000E-01 TIME STEP NUMBER 55770 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282778415E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.747371881E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.20536E-01 0.21041E+01 Friction velocity uk : 0.20536E-01 0.21041E+01 Dimensionless distance yplus : 0.19920E-01 0.20660E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 4.585962130e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29429E+08 1 0.17933E-09 0.23592E+02 0.18975E+04 c Velocity[X] 0.12049E+02 c Velocity[Y] 0.11544E+02 c Velocity[Z] 0.16365E-05 c Pressure 0.14001E-03 127 0.80273E-04 0.16466E-02 0.17352E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -20.287 31.83 5.6062 7.9982 v Velocity[Y] -22.482 23.778 -0.14342 -0.00077664 v Velocity[Z] -3.0219 2.9818 2.854e-06 -5.387e-08 v ǁVelocityǁ 0.001003 31.9 7.2929 8.0515 v Pressure -99806 2.409e+05 68786 37842 v TurbVisc 1.712e-21 0.0098196 0.00015071 1.5698e-05 v CourantNb 3.2405e-08 0.011776 0.00016749 4.9155e-06 v FourierNb 1.2425e-07 0.047054 0.0001458 2.3959e-07 v total_pressure 1519 3.4223e+05 1.7011e+05 1.3917e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.066 0.099644 0.0028394 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.219e-07 0.052313 0.00031329 5.1551e-06 INSTANT 0.875573000E-01 TIME STEP NUMBER 55771 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282784455E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.747841352E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19742E-01 0.21042E+01 Friction velocity uk : 0.19742E-01 0.21042E+01 Dimensionless distance yplus : 0.19150E-01 0.20661E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 5.079444756e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29429E+08 1 0.17933E-09 0.23617E+02 0.18984E+04 c Velocity[X] 0.12063E+02 c Velocity[Y] 0.11554E+02 c Velocity[Z] 0.16497E-05 c Pressure 0.13493E-03 9 0.56200E-04 0.15857E-02 0.12891E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -20.298 31.848 5.6063 7.9983 v Velocity[Y] -22.494 23.792 -0.14342 -0.00077734 v Velocity[Z] -3.0217 2.982 2.8531e-06 -5.387e-08 v ǁVelocityǁ 0.0010079 31.918 7.2945 8.0517 v Pressure -98825 2.4216e+05 69834 38372 v TurbVisc 1.2668e-21 0.009839 0.00015077 1.5724e-05 v CourantNb 3.1917e-08 0.011776 0.00016749 4.9156e-06 v FourierNb 1.2425e-07 0.047055 0.0001458 2.3977e-07 v total_pressure 2500.3 3.4348e+05 1.7116e+05 1.397e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0661 0.099631 0.0028394 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2191e-07 0.052314 0.00031329 5.1554e-06 INSTANT 0.875574000E-01 TIME STEP NUMBER 55772 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282790603E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.748317887E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.47705E-02 0.21043E+01 Friction velocity uk : 0.47705E-02 0.21043E+01 Dimensionless distance yplus : 0.47155E-02 0.20662E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 5.731349764e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29430E+08 1 0.17933E-09 0.23639E+02 0.18992E+04 c Velocity[X] 0.12078E+02 c Velocity[Y] 0.11560E+02 c Velocity[Z] 0.16541E-05 c Pressure 0.13211E-03 167 0.75872E-04 0.15515E-02 0.16576E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -20.309 31.867 5.6063 7.9985 v Velocity[Y] -22.507 23.806 -0.14342 -0.00077973 v Velocity[Z] -3.0216 2.9822 2.8523e-06 -5.387e-08 v ǁVelocityǁ 0.0010066 31.937 7.2961 8.0519 v Pressure -97849 2.434e+05 70857 38988 v TurbVisc 2.0946e-21 0.0098583 0.00015084 1.575e-05 v CourantNb 3.1932e-08 0.011776 0.00016749 4.9158e-06 v FourierNb 1.2425e-07 0.047055 0.0001458 2.3995e-07 v total_pressure 3475.6 3.4473e+05 1.7218e+05 1.4031e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0662 0.099614 0.0028394 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2192e-07 0.052315 0.00031329 5.1557e-06 INSTANT 0.875575000E-01 TIME STEP NUMBER 55773 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282796870E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.748802663E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.24252E-02 0.21044E+01 Friction velocity uk : 0.24252E-02 0.21044E+01 Dimensionless distance yplus : 0.23972E-02 0.20664E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 6.069196389e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29430E+08 1 0.17932E-09 0.23662E+02 0.19001E+04 c Velocity[X] 0.12094E+02 c Velocity[Y] 0.11568E+02 c Velocity[Z] 0.16538E-05 c Pressure 0.12877E-03 55 0.80911E-04 0.15112E-02 0.15600E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -20.32 31.885 5.6064 7.9986 v Velocity[Y] -22.52 23.82 -0.14341 -0.00078039 v Velocity[Z] -3.0214 2.9825 2.8515e-06 -5.387e-08 v ǁVelocityǁ 0.0010029 31.955 7.2977 8.0521 v Pressure -96948 2.4459e+05 71852 39570 v TurbVisc 1.6035e-21 0.0098777 0.0001509 1.5777e-05 v CourantNb 3.2061e-08 0.011776 0.0001675 4.9159e-06 v FourierNb 1.2425e-07 0.047056 0.0001458 2.4014e-07 v total_pressure 4376.5 3.4591e+05 1.7318e+05 1.409e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0664 0.099599 0.0028393 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2194e-07 0.052316 0.0003133 5.156e-06 INSTANT 0.875576000E-01 TIME STEP NUMBER 55774 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282803102E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.749290037E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.16629E-01 0.21046E+01 Friction velocity uk : 0.16629E-01 0.21046E+01 Dimensionless distance yplus : 0.16437E-01 0.20665E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 6.631921710e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29431E+08 1 0.17932E-09 0.23686E+02 0.19009E+04 c Velocity[X] 0.12108E+02 c Velocity[Y] 0.11578E+02 c Velocity[Z] 0.16605E-05 c Pressure 0.12564E-03 214 0.94017E-04 0.14735E-02 0.14221E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -20.331 31.904 5.6065 7.9987 v Velocity[Y] -22.532 23.834 -0.14341 -0.00078313 v Velocity[Z] -3.0213 2.9827 2.8507e-06 -5.387e-08 v ǁVelocityǁ 0.00099534 31.974 7.2993 8.0524 v Pressure -96072 2.4574e+05 72792 40065 v TurbVisc 1.0384e-21 0.0098971 0.00015097 1.5803e-05 v CourantNb 3.2026e-08 0.011776 0.0001675 4.916e-06 v FourierNb 1.2425e-07 0.047057 0.0001458 2.4032e-07 v total_pressure 5252.5 3.4707e+05 1.7412e+05 1.4139e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0665 0.099589 0.0028392 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2195e-07 0.052318 0.0003133 5.1563e-06 INSTANT 0.875577000E-01 TIME STEP NUMBER 55775 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282809616E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.749783371E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.17588E-01 0.21048E+01 Friction velocity uk : 0.17588E-01 0.21048E+01 Dimensionless distance yplus : 0.17061E-01 0.20667E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 7.144863422e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29432E+08 1 0.17932E-09 0.23703E+02 0.19015E+04 c Velocity[X] 0.12123E+02 c Velocity[Y] 0.11580E+02 c Velocity[Z] 0.16642E-05 c Pressure 0.12260E-03 493 0.79715E-04 0.14367E-02 0.13142E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -20.343 31.922 5.6066 7.9988 v Velocity[Y] -22.545 23.848 -0.14341 -0.00078485 v Velocity[Z] -3.0211 2.9829 2.8498e-06 -5.387e-08 v ǁVelocityǁ 0.00093647 31.993 7.3009 8.0526 v Pressure -95258 2.4685e+05 73689 40598 v TurbVisc 1.0228e-21 0.0099164 0.00015103 1.583e-05 v CourantNb 3.201e-08 0.011776 0.0001675 4.9161e-06 v FourierNb 1.2425e-07 0.047058 0.0001458 2.405e-07 v total_pressure 6067.2 3.4818e+05 1.7501e+05 1.4192e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0667 0.099576 0.0028391 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2196e-07 0.052319 0.0003133 5.1566e-06 INSTANT 0.875578000E-01 TIME STEP NUMBER 55776 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282816069E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.750282998E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.17643E-01 0.21050E+01 Friction velocity uk : 0.17643E-01 0.21050E+01 Dimensionless distance yplus : 0.17114E-01 0.20670E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 7.655877583e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29432E+08 1 0.17932E-09 0.23728E+02 0.19024E+04 c Velocity[X] 0.12137E+02 c Velocity[Y] 0.11590E+02 c Velocity[Z] 0.16717E-05 c Pressure 0.11732E-03 9 0.54917E-04 0.13740E-02 0.10400E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -20.354 31.941 5.6067 7.999 v Velocity[Y] -22.558 23.862 -0.14341 -0.00078546 v Velocity[Z] -3.021 2.9831 2.849e-06 -5.387e-08 v ǁVelocityǁ 0.00084217 32.011 7.3025 8.0529 v Pressure -94493 2.4792e+05 74540 41040 v TurbVisc 1.1019e-21 0.0099358 0.0001511 1.5857e-05 v CourantNb 3.1987e-08 0.011775 0.00016751 4.9162e-06 v FourierNb 1.2425e-07 0.04706 0.0001458 2.4069e-07 v total_pressure 6832.3 3.4924e+05 1.7587e+05 1.4237e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.067 0.099559 0.002839 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2198e-07 0.052321 0.00031331 5.1569e-06 INSTANT 0.875579000E-01 TIME STEP NUMBER 55777 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282822618E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.750789248E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.18072E-01 0.21053E+01 Friction velocity uk : 0.18072E-01 0.21053E+01 Dimensionless distance yplus : 0.17530E-01 0.20672E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 8.304197988e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29433E+08 1 0.17932E-09 0.23749E+02 0.19032E+04 c Velocity[X] 0.12152E+02 c Velocity[Y] 0.11597E+02 c Velocity[Z] 0.16743E-05 c Pressure 0.11470E-03 154 0.75598E-04 0.13423E-02 0.12926E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -20.365 31.959 5.6068 7.9991 v Velocity[Y] -22.571 23.877 -0.14341 -0.00078803 v Velocity[Z] -3.0208 2.9833 2.8482e-06 -5.387e-08 v ǁVelocityǁ 0.0007592 32.03 7.3041 8.0531 v Pressure -93749 2.4896e+05 75354 41510 v TurbVisc 1.2133e-21 0.0099552 0.00015116 1.5883e-05 v CourantNb 3.1839e-08 0.011775 0.00016751 4.9164e-06 v FourierNb 1.2425e-07 0.047061 0.0001458 2.4087e-07 v total_pressure 7575.5 3.5028e+05 1.7668e+05 1.4284e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0672 0.099538 0.0028388 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2199e-07 0.052324 0.00031331 5.1572e-06 INSTANT 0.875580000E-01 TIME STEP NUMBER 55778 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282829280E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.751302167E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.17454E-01 0.21056E+01 Friction velocity uk : 0.17454E-01 0.21056E+01 Dimensionless distance yplus : 0.16788E-01 0.20675E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 8.584919822e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29433E+08 1 0.17932E-09 0.23772E+02 0.19041E+04 c Velocity[X] 0.12167E+02 c Velocity[Y] 0.11606E+02 c Velocity[Z] 0.16772E-05 c Pressure 0.11152E-03 54 0.80832E-04 0.13042E-02 0.12629E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -20.376 31.978 5.6069 7.9992 v Velocity[Y] -22.584 23.891 -0.14341 -0.00078885 v Velocity[Z] -3.0207 2.9835 2.8474e-06 -5.387e-08 v ǁVelocityǁ 0.00068102 32.049 7.3058 8.0533 v Pressure -93079 2.4992e+05 76134 41969 v TurbVisc 1.3028e-21 0.0099745 0.00015123 1.591e-05 v CourantNb 3.1914e-08 0.011775 0.00016751 4.9165e-06 v FourierNb 1.2425e-07 0.047063 0.0001458 2.4106e-07 v total_pressure 8245.5 3.5125e+05 1.7746e+05 1.4329e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0675 0.099514 0.0028386 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.22e-07 0.052326 0.00031331 5.1575e-06 INSTANT 0.875581000E-01 TIME STEP NUMBER 55779 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282835879E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.751816281E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.14454E-01 0.21059E+01 Friction velocity uk : 0.14454E-01 0.21059E+01 Dimensionless distance yplus : 0.13902E-01 0.20678E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 9.155955079e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29434E+08 1 0.17932E-09 0.23795E+02 0.19049E+04 c Velocity[X] 0.12180E+02 c Velocity[Y] 0.11615E+02 c Velocity[Z] 0.16821E-05 c Pressure 0.10865E-03 231 0.93779E-04 0.12697E-02 0.11973E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -20.387 31.997 5.607 7.9994 v Velocity[Y] -22.597 23.905 -0.14341 -0.00079174 v Velocity[Z] -3.0205 2.9838 2.8465e-06 -5.387e-08 v ǁVelocityǁ 0.00061343 32.068 7.3074 8.0536 v Pressure -92436 2.5086e+05 76867 42362 v TurbVisc 9.9394e-22 0.0099939 0.0001513 1.5937e-05 v CourantNb 3.2867e-08 0.011775 0.00016752 4.9166e-06 v FourierNb 1.2425e-07 0.047065 0.0001458 2.4124e-07 v total_pressure 8889 3.5219e+05 1.7819e+05 1.4369e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0678 0.099487 0.0028383 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2202e-07 0.052329 0.00031331 5.1579e-06 INSTANT 0.875582000E-01 TIME STEP NUMBER 55780 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282842739E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.752335805E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10426E-01 0.21063E+01 Friction velocity uk : 0.10426E-01 0.21063E+01 Dimensionless distance yplus : 0.10028E-01 0.20682E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 9.656892123e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29435E+08 1 0.17932E-09 0.23812E+02 0.19055E+04 c Velocity[X] 0.12194E+02 c Velocity[Y] 0.11618E+02 c Velocity[Z] 0.16846E-05 c Pressure 0.10595E-03 84 0.79425E-04 0.12373E-02 0.99945E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -20.399 32.015 5.6071 7.9995 v Velocity[Y] -22.61 23.92 -0.14341 -0.0007934 v Velocity[Z] -3.0204 2.984 2.8457e-06 -5.387e-08 v ǁVelocityǁ 0.0005701 32.086 7.309 8.0538 v Pressure -91866 2.5174e+05 77548 42762 v TurbVisc 1.0161e-21 0.010013 0.00015136 1.5964e-05 v CourantNb 3.6628e-08 0.011775 0.00016752 4.9167e-06 v FourierNb 1.2425e-07 0.047068 0.0001458 2.4143e-07 v total_pressure 9459.1 3.5306e+05 1.7887e+05 1.4409e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0682 0.099455 0.0028379 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2203e-07 0.052332 0.00031332 5.1582e-06 INSTANT 0.875583000E-01 TIME STEP NUMBER 55781 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282849526E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.752859913E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.21452E-02 0.21066E+01 Friction velocity uk : 0.21452E-02 0.21066E+01 Dimensionless distance yplus : 0.20633E-02 0.20685E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.012660210e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29435E+08 1 0.17932E-09 0.23837E+02 0.19064E+04 c Velocity[X] 0.12208E+02 c Velocity[Y] 0.11628E+02 c Velocity[Z] 0.16898E-05 c Pressure 0.10074E-03 9 0.53818E-04 0.11756E-02 0.72108E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -20.41 32.034 5.6072 7.9996 v Velocity[Y] -22.622 23.934 -0.14342 -0.00079439 v Velocity[Z] -3.0202 2.9842 2.8449e-06 -5.387e-08 v ǁVelocityǁ 0.00055951 32.105 7.3107 8.0541 v Pressure -91362 2.5256e+05 78173 43062 v TurbVisc 9.4537e-22 0.010033 0.00015143 1.5991e-05 v CourantNb 4.0401e-08 0.011775 0.00016752 4.9169e-06 v FourierNb 1.2425e-07 0.04707 0.0001458 2.4162e-07 v total_pressure 9963.1 3.5388e+05 1.795e+05 1.4439e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0685 0.09942 0.0028375 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2204e-07 0.052335 0.00031332 5.1585e-06 INSTANT 0.875584000E-01 TIME STEP NUMBER 55782 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282856362E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.753389148E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.40426E-02 0.21071E+01 Friction velocity uk : 0.40426E-02 0.21071E+01 Dimensionless distance yplus : 0.38883E-02 0.20689E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.073933604e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29436E+08 1 0.17932E-09 0.23857E+02 0.19072E+04 c Velocity[X] 0.12222E+02 c Velocity[Y] 0.11636E+02 c Velocity[Z] 0.16941E-05 c Pressure 0.98689E-04 154 0.75101E-04 0.11508E-02 0.10415E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -20.421 32.052 5.6073 7.9998 v Velocity[Y] -22.635 23.949 -0.14342 -0.00079712 v Velocity[Z] -3.0201 2.9844 2.8441e-06 -5.387e-08 v ǁVelocityǁ 0.00055295 32.124 7.3123 8.0543 v Pressure -90875 2.5335e+05 78776 43425 v TurbVisc 7.2331e-22 0.010052 0.0001515 1.6018e-05 v CourantNb 4.4598e-08 0.011774 0.00016753 4.917e-06 v FourierNb 1.2425e-07 0.047073 0.00014579 2.418e-07 v total_pressure 10450 3.5468e+05 1.801e+05 1.4475e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0689 0.099379 0.002837 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2206e-07 0.052339 0.00031332 5.1588e-06 INSTANT 0.875585000E-01 TIME STEP NUMBER 55783 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282863324E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.753923771E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.72481E-02 0.21075E+01 Friction velocity uk : 0.72481E-02 0.21075E+01 Dimensionless distance yplus : 0.69714E-02 0.20694E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.100491517e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29437E+08 1 0.17933E-09 0.23880E+02 0.19080E+04 c Velocity[X] 0.12236E+02 c Velocity[Y] 0.11644E+02 c Velocity[Z] 0.16998E-05 c Pressure 0.96043E-04 48 0.80295E-04 0.11192E-02 0.10125E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -20.432 32.071 5.6074 7.9999 v Velocity[Y] -22.648 23.964 -0.14342 -0.00079812 v Velocity[Z] -3.0199 2.9846 2.8433e-06 -5.3871e-08 v ǁVelocityǁ 0.00055973 32.143 7.314 8.0546 v Pressure -90461 2.5406e+05 79331 43754 v TurbVisc 1.1554e-21 0.010071 0.00015157 1.6045e-05 v CourantNb 4.3602e-08 0.011774 0.00016753 4.9171e-06 v FourierNb 1.2425e-07 0.047075 0.00014579 2.4199e-07 v total_pressure 10864 3.5539e+05 1.8066e+05 1.4508e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0694 0.099341 0.0028367 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2207e-07 0.052343 0.00031332 5.1591e-06 INSTANT 0.875586000E-01 TIME STEP NUMBER 55784 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282870193E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.754459850E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12834E-01 0.21079E+01 Friction velocity uk : 0.12834E-01 0.21079E+01 Dimensionless distance yplus : 0.12344E-01 0.20698E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.153322744e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29437E+08 1 0.17933E-09 0.23902E+02 0.19088E+04 c Velocity[X] 0.12248E+02 c Velocity[Y] 0.11654E+02 c Velocity[Z] 0.17038E-05 c Pressure 0.93882E-04 301 0.93369E-04 0.10932E-02 0.98837E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -20.444 32.09 5.6076 8.0001 v Velocity[Y] -22.662 23.979 -0.14343 -0.00080118 v Velocity[Z] -3.0198 2.9849 2.8424e-06 -5.3871e-08 v ǁVelocityǁ 0.00056223 32.161 7.3156 8.0548 v Pressure -90074 2.5474e+05 79839 44020 v TurbVisc 1.1213e-21 0.010091 0.00015164 1.6073e-05 v CourantNb 2.7274e-08 0.011774 0.00016753 4.9173e-06 v FourierNb 1.2425e-07 0.047078 0.00014579 2.4218e-07 v total_pressure 11251 3.5606e+05 1.8116e+05 1.4534e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0698 0.099306 0.0028365 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2209e-07 0.052347 0.00031333 5.1594e-06 INSTANT 0.875587000E-01 TIME STEP NUMBER 55785 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282877299E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.754999480E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15310E-01 0.21084E+01 Friction velocity uk : 0.15310E-01 0.21084E+01 Dimensionless distance yplus : 0.14863E-01 0.20703E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.198630521e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29438E+08 1 0.17933E-09 0.23918E+02 0.19093E+04 c Velocity[X] 0.12261E+02 c Velocity[Y] 0.11656E+02 c Velocity[Z] 0.17084E-05 c Pressure 0.92001E-04 97 0.79114E-04 0.10705E-02 0.75252E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -20.455 32.108 5.6077 8.0002 v Velocity[Y] -22.675 23.993 -0.14343 -0.00080299 v Velocity[Z] -3.0196 2.9851 2.8416e-06 -5.3871e-08 v ǁVelocityǁ 0.00056379 32.18 7.3173 8.0551 v Pressure -89755 2.5535e+05 80294 44291 v TurbVisc 1.264e-21 0.01011 0.00015171 1.61e-05 v CourantNb 3.4852e-08 0.011774 0.00016754 4.9174e-06 v FourierNb 1.2425e-07 0.047081 0.00014579 2.4237e-07 v total_pressure 11570 3.5667e+05 1.8162e+05 1.4562e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0703 0.099265 0.0028362 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.221e-07 0.052351 0.00031333 5.1598e-06 INSTANT 0.875588000E-01 TIME STEP NUMBER 55786 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282884321E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.755542332E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11741E-01 0.21089E+01 Friction velocity uk : 0.11741E-01 0.21089E+01 Dimensionless distance yplus : 0.11398E-01 0.20707E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.241242616e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29438E+08 1 0.17934E-09 0.23941E+02 0.19102E+04 c Velocity[X] 0.12274E+02 c Velocity[Y] 0.11667E+02 c Velocity[Z] 0.17216E-05 c Pressure 0.87346E-04 12 0.54214E-04 0.10156E-02 0.50640E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -20.467 32.127 5.6078 8.0003 v Velocity[Y] -22.688 24.008 -0.14344 -0.00080411 v Velocity[Z] -3.0195 2.9853 2.8408e-06 -5.3871e-08 v ǁVelocityǁ 0.00059165 32.199 7.3189 8.0553 v Pressure -89487 2.5589e+05 80695 44481 v TurbVisc 1.2752e-21 0.01013 0.00015178 1.6128e-05 v CourantNb 4.0276e-08 0.011774 0.00016754 4.9175e-06 v FourierNb 1.2425e-07 0.047085 0.00014579 2.4256e-07 v total_pressure 11838 3.5721e+05 1.8202e+05 1.4581e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0707 0.099217 0.0028358 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2212e-07 0.052355 0.00031333 5.1601e-06 INSTANT 0.875589000E-01 TIME STEP NUMBER 55787 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282891364E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.756089178E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.74552E-02 0.21094E+01 Friction velocity uk : 0.74552E-02 0.21094E+01 Dimensionless distance yplus : 0.72544E-02 0.20712E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.292583689e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29439E+08 1 0.17934E-09 0.23961E+02 0.19109E+04 c Velocity[X] 0.12286E+02 c Velocity[Y] 0.11675E+02 c Velocity[Z] 0.17241E-05 c Pressure 0.86445E-04 544 0.75115E-04 0.10044E-02 0.82378E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -20.478 32.146 5.608 8.0005 v Velocity[Y] -22.701 24.023 -0.14345 -0.00080725 v Velocity[Z] -3.0193 2.9855 2.84e-06 -5.3871e-08 v ǁVelocityǁ 0.00057829 32.218 7.3206 8.0556 v Pressure -89244 2.564e+05 81068 44694 v TurbVisc 7.1349e-22 0.010149 0.00015185 1.6155e-05 v CourantNb 5.4307e-08 0.011773 0.00016754 4.9176e-06 v FourierNb 1.2425e-07 0.047088 0.00014579 2.4275e-07 v total_pressure 12081 3.5772e+05 1.8239e+05 1.4602e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0712 0.099161 0.0028353 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2213e-07 0.052359 0.00031333 5.1604e-06 INSTANT 0.875590000E-01 TIME STEP NUMBER 55788 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282898512E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.756639320E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.31214E-02 0.21099E+01 Friction velocity uk : 0.31214E-02 0.21099E+01 Dimensionless distance yplus : 0.30430E-02 0.20717E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.316259271e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29440E+08 1 0.17934E-09 0.23983E+02 0.19117E+04 c Velocity[X] 0.12299E+02 c Velocity[Y] 0.11683E+02 c Velocity[Z] 0.17278E-05 c Pressure 0.84910E-04 52 0.80494E-04 0.98589E-03 0.86027E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -20.49 32.164 5.6081 8.0006 v Velocity[Y] -22.714 24.038 -0.14346 -0.00080818 v Velocity[Z] -3.0192 2.9857 2.8392e-06 -5.3871e-08 v ǁVelocityǁ 0.00056727 32.237 7.3222 8.0558 v Pressure -89062 2.5683e+05 81391 44905 v TurbVisc 1.2347e-21 0.010168 0.00015192 1.6183e-05 v CourantNb 6.9611e-08 0.011773 0.00016755 4.9178e-06 v FourierNb 1.2425e-07 0.047091 0.00014579 2.4294e-07 v total_pressure 12263 3.5816e+05 1.8272e+05 1.4623e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0717 0.099101 0.0028348 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2214e-07 0.052364 0.00031334 5.1607e-06 INSTANT 0.875591000E-01 TIME STEP NUMBER 55789 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282905565E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.757191375E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.51762E-02 0.21104E+01 Friction velocity uk : 0.51762E-02 0.21104E+01 Dimensionless distance yplus : 0.51660E-02 0.20722E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.359377711e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29440E+08 1 0.17935E-09 0.24003E+02 0.19124E+04 c Velocity[X] 0.12310E+02 c Velocity[Y] 0.11693E+02 c Velocity[Z] 0.17324E-05 c Pressure 0.84028E-04 113 0.93479E-04 0.97495E-03 0.86171E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -20.501 32.183 5.6083 8.0008 v Velocity[Y] -22.727 24.053 -0.14347 -0.00081141 v Velocity[Z] -3.019 2.9859 2.8384e-06 -5.3871e-08 v ǁVelocityǁ 0.00062563 32.255 7.3239 8.0561 v Pressure -88914 2.5721e+05 81660 45013 v TurbVisc 1.8242e-21 0.010188 0.00015199 1.6211e-05 v CourantNb 7.4433e-08 0.011773 0.00016755 4.9179e-06 v FourierNb 1.2425e-07 0.047095 0.00014579 2.4313e-07 v total_pressure 12411 3.5854e+05 1.8299e+05 1.4634e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0722 0.099054 0.0028345 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2216e-07 0.052368 0.00031334 5.161e-06 INSTANT 0.875592000E-01 TIME STEP NUMBER 55790 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282912816E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.757745230E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.16606E-02 0.21109E+01 Friction velocity uk : 0.16606E-02 0.21109E+01 Dimensionless distance yplus : 0.16133E-02 0.20728E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.394444823e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29441E+08 1 0.17935E-09 0.24017E+02 0.19129E+04 c Velocity[X] 0.12322E+02 c Velocity[Y] 0.11695E+02 c Velocity[Z] 0.17398E-05 c Pressure 0.83512E-04 76 0.79300E-04 0.96825E-03 0.62565E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -20.513 32.202 5.6084 8.0009 v Velocity[Y] -22.741 24.068 -0.14348 -0.00081339 v Velocity[Z] -3.0189 2.9862 2.8375e-06 -5.3871e-08 v ǁVelocityǁ 0.00075885 32.274 7.3256 8.0563 v Pressure -88824 2.5754e+05 81897 45203 v TurbVisc 1.5265e-21 0.010207 0.00015206 1.6238e-05 v CourantNb 6.7629e-08 0.011773 0.00016756 4.918e-06 v FourierNb 1.2425e-07 0.047098 0.00014579 2.4332e-07 v total_pressure 12501 3.5886e+05 1.8322e+05 1.4653e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0728 0.099025 0.0028343 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2217e-07 0.052373 0.00031334 5.1614e-06 INSTANT 0.875593000E-01 TIME STEP NUMBER 55791 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282919974E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.758301348E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.50394E-02 0.21115E+01 Friction velocity uk : 0.50394E-02 0.21115E+01 Dimensionless distance yplus : 0.48503E-02 0.20733E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.425331579e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29442E+08 1 0.17936E-09 0.24040E+02 0.19137E+04 c Velocity[X] 0.12334E+02 c Velocity[Y] 0.11706E+02 c Velocity[Z] 0.17503E-05 c Pressure 0.80018E-04 7 0.53850E-04 0.92708E-03 0.32460E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -20.524 32.22 5.6086 8.0011 v Velocity[Y] -22.754 24.084 -0.14348 -0.00081467 v Velocity[Z] -3.0187 2.9864 2.8367e-06 -5.3871e-08 v ǁVelocityǁ 0.00077391 32.293 7.3272 8.0566 v Pressure -88782 2.5779e+05 82038 45235 v TurbVisc 7.555e-22 0.010226 0.00015213 1.6266e-05 v CourantNb 5.0351e-08 0.011773 0.00016756 4.9182e-06 v FourierNb 1.2425e-07 0.047101 0.00014578 2.4351e-07 v total_pressure 12543 3.5911e+05 1.8336e+05 1.4656e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0733 0.099001 0.0028343 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2219e-07 0.052377 0.00031334 5.1617e-06 INSTANT 0.875594000E-01 TIME STEP NUMBER 55792 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282927099E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.758859559E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.78302E-02 0.21120E+01 Friction velocity uk : 0.78302E-02 0.21120E+01 Dimensionless distance yplus : 0.77896E-02 0.20738E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.458433193e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29442E+08 1 0.17937E-09 0.24058E+02 0.19144E+04 c Velocity[X] 0.12344E+02 c Velocity[Y] 0.11714E+02 c Velocity[Z] 0.17562E-05 c Pressure 0.80738E-04 50 0.75491E-04 0.93473E-03 0.68788E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -20.536 32.239 5.6087 8.0012 v Velocity[Y] -22.768 24.099 -0.14349 -0.00081776 v Velocity[Z] -3.0186 2.9866 2.8359e-06 -5.3871e-08 v ǁVelocityǁ 0.00077347 32.312 7.3289 8.0568 v Pressure -88774 2.58e+05 82215 45326 v TurbVisc 4.2877e-22 0.010246 0.0001522 1.6294e-05 v CourantNb 3.823e-08 0.011772 0.00016756 4.9183e-06 v FourierNb 1.2425e-07 0.047105 0.00014578 2.437e-07 v total_pressure 12551 3.5933e+05 1.8354e+05 1.4665e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0738 0.098967 0.0028342 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.222e-07 0.052382 0.00031335 5.162e-06 INSTANT 0.875595000E-01 TIME STEP NUMBER 55793 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282934375E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.759421284E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13588E-01 0.21125E+01 Friction velocity uk : 0.13588E-01 0.21125E+01 Dimensionless distance yplus : 0.13518E-01 0.20743E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.474935402e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29443E+08 1 0.17937E-09 0.24077E+02 0.19151E+04 c Velocity[X] 0.12356E+02 c Velocity[Y] 0.11722E+02 c Velocity[Z] 0.17643E-05 c Pressure 0.80778E-04 362 0.80771E-04 0.93451E-03 0.76101E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -20.547 32.258 5.6089 8.0014 v Velocity[Y] -22.781 24.114 -0.14351 -0.00081885 v Velocity[Z] -3.0184 2.9868 2.8351e-06 -5.3871e-08 v ǁVelocityǁ 0.00077436 32.331 7.3306 8.0571 v Pressure -88807 2.5815e+05 82296 45428 v TurbVisc 6.8479e-22 0.010265 0.00015227 1.6322e-05 v CourantNb 1.6979e-08 0.011772 0.00016757 4.9184e-06 v FourierNb 1.2425e-07 0.047108 0.00014578 2.439e-07 v total_pressure 12518 3.5948e+05 1.8362e+05 1.4675e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0743 0.098957 0.0028343 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2222e-07 0.052386 0.00031335 5.1623e-06 INSTANT 0.875596000E-01 TIME STEP NUMBER 55794 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282941508E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.759982263E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12867E-01 0.21130E+01 Friction velocity uk : 0.12867E-01 0.21130E+01 Dimensionless distance yplus : 0.12384E-01 0.20748E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.496495665e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29444E+08 1 0.17938E-09 0.24096E+02 0.19157E+04 c Velocity[X] 0.12365E+02 c Velocity[Y] 0.11732E+02 c Velocity[Z] 0.17736E-05 c Pressure 0.81523E-04 130 0.93681E-04 0.94246E-03 0.86908E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -20.559 32.277 5.609 8.0015 v Velocity[Y] -22.795 24.129 -0.14352 -0.00082245 v Velocity[Z] -3.0183 2.987 2.8343e-06 -5.3871e-08 v ǁVelocityǁ 0.00077665 32.35 7.3323 8.0573 v Pressure -88891 2.5823e+05 82315 45363 v TurbVisc 6.6903e-22 0.010284 0.00015234 1.635e-05 v CourantNb 2.1015e-08 0.011772 0.00016757 4.9186e-06 v FourierNb 1.2425e-07 0.047111 0.00014578 2.4409e-07 v total_pressure 12434 3.5955e+05 1.8364e+05 1.4669e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0748 0.098941 0.0028344 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2223e-07 0.052391 0.00031335 5.1627e-06 INSTANT 0.875597000E-01 TIME STEP NUMBER 55795 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282948793E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.760544100E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12446E-01 0.21136E+01 Friction velocity uk : 0.12446E-01 0.21136E+01 Dimensionless distance yplus : 0.11978E-01 0.20753E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.514114298e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29444E+08 1 0.17939E-09 0.24109E+02 0.19161E+04 c Velocity[X] 0.12375E+02 c Velocity[Y] 0.11734E+02 c Velocity[Z] 0.17811E-05 c Pressure 0.82639E-04 83 0.79150E-04 0.95465E-03 0.51137E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -20.571 32.295 5.6092 8.0017 v Velocity[Y] -22.808 24.145 -0.14353 -0.00082456 v Velocity[Z] -3.0181 2.9872 2.8335e-06 -5.3871e-08 v ǁVelocityǁ 0.00078085 32.369 7.334 8.0576 v Pressure -89013 2.5827e+05 82316 45410 v TurbVisc 5.2314e-22 0.010304 0.00015241 1.6378e-05 v CourantNb 3.7209e-08 0.011772 0.00016758 4.9187e-06 v FourierNb 1.2425e-07 0.047115 0.00014578 2.4428e-07 v total_pressure 12312 3.5959e+05 1.8364e+05 1.4673e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0753 0.098915 0.0028344 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2225e-07 0.052395 0.00031336 5.163e-06 INSTANT 0.875598000E-01 TIME STEP NUMBER 55796 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282955984E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.761108032E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.18640E-02 0.21141E+01 Friction velocity uk : 0.18640E-02 0.21141E+01 Dimensionless distance yplus : 0.18306E-02 0.20758E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.523784342e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29445E+08 1 0.17940E-09 0.24129E+02 0.19169E+04 c Velocity[X] 0.12385E+02 c Velocity[Y] 0.11744E+02 c Velocity[Z] 0.17936E-05 c Pressure 0.80742E-04 6 0.53653E-04 0.93207E-03 0.30557E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -20.582 32.314 5.6093 8.0018 v Velocity[Y] -22.822 24.16 -0.14354 -0.00082602 v Velocity[Z] -3.018 2.9875 2.8327e-06 -5.3871e-08 v ǁVelocityǁ 0.00078747 32.388 7.3356 8.0578 v Pressure -89169 2.5825e+05 82288 45401 v TurbVisc 4.7449e-22 0.010323 0.00015249 1.6406e-05 v CourantNb 5.32e-09 0.011772 0.00016758 4.9188e-06 v FourierNb 1.2425e-07 0.047118 0.00014578 2.4448e-07 v total_pressure 12156 3.5957e+05 1.8361e+05 1.4673e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0758 0.098878 0.0028343 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2227e-07 0.052399 0.00031336 5.1633e-06 INSTANT 0.875599000E-01 TIME STEP NUMBER 55797 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282963135E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.761672911E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.57484E-02 0.21146E+01 Friction velocity uk : 0.57484E-02 0.21146E+01 Dimensionless distance yplus : 0.55768E-02 0.20763E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.521787013e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29446E+08 1 0.17941E-09 0.24143E+02 0.19173E+04 c Velocity[X] 0.12393E+02 c Velocity[Y] 0.11750E+02 c Velocity[Z] 0.17997E-05 c Pressure 0.83044E-04 15 0.99820E-04 0.95794E-03 0.37722E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -20.594 32.333 5.6095 8.0019 v Velocity[Y] -22.835 24.175 -0.14355 -0.00082817 v Velocity[Z] -3.0178 2.9877 2.8318e-06 -5.3871e-08 v ǁVelocityǁ 0.00079812 32.407 7.3373 8.0581 v Pressure -89398 2.5815e+05 82122 45251 v TurbVisc 7.3784e-23 0.010343 0.00015256 1.6435e-05 v CourantNb 2.2136e-08 0.011772 0.00016758 4.919e-06 v FourierNb 1.2425e-07 0.047121 0.00014578 2.4467e-07 v total_pressure 11927 3.5947e+05 1.8345e+05 1.4658e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0763 0.098852 0.0028343 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2228e-07 0.052403 0.00031336 5.1637e-06 INSTANT 0.875600000E-01 TIME STEP NUMBER 55798 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282970305E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.762234803E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15251E-01 0.21151E+01 Friction velocity uk : 0.15251E-01 0.21151E+01 Dimensionless distance yplus : 0.14678E-01 0.20768E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.535141525e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29446E+08 1 0.17941E-09 0.24159E+02 0.19179E+04 c Velocity[X] 0.12402E+02 c Velocity[Y] 0.11757E+02 c Velocity[Z] 0.18064E-05 c Pressure 0.84059E-04 83 0.83465E-04 0.96894E-03 0.20788E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -20.606 32.352 5.6096 8.0021 v Velocity[Y] -22.849 24.19 -0.14356 -0.00083071 v Velocity[Z] -3.0177 2.9879 2.831e-06 -5.3871e-08 v ǁVelocityǁ 0.00081253 32.426 7.339 8.0583 v Pressure -89623 2.5803e+05 81999 45204 v TurbVisc 4.8894e-22 0.010362 0.00015263 1.6463e-05 v CourantNb 1.2782e-08 0.011771 0.00016759 4.9191e-06 v FourierNb 1.2425e-07 0.047124 0.00014578 2.4487e-07 v total_pressure 11702 3.5935e+05 1.8332e+05 1.4653e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0768 0.098845 0.0028346 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.223e-07 0.052407 0.00031337 5.164e-06 INSTANT 0.875601000E-01 TIME STEP NUMBER 55799 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282977500E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.762805206E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.61294E-02 0.21156E+01 Friction velocity uk : 0.61294E-02 0.21156E+01 Dimensionless distance yplus : 0.60850E-02 0.20773E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.523087758e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29447E+08 1 0.17942E-09 0.24178E+02 0.19186E+04 c Velocity[X] 0.12410E+02 c Velocity[Y] 0.11768E+02 c Velocity[Z] 0.18195E-05 c Pressure 0.84962E-04 7 0.52389E-04 0.97863E-03 0.37131E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -20.618 32.371 5.6097 8.0022 v Velocity[Y] -22.863 24.206 -0.14357 -0.000834 v Velocity[Z] -3.0175 2.9881 2.8302e-06 -5.3871e-08 v ǁVelocityǁ 0.00083026 32.445 7.3407 8.0586 v Pressure -89896 2.5784e+05 81832 45105 v TurbVisc 1.2041e-21 0.010381 0.0001527 1.6492e-05 v CourantNb 3.8762e-08 0.011771 0.00016759 4.9193e-06 v FourierNb 1.2425e-07 0.047127 0.00014578 2.4507e-07 v total_pressure 11429 3.5917e+05 1.8316e+05 1.4643e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0773 0.098825 0.0028348 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2231e-07 0.052411 0.00031337 5.1643e-06 INSTANT 0.875602000E-01 TIME STEP NUMBER 55800 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282984710E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.763371786E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.85224E-02 0.21160E+01 Friction velocity uk : 0.85224E-02 0.21160E+01 Dimensionless distance yplus : 0.85507E-02 0.20777E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.505572776e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29448E+08 1 0.17943E-09 0.24193E+02 0.19191E+04 c Velocity[X] 0.12419E+02 c Velocity[Y] 0.11775E+02 c Velocity[Z] 0.18285E-05 c Pressure 0.88071E-04 48 0.76295E-04 0.10137E-02 0.73934E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -20.629 32.39 5.6099 8.0024 v Velocity[Y] -22.876 24.221 -0.14358 -0.00083551 v Velocity[Z] -3.0174 2.9883 2.8294e-06 -5.3871e-08 v ǁVelocityǁ 0.00085699 32.464 7.3424 8.0589 v Pressure -90229 2.5758e+05 81549 44959 v TurbVisc 8.8415e-22 0.010401 0.00015278 1.652e-05 v CourantNb 2.9009e-08 0.011771 0.0001676 4.9194e-06 v FourierNb 1.2425e-07 0.047129 0.00014578 2.4526e-07 v total_pressure 11096 3.5891e+05 1.8287e+05 1.4628e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0777 0.098818 0.0028351 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2233e-07 0.052415 0.00031337 5.1646e-06 INSTANT 0.875603000E-01 TIME STEP NUMBER 55801 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282991783E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.763935431E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.28157E-02 0.21165E+01 Friction velocity uk : 0.28157E-02 0.21165E+01 Dimensionless distance yplus : 0.27541E-02 0.20782E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.497534048e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29448E+08 1 0.17944E-09 0.24210E+02 0.19196E+04 c Velocity[X] 0.12426E+02 c Velocity[Y] 0.11784E+02 c Velocity[Z] 0.18332E-05 c Pressure 0.90439E-04 66 0.80601E-04 0.10402E-02 0.83926E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -20.641 32.409 5.61 8.0025 v Velocity[Y] -22.89 24.237 -0.14359 -0.0008389 v Velocity[Z] -3.0172 2.9885 2.8286e-06 -5.3871e-08 v ǁVelocityǁ 0.00088755 32.483 7.3441 8.0591 v Pressure -90582 2.5729e+05 81271 44762 v TurbVisc 1.905e-22 0.01042 0.00015285 1.6549e-05 v CourantNb 6.819e-09 0.011771 0.0001676 4.9195e-06 v FourierNb 1.2425e-07 0.047132 0.00014577 2.4546e-07 v total_pressure 10743 3.5862e+05 1.826e+05 1.4609e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0782 0.098828 0.0028354 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2234e-07 0.052418 0.00031338 5.165e-06 INSTANT 0.875604000E-01 TIME STEP NUMBER 55802 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282998978E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.764503661E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.75231E-02 0.21169E+01 Friction velocity uk : 0.75231E-02 0.21169E+01 Dimensionless distance yplus : 0.74331E-02 0.20786E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.469723296e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29449E+08 1 0.17946E-09 0.24226E+02 0.19202E+04 c Velocity[X] 0.12434E+02 c Velocity[Y] 0.11792E+02 c Velocity[Z] 0.18412E-05 c Pressure 0.93343E-04 114 0.93894E-04 0.10728E-02 0.88806E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -20.653 32.428 5.6102 8.0027 v Velocity[Y] -22.904 24.252 -0.1436 -0.00084023 v Velocity[Z] -3.017 2.9888 2.8278e-06 -5.3871e-08 v ǁVelocityǁ 0.00092363 32.502 7.3458 8.0594 v Pressure -90987 2.5695e+05 80942 44615 v TurbVisc 1.1257e-22 0.010439 0.00015292 1.6577e-05 v CourantNb 1.4331e-08 0.011771 0.00016761 4.9197e-06 v FourierNb 1.2425e-07 0.047134 0.00014577 2.4566e-07 v total_pressure 10338 3.5827e+05 1.8227e+05 1.4594e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0786 0.098846 0.0028359 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2236e-07 0.052422 0.00031338 5.1653e-06 INSTANT 0.875605000E-01 TIME STEP NUMBER 55803 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283005968E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.765069889E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.71617E-02 0.21173E+01 Friction velocity uk : 0.71617E-02 0.21173E+01 Dimensionless distance yplus : 0.70760E-02 0.20790E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.438891765e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29449E+08 1 0.17947E-09 0.24235E+02 0.19205E+04 c Velocity[X] 0.12440E+02 c Velocity[Y] 0.11795E+02 c Velocity[Z] 0.18505E-05 c Pressure 0.96436E-04 71 0.79606E-04 0.11075E-02 0.77759E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -20.665 32.447 5.6103 8.0028 v Velocity[Y] -22.918 24.267 -0.14361 -0.00084287 v Velocity[Z] -3.0169 2.989 2.827e-06 -5.3871e-08 v ǁVelocityǁ 0.00096441 32.521 7.3475 8.0596 v Pressure -91418 2.5654e+05 80550 44327 v TurbVisc 1.8997e-22 0.010459 0.000153 1.6606e-05 v CourantNb 2.4039e-08 0.01177 0.00016761 4.9198e-06 v FourierNb 1.2425e-07 0.047137 0.00014577 2.4586e-07 v total_pressure 9906.5 3.5787e+05 1.8187e+05 1.4565e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.079 0.09886 0.0028363 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2237e-07 0.052425 0.00031338 5.1656e-06 INSTANT 0.875606000E-01 TIME STEP NUMBER 55804 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283013033E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.765635473E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.48313E-02 0.21177E+01 Friction velocity uk : 0.48313E-02 0.21177E+01 Dimensionless distance yplus : 0.46940E-02 0.20794E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.403385257e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29450E+08 1 0.17948E-09 0.24252E+02 0.19211E+04 c Velocity[X] 0.12447E+02 c Velocity[Y] 0.11805E+02 c Velocity[Z] 0.18656E-05 c Pressure 0.96875E-04 9 0.54514E-04 0.11118E-02 0.50041E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -20.677 32.466 5.6104 8.0029 v Velocity[Y] -22.931 24.283 -0.14362 -0.00084631 v Velocity[Z] -3.0167 2.9892 2.8262e-06 -5.3871e-08 v ǁVelocityǁ 0.00099312 32.54 7.3491 8.0599 v Pressure -91878 2.5611e+05 80143 44142 v TurbVisc 1.1255e-22 0.010478 0.00015307 1.6635e-05 v CourantNb 1.0961e-08 0.01177 0.00016762 4.9199e-06 v FourierNb 1.2425e-07 0.047139 0.00014577 2.4605e-07 v total_pressure 9447 3.5743e+05 1.8147e+05 1.4547e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0794 0.098872 0.0028366 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2239e-07 0.052428 0.00031339 5.166e-06 INSTANT 0.875607000E-01 TIME STEP NUMBER 55805 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283020084E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.766200291E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.48904E-02 0.21181E+01 Friction velocity uk : 0.48904E-02 0.21181E+01 Dimensionless distance yplus : 0.47633E-02 0.20798E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.350876104e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29451E+08 1 0.17949E-09 0.24265E+02 0.19215E+04 c Velocity[X] 0.12453E+02 c Velocity[Y] 0.11812E+02 c Velocity[Z] 0.18645E-05 c Pressure 0.10077E-03 247 0.75664E-04 0.11556E-02 0.93567E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -20.689 32.485 5.6106 8.0031 v Velocity[Y] -22.945 24.298 -0.14363 -0.0008479 v Velocity[Z] -3.0166 2.9894 2.8254e-06 -5.3871e-08 v ǁVelocityǁ 0.0010199 32.56 7.3508 8.0601 v Pressure -92398 2.5559e+05 79656 43841 v TurbVisc 1.9032e-21 0.010497 0.00015315 1.6663e-05 v CourantNb 2.0034e-08 0.01177 0.00016762 4.92e-06 v FourierNb 1.2425e-07 0.047141 0.00014577 2.4625e-07 v total_pressure 8926.8 3.5692e+05 1.8098e+05 1.4517e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0798 0.098886 0.002837 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.224e-07 0.052431 0.00031339 5.1663e-06 INSTANT 0.875608000E-01 TIME STEP NUMBER 55806 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283026994E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.766763117E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.59977E-02 0.21185E+01 Friction velocity uk : 0.59977E-02 0.21185E+01 Dimensionless distance yplus : 0.58313E-02 0.20802E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.321682421e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29451E+08 1 0.17950E-09 0.24279E+02 0.19220E+04 c Velocity[X] 0.12458E+02 c Velocity[Y] 0.11821E+02 c Velocity[Z] 0.18685E-05 c Pressure 0.10400E-03 65 0.80810E-04 0.11917E-02 0.97726E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -20.701 32.504 5.6107 8.0032 v Velocity[Y] -22.959 24.313 -0.14364 -0.00085143 v Velocity[Z] -3.0164 2.9896 2.8246e-06 -5.3871e-08 v ǁVelocityǁ 0.0010546 32.579 7.3525 8.0604 v Pressure -92933 2.5506e+05 79147 43545 v TurbVisc 1.4874e-22 0.010517 0.00015322 1.6692e-05 v CourantNb 2.7404e-08 0.01177 0.00016762 4.9202e-06 v FourierNb 1.2425e-07 0.047143 0.00014577 2.4645e-07 v total_pressure 8391.9 3.5639e+05 1.8047e+05 1.4487e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0802 0.098904 0.0028374 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2242e-07 0.052434 0.0003134 5.1666e-06 INSTANT 0.875609000E-01 TIME STEP NUMBER 55807 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283034011E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.767326323E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.38772E-02 0.21189E+01 Friction velocity uk : 0.38772E-02 0.21189E+01 Dimensionless distance yplus : 0.37640E-02 0.20805E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.263326155e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29452E+08 1 0.17951E-09 0.24293E+02 0.19224E+04 c Velocity[X] 0.12464E+02 c Velocity[Y] 0.11828E+02 c Velocity[Z] 0.18733E-05 c Pressure 0.10757E-03 300 0.94167E-04 0.12318E-02 0.10840E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -20.712 32.523 5.6108 8.0034 v Velocity[Y] -22.973 24.329 -0.14365 -0.00085284 v Velocity[Z] -3.0163 2.9898 2.8238e-06 -5.3871e-08 v ǁVelocityǁ 0.0010348 32.598 7.3542 8.0606 v Pressure -93531 2.5446e+05 78577 43223 v TurbVisc 2.1724e-22 0.010536 0.00015329 1.6721e-05 v CourantNb 2.0292e-08 0.01177 0.00016763 4.9203e-06 v FourierNb 1.2425e-07 0.047145 0.00014577 2.4665e-07 v total_pressure 7793.8 3.5578e+05 1.799e+05 1.4455e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0805 0.098923 0.0028378 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2243e-07 0.052437 0.0003134 5.167e-06 INSTANT 0.875610000E-01 TIME STEP NUMBER 55808 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283040781E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.767887452E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.34237E-02 0.21192E+01 Friction velocity uk : 0.34237E-02 0.21192E+01 Dimensionless distance yplus : 0.34342E-02 0.20809E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.206205782e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29453E+08 1 0.17953E-09 0.24299E+02 0.19226E+04 c Velocity[X] 0.12469E+02 c Velocity[Y] 0.11831E+02 c Velocity[Z] 0.18795E-05 c Pressure 0.11130E-03 77 0.79657E-04 0.12736E-02 0.95118E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -20.724 32.542 5.6109 8.0035 v Velocity[Y] -22.987 24.344 -0.14366 -0.00085562 v Velocity[Z] -3.0161 2.9901 2.823e-06 -5.3871e-08 v ǁVelocityǁ 0.00098581 32.617 7.3559 8.0609 v Pressure -94146 2.5382e+05 77972 42847 v TurbVisc 3.6672e-22 0.010556 0.00015337 1.6751e-05 v CourantNb 3.3942e-08 0.01177 0.00016763 4.9204e-06 v FourierNb 1.2425e-07 0.047146 0.00014577 2.4685e-07 v total_pressure 7179.2 3.5514e+05 1.793e+05 1.4417e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0809 0.098945 0.0028383 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2245e-07 0.052439 0.0003134 5.1673e-06 INSTANT 0.875611000E-01 TIME STEP NUMBER 55809 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283047620E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.768446928E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.55663E-02 0.21195E+01 Friction velocity uk : 0.55663E-02 0.21195E+01 Dimensionless distance yplus : 0.54819E-02 0.20812E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.146413041e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29453E+08 1 0.17954E-09 0.24314E+02 0.19231E+04 c Velocity[X] 0.12474E+02 c Velocity[Y] 0.11840E+02 c Velocity[Z] 0.18870E-05 c Pressure 0.11259E-03 9 0.54101E-04 0.12874E-02 0.75740E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -20.736 32.562 5.6111 8.0036 v Velocity[Y] -23.001 24.36 -0.14367 -0.00085914 v Velocity[Z] -3.016 2.9903 2.8221e-06 -5.3871e-08 v ǁVelocityǁ 0.00094028 32.637 7.3576 8.0611 v Pressure -94792 2.5314e+05 77329 42527 v TurbVisc 4.1336e-22 0.010575 0.00015344 1.678e-05 v CourantNb 5.1481e-08 0.01177 0.00016764 4.9206e-06 v FourierNb 1.2425e-07 0.047148 0.00014577 2.4705e-07 v total_pressure 6532.9 3.5447e+05 1.7865e+05 1.4385e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0812 0.098977 0.0028389 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2246e-07 0.052442 0.00031341 5.1676e-06 INSTANT 0.875612000E-01 TIME STEP NUMBER 55810 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283054410E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.769003713E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.36765E-02 0.21198E+01 Friction velocity uk : 0.36765E-02 0.21198E+01 Dimensionless distance yplus : 0.35623E-02 0.20815E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.070235802e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29454E+08 1 0.17955E-09 0.24325E+02 0.19235E+04 c Velocity[X] 0.12478E+02 c Velocity[Y] 0.11847E+02 c Velocity[Z] 0.18880E-05 c Pressure 0.11688E-03 148 0.75449E-04 0.13354E-02 0.11832E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -20.748 32.581 5.6112 8.0038 v Velocity[Y] -23.015 24.375 -0.14367 -0.0008609 v Velocity[Z] -3.0158 2.9905 2.8213e-06 -5.3871e-08 v ǁVelocityǁ 0.00089534 32.656 7.3592 8.0614 v Pressure -95506 2.524e+05 76639 42096 v TurbVisc 3.0661e-21 0.010594 0.00015352 1.6808e-05 v CourantNb 5.5772e-08 0.011769 0.00016764 4.9207e-06 v FourierNb 1.2425e-07 0.047149 0.00014577 2.4725e-07 v total_pressure 5818.7 3.5372e+05 1.7796e+05 1.4342e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0815 0.099009 0.0028395 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2248e-07 0.052444 0.00031341 5.1679e-06 INSTANT 0.875613000E-01 TIME STEP NUMBER 55811 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283061065E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.769558741E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.99265E-02 0.21201E+01 Friction velocity uk : 0.99265E-02 0.21201E+01 Dimensionless distance yplus : 0.96181E-02 0.20818E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.022544610e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29454E+08 1 0.17957E-09 0.24337E+02 0.19239E+04 c Velocity[X] 0.12482E+02 c Velocity[Y] 0.11855E+02 c Velocity[Z] 0.18901E-05 c Pressure 0.12044E-03 67 0.80619E-04 0.13751E-02 0.12550E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -20.76 32.6 5.6113 8.0039 v Velocity[Y] -23.029 24.391 -0.14368 -0.00086452 v Velocity[Z] -3.0156 2.9907 2.8205e-06 -5.3871e-08 v ǁVelocityǁ 0.00085381 32.676 7.3609 8.0616 v Pressure -96237 2.5163e+05 75890 41645 v TurbVisc 8.0239e-22 0.010614 0.00015359 1.6838e-05 v CourantNb 5.2126e-08 0.011769 0.00016765 4.9208e-06 v FourierNb 1.2425e-07 0.047151 0.00014577 2.4746e-07 v total_pressure 5088.3 3.5295e+05 1.7722e+05 1.4297e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0818 0.099042 0.0028401 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2249e-07 0.052446 0.00031342 5.1683e-06 INSTANT 0.875614000E-01 TIME STEP NUMBER 55812 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283067789E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.770110122E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.63857E-02 0.21204E+01 Friction velocity uk : 0.63857E-02 0.21204E+01 Dimensionless distance yplus : 0.63689E-02 0.20821E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 9.481182528e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29455E+08 1 0.17958E-09 0.24349E+02 0.19242E+04 c Velocity[X] 0.12487E+02 c Velocity[Y] 0.11862E+02 c Velocity[Z] 0.18925E-05 c Pressure 0.12433E-03 305 0.93730E-04 0.14184E-02 0.12929E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -20.772 32.619 5.6114 8.004 v Velocity[Y] -23.043 24.406 -0.14368 -0.00086606 v Velocity[Z] -3.0155 2.9909 2.8197e-06 -5.3872e-08 v ǁVelocityǁ 0.00081362 32.695 7.3626 8.0619 v Pressure -97030 2.508e+05 75104 41206 v TurbVisc 9.1062e-22 0.010633 0.00015367 1.6867e-05 v CourantNb 4.5261e-08 0.011769 0.00016765 4.921e-06 v FourierNb 1.2425e-07 0.047152 0.00014577 2.4766e-07 v total_pressure 4295.4 3.5212e+05 1.7643e+05 1.4253e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0821 0.099068 0.0028405 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2251e-07 0.052448 0.00031342 5.1686e-06 INSTANT 0.875615000E-01 TIME STEP NUMBER 55813 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283074251E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.770660821E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10475E-01 0.21207E+01 Friction velocity uk : 0.10475E-01 0.21207E+01 Dimensionless distance yplus : 0.10169E-01 0.20823E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 8.775461707e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29456E+08 1 0.17960E-09 0.24353E+02 0.19244E+04 c Velocity[X] 0.12489E+02 c Velocity[Y] 0.11864E+02 c Velocity[Z] 0.18944E-05 c Pressure 0.12827E-03 89 0.79356E-04 0.14624E-02 0.12237E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -20.784 32.639 5.6115 8.0042 v Velocity[Y] -23.057 24.422 -0.14369 -0.00086894 v Velocity[Z] -3.0153 2.9911 2.8189e-06 -5.3872e-08 v ǁVelocityǁ 0.00077517 32.714 7.3643 8.0621 v Pressure -97841 2.4993e+05 74284 40709 v TurbVisc 1.1191e-21 0.010652 0.00015375 1.6897e-05 v CourantNb 3.6181e-08 0.011769 0.00016765 4.9211e-06 v FourierNb 1.2425e-07 0.047153 0.00014577 2.4786e-07 v total_pressure 3484.1 3.5126e+05 1.7561e+05 1.4203e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0823 0.099101 0.002841 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2252e-07 0.05245 0.00031342 5.1689e-06 INSTANT 0.875616000E-01 TIME STEP NUMBER 55814 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283080764E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.771208403E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10902E-01 0.21209E+01 Friction velocity uk : 0.10902E-01 0.21209E+01 Dimensionless distance yplus : 0.10584E-01 0.20826E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 8.074140860e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29456E+08 1 0.17961E-09 0.24366E+02 0.19248E+04 c Velocity[X] 0.12493E+02 c Velocity[Y] 0.11873E+02 c Velocity[Z] 0.18997E-05 c Pressure 0.13005E-03 9 0.54707E-04 0.14816E-02 0.10291E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -20.796 32.658 5.6116 8.0043 v Velocity[Y] -23.071 24.437 -0.14369 -0.00087256 v Velocity[Z] -3.0152 2.9913 2.8181e-06 -5.3872e-08 v ǁVelocityǁ 0.00074415 32.734 7.3659 8.0623 v Pressure -98684 2.4904e+05 73422 40271 v TurbVisc 1.3579e-21 0.010672 0.00015382 1.6926e-05 v CourantNb 2.5042e-08 0.011769 0.00016766 4.9212e-06 v FourierNb 1.2425e-07 0.047154 0.00014577 2.4807e-07 v total_pressure 2640.8 3.5037e+05 1.7475e+05 1.416e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0826 0.099126 0.0028413 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2254e-07 0.052451 0.00031343 5.1693e-06 INSTANT 0.875617000E-01 TIME STEP NUMBER 55815 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283087197E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.771751912E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11391E-01 0.21212E+01 Friction velocity uk : 0.11391E-01 0.21212E+01 Dimensionless distance yplus : 0.11058E-01 0.20828E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 7.249156746e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29457E+08 1 0.17963E-09 0.24375E+02 0.19251E+04 c Velocity[X] 0.12496E+02 c Velocity[Y] 0.11879E+02 c Velocity[Z] 0.18977E-05 c Pressure 0.13440E-03 153 0.75371E-04 0.15299E-02 0.14889E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -20.808 32.677 5.6116 8.0044 v Velocity[Y] -23.085 24.453 -0.14369 -0.00087443 v Velocity[Z] -3.015 2.9916 2.8173e-06 -5.3872e-08 v ǁVelocityǁ 0.0007029 32.753 7.3676 8.0626 v Pressure -99611 2.4807e+05 72526 39713 v TurbVisc 7.1032e-21 0.010691 0.0001539 1.6955e-05 v CourantNb 2.3199e-08 0.011769 0.00016766 4.9213e-06 v FourierNb 1.2425e-07 0.047155 0.00014577 2.4827e-07 v total_pressure 1714.2 3.4939e+05 1.7385e+05 1.4104e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0828 0.099145 0.0028416 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2255e-07 0.052453 0.00031343 5.1696e-06 INSTANT 0.875618000E-01 TIME STEP NUMBER 55816 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283093496E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.772292740E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.79819E-02 0.21214E+01 Friction velocity uk : 0.79819E-02 0.21214E+01 Dimensionless distance yplus : 0.78365E-02 0.20830E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 6.744359718e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29457E+08 1 0.17964E-09 0.24385E+02 0.19254E+04 c Velocity[X] 0.12498E+02 c Velocity[Y] 0.11887E+02 c Velocity[Z] 0.18963E-05 c Pressure 0.13806E-03 66 0.80425E-04 0.15705E-02 0.15555E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -20.82 32.696 5.6117 8.0046 v Velocity[Y] -23.099 24.468 -0.1437 -0.00087817 v Velocity[Z] -3.0149 2.9918 2.8165e-06 -5.3872e-08 v ǁVelocityǁ 0.00066935 32.773 7.3693 8.0628 v Pressure -1.0055e+05 2.4709e+05 71561 39138 v TurbVisc 2.4108e-21 0.01071 0.00015397 1.6985e-05 v CourantNb 3.2188e-08 0.011769 0.00016766 4.9215e-06 v FourierNb 1.2425e-07 0.047156 0.00014577 2.4847e-07 v total_pressure 777.61 3.4841e+05 1.7289e+05 1.4046e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.083 0.099161 0.0028418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2257e-07 0.052454 0.00031344 5.1699e-06 INSTANT 0.875619000E-01 TIME STEP NUMBER 55817 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283099839E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.772828514E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.59020E-02 0.21216E+01 Friction velocity uk : 0.59020E-02 0.21216E+01 Dimensionless distance yplus : 0.57945E-02 0.20832E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 6.017086545e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29458E+08 1 0.17966E-09 0.24395E+02 0.19257E+04 c Velocity[X] 0.12501E+02 c Velocity[Y] 0.11894E+02 c Velocity[Z] 0.18959E-05 c Pressure 0.14198E-03 304 0.93548E-04 0.16139E-02 0.15682E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -20.832 32.716 5.6118 8.0047 v Velocity[Y] -23.113 24.484 -0.1437 -0.00087981 v Velocity[Z] -3.0147 2.992 2.8157e-06 -5.3872e-08 v ǁVelocityǁ 0.00063666 32.792 7.371 8.0631 v Pressure -1.0155e+05 2.4604e+05 70566 38582 v TurbVisc 2.2083e-21 0.01073 0.00015405 1.7015e-05 v CourantNb 3.6715e-08 0.011768 0.00016767 4.9216e-06 v FourierNb 1.2425e-07 0.047156 0.00014577 2.4868e-07 v total_pressure -228.5 3.4737e+05 1.7189e+05 1.3991e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0832 0.099174 0.0028419 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2258e-07 0.052456 0.00031344 5.1702e-06 INSTANT 0.875620000E-01 TIME STEP NUMBER 55818 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283105894E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.773363234E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10187E-01 0.21218E+01 Friction velocity uk : 0.10187E-01 0.21218E+01 Dimensionless distance yplus : 0.10001E-01 0.20834E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 5.366075779e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29458E+08 1 0.17967E-09 0.24398E+02 0.19257E+04 c Velocity[X] 0.12503E+02 c Velocity[Y] 0.11895E+02 c Velocity[Z] 0.18960E-05 c Pressure 0.14592E-03 124 0.79461E-04 0.16575E-02 0.15491E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -20.844 32.735 5.6119 8.0048 v Velocity[Y] -23.127 24.5 -0.1437 -0.0008828 v Velocity[Z] -3.0145 2.9922 2.8149e-06 -5.3872e-08 v ǁVelocityǁ 0.00060552 32.811 7.3726 8.0633 v Pressure -1.0258e+05 2.4497e+05 69540 37965 v TurbVisc 2.4434e-21 0.010749 0.00015412 1.7045e-05 v CourantNb 4.2719e-08 0.011768 0.00016767 4.9217e-06 v FourierNb 1.2425e-07 0.047157 0.00014577 2.4888e-07 v total_pressure -1255.9 3.4629e+05 1.7086e+05 1.3929e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0834 0.099188 0.002842 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.226e-07 0.052457 0.00031344 5.1706e-06 INSTANT 0.875621000E-01 TIME STEP NUMBER 55819 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283111988E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.773893363E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11253E-01 0.21220E+01 Friction velocity uk : 0.11253E-01 0.21220E+01 Dimensionless distance yplus : 0.10924E-01 0.20836E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 4.749378400e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29459E+08 1 0.17969E-09 0.24409E+02 0.19261E+04 c Velocity[X] 0.12505E+02 c Velocity[Y] 0.11904E+02 c Velocity[Z] 0.19056E-05 c Pressure 0.14790E-03 9 0.55754E-04 0.16787E-02 0.13278E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -20.856 32.754 5.6119 8.0049 v Velocity[Y] -23.141 24.515 -0.1437 -0.00088653 v Velocity[Z] -3.0144 2.9924 2.8141e-06 -5.3872e-08 v ǁVelocityǁ 0.00058296 32.831 7.3743 8.0635 v Pressure -1.0364e+05 2.4387e+05 68475 37418 v TurbVisc 2.5876e-21 0.010768 0.0001542 1.7075e-05 v CourantNb 4.4845e-08 0.011768 0.00016767 4.9218e-06 v FourierNb 1.2425e-07 0.047157 0.00014577 2.4909e-07 v total_pressure -2316.8 3.4519e+05 1.698e+05 1.3874e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0836 0.099199 0.002842 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2261e-07 0.052458 0.00031345 5.1709e-06 INSTANT 0.875622000E-01 TIME STEP NUMBER 55820 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283117969E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.774418162E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.67905E-02 0.21222E+01 Friction velocity uk : 0.67905E-02 0.21222E+01 Dimensionless distance yplus : 0.65761E-02 0.20838E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 4.087461301e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29460E+08 1 0.17970E-09 0.24416E+02 0.19263E+04 c Velocity[X] 0.12507E+02 c Velocity[Y] 0.11909E+02 c Velocity[Z] 0.18996E-05 c Pressure 0.15212E-03 167 0.75247E-04 0.17253E-02 0.18455E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -20.868 32.774 5.612 8.005 v Velocity[Y] -23.155 24.531 -0.1437 -0.00088852 v Velocity[Z] -3.0142 2.9926 2.8133e-06 -5.3872e-08 v ǁVelocityǁ 0.00054912 32.85 7.3759 8.0638 v Pressure -1.0479e+05 2.4269e+05 67378 36739 v TurbVisc 9.8616e-21 0.010788 0.00015428 1.7104e-05 v CourantNb 4.6464e-08 0.011768 0.00016767 4.9219e-06 v FourierNb 1.2425e-07 0.047158 0.00014578 2.4929e-07 v total_pressure -3466.7 3.4402e+05 1.687e+05 1.3806e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0838 0.099205 0.002842 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2263e-07 0.052459 0.00031345 5.1712e-06 INSTANT 0.875623000E-01 TIME STEP NUMBER 55821 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283123825E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.774939039E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.47577E-02 0.21223E+01 Friction velocity uk : 0.47577E-02 0.21223E+01 Dimensionless distance yplus : 0.46074E-02 0.20839E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 3.653195587e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29460E+08 1 0.17972E-09 0.24424E+02 0.19265E+04 c Velocity[X] 0.12508E+02 c Velocity[Y] 0.11916E+02 c Velocity[Z] 0.18942E-05 c Pressure 0.15570E-03 74 0.80485E-04 0.17647E-02 0.18927E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -20.88 32.793 5.6121 8.0052 v Velocity[Y] -23.169 24.546 -0.1437 -0.00089239 v Velocity[Z] -3.0141 2.9928 2.8125e-06 -5.3872e-08 v ǁVelocityǁ 0.00052445 32.87 7.3776 8.064 v Pressure -1.0595e+05 2.4151e+05 66211 36049 v TurbVisc 5.2061e-21 0.010807 0.00015435 1.7134e-05 v CourantNb 4.7457e-08 0.011768 0.00016768 4.922e-06 v FourierNb 1.2425e-07 0.047158 0.00014578 2.495e-07 v total_pressure -4627.4 3.4283e+05 1.6754e+05 1.3737e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0839 0.099211 0.0028419 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2264e-07 0.052459 0.00031345 5.1715e-06 INSTANT 0.875624000E-01 TIME STEP NUMBER 55822 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283129694E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.775454637E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19006E-02 0.21225E+01 Friction velocity uk : 0.19006E-02 0.21225E+01 Dimensionless distance yplus : 0.18406E-02 0.20841E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 3.154106495e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29461E+08 1 0.17974E-09 0.24432E+02 0.19267E+04 c Velocity[X] 0.12510E+02 c Velocity[Y] 0.11922E+02 c Velocity[Z] 0.18928E-05 c Pressure 0.15949E-03 302 0.93221E-04 0.18063E-02 0.18830E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -20.892 32.812 5.6121 8.0053 v Velocity[Y] -23.184 24.562 -0.1437 -0.00089416 v Velocity[Z] -3.0139 2.9931 2.8117e-06 -5.3872e-08 v ǁVelocityǁ 0.00050199 32.889 7.3793 8.0642 v Pressure -1.0718e+05 2.4028e+05 65021 35387 v TurbVisc 6.0788e-21 0.010826 0.00015443 1.7164e-05 v CourantNb 4.9248e-08 0.011768 0.00016768 4.9222e-06 v FourierNb 1.2425e-07 0.047158 0.00014578 2.4971e-07 v total_pressure -5858.8 3.416e+05 1.6635e+05 1.3671e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0841 0.099213 0.0028418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2265e-07 0.05246 0.00031346 5.1719e-06 INSTANT 0.875625000E-01 TIME STEP NUMBER 55823 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283135257E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.775968129E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.29404E-02 0.21226E+01 Friction velocity uk : 0.29404E-02 0.21226E+01 Dimensionless distance yplus : 0.28476E-02 0.20842E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 2.723306549e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29461E+08 1 0.17975E-09 0.24433E+02 0.19267E+04 c Velocity[X] 0.12511E+02 c Velocity[Y] 0.11923E+02 c Velocity[Z] 0.18935E-05 c Pressure 0.16326E-03 111 0.79187E-04 0.18476E-02 0.19161E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -20.904 32.831 5.6122 8.0054 v Velocity[Y] -23.198 24.578 -0.1437 -0.00089727 v Velocity[Z] -3.0138 2.9933 2.8109e-06 -5.3872e-08 v ǁVelocityǁ 0.00048243 32.908 7.3809 8.0644 v Pressure -1.0844e+05 2.3902e+05 63802 34659 v TurbVisc 4.0071e-21 0.010846 0.0001545 1.7194e-05 v CourantNb 5.1177e-08 0.011768 0.00016768 4.9223e-06 v FourierNb 1.2425e-07 0.047158 0.00014578 2.4991e-07 v total_pressure -7115 3.4035e+05 1.6513e+05 1.3598e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0842 0.099215 0.0028416 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2267e-07 0.052461 0.00031346 5.1722e-06 INSTANT 0.875626000E-01 TIME STEP NUMBER 55824 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283140840E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.776475782E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.35277E-02 0.21227E+01 Friction velocity uk : 0.35277E-02 0.21227E+01 Dimensionless distance yplus : 0.34163E-02 0.20843E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 2.341045459e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29462E+08 1 0.17977E-09 0.24443E+02 0.19270E+04 c Velocity[X] 0.12512E+02 c Velocity[Y] 0.11930E+02 c Velocity[Z] 0.19074E-05 c Pressure 0.16525E-03 9 0.56442E-04 0.18687E-02 0.16519E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -20.917 32.85 5.6122 8.0055 v Velocity[Y] -23.212 24.593 -0.14369 -0.00090112 v Velocity[Z] -3.0136 2.9935 2.8101e-06 -5.3872e-08 v ǁVelocityǁ 0.0004703 32.928 7.3826 8.0647 v Pressure -1.0973e+05 2.3775e+05 62552 34017 v TurbVisc 5.564e-21 0.010865 0.00015458 1.7224e-05 v CourantNb 5.3135e-08 0.011767 0.00016769 4.9224e-06 v FourierNb 1.2425e-07 0.047158 0.00014578 2.5012e-07 v total_pressure -8401.5 3.3908e+05 1.6388e+05 1.3534e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0843 0.099215 0.0028414 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2268e-07 0.052461 0.00031346 5.1725e-06 INSTANT 0.875627000E-01 TIME STEP NUMBER 55825 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283146285E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.776977013E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.41047E-02 0.21228E+01 Friction velocity uk : 0.41047E-02 0.21228E+01 Dimensionless distance yplus : 0.39751E-02 0.20844E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.961188484e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29462E+08 1 0.17979E-09 0.24446E+02 0.19271E+04 c Velocity[X] 0.12513E+02 c Velocity[Y] 0.11933E+02 c Velocity[Z] 0.18985E-05 c Pressure 0.16918E-03 134 0.99968E-04 0.19118E-02 0.21367E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -20.929 32.87 5.6122 8.0056 v Velocity[Y] -23.226 24.609 -0.14369 -0.00090459 v Velocity[Z] -3.0134 2.9937 2.8094e-06 -5.3872e-08 v ǁVelocityǁ 0.00045356 32.947 7.3842 8.0649 v Pressure -1.111e+05 2.3639e+05 61270 33213 v TurbVisc 1.0915e-20 0.010884 0.00015466 1.7254e-05 v CourantNb 5.5826e-08 0.011767 0.00016769 4.9225e-06 v FourierNb 1.2425e-07 0.047158 0.00014578 2.5033e-07 v total_pressure -9776.9 3.3772e+05 1.6259e+05 1.3454e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0844 0.099213 0.0028412 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.227e-07 0.052461 0.00031347 5.1728e-06 INSTANT 0.875628000E-01 TIME STEP NUMBER 55826 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283151624E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.777472263E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.41475E-02 0.21229E+01 Friction velocity uk : 0.41475E-02 0.21229E+01 Dimensionless distance yplus : 0.40165E-02 0.20845E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.752623438e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29463E+08 1 0.17980E-09 0.24451E+02 0.19272E+04 c Velocity[X] 0.12513E+02 c Velocity[Y] 0.11937E+02 c Velocity[Z] 0.18906E-05 c Pressure 0.17222E-03 23 0.83384E-04 0.19448E-02 0.19408E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -20.941 32.889 5.6123 8.0057 v Velocity[Y] -23.241 24.625 -0.14369 -0.00090742 v Velocity[Z] -3.0133 2.9939 2.8086e-06 -5.3872e-08 v ǁVelocityǁ 0.00044441 32.966 7.3859 8.0651 v Pressure -1.125e+05 2.3505e+05 59927 32472 v TurbVisc 7.9794e-21 0.010904 0.00015473 1.7285e-05 v CourantNb 5.5818e-08 0.011767 0.00016769 4.9226e-06 v FourierNb 1.2425e-07 0.047158 0.00014578 2.5054e-07 v total_pressure -11171 3.3637e+05 1.6125e+05 1.338e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0845 0.099211 0.002841 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2271e-07 0.052461 0.00031347 5.1732e-06 INSTANT 0.875629000E-01 TIME STEP NUMBER 55827 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283156846E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.777961821E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.49002E-02 0.21230E+01 Friction velocity uk : 0.49002E-02 0.21230E+01 Dimensionless distance yplus : 0.47455E-02 0.20846E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.567729591e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29463E+08 1 0.17982E-09 0.24460E+02 0.19274E+04 c Velocity[X] 0.12515E+02 c Velocity[Y] 0.11944E+02 c Velocity[Z] 0.19044E-05 c Pressure 0.17506E-03 9 0.55378E-04 0.19753E-02 0.19112E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -20.953 32.908 5.6123 8.0058 v Velocity[Y] -23.255 24.64 -0.14368 -0.00090928 v Velocity[Z] -3.0131 2.9941 2.8078e-06 -5.3872e-08 v ǁVelocityǁ 0.00044005 32.986 7.3875 8.0653 v Pressure -1.1394e+05 2.3367e+05 58550 31754 v TurbVisc 3.3695e-21 0.010923 0.00015481 1.7315e-05 v CourantNb 4.8996e-08 0.011767 0.00016769 4.9227e-06 v FourierNb 1.2425e-07 0.047157 0.00014578 2.5075e-07 v total_pressure -12612 3.3499e+05 1.5987e+05 1.3308e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0846 0.099207 0.0028408 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2272e-07 0.052461 0.00031348 5.1735e-06 INSTANT 0.875630000E-01 TIME STEP NUMBER 55828 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283161879E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.778448318E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.41218E-02 0.21230E+01 Friction velocity uk : 0.41218E-02 0.21230E+01 Dimensionless distance yplus : 0.39916E-02 0.20846E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.344925344e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29463E+08 1 0.17984E-09 0.24462E+02 0.19275E+04 c Velocity[X] 0.12514E+02 c Velocity[Y] 0.11948E+02 c Velocity[Z] 0.19016E-05 c Pressure 0.17885E-03 28 0.99843E-04 0.20166E-02 0.25535E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -20.966 32.927 5.6124 8.0059 v Velocity[Y] -23.27 24.656 -0.14368 -0.00091229 v Velocity[Z] -3.013 2.9943 2.807e-06 -5.3872e-08 v ǁVelocityǁ 0.00043679 33.005 7.3892 8.0655 v Pressure -1.1545e+05 2.3221e+05 57162 30839 v TurbVisc 1.0272e-20 0.010942 0.00015489 1.7345e-05 v CourantNb 4.8834e-08 0.011767 0.00016769 4.9228e-06 v FourierNb 1.2425e-07 0.047157 0.00014578 2.5096e-07 v total_pressure -14122 3.3354e+05 1.5849e+05 1.3216e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0846 0.0992 0.0028405 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2274e-07 0.052461 0.00031348 5.1738e-06 INSTANT 0.875631000E-01 TIME STEP NUMBER 55829 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283166868E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.778928330E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.36014E-02 0.21231E+01 Friction velocity uk : 0.36014E-02 0.21231E+01 Dimensionless distance yplus : 0.34877E-02 0.20847E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.313960996e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29464E+08 1 0.17985E-09 0.24466E+02 0.19275E+04 c Velocity[X] 0.12514E+02 c Velocity[Y] 0.11952E+02 c Velocity[Z] 0.18945E-05 c Pressure 0.18174E-03 76 0.84825E-04 0.20478E-02 0.23612E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -20.978 32.947 5.6124 8.006 v Velocity[Y] -23.284 24.671 -0.14368 -0.0009156 v Velocity[Z] -3.0128 2.9945 2.8062e-06 -5.3872e-08 v ǁVelocityǁ 0.00043642 33.024 7.3908 8.0658 v Pressure -1.1698e+05 2.3076e+05 55714 29978 v TurbVisc 8.9433e-21 0.010962 0.00015496 1.7376e-05 v CourantNb 4.5981e-08 0.011767 0.0001677 4.9229e-06 v FourierNb 1.2425e-07 0.047156 0.00014579 2.5117e-07 v total_pressure -15654 3.3209e+05 1.5704e+05 1.313e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0847 0.099195 0.0028402 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2275e-07 0.052461 0.00031348 5.1741e-06 INSTANT 0.875632000E-01 TIME STEP NUMBER 55830 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283171713E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.779401073E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19218E-02 0.21231E+01 Friction velocity uk : 0.19218E-02 0.21231E+01 Dimensionless distance yplus : 0.18611E-02 0.20847E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.310928793e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29464E+08 1 0.17987E-09 0.24474E+02 0.19278E+04 c Velocity[X] 0.12515E+02 c Velocity[Y] 0.11959E+02 c Velocity[Z] 0.18953E-05 c Pressure 0.18441E-03 10 0.57579E-04 0.20763E-02 0.22040E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -20.99 32.966 5.6124 8.0061 v Velocity[Y] -23.299 24.687 -0.14367 -0.0009196 v Velocity[Z] -3.0126 2.9948 2.8054e-06 -5.3872e-08 v ǁVelocityǁ 0.00043684 33.044 7.3925 8.066 v Pressure -1.1854e+05 2.293e+05 54242 29202 v TurbVisc 9.2607e-21 0.010981 0.00015504 1.7406e-05 v CourantNb 4.5953e-08 0.011767 0.0001677 4.9231e-06 v FourierNb 1.2425e-07 0.047155 0.00014579 2.5138e-07 v total_pressure -17210 3.3062e+05 1.5557e+05 1.3053e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0847 0.09919 0.0028399 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2276e-07 0.05246 0.00031349 5.1744e-06 INSTANT 0.875633000E-01 TIME STEP NUMBER 55831 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283176442E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.779869227E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.36378E-02 0.21231E+01 Friction velocity uk : 0.36378E-02 0.21231E+01 Dimensionless distance yplus : 0.35230E-02 0.20847E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.164977100e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29465E+08 1 0.17989E-09 0.24478E+02 0.19279E+04 c Velocity[X] 0.12516E+02 c Velocity[Y] 0.11963E+02 c Velocity[Z] 0.18936E-05 c Pressure 0.18793E-03 371 0.77554E-04 0.21144E-02 0.26683E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -21.003 32.985 5.6125 8.0062 v Velocity[Y] -23.313 24.703 -0.14367 -0.00092193 v Velocity[Z] -3.0125 2.995 2.8046e-06 -5.3872e-08 v ǁVelocityǁ 0.00044309 33.063 7.3941 8.0662 v Pressure -1.2017e+05 2.2776e+05 52775 28359 v TurbVisc 5.6405e-21 0.011 0.00015511 1.7437e-05 v CourantNb 4.5444e-08 0.011766 0.0001677 4.9232e-06 v FourierNb 1.2425e-07 0.047155 0.00014579 2.5158e-07 v total_pressure -18848 3.2908e+05 1.541e+05 1.2968e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0847 0.099183 0.0028396 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2278e-07 0.05246 0.00031349 5.1747e-06 INSTANT 0.875634000E-01 TIME STEP NUMBER 55832 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283181030E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.780327444E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.33816E-02 0.21231E+01 Friction velocity uk : 0.33816E-02 0.21231E+01 Dimensionless distance yplus : 0.32749E-02 0.20847E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.316421112e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29465E+08 1 0.17990E-09 0.24484E+02 0.19280E+04 c Velocity[X] 0.12515E+02 c Velocity[Y] 0.11968E+02 c Velocity[Z] 0.18915E-05 c Pressure 0.19094E-03 93 0.82486E-04 0.21467E-02 0.29629E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -21.015 33.004 5.6125 8.0063 v Velocity[Y] -23.328 24.718 -0.14366 -0.00092629 v Velocity[Z] -3.0123 2.9952 2.8038e-06 -5.3872e-08 v ǁVelocityǁ 0.00043857 33.082 7.3958 8.0664 v Pressure -1.2182e+05 2.2623e+05 51221 27410 v TurbVisc 1.0584e-20 0.01102 0.00015519 1.7467e-05 v CourantNb 4.5218e-08 0.011766 0.0001677 4.9233e-06 v FourierNb 1.2425e-07 0.047154 0.00014579 2.518e-07 v total_pressure -20499 3.2755e+05 1.5255e+05 1.2874e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0847 0.099178 0.0028394 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2279e-07 0.052459 0.00031349 5.1751e-06 INSTANT 0.875635000E-01 TIME STEP NUMBER 55833 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283185550E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.780782816E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.29874E-02 0.21231E+01 Friction velocity uk : 0.29874E-02 0.21231E+01 Dimensionless distance yplus : 0.28931E-02 0.20847E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.426726102e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29466E+08 1 0.17992E-09 0.24489E+02 0.19281E+04 c Velocity[X] 0.12516E+02 c Velocity[Y] 0.11972E+02 c Velocity[Z] 0.18915E-05 c Pressure 0.19400E-03 237 0.95591E-04 0.21794E-02 0.26188E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -21.028 33.023 5.6125 8.0064 v Velocity[Y] -23.342 24.733 -0.14366 -0.00092823 v Velocity[Z] -3.0122 2.9954 2.803e-06 -5.3872e-08 v ǁVelocityǁ 0.0004362 33.102 7.3974 8.0666 v Pressure -1.2352e+05 2.2467e+05 49689 26636 v TurbVisc 8.9275e-21 0.011039 0.00015527 1.7498e-05 v CourantNb 4.5076e-08 0.011766 0.00016771 4.9234e-06 v FourierNb 1.2425e-07 0.047153 0.00014579 2.5201e-07 v total_pressure -22197 3.2599e+05 1.5101e+05 1.2796e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0847 0.099173 0.0028392 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.228e-07 0.052459 0.0003135 5.1754e-06 INSTANT 0.875636000E-01 TIME STEP NUMBER 55834 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283189773E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.781230360E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.21722E-02 0.21231E+01 Friction velocity uk : 0.21722E-02 0.21231E+01 Dimensionless distance yplus : 0.21036E-02 0.20847E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.570835337e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29466E+08 1 0.17994E-09 0.24487E+02 0.19280E+04 c Velocity[X] 0.12515E+02 c Velocity[Y] 0.11971E+02 c Velocity[Z] 0.18925E-05 c Pressure 0.19693E-03 124 0.81261E-04 0.22108E-02 0.30930E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -21.04 33.042 5.6125 8.0065 v Velocity[Y] -23.357 24.749 -0.14365 -0.00093169 v Velocity[Z] -3.012 2.9956 2.8022e-06 -5.3872e-08 v ǁVelocityǁ 0.00043567 33.121 7.3991 8.0668 v Pressure -1.2526e+05 2.2307e+05 48095 25649 v TurbVisc 2.4589e-21 0.011058 0.00015534 1.7529e-05 v CourantNb 4.4926e-08 0.011766 0.00016771 4.9235e-06 v FourierNb 1.2425e-07 0.047152 0.00014579 2.5222e-07 v total_pressure -23931 3.244e+05 1.4942e+05 1.2697e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0847 0.099169 0.002839 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2281e-07 0.052458 0.0003135 5.1757e-06 INSTANT 0.875637000E-01 TIME STEP NUMBER 55835 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283193959E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.781668666E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.27834E-02 0.21231E+01 Friction velocity uk : 0.27834E-02 0.21231E+01 Dimensionless distance yplus : 0.26955E-02 0.20847E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.725099415e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29466E+08 1 0.17995E-09 0.24494E+02 0.19282E+04 c Velocity[X] 0.12516E+02 c Velocity[Y] 0.11978E+02 c Velocity[Z] 0.19007E-05 c Pressure 0.19828E-03 10 0.59319E-04 0.22243E-02 0.25941E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -21.053 33.062 5.6126 8.0065 v Velocity[Y] -23.371 24.764 -0.14365 -0.00093592 v Velocity[Z] -3.0118 2.9958 2.8014e-06 -5.3872e-08 v ǁVelocityǁ 0.00043545 33.14 7.4008 8.067 v Pressure -1.27e+05 2.2149e+05 46503 24817 v TurbVisc 9.8303e-21 0.011078 0.00015542 1.756e-05 v CourantNb 4.4932e-08 0.011766 0.00016771 4.9236e-06 v FourierNb 1.2425e-07 0.047151 0.0001458 2.5243e-07 v total_pressure -25675 3.2281e+05 1.4783e+05 1.2614e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0847 0.099167 0.0028388 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2283e-07 0.052457 0.00031351 5.176e-06 INSTANT 0.875638000E-01 TIME STEP NUMBER 55836 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283197955E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.782098703E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.40601E-02 0.21231E+01 Friction velocity uk : 0.40601E-02 0.21231E+01 Dimensionless distance yplus : 0.39319E-02 0.20847E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.908321763e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29467E+08 1 0.17997E-09 0.24497E+02 0.19283E+04 c Velocity[X] 0.12516E+02 c Velocity[Y] 0.11981E+02 c Velocity[Z] 0.18987E-05 c Pressure 0.20123E-03 148 0.76988E-04 0.22558E-02 0.33557E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -21.065 33.081 5.6126 8.0066 v Velocity[Y] -23.386 24.779 -0.14364 -0.00093842 v Velocity[Z] -3.0117 2.996 2.8006e-06 -5.3872e-08 v ǁVelocityǁ 0.00043665 33.159 7.4024 8.0672 v Pressure -1.2883e+05 2.1981e+05 44868 23848 v TurbVisc 9.0702e-21 0.011097 0.00015549 1.759e-05 v CourantNb 4.4916e-08 0.011766 0.00016771 4.9237e-06 v FourierNb 1.2425e-07 0.04715 0.0001458 2.5264e-07 v total_pressure -27507 3.2114e+05 1.4619e+05 1.2517e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0847 0.099163 0.0028387 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2284e-07 0.052456 0.00031351 5.1763e-06 INSTANT 0.875639000E-01 TIME STEP NUMBER 55837 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283201847E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.782517652E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.37892E-02 0.21230E+01 Friction velocity uk : 0.37892E-02 0.21230E+01 Dimensionless distance yplus : 0.36696E-02 0.20846E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 2.072960860e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29467E+08 1 0.17999E-09 0.24502E+02 0.19284E+04 c Velocity[X] 0.12515E+02 c Velocity[Y] 0.11986E+02 c Velocity[Z] 0.18967E-05 c Pressure 0.20383E-03 38 0.82678E-04 0.22832E-02 0.35847E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -21.078 33.1 5.6126 8.0067 v Velocity[Y] -23.4 24.795 -0.14364 -0.00094299 v Velocity[Z] -3.0115 2.9962 2.7998e-06 -5.3872e-08 v ǁVelocityǁ 0.00043836 33.179 7.4041 8.0674 v Pressure -1.3066e+05 2.1817e+05 43175 22808 v TurbVisc 9.533e-21 0.011116 0.00015557 1.7621e-05 v CourantNb 4.4856e-08 0.011766 0.00016771 4.9238e-06 v FourierNb 1.2425e-07 0.047149 0.0001458 2.5286e-07 v total_pressure -29338 3.195e+05 1.445e+05 1.2413e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0846 0.099164 0.0028386 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2285e-07 0.052455 0.00031351 5.1766e-06 INSTANT 0.875640000E-01 TIME STEP NUMBER 55838 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283205652E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.782936404E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.29996E-02 0.21230E+01 Friction velocity uk : 0.29996E-02 0.21230E+01 Dimensionless distance yplus : 0.29049E-02 0.20846E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 2.353475058e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29467E+08 1 0.18000E-09 0.24506E+02 0.19285E+04 c Velocity[X] 0.12516E+02 c Velocity[Y] 0.11990E+02 c Velocity[Z] 0.18946E-05 c Pressure 0.20640E-03 198 0.95690E-04 0.23103E-02 0.31422E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -21.09 33.119 5.6126 8.0068 v Velocity[Y] -23.415 24.81 -0.14364 -0.00094511 v Velocity[Z] -3.0113 2.9965 2.7991e-06 -5.3872e-08 v ǁVelocityǁ 0.00044052 33.198 7.4057 8.0675 v Pressure -1.3253e+05 2.1651e+05 41511 21962 v TurbVisc 9.2865e-21 0.011136 0.00015564 1.7652e-05 v CourantNb 4.4934e-08 0.011765 0.00016772 4.9239e-06 v FourierNb 1.2425e-07 0.047147 0.0001458 2.5307e-07 v total_pressure -31201 3.1783e+05 1.4284e+05 1.2329e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0846 0.099165 0.0028385 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2286e-07 0.052454 0.00031352 5.177e-06 INSTANT 0.875641000E-01 TIME STEP NUMBER 55839 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283209151E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.783346101E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.27063E-02 0.21229E+01 Friction velocity uk : 0.27063E-02 0.21229E+01 Dimensionless distance yplus : 0.26208E-02 0.20845E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 2.597211246e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29468E+08 1 0.18002E-09 0.24503E+02 0.19283E+04 c Velocity[X] 0.12515E+02 c Velocity[Y] 0.11988E+02 c Velocity[Z] 0.18956E-05 c Pressure 0.20883E-03 134 0.81365E-04 0.23359E-02 0.37342E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -21.103 33.138 5.6127 8.0068 v Velocity[Y] -23.43 24.825 -0.14363 -0.00094877 v Velocity[Z] -3.0112 2.9967 2.7983e-06 -5.3872e-08 v ǁVelocityǁ 0.00044366 33.217 7.4074 8.0677 v Pressure -1.3442e+05 2.148e+05 39789 20894 v TurbVisc 7.2446e-21 0.011155 0.00015572 1.7684e-05 v CourantNb 4.4968e-08 0.011765 0.00016772 4.924e-06 v FourierNb 1.2425e-07 0.047146 0.0001458 2.5329e-07 v total_pressure -33097 3.1613e+05 1.4111e+05 1.2222e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0845 0.099167 0.0028385 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2287e-07 0.052453 0.00031352 5.1773e-06 INSTANT 0.875642000E-01 TIME STEP NUMBER 55840 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283212599E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.783744522E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.32758E-02 0.21229E+01 Friction velocity uk : 0.32758E-02 0.21229E+01 Dimensionless distance yplus : 0.31724E-02 0.20845E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 2.815581221e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29468E+08 1 0.18003E-09 0.24510E+02 0.19285E+04 c Velocity[X] 0.12516E+02 c Velocity[Y] 0.11994E+02 c Velocity[Z] 0.19032E-05 c Pressure 0.20973E-03 10 0.60273E-04 0.23442E-02 0.31115E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -21.116 33.157 5.6127 8.0069 v Velocity[Y] -23.444 24.84 -0.14363 -0.00095321 v Velocity[Z] -3.011 2.9969 2.7975e-06 -5.3872e-08 v ǁVelocityǁ 0.00044232 33.236 7.409 8.0679 v Pressure -1.3631e+05 2.1312e+05 38075 20001 v TurbVisc 8.8615e-21 0.011174 0.0001558 1.7715e-05 v CourantNb 4.5073e-08 0.011765 0.00016772 4.9241e-06 v FourierNb 1.2425e-07 0.047145 0.0001458 2.535e-07 v total_pressure -34990 3.1445e+05 1.394e+05 1.2133e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0845 0.099172 0.0028386 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2288e-07 0.052452 0.00031353 5.1776e-06 INSTANT 0.875643000E-01 TIME STEP NUMBER 55841 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283215841E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.784132596E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.20064E-02 0.21229E+01 Friction velocity uk : 0.20064E-02 0.21229E+01 Dimensionless distance yplus : 0.19430E-02 0.20845E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 3.046371604e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29468E+08 1 0.18005E-09 0.24512E+02 0.19285E+04 c Velocity[X] 0.12516E+02 c Velocity[Y] 0.11997E+02 c Velocity[Z] 0.18997E-05 c Pressure 0.21214E-03 149 0.77260E-04 0.23694E-02 0.40222E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -21.128 33.176 5.6127 8.007 v Velocity[Y] -23.459 24.855 -0.14363 -0.00095591 v Velocity[Z] -3.0109 2.9971 2.7967e-06 -5.3873e-08 v ǁVelocityǁ 0.00045037 33.256 7.4107 8.0681 v Pressure -1.3829e+05 2.1135e+05 36326 18960 v TurbVisc 8.0864e-21 0.011194 0.00015587 1.7745e-05 v CourantNb 4.5092e-08 0.011765 0.00016772 4.9242e-06 v FourierNb 1.2425e-07 0.047144 0.00014581 2.5371e-07 v total_pressure -36965 3.1268e+05 1.3765e+05 1.2028e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0845 0.099176 0.0028386 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.229e-07 0.052451 0.00031353 5.1779e-06 INSTANT 0.875644000E-01 TIME STEP NUMBER 55842 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283218979E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.784507520E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.41876E-02 0.21228E+01 Friction velocity uk : 0.41876E-02 0.21228E+01 Dimensionless distance yplus : 0.40554E-02 0.20844E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 3.177960992e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29469E+08 1 0.18006E-09 0.24516E+02 0.19286E+04 c Velocity[X] 0.12515E+02 c Velocity[Y] 0.12001E+02 c Velocity[Z] 0.18957E-05 c Pressure 0.21420E-03 29 0.83382E-04 0.23907E-02 0.42665E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -21.141 33.195 5.6128 8.007 v Velocity[Y] -23.473 24.87 -0.14363 -0.00096072 v Velocity[Z] -3.0107 2.9973 2.7959e-06 -5.3873e-08 v ǁVelocityǁ 0.0004539 33.275 7.4124 8.0683 v Pressure -1.4025e+05 2.0962e+05 34518 17852 v TurbVisc 8.3554e-21 0.011213 0.00015595 1.7777e-05 v CourantNb 4.5017e-08 0.011765 0.00016773 4.9243e-06 v FourierNb 1.2425e-07 0.047142 0.00014581 2.5393e-07 v total_pressure -38926 3.1094e+05 1.3584e+05 1.1918e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0844 0.099185 0.0028387 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2291e-07 0.05245 0.00031354 5.1782e-06 INSTANT 0.875645000E-01 TIME STEP NUMBER 55843 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283222014E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.784880616E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.58458E-02 0.21228E+01 Friction velocity uk : 0.58458E-02 0.21228E+01 Dimensionless distance yplus : 0.56612E-02 0.20844E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 3.451364135e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29469E+08 1 0.18008E-09 0.24520E+02 0.19287E+04 c Velocity[X] 0.12516E+02 c Velocity[Y] 0.12004E+02 c Velocity[Z] 0.18919E-05 c Pressure 0.21624E-03 230 0.96463E-04 0.24118E-02 0.37450E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -21.154 33.214 5.6128 8.0071 v Velocity[Y] -23.488 24.885 -0.14363 -0.00096303 v Velocity[Z] -3.0105 2.9975 2.7951e-06 -5.3873e-08 v ǁVelocityǁ 0.00045758 33.294 7.414 8.0684 v Pressure -1.4224e+05 2.0787e+05 32747 16947 v TurbVisc 8.1412e-21 0.011232 0.00015602 1.7808e-05 v CourantNb 4.5013e-08 0.011765 0.00016773 4.9244e-06 v FourierNb 1.2425e-07 0.047141 0.00014581 2.5415e-07 v total_pressure -40912 3.0919e+05 1.3407e+05 1.1827e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0844 0.099195 0.0028389 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2292e-07 0.052449 0.00031354 5.1785e-06 INSTANT 0.875646000E-01 TIME STEP NUMBER 55844 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283224732E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.785243577E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.94784E-02 0.21228E+01 Friction velocity uk : 0.94784E-02 0.21228E+01 Dimensionless distance yplus : 0.92258E-02 0.20844E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 3.646129602e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29469E+08 1 0.18009E-09 0.24517E+02 0.19285E+04 c Velocity[X] 0.12516E+02 c Velocity[Y] 0.12001E+02 c Velocity[Z] 0.18911E-05 c Pressure 0.21815E-03 137 0.82031E-04 0.24313E-02 0.44187E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -21.166 33.233 5.6128 8.0071 v Velocity[Y] -23.502 24.899 -0.14363 -0.00096692 v Velocity[Z] -3.0104 2.9977 2.7943e-06 -5.3873e-08 v ǁVelocityǁ 0.00046207 33.313 7.4157 8.0686 v Pressure -1.4424e+05 2.0608e+05 30925 15821 v TurbVisc 9.464e-21 0.011251 0.00015609 1.784e-05 v CourantNb 4.4893e-08 0.011764 0.00016773 4.9244e-06 v FourierNb 1.2425e-07 0.04714 0.00014581 2.5436e-07 v total_pressure -42919 3.0741e+05 1.3225e+05 1.1715e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0844 0.099206 0.002839 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2293e-07 0.052448 0.00031354 5.1788e-06 INSTANT 0.875647000E-01 TIME STEP NUMBER 55845 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283227393E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.785593932E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.90560E-02 0.21228E+01 Friction velocity uk : 0.90560E-02 0.21228E+01 Dimensionless distance yplus : 0.88660E-02 0.20844E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 3.799139109e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29469E+08 1 0.18010E-09 0.24523E+02 0.19287E+04 c Velocity[X] 0.12517E+02 c Velocity[Y] 0.12007E+02 c Velocity[Z] 0.18975E-05 c Pressure 0.21854E-03 10 0.61232E-04 0.24339E-02 0.37079E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -21.179 33.252 5.6129 8.0072 v Velocity[Y] -23.517 24.914 -0.14363 -0.0009716 v Velocity[Z] -3.0102 2.9979 2.7935e-06 -5.3873e-08 v ǁVelocityǁ 0.00045883 33.332 7.4174 8.0688 v Pressure -1.4624e+05 2.0433e+05 29112 14875 v TurbVisc 7.5883e-21 0.011271 0.00015617 1.7871e-05 v CourantNb 4.4787e-08 0.011764 0.00016774 4.9245e-06 v FourierNb 1.2425e-07 0.047139 0.00014581 2.5458e-07 v total_pressure -44912 3.0565e+05 1.3044e+05 1.162e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0844 0.099218 0.0028392 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2294e-07 0.052447 0.00031355 5.1791e-06 INSTANT 0.875648000E-01 TIME STEP NUMBER 55846 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283229833E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.785932672E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.72845E-02 0.21228E+01 Friction velocity uk : 0.72845E-02 0.21228E+01 Dimensionless distance yplus : 0.71316E-02 0.20844E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 3.958031713e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29470E+08 1 0.18012E-09 0.24526E+02 0.19287E+04 c Velocity[X] 0.12517E+02 c Velocity[Y] 0.12009E+02 c Velocity[Z] 0.18914E-05 c Pressure 0.22043E-03 155 0.78170E-04 0.24532E-02 0.47738E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -21.192 33.271 5.6129 8.0072 v Velocity[Y] -23.532 24.929 -0.14363 -0.00097452 v Velocity[Z] -3.01 2.9981 2.7928e-06 -5.3873e-08 v ǁVelocityǁ 0.00047196 33.351 7.419 8.069 v Pressure -1.4831e+05 2.0248e+05 27276 13774 v TurbVisc 7.0841e-21 0.01129 0.00015624 1.7902e-05 v CourantNb 4.4586e-08 0.011764 0.00016774 4.9246e-06 v FourierNb 1.2425e-07 0.047138 0.00014581 2.5479e-07 v total_pressure -46980 3.038e+05 1.286e+05 1.151e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0844 0.099229 0.0028394 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2295e-07 0.052447 0.00031355 5.1794e-06 INSTANT 0.875649000E-01 TIME STEP NUMBER 55847 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283232169E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.786257709E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.78639E-02 0.21228E+01 Friction velocity uk : 0.78639E-02 0.21228E+01 Dimensionless distance yplus : 0.76990E-02 0.20844E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 3.963755705e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29470E+08 1 0.18013E-09 0.24530E+02 0.19288E+04 c Velocity[X] 0.12517E+02 c Velocity[Y] 0.12013E+02 c Velocity[Z] 0.18847E-05 c Pressure 0.22194E-03 29 0.84295E-04 0.24683E-02 0.49994E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -21.205 33.29 5.6129 8.0073 v Velocity[Y] -23.546 24.943 -0.14363 -0.00097958 v Velocity[Z] -3.0099 2.9983 2.792e-06 -5.3873e-08 v ǁVelocityǁ 0.00047768 33.37 7.4207 8.0691 v Pressure -1.5035e+05 2.0067e+05 25380 12615 v TurbVisc 6.858e-21 0.011309 0.00015632 1.7934e-05 v CourantNb 4.411e-08 0.011764 0.00016774 4.9247e-06 v FourierNb 1.2425e-07 0.047137 0.00014581 2.5501e-07 v total_pressure -49025 3.02e+05 1.267e+05 1.1394e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0844 0.099244 0.0028396 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2296e-07 0.052446 0.00031356 5.1797e-06 INSTANT 0.875650000E-01 TIME STEP NUMBER 55848 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283234394E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.786578859E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.52678E-02 0.21228E+01 Friction velocity uk : 0.52678E-02 0.21228E+01 Dimensionless distance yplus : 0.51573E-02 0.20844E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 4.143423540e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29470E+08 1 0.18014E-09 0.24533E+02 0.19289E+04 c Velocity[X] 0.12518E+02 c Velocity[Y] 0.12015E+02 c Velocity[Z] 0.18776E-05 c Pressure 0.22346E-03 230 0.97542E-04 0.24834E-02 0.43831E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -21.217 33.308 5.613 8.0073 v Velocity[Y] -23.561 24.958 -0.14363 -0.00098211 v Velocity[Z] -3.0097 2.9986 2.7912e-06 -5.3873e-08 v ǁVelocityǁ 0.00048434 33.389 7.4224 8.0693 v Pressure -1.5241e+05 1.9885e+05 23529 11665 v TurbVisc 6.5194e-21 0.011329 0.00015639 1.7965e-05 v CourantNb 4.3755e-08 0.011764 0.00016775 4.9248e-06 v FourierNb 1.2425e-07 0.047136 0.00014582 2.5523e-07 v total_pressure -51083 3.0018e+05 1.2485e+05 1.1299e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0844 0.099259 0.0028399 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2297e-07 0.052445 0.00031356 5.18e-06 INSTANT 0.875651000E-01 TIME STEP NUMBER 55849 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283236290E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.786889714E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.45893E-02 0.21229E+01 Friction velocity uk : 0.45893E-02 0.21229E+01 Dimensionless distance yplus : 0.44930E-02 0.20845E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 4.215832828e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29470E+08 1 0.18015E-09 0.24530E+02 0.19287E+04 c Velocity[X] 0.12518E+02 c Velocity[Y] 0.12012E+02 c Velocity[Z] 0.18757E-05 c Pressure 0.22483E-03 99 0.83019E-04 0.24968E-02 0.51455E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -21.23 33.327 5.613 8.0074 v Velocity[Y] -23.575 24.973 -0.14363 -0.00098625 v Velocity[Z] -3.0095 2.9988 2.7904e-06 -5.3873e-08 v ǁVelocityǁ 0.00049269 33.408 7.424 8.0694 v Pressure -1.5448e+05 1.97e+05 21630 10492 v TurbVisc 7.7277e-21 0.011348 0.00015647 1.7997e-05 v CourantNb 4.3301e-08 0.011764 0.00016775 4.9249e-06 v FourierNb 1.2425e-07 0.047136 0.00014582 2.5545e-07 v total_pressure -53156 2.9833e+05 1.2296e+05 1.1182e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0845 0.099273 0.0028401 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2298e-07 0.052445 0.00031357 5.1803e-06 INSTANT 0.875652000E-01 TIME STEP NUMBER 55850 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283238124E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.787186632E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.51117E-02 0.21229E+01 Friction velocity uk : 0.51117E-02 0.21229E+01 Dimensionless distance yplus : 0.50044E-02 0.20845E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 4.243172288e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29470E+08 1 0.18017E-09 0.24536E+02 0.19289E+04 c Velocity[X] 0.12520E+02 c Velocity[Y] 0.12017E+02 c Velocity[Z] 0.18791E-05 c Pressure 0.22468E-03 10 0.62213E-04 0.24934E-02 0.42971E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -21.243 33.346 5.613 8.0074 v Velocity[Y] -23.59 24.987 -0.14364 -0.00099117 v Velocity[Z] -3.0094 2.999 2.7896e-06 -5.3873e-08 v ǁVelocityǁ 0.00049066 33.426 7.4257 8.0696 v Pressure -1.5653e+05 1.9518e+05 19745 9507.6 v TurbVisc 5.9997e-21 0.011367 0.00015654 1.8028e-05 v CourantNb 4.583e-08 0.011764 0.00016775 4.925e-06 v FourierNb 1.2425e-07 0.047135 0.00014582 2.5566e-07 v total_pressure -55205 2.965e+05 1.2107e+05 1.1083e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0845 0.099289 0.0028403 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2299e-07 0.052445 0.00031357 5.1806e-06 INSTANT 0.875653000E-01 TIME STEP NUMBER 55851 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283239729E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.787471041E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.33990E-02 0.21230E+01 Friction velocity uk : 0.33990E-02 0.21230E+01 Dimensionless distance yplus : 0.33277E-02 0.20846E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 4.270373948e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29470E+08 1 0.18018E-09 0.24539E+02 0.19289E+04 c Velocity[X] 0.12521E+02 c Velocity[Y] 0.12018E+02 c Velocity[Z] 0.18672E-05 c Pressure 0.22605E-03 129 0.79117E-04 0.25069E-02 0.54481E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -21.256 33.364 5.6131 8.0074 v Velocity[Y] -23.604 25.001 -0.14364 -0.00099434 v Velocity[Z] -3.0092 2.9992 2.7888e-06 -5.3873e-08 v ǁVelocityǁ 0.00051344 33.445 7.4274 8.0697 v Pressure -1.5865e+05 1.9327e+05 17853 8373.8 v TurbVisc 6.1994e-21 0.011387 0.00015661 1.806e-05 v CourantNb 4.5266e-08 0.011763 0.00016775 4.9251e-06 v FourierNb 1.2425e-07 0.047135 0.00014582 2.5588e-07 v total_pressure -57323 2.9459e+05 1.1918e+05 1.097e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0846 0.099304 0.0028405 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.23e-07 0.052445 0.00031357 5.1809e-06 INSTANT 0.875654000E-01 TIME STEP NUMBER 55852 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283241233E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.787741532E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.54661E-02 0.21231E+01 Friction velocity uk : 0.54661E-02 0.21231E+01 Dimensionless distance yplus : 0.53515E-02 0.20847E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 4.141909364e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29471E+08 1 0.18019E-09 0.24543E+02 0.19290E+04 c Velocity[X] 0.12522E+02 c Velocity[Y] 0.12021E+02 c Velocity[Z] 0.18559E-05 c Pressure 0.22699E-03 30 0.85178E-04 0.25155E-02 0.57569E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -21.268 33.383 5.6131 8.0075 v Velocity[Y] -23.618 25.016 -0.14364 -0.00099966 v Velocity[Z] -3.009 2.9994 2.7881e-06 -5.3873e-08 v ǁVelocityǁ 0.00052637 33.464 7.429 8.0699 v Pressure -1.6074e+05 1.914e+05 15887 7160 v TurbVisc 5.312e-21 0.011406 0.00015669 1.8092e-05 v CourantNb 4.4635e-08 0.011763 0.00016776 4.9251e-06 v FourierNb 1.2425e-07 0.047134 0.00014582 2.561e-07 v total_pressure -59410 2.9272e+05 1.1721e+05 1.0849e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0847 0.099321 0.0028408 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2301e-07 0.052445 0.00031358 5.1812e-06 INSTANT 0.875655000E-01 TIME STEP NUMBER 55853 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283242613E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.788006233E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.79042E-02 0.21232E+01 Friction velocity uk : 0.79042E-02 0.21232E+01 Dimensionless distance yplus : 0.76146E-02 0.20848E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 4.205719839e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29471E+08 1 0.18020E-09 0.24546E+02 0.19291E+04 c Velocity[X] 0.12523E+02 c Velocity[Y] 0.12023E+02 c Velocity[Z] 0.18494E-05 c Pressure 0.22799E-03 156 0.98676E-04 0.25248E-02 0.48999E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -21.281 33.401 5.6132 8.0075 v Velocity[Y] -23.633 25.03 -0.14365 -0.0010024 v Velocity[Z] -3.0089 2.9996 2.7873e-06 -5.3873e-08 v ǁVelocityǁ 0.00054285 33.482 7.4307 8.07 v Pressure -1.6282e+05 1.8952e+05 13989 6189.9 v TurbVisc 4.797e-21 0.011425 0.00015676 1.8124e-05 v CourantNb 4.436e-08 0.011763 0.00016776 4.9252e-06 v FourierNb 1.2425e-07 0.047134 0.00014582 2.5632e-07 v total_pressure -61500 2.9084e+05 1.1531e+05 1.0751e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0848 0.099338 0.002841 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2301e-07 0.052445 0.00031358 5.1815e-06 INSTANT 0.875656000E-01 TIME STEP NUMBER 55854 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283243654E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.788261428E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.96553E-02 0.21233E+01 Friction velocity uk : 0.96553E-02 0.21233E+01 Dimensionless distance yplus : 0.93015E-02 0.20849E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 4.142190146e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29471E+08 1 0.18021E-09 0.24543E+02 0.19289E+04 c Velocity[X] 0.12524E+02 c Velocity[Y] 0.12019E+02 c Velocity[Z] 0.18423E-05 c Pressure 0.22882E-03 330 0.83928E-04 0.25322E-02 0.57102E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -21.294 33.419 5.6132 8.0075 v Velocity[Y] -23.647 25.044 -0.14365 -0.0010068 v Velocity[Z] -3.0087 2.9998 2.7865e-06 -5.3873e-08 v ǁVelocityǁ 0.00056018 33.501 7.4324 8.0702 v Pressure -1.6493e+05 1.8761e+05 12036 4991.3 v TurbVisc 4.453e-21 0.011444 0.00015683 1.8155e-05 v CourantNb 4.4212e-08 0.011763 0.00016776 4.9253e-06 v FourierNb 1.2425e-07 0.047133 0.00014582 2.5654e-07 v total_pressure -63601 2.8894e+05 1.1336e+05 1.0632e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0849 0.099355 0.0028412 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2302e-07 0.052445 0.00031359 5.1818e-06 INSTANT 0.875657000E-01 TIME STEP NUMBER 55855 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283244645E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.788501564E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10176E-01 0.21234E+01 Friction velocity uk : 0.10176E-01 0.21234E+01 Dimensionless distance yplus : 0.98787E-02 0.20850E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 4.082455741e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29471E+08 1 0.18022E-09 0.24550E+02 0.19291E+04 c Velocity[X] 0.12526E+02 c Velocity[Y] 0.12023E+02 c Velocity[Z] 0.18437E-05 c Pressure 0.22813E-03 10 0.63092E-04 0.25228E-02 0.47655E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -21.306 33.438 5.6132 8.0075 v Velocity[Y] -23.662 25.059 -0.14366 -0.001012 v Velocity[Z] -3.0085 3 2.7857e-06 -5.3873e-08 v ǁVelocityǁ 0.00056457 33.519 7.4341 8.0703 v Pressure -1.6699e+05 1.8572e+05 10107 3975.2 v TurbVisc 4.6368e-21 0.011464 0.0001569 1.8187e-05 v CourantNb 4.4524e-08 0.011763 0.00016777 4.9254e-06 v FourierNb 1.2425e-07 0.047133 0.00014582 2.5676e-07 v total_pressure -65665 2.8705e+05 1.1143e+05 1.053e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.085 0.099372 0.0028414 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2303e-07 0.052445 0.00031359 5.1821e-06 INSTANT 0.875658000E-01 TIME STEP NUMBER 55856 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283245385E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.788729866E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.70732E-02 0.21235E+01 Friction velocity uk : 0.70732E-02 0.21235E+01 Dimensionless distance yplus : 0.68140E-02 0.20851E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 3.994388668e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29471E+08 1 0.18023E-09 0.24552E+02 0.19292E+04 c Velocity[X] 0.12528E+02 c Velocity[Y] 0.12024E+02 c Velocity[Z] 0.18328E-05 c Pressure 0.22897E-03 142 0.79884E-04 0.25303E-02 0.59491E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -21.319 33.456 5.6133 8.0075 v Velocity[Y] -23.676 25.073 -0.14367 -0.0010154 v Velocity[Z] -3.0084 3.0002 2.7849e-06 -5.3873e-08 v ǁVelocityǁ 0.00060447 33.537 7.4357 8.0704 v Pressure -1.6913e+05 1.8375e+05 8176.9 2814.6 v TurbVisc 5.184e-21 0.011483 0.00015698 1.8219e-05 v CourantNb 2.9463e-08 0.011762 0.00016777 4.9255e-06 v FourierNb 1.2425e-07 0.047133 0.00014582 2.5698e-07 v total_pressure -67802 2.8508e+05 1.095e+05 1.0414e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0851 0.099386 0.0028416 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2304e-07 0.052446 0.00031359 5.1824e-06 INSTANT 0.875659000E-01 TIME STEP NUMBER 55857 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283246034E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.788943749E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.35864E-02 0.21237E+01 Friction velocity uk : 0.35864E-02 0.21237E+01 Dimensionless distance yplus : 0.34550E-02 0.20852E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 3.784834616e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29471E+08 1 0.18024E-09 0.24557E+02 0.19293E+04 c Velocity[X] 0.12530E+02 c Velocity[Y] 0.12026E+02 c Velocity[Z] 0.18213E-05 c Pressure 0.22938E-03 29 0.86143E-04 0.25330E-02 0.60683E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -21.332 33.474 5.6133 8.0075 v Velocity[Y] -23.69 25.087 -0.14368 -0.001021 v Velocity[Z] -3.0082 3.0004 2.7842e-06 -5.3873e-08 v ǁVelocityǁ 0.00063072 33.556 7.4374 8.0705 v Pressure -1.7122e+05 1.8183e+05 6182.7 1595.8 v TurbVisc 3.5798e-21 0.011502 0.00015705 1.8251e-05 v CourantNb 1.6911e-08 0.011762 0.00016777 4.9255e-06 v FourierNb 1.2425e-07 0.047133 0.00014582 2.572e-07 v total_pressure -69892 2.8316e+05 1.0751e+05 1.0292e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0852 0.099401 0.0028417 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2305e-07 0.052446 0.0003136 5.1827e-06 INSTANT 0.875660000E-01 TIME STEP NUMBER 55858 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283246555E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.789151725E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.63470E-02 0.21238E+01 Friction velocity uk : 0.63470E-02 0.21238E+01 Dimensionless distance yplus : 0.61145E-02 0.20854E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 3.761414021e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29471E+08 1 0.18024E-09 0.24561E+02 0.19294E+04 c Velocity[X] 0.12533E+02 c Velocity[Y] 0.12028E+02 c Velocity[Z] 0.18110E-05 c Pressure 0.22983E-03 172 0.99586E-04 0.25363E-02 0.52077E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -21.344 33.492 5.6134 8.0075 v Velocity[Y] -23.705 25.101 -0.14368 -0.001024 v Velocity[Z] -3.008 3.0007 2.7834e-06 -5.3873e-08 v ǁVelocityǁ 0.00066169 33.574 7.4391 8.0707 v Pressure -1.7331e+05 1.7989e+05 4253.9 600.86 v TurbVisc 3.2422e-21 0.011522 0.00015712 1.8283e-05 v CourantNb 7.6274e-09 0.011762 0.00016778 4.9256e-06 v FourierNb 1.2425e-07 0.047133 0.00014583 2.5742e-07 v total_pressure -71984 2.8122e+05 1.0558e+05 1.0193e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0854 0.099415 0.0028418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2306e-07 0.052446 0.0003136 5.183e-06 INSTANT 0.875661000E-01 TIME STEP NUMBER 55859 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283246736E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.789350424E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.95245E-02 0.21240E+01 Friction velocity uk : 0.95245E-02 0.21240E+01 Dimensionless distance yplus : 0.91755E-02 0.20855E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 3.628633795e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29471E+08 1 0.18025E-09 0.24557E+02 0.19292E+04 c Velocity[X] 0.12534E+02 c Velocity[Y] 0.12023E+02 c Velocity[Z] 0.18009E-05 c Pressure 0.23012E-03 378 0.84799E-04 0.25378E-02 0.58569E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -21.357 33.51 5.6134 8.0075 v Velocity[Y] -23.719 25.115 -0.14369 -0.0010284 v Velocity[Z] -3.0079 3.0009 2.7826e-06 -5.3873e-08 v ǁVelocityǁ 0.00069341 33.592 7.4407 8.0708 v Pressure -1.754e+05 1.7794e+05 2281.9 -598.27 v TurbVisc 2.9561e-21 0.011541 0.00015719 1.8315e-05 v CourantNb 8.5987e-09 0.011762 0.00016778 4.9257e-06 v FourierNb 1.2425e-07 0.047133 0.00014583 2.5764e-07 v total_pressure -74076 2.7926e+05 1.0361e+05 1.0073e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0855 0.099428 0.0028419 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2306e-07 0.052447 0.00031361 5.1833e-06 INSTANT 0.875662000E-01 TIME STEP NUMBER 55860 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283246868E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.789534339E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11040E-01 0.21241E+01 Friction velocity uk : 0.11040E-01 0.21241E+01 Dimensionless distance yplus : 0.10635E-01 0.20857E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 3.512654297e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29471E+08 1 0.18025E-09 0.24564E+02 0.19294E+04 c Velocity[X] 0.12537E+02 c Velocity[Y] 0.12027E+02 c Velocity[Z] 0.18022E-05 c Pressure 0.22885E-03 10 0.63899E-04 0.25220E-02 0.49650E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -21.369 33.527 5.6134 8.0075 v Velocity[Y] -23.733 25.129 -0.1437 -0.0010341 v Velocity[Z] -3.0077 3.0011 2.7818e-06 -5.3873e-08 v ǁVelocityǁ 0.00070829 33.61 7.4424 8.0709 v Pressure -1.7748e+05 1.76e+05 330.88 -1644.8 v TurbVisc 2.7032e-21 0.01156 0.00015726 1.8347e-05 v CourantNb 1.4102e-08 0.011762 0.00016778 4.9258e-06 v FourierNb 1.2425e-07 0.047133 0.00014583 2.5786e-07 v total_pressure -76153 2.7732e+05 1.0166e+05 99680 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0857 0.09944 0.002842 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2307e-07 0.052447 0.00031361 5.1836e-06 INSTANT 0.875663000E-01 TIME STEP NUMBER 55861 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283246737E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.789706515E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11636E-01 0.21243E+01 Friction velocity uk : 0.11636E-01 0.21243E+01 Dimensionless distance yplus : 0.11210E-01 0.20859E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 3.355005491e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29471E+08 1 0.18026E-09 0.24567E+02 0.19295E+04 c Velocity[X] 0.12540E+02 c Velocity[Y] 0.12027E+02 c Velocity[Z] 0.17882E-05 c Pressure 0.22917E-03 190 0.80737E-04 0.25238E-02 0.59343E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -21.382 33.545 5.6135 8.0075 v Velocity[Y] -23.748 25.143 -0.14371 -0.0010377 v Velocity[Z] -3.0075 3.0013 2.781e-06 -5.3873e-08 v ǁVelocityǁ 0.00076617 33.628 7.4441 8.071 v Pressure -1.796e+05 1.7398e+05 -1611.4 -2800.9 v TurbVisc 2.5892e-21 0.011579 0.00015733 1.838e-05 v CourantNb 2.9298e-08 0.011762 0.00016779 4.9258e-06 v FourierNb 1.2425e-07 0.047133 0.00014583 2.5808e-07 v total_pressure -78272 2.7531e+05 99714 98524 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0859 0.099448 0.002842 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2308e-07 0.052448 0.00031361 5.1839e-06 INSTANT 0.875664000E-01 TIME STEP NUMBER 55862 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283246525E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.789864891E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.99904E-02 0.21244E+01 Friction velocity uk : 0.99904E-02 0.21244E+01 Dimensionless distance yplus : 0.96243E-02 0.20860E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 3.143162735e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29471E+08 1 0.18027E-09 0.24572E+02 0.19296E+04 c Velocity[X] 0.12543E+02 c Velocity[Y] 0.12028E+02 c Velocity[Z] 0.17743E-05 c Pressure 0.22905E-03 30 0.86962E-04 0.25207E-02 0.59859E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -21.394 33.563 5.6135 8.0075 v Velocity[Y] -23.762 25.157 -0.14372 -0.0010436 v Velocity[Z] -3.0074 3.0015 2.7803e-06 -5.3873e-08 v ǁVelocityǁ 0.00080671 33.645 7.4457 8.0711 v Pressure -1.8167e+05 1.7202e+05 -3606.9 -4024.3 v TurbVisc 2.6916e-21 0.011599 0.0001574 1.8411e-05 v CourantNb 4.0585e-08 0.011761 0.00016779 4.9259e-06 v FourierNb 1.2425e-07 0.047133 0.00014583 2.583e-07 v total_pressure -80346 2.7334e+05 97718 97301 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.086 0.099458 0.002842 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2308e-07 0.052449 0.00031362 5.1842e-06 INSTANT 0.875665000E-01 TIME STEP NUMBER 55863 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283246184E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.790018558E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.59307E-02 0.21246E+01 Friction velocity uk : 0.59307E-02 0.21246E+01 Dimensionless distance yplus : 0.57134E-02 0.20861E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 3.058703110e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29471E+08 1 0.18027E-09 0.24570E+02 0.19295E+04 c Velocity[X] 0.12546E+02 c Velocity[Y] 0.12024E+02 c Velocity[Z] 0.17652E-05 c Pressure 0.22895E-03 161 0.75407E-04 0.25179E-02 0.48247E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -21.407 33.58 5.6135 8.0075 v Velocity[Y] -23.776 25.171 -0.14373 -0.001048 v Velocity[Z] -3.0072 3.0017 2.7795e-06 -5.3873e-08 v ǁVelocityǁ 0.00084973 33.663 7.4474 8.0713 v Pressure -1.8374e+05 1.7004e+05 -5539.2 -5032 v TurbVisc 2.0645e-21 0.011618 0.00015747 1.8444e-05 v CourantNb 3.7815e-08 0.011761 0.00016779 4.926e-06 v FourierNb 1.2425e-07 0.047133 0.00014583 2.5853e-07 v total_pressure -82419 2.7137e+05 95786 96293 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0861 0.099466 0.002842 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2309e-07 0.052449 0.00031362 5.1845e-06 INSTANT 0.875666000E-01 TIME STEP NUMBER 55864 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283245596E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.790162539E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.33898E-02 0.21247E+01 Friction velocity uk : 0.33898E-02 0.21247E+01 Dimensionless distance yplus : 0.32656E-02 0.20863E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 2.910101012e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29471E+08 1 0.18027E-09 0.24576E+02 0.19297E+04 c Velocity[X] 0.12549E+02 c Velocity[Y] 0.12027E+02 c Velocity[Z] 0.17668E-05 c Pressure 0.22745E-03 10 0.60083E-04 0.24997E-02 0.46120E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -21.419 33.598 5.6136 8.0075 v Velocity[Y] -23.79 25.185 -0.14374 -0.0010517 v Velocity[Z] -3.007 3.0019 2.7787e-06 -5.3873e-08 v ǁVelocityǁ 0.00087093 33.681 7.449 8.0714 v Pressure -1.8579e+05 1.6808e+05 -7483.1 -6061.7 v TurbVisc 1.9078e-21 0.011637 0.00015754 1.8477e-05 v CourantNb 3.5961e-08 0.011761 0.0001678 4.926e-06 v FourierNb 1.2425e-07 0.047132 0.00014583 2.5875e-07 v total_pressure -84469 2.6941e+05 93842 95263 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0863 0.099472 0.0028419 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.231e-07 0.052449 0.00031363 5.1848e-06 INSTANT 0.875667000E-01 TIME STEP NUMBER 55865 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283244675E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.790292740E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.39384E-02 0.21248E+01 Friction velocity uk : 0.39384E-02 0.21248E+01 Dimensionless distance yplus : 0.38462E-02 0.20864E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 2.722628211e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29471E+08 1 0.18028E-09 0.24577E+02 0.19297E+04 c Velocity[X] 0.12553E+02 c Velocity[Y] 0.12024E+02 c Velocity[Z] 0.17539E-05 c Pressure 0.22719E-03 42 0.96305E-04 0.24950E-02 0.56229E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -21.432 33.615 5.6136 8.0075 v Velocity[Y] -23.805 25.199 -0.14375 -0.0010564 v Velocity[Z] -3.0069 3.0021 2.7779e-06 -5.3873e-08 v ǁVelocityǁ 0.00094145 33.698 7.4507 8.0715 v Pressure -1.8787e+05 1.6605e+05 -9412.1 -7274.2 v TurbVisc 1.7372e-21 0.011657 0.00015761 1.8508e-05 v CourantNb 2.0506e-08 0.011761 0.0001678 4.9261e-06 v FourierNb 1.2425e-07 0.047132 0.00014583 2.5897e-07 v total_pressure -86547 2.6738e+05 91913 94051 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0864 0.099476 0.0028419 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.231e-07 0.05245 0.00031363 5.1851e-06 INSTANT 0.875668000E-01 TIME STEP NUMBER 55866 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283243775E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.790408219E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.37211E-02 0.21249E+01 Friction velocity uk : 0.37211E-02 0.21249E+01 Dimensionless distance yplus : 0.36340E-02 0.20865E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 2.575996481e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29471E+08 1 0.18028E-09 0.24580E+02 0.19297E+04 c Velocity[X] 0.12557E+02 c Velocity[Y] 0.12023E+02 c Velocity[Z] 0.17402E-05 c Pressure 0.22630E-03 73 0.81050E-04 0.24836E-02 0.53393E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -21.444 33.632 5.6136 8.0075 v Velocity[Y] -23.819 25.212 -0.14376 -0.0010614 v Velocity[Z] -3.0067 3.0023 2.7772e-06 -5.3873e-08 v ǁVelocityǁ 0.00098494 33.716 7.4524 8.0716 v Pressure -1.8993e+05 1.6405e+05 -11404 -8490.3 v TurbVisc 1.6599e-21 0.011676 0.00015768 1.8541e-05 v CourantNb 2.0118e-08 0.011761 0.0001678 4.9262e-06 v FourierNb 1.2425e-07 0.047132 0.00014583 2.5919e-07 v total_pressure -88603 2.6537e+05 89921 92835 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0865 0.099486 0.0028419 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2311e-07 0.05245 0.00031363 5.1853e-06 INSTANT 0.875669000E-01 TIME STEP NUMBER 55867 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283242673E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.790516884E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.90464E-02 0.21250E+01 Friction velocity uk : 0.90464E-02 0.21250E+01 Dimensionless distance yplus : 0.88345E-02 0.20866E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 2.425844611e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29471E+08 1 0.18028E-09 0.24587E+02 0.19300E+04 c Velocity[X] 0.12561E+02 c Velocity[Y] 0.12026E+02 c Velocity[Z] 0.17410E-05 c Pressure 0.22521E-03 10 0.57355E-04 0.24700E-02 0.45657E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -21.456 33.649 5.6136 8.0075 v Velocity[Y] -23.833 25.226 -0.14377 -0.001067 v Velocity[Z] -3.0065 3.0025 2.7764e-06 -5.3873e-08 v ǁVelocityǁ 0.0010049 33.733 7.454 8.0717 v Pressure -1.9195e+05 1.6208e+05 -13353 -9543.3 v TurbVisc 1.7908e-21 0.011695 0.00015775 1.8573e-05 v CourantNb 1.5097e-08 0.01176 0.0001678 4.9262e-06 v FourierNb 1.2425e-07 0.047131 0.00014583 2.5941e-07 v total_pressure -90627 2.634e+05 87972 91782 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0866 0.099495 0.0028419 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2312e-07 0.052449 0.00031364 5.1856e-06 INSTANT 0.875670000E-01 TIME STEP NUMBER 55868 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283241402E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.790618804E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15286E-01 0.21251E+01 Friction velocity uk : 0.15286E-01 0.21251E+01 Dimensionless distance yplus : 0.14928E-01 0.20867E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 2.093087746e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29471E+08 1 0.18029E-09 0.24587E+02 0.19299E+04 c Velocity[X] 0.12565E+02 c Velocity[Y] 0.12022E+02 c Velocity[Z] 0.17297E-05 c Pressure 0.22472E-03 99 0.98849E-04 0.24629E-02 0.48438E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -21.469 33.667 5.6137 8.0074 v Velocity[Y] -23.847 25.24 -0.14378 -0.0010724 v Velocity[Z] -3.0063 3.0027 2.7756e-06 -5.3873e-08 v ǁVelocityǁ 0.0010739 33.75 7.4557 8.0717 v Pressure -1.9399e+05 1.6012e+05 -15232 -10644 v TurbVisc 1.2853e-21 0.011714 0.00015782 1.8606e-05 v CourantNb 1.2014e-08 0.01176 0.00016781 4.9263e-06 v FourierNb 1.2425e-07 0.047131 0.00014584 2.5964e-07 v total_pressure -92661 2.6145e+05 86093 90681 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0867 0.0995 0.0028418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2312e-07 0.05245 0.00031364 5.1859e-06 INSTANT 0.875671000E-01 TIME STEP NUMBER 55869 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283239997E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.790706753E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13225E-01 0.21252E+01 Friction velocity uk : 0.13225E-01 0.21252E+01 Dimensionless distance yplus : 0.12800E-01 0.20867E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 2.014923016e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29470E+08 1 0.18029E-09 0.24590E+02 0.19300E+04 c Velocity[X] 0.12569E+02 c Velocity[Y] 0.12021E+02 c Velocity[Z] 0.17169E-05 c Pressure 0.22350E-03 41 0.82622E-04 0.24479E-02 0.44289E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -21.481 33.684 5.6137 8.0074 v Velocity[Y] -23.862 25.253 -0.14379 -0.0010772 v Velocity[Z] -3.0062 3.0029 2.7748e-06 -5.3874e-08 v ǁVelocityǁ 0.001118 33.767 7.4573 8.0718 v Pressure -1.9599e+05 1.5822e+05 -17169 -11714 v TurbVisc 1.3029e-21 0.011734 0.00015789 1.8639e-05 v CourantNb 1.1031e-08 0.01176 0.00016781 4.9263e-06 v FourierNb 1.2425e-07 0.04713 0.00014584 2.5987e-07 v total_pressure -94669 2.5954e+05 84156 89611 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0867 0.099508 0.0028418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2313e-07 0.052449 0.00031365 5.1862e-06 INSTANT 0.875672000E-01 TIME STEP NUMBER 55870 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283238399E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.790786639E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10662E-01 0.21252E+01 Friction velocity uk : 0.10662E-01 0.21252E+01 Dimensionless distance yplus : 0.10320E-01 0.20867E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.822604165e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29470E+08 1 0.18029E-09 0.24597E+02 0.19302E+04 c Velocity[X] 0.12574E+02 c Velocity[Y] 0.12024E+02 c Velocity[Z] 0.17182E-05 c Pressure 0.22195E-03 10 0.58566E-04 0.24293E-02 0.41446E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -21.493 33.701 5.6137 8.0074 v Velocity[Y] -23.876 25.267 -0.1438 -0.001081 v Velocity[Z] -3.006 3.0032 2.7741e-06 -5.3874e-08 v ǁVelocityǁ 0.0011378 33.785 7.459 8.0719 v Pressure -1.98e+05 1.5631e+05 -19095 -12741 v TurbVisc 1.2218e-21 0.011753 0.00015796 1.8672e-05 v CourantNb 1.383e-08 0.01176 0.00016781 4.9264e-06 v FourierNb 1.2425e-07 0.047129 0.00014584 2.6009e-07 v total_pressure -96671 2.5764e+05 82230 88584 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0867 0.099513 0.0028417 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2313e-07 0.052448 0.00031365 5.1865e-06 INSTANT 0.875673000E-01 TIME STEP NUMBER 55871 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283236547E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.790857041E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.84218E-02 0.21252E+01 Friction velocity uk : 0.84218E-02 0.21252E+01 Dimensionless distance yplus : 0.81514E-02 0.20868E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.476470885e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29470E+08 1 0.18029E-09 0.24598E+02 0.19302E+04 c Velocity[X] 0.12578E+02 c Velocity[Y] 0.12020E+02 c Velocity[Z] 0.17110E-05 c Pressure 0.22112E-03 25 0.99903E-04 0.24186E-02 0.47517E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -21.505 33.718 5.6137 8.0073 v Velocity[Y] -23.89 25.28 -0.14382 -0.0010859 v Velocity[Z] -3.0058 3.0034 2.7733e-06 -5.3874e-08 v ǁVelocityǁ 0.0011956 33.802 7.4606 8.072 v Pressure -1.9999e+05 1.5441e+05 -20964 -13907 v TurbVisc 1.4192e-21 0.011772 0.00015803 1.8703e-05 v CourantNb 1.32e-08 0.01176 0.00016781 4.9264e-06 v FourierNb 1.2425e-07 0.047128 0.00014584 2.6031e-07 v total_pressure -98667 2.5573e+05 80361 87418 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0868 0.099516 0.0028416 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2314e-07 0.052448 0.00031365 5.1867e-06 INSTANT 0.875674000E-01 TIME STEP NUMBER 55872 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283234645E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.790914621E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.60807E-02 0.21252E+01 Friction velocity uk : 0.60807E-02 0.21252E+01 Dimensionless distance yplus : 0.58855E-02 0.20868E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.323793458e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29470E+08 1 0.18029E-09 0.24601E+02 0.19303E+04 c Velocity[X] 0.12583E+02 c Velocity[Y] 0.12018E+02 c Velocity[Z] 0.16995E-05 c Pressure 0.21957E-03 116 0.85023E-04 0.24000E-02 0.44773E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -21.518 33.734 5.6137 8.0073 v Velocity[Y] -23.904 25.293 -0.14383 -0.0010912 v Velocity[Z] -3.0057 3.0036 2.7725e-06 -5.3874e-08 v ǁVelocityǁ 0.0012415 33.819 7.4622 8.0721 v Pressure -2.0197e+05 1.5251e+05 -22883 -15078 v TurbVisc 1.07e-21 0.011791 0.00015809 1.8736e-05 v CourantNb 1.4045e-08 0.011759 0.00016782 4.9265e-06 v FourierNb 1.2425e-07 0.047126 0.00014584 2.6053e-07 v total_pressure -1.0064e+05 2.5383e+05 78442 86247 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0868 0.099521 0.0028416 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2314e-07 0.052446 0.00031366 5.187e-06 INSTANT 0.875675000E-01 TIME STEP NUMBER 55873 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283232531E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.790965244E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.50538E-02 0.21251E+01 Friction velocity uk : 0.50538E-02 0.21251E+01 Dimensionless distance yplus : 0.48916E-02 0.20867E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.088271929e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29470E+08 1 0.18028E-09 0.24609E+02 0.19305E+04 c Velocity[X] 0.12588E+02 c Velocity[Y] 0.12020E+02 c Velocity[Z] 0.16971E-05 c Pressure 0.21772E-03 10 0.59884E-04 0.23782E-02 0.37914E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -21.53 33.751 5.6137 8.0072 v Velocity[Y] -23.918 25.306 -0.14384 -0.0010972 v Velocity[Z] -3.0055 3.0038 2.7717e-06 -5.3874e-08 v ǁVelocityǁ 0.0012523 33.836 7.4639 8.0722 v Pressure -2.0391e+05 1.5068e+05 -24769 -16079 v TurbVisc 1.6792e-21 0.011811 0.00015816 1.8768e-05 v CourantNb 1.3822e-08 0.011759 0.00016782 4.9265e-06 v FourierNb 1.2425e-07 0.047125 0.00014584 2.6076e-07 v total_pressure -1.0258e+05 2.52e+05 76556 85246 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0867 0.099526 0.0028415 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2315e-07 0.052445 0.00031366 5.1873e-06 INSTANT 0.875676000E-01 TIME STEP NUMBER 55874 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283230272E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.791007755E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.40101E-02 0.21251E+01 Friction velocity uk : 0.40101E-02 0.21251E+01 Dimensionless distance yplus : 0.38814E-02 0.20866E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 6.307497621e-03 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29470E+08 1 0.18028E-09 0.24612E+02 0.19306E+04 c Velocity[X] 0.12594E+02 c Velocity[Y] 0.12018E+02 c Velocity[Z] 0.16885E-05 c Pressure 0.21659E-03 158 0.77967E-04 0.23643E-02 0.41889E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -21.542 33.768 5.6137 8.0072 v Velocity[Y] -23.932 25.319 -0.14384 -0.0011015 v Velocity[Z] -3.0053 3.004 2.771e-06 -5.3874e-08 v ǁVelocityǁ 0.0013093 33.853 7.4655 8.0722 v Pressure -2.0595e+05 1.4881e+05 -26592 -17125 v TurbVisc 8.7121e-22 0.01183 0.00015823 1.8802e-05 v CourantNb 1.3298e-08 0.011759 0.00016782 4.9266e-06 v FourierNb 1.2425e-07 0.047123 0.00014584 2.6099e-07 v total_pressure -1.0463e+05 2.5014e+05 74733 84200 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0866 0.099528 0.0028414 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2315e-07 0.052443 0.00031367 5.1876e-06 INSTANT 0.875677000E-01 TIME STEP NUMBER 55875 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283227867E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.791036787E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.39056E-02 0.21249E+01 Friction velocity uk : 0.39056E-02 0.21249E+01 Dimensionless distance yplus : 0.37802E-02 0.20865E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 4.594252722e-03 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29469E+08 1 0.18028E-09 0.24617E+02 0.19308E+04 c Velocity[X] 0.12599E+02 c Velocity[Y] 0.12018E+02 c Velocity[Z] 0.16770E-05 c Pressure 0.21501E-03 188 0.83207E-04 0.23455E-02 0.42769E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -21.554 33.785 5.6136 8.0071 v Velocity[Y] -23.947 25.332 -0.14385 -0.0011079 v Velocity[Z] -3.0052 3.0042 2.7702e-06 -5.3874e-08 v ǁVelocityǁ 0.0013383 33.869 7.4671 8.0723 v Pressure -2.0806e+05 1.47e+05 -28471 -18265 v TurbVisc 1.212e-21 0.011849 0.00015829 1.8834e-05 v CourantNb 1.1624e-08 0.011759 0.00016783 4.9266e-06 v FourierNb 1.2425e-07 0.047121 0.00014585 2.6121e-07 v total_pressure -1.0674e+05 2.4832e+05 72854 83060 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0865 0.099532 0.0028414 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2316e-07 0.052441 0.00031367 5.1878e-06 INSTANT 0.875678000E-01 TIME STEP NUMBER 55876 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283225359E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.791061844E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.49560E-02 0.21248E+01 Friction velocity uk : 0.49560E-02 0.21248E+01 Dimensionless distance yplus : 0.47969E-02 0.20864E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 9.307192291e-04 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29469E+08 1 0.18028E-09 0.24622E+02 0.19310E+04 c Velocity[X] 0.12604E+02 c Velocity[Y] 0.12018E+02 c Velocity[Z] 0.16698E-05 c Pressure 0.21342E-03 203 0.96031E-04 0.23266E-02 0.35203E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -21.566 33.801 5.6136 8.0071 v Velocity[Y] -23.961 25.345 -0.14386 -0.0011118 v Velocity[Z] -3.005 3.0044 2.7694e-06 -5.3874e-08 v ǁVelocityǁ 0.0013074 33.886 7.4688 8.0724 v Pressure -2.1016e+05 1.4521e+05 -30269 -19175 v TurbVisc 7.4627e-22 0.011868 0.00015836 1.8868e-05 v CourantNb 1.2201e-08 0.011759 0.00016783 4.9267e-06 v FourierNb 1.2425e-07 0.047119 0.00014585 2.6144e-07 v total_pressure -1.0883e+05 2.4653e+05 71056 82150 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0864 0.099535 0.0028413 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2316e-07 0.052439 0.00031368 5.1881e-06 INSTANT 0.875679000E-01 TIME STEP NUMBER 55877 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283222519E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.791076378E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.53206E-02 0.21246E+01 Friction velocity uk : 0.53206E-02 0.21246E+01 Dimensionless distance yplus : 0.51498E-02 0.20862E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -2.860669968e-03 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29469E+08 1 0.18027E-09 0.24620E+02 0.19308E+04 c Velocity[X] 0.12610E+02 c Velocity[Y] 0.12010E+02 c Velocity[Z] 0.16641E-05 c Pressure 0.21167E-03 131 0.81682E-04 0.23060E-02 0.39595E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -21.578 33.818 5.6136 8.007 v Velocity[Y] -23.975 25.358 -0.14387 -0.0011173 v Velocity[Z] -3.0048 3.0046 2.7687e-06 -5.3874e-08 v ǁVelocityǁ 0.0012581 33.903 7.4704 8.0724 v Pressure -2.1226e+05 1.4351e+05 -32094 -20308 v TurbVisc 8.7763e-22 0.011888 0.00015843 1.8899e-05 v CourantNb 1.4399e-08 0.011758 0.00016783 4.9267e-06 v FourierNb 1.2425e-07 0.047116 0.00014585 2.6166e-07 v total_pressure -1.1094e+05 2.4483e+05 69231 81017 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0862 0.099537 0.0028413 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2316e-07 0.052436 0.00031368 5.1884e-06 INSTANT 0.875680000E-01 TIME STEP NUMBER 55878 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283219635E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.791078602E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.73595E-02 0.21244E+01 Friction velocity uk : 0.73595E-02 0.21244E+01 Dimensionless distance yplus : 0.71233E-02 0.20860E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -7.109611026e-03 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29469E+08 1 0.18027E-09 0.24627E+02 0.19311E+04 c Velocity[X] 0.12615E+02 c Velocity[Y] 0.12012E+02 c Velocity[Z] 0.16664E-05 c Pressure 0.20833E-03 10 0.60361E-04 0.22681E-02 0.31046E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -21.59 33.834 5.6136 8.007 v Velocity[Y] -23.989 25.371 -0.14388 -0.0011235 v Velocity[Z] -3.0046 3.0048 2.7679e-06 -5.3874e-08 v ǁVelocityǁ 0.0012239 33.92 7.472 8.0725 v Pressure -2.143e+05 1.4187e+05 -33867 -21237 v TurbVisc 1.0758e-21 0.011907 0.00015849 1.8932e-05 v CourantNb 2.2721e-08 0.011758 0.00016783 4.9268e-06 v FourierNb 1.2425e-07 0.047113 0.00014585 2.6188e-07 v total_pressure -1.1298e+05 2.432e+05 67458 80088 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.086 0.099539 0.0028412 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2317e-07 0.052433 0.00031368 5.1887e-06 INSTANT 0.875681000E-01 TIME STEP NUMBER 55879 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283216541E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.791070871E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.68771E-02 0.21242E+01 Friction velocity uk : 0.68771E-02 0.21242E+01 Dimensionless distance yplus : 0.66367E-02 0.20858E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.285266628e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29468E+08 1 0.18026E-09 0.24631E+02 0.19312E+04 c Velocity[X] 0.12621E+02 c Velocity[Y] 0.12010E+02 c Velocity[Z] 0.16571E-05 c Pressure 0.20660E-03 149 0.77228E-04 0.22478E-02 0.37175E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -21.603 33.851 5.6135 8.0069 v Velocity[Y] -24.003 25.383 -0.14388 -0.001128 v Velocity[Z] -3.0045 3.005 2.7671e-06 -5.3874e-08 v ǁVelocityǁ 0.0011688 33.936 7.4736 8.0725 v Pressure -2.1639e+05 1.402e+05 -35634 -22287 v TurbVisc 1.0357e-21 0.011926 0.00015856 1.8966e-05 v CourantNb 3.556e-08 0.011758 0.00016783 4.9268e-06 v FourierNb 1.2425e-07 0.04711 0.00014585 2.6212e-07 v total_pressure -1.1507e+05 2.4152e+05 65691 79038 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0858 0.099537 0.0028411 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2317e-07 0.05243 0.00031369 5.1889e-06 INSTANT 0.875682000E-01 TIME STEP NUMBER 55880 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283213348E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.791050854E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.40392E-02 0.21239E+01 Friction velocity uk : 0.40392E-02 0.21239E+01 Dimensionless distance yplus : 0.38979E-02 0.20855E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.640464878e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29468E+08 1 0.18026E-09 0.24636E+02 0.19314E+04 c Velocity[X] 0.12628E+02 c Velocity[Y] 0.12009E+02 c Velocity[Z] 0.16470E-05 c Pressure 0.20451E-03 29 0.83154E-04 0.22237E-02 0.36759E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -21.615 33.867 5.6135 8.0068 v Velocity[Y] -24.017 25.396 -0.14389 -0.0011346 v Velocity[Z] -3.0043 3.0052 2.7664e-06 -5.3874e-08 v ǁVelocityǁ 0.0011272 33.953 7.4752 8.0726 v Pressure -2.184e+05 1.3858e+05 -37420 -23387 v TurbVisc 9.1392e-22 0.011945 0.00015862 1.8998e-05 v CourantNb 5.8393e-08 0.011758 0.00016784 4.9268e-06 v FourierNb 1.2425e-07 0.047107 0.00014586 2.6234e-07 v total_pressure -1.1708e+05 2.3991e+05 63905 77938 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0855 0.099537 0.002841 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2318e-07 0.052427 0.00031369 5.1892e-06 INSTANT 0.875683000E-01 TIME STEP NUMBER 55881 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283210062E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.791029462E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.74100E-02 0.21236E+01 Friction velocity uk : 0.74100E-02 0.21236E+01 Dimensionless distance yplus : 0.72365E-02 0.20852E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -2.172758249e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29468E+08 1 0.18025E-09 0.24641E+02 0.19315E+04 c Velocity[X] 0.12633E+02 c Velocity[Y] 0.12008E+02 c Velocity[Z] 0.16373E-05 c Pressure 0.20243E-03 199 0.95913E-04 0.21996E-02 0.30073E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -21.627 33.884 5.6134 8.0068 v Velocity[Y] -24.03 25.408 -0.14389 -0.0011388 v Velocity[Z] -3.0041 3.0054 2.7656e-06 -5.3874e-08 v ǁVelocityǁ 0.001088 33.97 7.4768 8.0726 v Pressure -2.2039e+05 1.3699e+05 -39125 -24250 v TurbVisc 9.3706e-22 0.011965 0.00015868 1.9032e-05 v CourantNb 2.621e-08 0.011758 0.00016784 4.9269e-06 v FourierNb 1.2425e-07 0.047104 0.00014586 2.6257e-07 v total_pressure -1.1907e+05 2.3832e+05 62200 77075 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0852 0.099544 0.0028411 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2318e-07 0.052423 0.0003137 5.1895e-06 INSTANT 0.875684000E-01 TIME STEP NUMBER 55882 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283206462E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.790998958E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13113E-01 0.21233E+01 Friction velocity uk : 0.13113E-01 0.21233E+01 Dimensionless distance yplus : 0.12692E-01 0.20849E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -2.739185544e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29467E+08 1 0.18024E-09 0.24639E+02 0.19314E+04 c Velocity[X] 0.12639E+02 c Velocity[Y] 0.12000E+02 c Velocity[Z] 0.16300E-05 c Pressure 0.20021E-03 174 0.81642E-04 0.21741E-02 0.33345E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -21.639 33.9 5.6134 8.0067 v Velocity[Y] -24.044 25.42 -0.1439 -0.0011444 v Velocity[Z] -3.0039 3.0056 2.7648e-06 -5.3874e-08 v ǁVelocityǁ 0.0010523 33.986 7.4784 8.0727 v Pressure -2.2238e+05 1.3541e+05 -40843 -25322 v TurbVisc 1.0547e-21 0.011984 0.00015875 1.9064e-05 v CourantNb 1.0409e-08 0.011757 0.00016784 4.9269e-06 v FourierNb 1.2425e-07 0.0471 0.00014586 2.6279e-07 v total_pressure -1.2105e+05 2.3674e+05 60482 76003 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0849 0.099551 0.0028411 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2318e-07 0.052419 0.0003137 5.1897e-06 INSTANT 0.875685000E-01 TIME STEP NUMBER 55883 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283202824E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.790956247E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.14731E-01 0.21229E+01 Friction velocity uk : 0.14731E-01 0.21229E+01 Dimensionless distance yplus : 0.14196E-01 0.20845E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -3.337349497e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29467E+08 1 0.18024E-09 0.24646E+02 0.19316E+04 c Velocity[X] 0.12644E+02 c Velocity[Y] 0.12001E+02 c Velocity[Z] 0.16317E-05 c Pressure 0.19629E-03 10 0.60013E-04 0.21301E-02 0.26065E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -21.651 33.917 5.6133 8.0066 v Velocity[Y] -24.058 25.432 -0.1439 -0.0011509 v Velocity[Z] -3.0038 3.0058 2.764e-06 -5.3874e-08 v ǁVelocityǁ 0.001034 34.003 7.48 8.0727 v Pressure -2.2429e+05 1.339e+05 -42511 -26198 v TurbVisc 9.5479e-22 0.012003 0.00015881 1.9097e-05 v CourantNb 5.9901e-09 0.011757 0.00016784 4.927e-06 v FourierNb 1.2425e-07 0.047096 0.00014586 2.6302e-07 v total_pressure -1.2297e+05 2.3523e+05 58814 75127 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0845 0.099556 0.0028412 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2319e-07 0.052415 0.00031371 5.19e-06 INSTANT 0.875686000E-01 TIME STEP NUMBER 55884 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283198986E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.790902753E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12841E-01 0.21225E+01 Friction velocity uk : 0.12841E-01 0.21225E+01 Dimensionless distance yplus : 0.12375E-01 0.20841E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -4.097429425e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29467E+08 1 0.18023E-09 0.24649E+02 0.19317E+04 c Velocity[X] 0.12651E+02 c Velocity[Y] 0.11998E+02 c Velocity[Z] 0.16221E-05 c Pressure 0.19414E-03 146 0.77497E-04 0.21054E-02 0.31097E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -21.663 33.933 5.6132 8.0065 v Velocity[Y] -24.072 25.444 -0.14391 -0.0011556 v Velocity[Z] -3.0036 3.006 2.7633e-06 -5.3874e-08 v ǁVelocityǁ 0.00099939 34.019 7.4816 8.0728 v Pressure -2.2624e+05 1.3234e+05 -44158 -27175 v TurbVisc 1.0465e-21 0.012022 0.00015887 1.9131e-05 v CourantNb 3.3939e-08 0.011757 0.00016784 4.927e-06 v FourierNb 1.2425e-07 0.047092 0.00014587 2.6325e-07 v total_pressure -1.2492e+05 2.3366e+05 57167 74150 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0841 0.099556 0.0028411 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2319e-07 0.052411 0.00031371 5.1902e-06 INSTANT 0.875687000E-01 TIME STEP NUMBER 55885 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283195054E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.790836690E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10422E-01 0.21221E+01 Friction velocity uk : 0.10422E-01 0.21221E+01 Dimensionless distance yplus : 0.10044E-01 0.20837E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -4.601995586e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29466E+08 1 0.18022E-09 0.24654E+02 0.19319E+04 c Velocity[X] 0.12658E+02 c Velocity[Y] 0.11997E+02 c Velocity[Z] 0.16113E-05 c Pressure 0.19156E-03 59 0.83280E-04 0.20761E-02 0.31062E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -21.675 33.949 5.6132 8.0064 v Velocity[Y] -24.086 25.456 -0.14391 -0.0011625 v Velocity[Z] -3.0034 3.0062 2.7625e-06 -5.3874e-08 v ǁVelocityǁ 0.00098027 34.035 7.4832 8.0728 v Pressure -2.2811e+05 1.3085e+05 -45826 -28207 v TurbVisc 9.4558e-22 0.012042 0.00015894 1.9164e-05 v CourantNb 5.0081e-08 0.011757 0.00016784 4.927e-06 v FourierNb 1.2425e-07 0.047088 0.00014587 2.6347e-07 v total_pressure -1.2678e+05 2.3217e+05 55499 73118 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0837 0.099557 0.0028411 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2319e-07 0.052406 0.00031371 5.1905e-06 INSTANT 0.875688000E-01 TIME STEP NUMBER 55886 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283191041E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.790767273E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.74964E-02 0.21217E+01 Friction velocity uk : 0.74964E-02 0.21217E+01 Dimensionless distance yplus : 0.72246E-02 0.20833E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -5.306730018e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29466E+08 1 0.18021E-09 0.24659E+02 0.19320E+04 c Velocity[X] 0.12663E+02 c Velocity[Y] 0.11996E+02 c Velocity[Z] 0.16007E-05 c Pressure 0.18905E-03 192 0.96254E-04 0.20476E-02 0.25379E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -21.686 33.965 5.6131 8.0064 v Velocity[Y] -24.099 25.468 -0.14391 -0.0011668 v Velocity[Z] -3.0033 3.0064 2.7617e-06 -5.3874e-08 v ǁVelocityǁ 0.00096719 34.052 7.4848 8.0729 v Pressure -2.2995e+05 1.2938e+05 -47407 -29006 v TurbVisc 9.5201e-22 0.012061 0.000159 1.9198e-05 v CourantNb 4.2661e-08 0.011757 0.00016785 4.927e-06 v FourierNb 1.2425e-07 0.047083 0.00014587 2.6371e-07 v total_pressure -1.2862e+05 2.307e+05 53918 72319 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0833 0.099554 0.002841 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2319e-07 0.052401 0.00031372 5.1908e-06 INSTANT 0.875689000E-01 TIME STEP NUMBER 55887 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283186727E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.790689419E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.30327E-02 0.21212E+01 Friction velocity uk : 0.30327E-02 0.21212E+01 Dimensionless distance yplus : 0.29227E-02 0.20829E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -6.021554399e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29466E+08 1 0.18020E-09 0.24656E+02 0.19319E+04 c Velocity[X] 0.12669E+02 c Velocity[Y] 0.11987E+02 c Velocity[Z] 0.15938E-05 c Pressure 0.18645E-03 111 0.81810E-04 0.20181E-02 0.28055E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -21.698 33.982 5.613 8.0063 v Velocity[Y] -24.113 25.48 -0.14391 -0.0011727 v Velocity[Z] -3.0031 3.0067 2.761e-06 -5.3874e-08 v ǁVelocityǁ 0.00096016 34.068 7.4864 8.0729 v Pressure -2.3176e+05 1.2793e+05 -48999 -30006 v TurbVisc 1.237e-21 0.01208 0.00015906 1.923e-05 v CourantNb 4.7392e-08 0.011757 0.00016785 4.9271e-06 v FourierNb 1.2425e-07 0.047079 0.00014588 2.6393e-07 v total_pressure -1.3044e+05 2.2925e+05 52326 71319 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0829 0.099547 0.0028408 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.232e-07 0.052396 0.00031372 5.191e-06 INSTANT 0.875690000E-01 TIME STEP NUMBER 55888 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283182383E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.790599429E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.32198E-02 0.21208E+01 Friction velocity uk : 0.32198E-02 0.21208E+01 Dimensionless distance yplus : 0.31031E-02 0.20824E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -6.728715376e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29465E+08 1 0.18019E-09 0.24663E+02 0.19321E+04 c Velocity[X] 0.12675E+02 c Velocity[Y] 0.11988E+02 c Velocity[Z] 0.15921E-05 c Pressure 0.18201E-03 10 0.59137E-04 0.19688E-02 0.21661E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -21.71 33.998 5.6129 8.0062 v Velocity[Y] -24.126 25.492 -0.14391 -0.0011794 v Velocity[Z] -3.0029 3.0069 2.7602e-06 -5.3874e-08 v ǁVelocityǁ 0.00097135 34.084 7.4879 8.0729 v Pressure -2.3351e+05 1.2654e+05 -50536 -30811 v TurbVisc 1.0776e-21 0.012099 0.00015912 1.9263e-05 v CourantNb 7.3648e-08 0.011756 0.00016785 4.9271e-06 v FourierNb 1.2425e-07 0.047074 0.00014588 2.6416e-07 v total_pressure -1.3219e+05 2.2786e+05 50789 70514 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0824 0.099544 0.0028406 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.232e-07 0.052391 0.00031373 5.1913e-06 INSTANT 0.875691000E-01 TIME STEP NUMBER 55889 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283177867E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.790499113E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.26037E-02 0.21203E+01 Friction velocity uk : 0.26037E-02 0.21203E+01 Dimensionless distance yplus : 0.25093E-02 0.20820E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -7.586010948e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29465E+08 1 0.18018E-09 0.24665E+02 0.19322E+04 c Velocity[X] 0.12681E+02 c Velocity[Y] 0.11984E+02 c Velocity[Z] 0.15799E-05 c Pressure 0.17956E-03 365 0.77359E-04 0.19411E-02 0.25919E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -21.722 34.014 5.6128 8.0061 v Velocity[Y] -24.14 25.503 -0.14391 -0.0011844 v Velocity[Z] -3.0027 3.0071 2.7594e-06 -5.3874e-08 v ǁVelocityǁ 0.00097073 34.101 7.4895 8.0729 v Pressure -2.3528e+05 1.2512e+05 -52040 -31706 v TurbVisc 1.2426e-21 0.012119 0.00015918 1.9298e-05 v CourantNb 5.4962e-08 0.011756 0.00016785 4.9271e-06 v FourierNb 1.2425e-07 0.04707 0.00014588 2.644e-07 v total_pressure -1.3395e+05 2.2644e+05 49285 69619 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.082 0.099539 0.0028404 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.232e-07 0.052386 0.00031373 5.1915e-06 INSTANT 0.875692000E-01 TIME STEP NUMBER 55890 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283173243E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.790387493E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.25385E-02 0.21198E+01 Friction velocity uk : 0.25385E-02 0.21198E+01 Dimensionless distance yplus : 0.24465E-02 0.20815E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -8.155414361e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29465E+08 1 0.18017E-09 0.24670E+02 0.19323E+04 c Velocity[X] 0.12688E+02 c Velocity[Y] 0.11982E+02 c Velocity[Z] 0.15676E-05 c Pressure 0.17658E-03 92 0.82871E-04 0.19077E-02 0.26279E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -21.734 34.03 5.6127 8.006 v Velocity[Y] -24.153 25.515 -0.14391 -0.0011914 v Velocity[Z] -3.0026 3.0073 2.7587e-06 -5.3874e-08 v ǁVelocityǁ 0.0009863 34.117 7.4911 8.073 v Pressure -2.3696e+05 1.2376e+05 -53566 -32658 v TurbVisc 1.2476e-21 0.012138 0.00015924 1.933e-05 v CourantNb 3.3709e-08 0.011756 0.00016785 4.9271e-06 v FourierNb 1.2425e-07 0.047065 0.00014589 2.6462e-07 v total_pressure -1.3564e+05 2.2508e+05 47759 68667 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0815 0.099534 0.0028403 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.232e-07 0.05238 0.00031374 5.1918e-06 INSTANT 0.875693000E-01 TIME STEP NUMBER 55891 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283168565E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.790270626E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.33301E-02 0.21193E+01 Friction velocity uk : 0.33301E-02 0.21193E+01 Dimensionless distance yplus : 0.32093E-02 0.20810E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -8.893140734e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29464E+08 1 0.18016E-09 0.24673E+02 0.19324E+04 c Velocity[X] 0.12693E+02 c Velocity[Y] 0.11981E+02 c Velocity[Z] 0.15568E-05 c Pressure 0.17376E-03 192 0.95844E-04 0.18761E-02 0.21383E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -21.746 34.046 5.6126 8.0059 v Velocity[Y] -24.167 25.526 -0.14391 -0.001196 v Velocity[Z] -3.0024 3.0075 2.7579e-06 -5.3874e-08 v ǁVelocityǁ 0.0010096 34.133 7.4926 8.073 v Pressure -2.3861e+05 1.2242e+05 -55003 -33379 v TurbVisc 1.4609e-21 0.012157 0.0001593 1.9365e-05 v CourantNb 1.1306e-08 0.011756 0.00016785 4.9272e-06 v FourierNb 1.2425e-07 0.04706 0.00014589 2.6486e-07 v total_pressure -1.3729e+05 2.2374e+05 46322 67946 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.081 0.099523 0.00284 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.232e-07 0.052374 0.00031374 5.192e-06 INSTANT 0.875694000E-01 TIME STEP NUMBER 55892 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283163595E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.790146372E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.37631E-02 0.21188E+01 Friction velocity uk : 0.37631E-02 0.21188E+01 Dimensionless distance yplus : 0.36267E-02 0.20805E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -9.604343629e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29464E+08 1 0.18014E-09 0.24670E+02 0.19322E+04 c Velocity[X] 0.12699E+02 c Velocity[Y] 0.11971E+02 c Velocity[Z] 0.15481E-05 c Pressure 0.17087E-03 376 0.81474E-04 0.18437E-02 0.23087E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -21.757 34.062 5.6125 8.0058 v Velocity[Y] -24.18 25.538 -0.14391 -0.0012019 v Velocity[Z] -3.0022 3.0077 2.7572e-06 -5.3874e-08 v ǁVelocityǁ 0.0010402 34.149 7.4942 8.073 v Pressure -2.4023e+05 1.2111e+05 -56437 -34275 v TurbVisc 1.7172e-21 0.012176 0.00015936 1.9397e-05 v CourantNb 1.6439e-08 0.011756 0.00016785 4.9272e-06 v FourierNb 1.2425e-07 0.047055 0.00014589 2.6508e-07 v total_pressure -1.3891e+05 2.2244e+05 44888 67050 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0805 0.099509 0.0028397 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2321e-07 0.052369 0.00031375 5.1923e-06 INSTANT 0.875695000E-01 TIME STEP NUMBER 55893 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283158620E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.790010302E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.54915E-02 0.21183E+01 Friction velocity uk : 0.54915E-02 0.21183E+01 Dimensionless distance yplus : 0.52923E-02 0.20800E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.028603736e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29463E+08 1 0.18013E-09 0.24676E+02 0.19325E+04 c Velocity[X] 0.12704E+02 c Velocity[Y] 0.11972E+02 c Velocity[Z] 0.15434E-05 c Pressure 0.16598E-03 10 0.58558E-04 0.17898E-02 0.18412E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -21.769 34.077 5.6124 8.0057 v Velocity[Y] -24.193 25.549 -0.1439 -0.0012091 v Velocity[Z] -3.002 3.0079 2.7564e-06 -5.3874e-08 v ǁVelocityǁ 0.0010904 34.165 7.4958 8.073 v Pressure -2.4179e+05 1.1985e+05 -57832 -35023 v TurbVisc 1.6876e-21 0.012195 0.00015942 1.943e-05 v CourantNb 3.1005e-08 0.011756 0.00016785 4.9272e-06 v FourierNb 1.2425e-07 0.04705 0.0001459 2.6531e-07 v total_pressure -1.4047e+05 2.2118e+05 43493 66302 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.08 0.099492 0.0028393 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2321e-07 0.052363 0.00031375 5.1925e-06 INSTANT 0.875696000E-01 TIME STEP NUMBER 55894 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283153474E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.789863899E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.39257E-02 0.21178E+01 Friction velocity uk : 0.39257E-02 0.21178E+01 Dimensionless distance yplus : 0.39154E-02 0.20795E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.101515220e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29463E+08 1 0.18012E-09 0.24678E+02 0.19325E+04 c Velocity[X] 0.12710E+02 c Velocity[Y] 0.11967E+02 c Velocity[Z] 0.15313E-05 c Pressure 0.16335E-03 353 0.77373E-04 0.17604E-02 0.21705E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -21.781 34.093 5.6123 8.0056 v Velocity[Y] -24.206 25.56 -0.1439 -0.0012143 v Velocity[Z] -3.0019 3.0081 2.7556e-06 -5.3874e-08 v ǁVelocityǁ 0.0010747 34.181 7.4973 8.0731 v Pressure -2.4335e+05 1.1857e+05 -59171 -35825 v TurbVisc 1.8652e-21 0.012215 0.00015948 1.9465e-05 v CourantNb 1.6563e-08 0.011756 0.00016785 4.9272e-06 v FourierNb 1.2425e-07 0.047045 0.0001459 2.6555e-07 v total_pressure -1.4202e+05 2.199e+05 42154 65500 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0795 0.099475 0.0028389 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2321e-07 0.052358 0.00031375 5.1928e-06 INSTANT 0.875697000E-01 TIME STEP NUMBER 55895 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283148227E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.789707565E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.96234E-02 0.21173E+01 Friction velocity uk : 0.96234E-02 0.21173E+01 Dimensionless distance yplus : 0.93498E-02 0.20790E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.155803558e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29462E+08 1 0.18010E-09 0.24681E+02 0.19326E+04 c Velocity[X] 0.12716E+02 c Velocity[Y] 0.11965E+02 c Velocity[Z] 0.15209E-05 c Pressure 0.16010E-03 414 0.82987E-04 0.17243E-02 0.22530E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -21.792 34.109 5.6122 8.0055 v Velocity[Y] -24.219 25.571 -0.1439 -0.0012217 v Velocity[Z] -3.0017 3.0083 2.7549e-06 -5.3874e-08 v ǁVelocityǁ 0.0010289 34.197 7.4989 8.0731 v Pressure -2.4484e+05 1.1735e+05 -60543 -36701 v TurbVisc 2.1919e-21 0.012234 0.00015954 1.9498e-05 v CourantNb 1.817e-08 0.011755 0.00016785 4.9272e-06 v FourierNb 1.2425e-07 0.047039 0.0001459 2.6577e-07 v total_pressure -1.4351e+05 2.1867e+05 40782 64624 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.079 0.09947 0.0028386 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2321e-07 0.052352 0.00031376 5.193e-06 INSTANT 0.875698000E-01 TIME STEP NUMBER 55896 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283142953E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.789545014E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12010E-01 0.21168E+01 Friction velocity uk : 0.12010E-01 0.21168E+01 Dimensionless distance yplus : 0.11574E-01 0.20785E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.210772216e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29462E+08 1 0.18009E-09 0.24684E+02 0.19327E+04 c Velocity[X] 0.12721E+02 c Velocity[Y] 0.11963E+02 c Velocity[Z] 0.15072E-05 c Pressure 0.15711E-03 190 0.96019E-04 0.16911E-02 0.17069E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -21.804 34.125 5.6121 8.0054 v Velocity[Y] -24.232 25.582 -0.14389 -0.0012264 v Velocity[Z] -3.0015 3.0085 2.7541e-06 -5.3875e-08 v ǁVelocityǁ 0.00098096 34.213 7.5004 8.0731 v Pressure -2.4626e+05 1.1617e+05 -61796 -37282 v TurbVisc 2.464e-21 0.012253 0.0001596 1.9533e-05 v CourantNb 1.5947e-08 0.011755 0.00016786 4.9272e-06 v FourierNb 1.2425e-07 0.047034 0.00014591 2.6601e-07 v total_pressure -1.4494e+05 2.1749e+05 39529 64043 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0785 0.099458 0.0028382 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2321e-07 0.052346 0.00031376 5.1933e-06 INSTANT 0.875699000E-01 TIME STEP NUMBER 55897 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283137393E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.789377024E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10553E-01 0.21162E+01 Friction velocity uk : 0.10553E-01 0.21162E+01 Dimensionless distance yplus : 0.10393E-01 0.20780E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.263717174e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29461E+08 1 0.18007E-09 0.24679E+02 0.19325E+04 c Velocity[X] 0.12726E+02 c Velocity[Y] 0.11953E+02 c Velocity[Z] 0.14963E-05 c Pressure 0.15401E-03 129 0.81558E-04 0.16567E-02 0.20004E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -21.815 34.14 5.6119 8.0053 v Velocity[Y] -24.245 25.593 -0.14389 -0.0012328 v Velocity[Z] -3.0013 3.0087 2.7533e-06 -5.3875e-08 v ǁVelocityǁ 0.00093376 34.229 7.502 8.0731 v Pressure -2.4768e+05 1.15e+05 -63074 -38117 v TurbVisc 2.5304e-21 0.012272 0.00015966 1.9565e-05 v CourantNb 2.7124e-08 0.011755 0.00016786 4.9273e-06 v FourierNb 1.2425e-07 0.047029 0.00014591 2.6623e-07 v total_pressure -1.4636e+05 2.1632e+05 38251 63208 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.078 0.099441 0.0028376 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2321e-07 0.05234 0.00031377 5.1935e-06 INSTANT 0.875700000E-01 TIME STEP NUMBER 55898 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283131838E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.789196741E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.64992E-02 0.21157E+01 Friction velocity uk : 0.64992E-02 0.21157E+01 Dimensionless distance yplus : 0.64006E-02 0.20775E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.308778652e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29461E+08 1 0.18006E-09 0.24684E+02 0.19326E+04 c Velocity[X] 0.12731E+02 c Velocity[Y] 0.11953E+02 c Velocity[Z] 0.14987E-05 c Pressure 0.14876E-03 9 0.57459E-04 0.15992E-02 0.14287E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -21.827 34.156 5.6118 8.0051 v Velocity[Y] -24.258 25.604 -0.14388 -0.00124 v Velocity[Z] -3.0011 3.0089 2.7526e-06 -5.3875e-08 v ǁVelocityǁ 0.00087513 34.244 7.5035 8.0731 v Pressure -2.4902e+05 1.1389e+05 -64285 -38735 v TurbVisc 2.8779e-21 0.012292 0.00015971 1.9598e-05 v CourantNb 4.0734e-08 0.011755 0.00016786 4.9273e-06 v FourierNb 1.2425e-07 0.047024 0.00014591 2.6646e-07 v total_pressure -1.4769e+05 2.1521e+05 37040 62590 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0775 0.09942 0.0028371 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2322e-07 0.052334 0.00031377 5.1937e-06 INSTANT 0.875701000E-01 TIME STEP NUMBER 55899 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283126162E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.789007656E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.23268E-02 0.21152E+01 Friction velocity uk : 0.23268E-02 0.21152E+01 Dimensionless distance yplus : 0.22533E-02 0.20770E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.353421007e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29460E+08 1 0.18004E-09 0.24684E+02 0.19326E+04 c Velocity[X] 0.12736E+02 c Velocity[Y] 0.11948E+02 c Velocity[Z] 0.14830E-05 c Pressure 0.14605E-03 174 0.76996E-04 0.15691E-02 0.18424E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -21.838 34.171 5.6117 8.005 v Velocity[Y] -24.271 25.615 -0.14388 -0.0012454 v Velocity[Z] -3.001 3.0091 2.7518e-06 -5.3875e-08 v ǁVelocityǁ 0.00083787 34.26 7.505 8.0731 v Pressure -2.5036e+05 1.1276e+05 -65457 -39462 v TurbVisc 3.2015e-21 0.012311 0.00015977 1.9633e-05 v CourantNb 2.4478e-08 0.011755 0.00016786 4.9273e-06 v FourierNb 1.2425e-07 0.047019 0.00014592 2.667e-07 v total_pressure -1.4904e+05 2.1408e+05 35868 61863 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.077 0.099405 0.0028365 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2322e-07 0.052329 0.00031377 5.194e-06 INSTANT 0.875702000E-01 TIME STEP NUMBER 55900 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283120358E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.788810191E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.96499E-02 0.21147E+01 Friction velocity uk : 0.96499E-02 0.21147E+01 Dimensionless distance yplus : 0.92876E-02 0.20765E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.380758594e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29460E+08 1 0.18003E-09 0.24687E+02 0.19327E+04 c Velocity[X] 0.12741E+02 c Velocity[Y] 0.11945E+02 c Velocity[Z] 0.14662E-05 c Pressure 0.14264E-03 97 0.82392E-04 0.15315E-02 0.18147E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -21.85 34.187 5.6116 8.0049 v Velocity[Y] -24.284 25.626 -0.14388 -0.001253 v Velocity[Z] -3.0008 3.0093 2.7511e-06 -5.3875e-08 v ǁVelocityǁ 0.00079083 34.275 7.5066 8.0731 v Pressure -2.5163e+05 1.1169e+05 -66633 -40194 v TurbVisc 3.4772e-21 0.01233 0.00015983 1.9666e-05 v CourantNb 3.1582e-08 0.011755 0.00016786 4.9273e-06 v FourierNb 1.2425e-07 0.047014 0.00014592 2.6692e-07 v total_pressure -1.503e+05 2.1302e+05 34692 61131 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0765 0.099396 0.0028361 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2322e-07 0.052323 0.00031378 5.1942e-06 INSTANT 0.875703000E-01 TIME STEP NUMBER 55901 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283114558E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.788605559E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.66533E-02 0.21142E+01 Friction velocity uk : 0.66533E-02 0.21142E+01 Dimensionless distance yplus : 0.64035E-02 0.20760E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.403545309e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29459E+08 1 0.18001E-09 0.24688E+02 0.19327E+04 c Velocity[X] 0.12745E+02 c Velocity[Y] 0.11943E+02 c Velocity[Z] 0.14554E-05 c Pressure 0.13956E-03 224 0.95744E-04 0.14976E-02 0.15147E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -21.861 34.202 5.6114 8.0048 v Velocity[Y] -24.297 25.637 -0.14387 -0.0012581 v Velocity[Z] -3.0006 3.0095 2.7503e-06 -5.3875e-08 v ǁVelocityǁ 0.00074472 34.291 7.5081 8.0731 v Pressure -2.5284e+05 1.1065e+05 -67724 -40731 v TurbVisc 3.604e-21 0.012349 0.00015988 1.9701e-05 v CourantNb 2.8706e-08 0.011755 0.00016786 4.9273e-06 v FourierNb 1.2425e-07 0.047009 0.00014592 2.6716e-07 v total_pressure -1.5152e+05 2.1198e+05 33601 60594 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.076 0.099381 0.0028356 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2322e-07 0.052317 0.00031378 5.1945e-06 INSTANT 0.875704000E-01 TIME STEP NUMBER 55902 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283108490E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.788396155E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.54818E-02 0.21137E+01 Friction velocity uk : 0.54818E-02 0.21137E+01 Dimensionless distance yplus : 0.52768E-02 0.20755E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.420314289e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29459E+08 1 0.17999E-09 0.24682E+02 0.19324E+04 c Velocity[X] 0.12749E+02 c Velocity[Y] 0.11933E+02 c Velocity[Z] 0.14462E-05 c Pressure 0.13647E-03 107 0.81064E-04 0.14636E-02 0.15923E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -21.873 34.217 5.6113 8.0047 v Velocity[Y] -24.31 25.647 -0.14387 -0.0012648 v Velocity[Z] -3.0004 3.0097 2.7495e-06 -5.3875e-08 v ǁVelocityǁ 0.00070027 34.306 7.5096 8.0731 v Pressure -2.5403e+05 1.0965e+05 -68804 -41430 v TurbVisc 4.0016e-21 0.012368 0.00015994 1.9733e-05 v CourantNb 2.0163e-08 0.011754 0.00016786 4.9273e-06 v FourierNb 1.2425e-07 0.047004 0.00014593 2.6738e-07 v total_pressure -1.5271e+05 2.1097e+05 32521 59895 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0755 0.099367 0.002835 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2322e-07 0.052312 0.00031378 5.1947e-06 INSTANT 0.875705000E-01 TIME STEP NUMBER 55903 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283102445E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.788177201E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.49471E-02 0.21132E+01 Friction velocity uk : 0.49471E-02 0.21132E+01 Dimensionless distance yplus : 0.47622E-02 0.20750E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.429423696e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29458E+08 1 0.17998E-09 0.24685E+02 0.19326E+04 c Velocity[X] 0.12753E+02 c Velocity[Y] 0.11932E+02 c Velocity[Z] 0.14422E-05 c Pressure 0.13092E-03 9 0.56161E-04 0.14032E-02 0.11334E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -21.884 34.232 5.6112 8.0045 v Velocity[Y] -24.323 25.658 -0.14386 -0.0012723 v Velocity[Z] -3.0003 3.0099 2.7488e-06 -5.3875e-08 v ǁVelocityǁ 0.00065237 34.322 7.5112 8.0731 v Pressure -2.5515e+05 1.0869e+05 -69823 -41943 v TurbVisc 4.7099e-21 0.012388 0.00016 1.9767e-05 v CourantNb 8.9695e-09 0.011754 0.00016786 4.9273e-06 v FourierNb 1.2425e-07 0.046998 0.00014593 2.6762e-07 v total_pressure -1.5382e+05 2.1002e+05 31502 59382 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.075 0.09935 0.0028345 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2322e-07 0.052306 0.00031379 5.1949e-06 INSTANT 0.875706000E-01 TIME STEP NUMBER 55904 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283096307E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.787950272E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.42829E-02 0.21127E+01 Friction velocity uk : 0.42829E-02 0.21127E+01 Dimensionless distance yplus : 0.41498E-02 0.20745E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.430622034e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29458E+08 1 0.17996E-09 0.24684E+02 0.19325E+04 c Velocity[X] 0.12757E+02 c Velocity[Y] 0.11927E+02 c Velocity[Z] 0.14293E-05 c Pressure 0.12828E-03 372 0.76960E-04 0.13741E-02 0.15385E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -21.895 34.247 5.6111 8.0044 v Velocity[Y] -24.335 25.669 -0.14386 -0.001278 v Velocity[Z] -3.0001 3.0101 2.748e-06 -5.3875e-08 v ǁVelocityǁ 0.0006174 34.337 7.5127 8.0731 v Pressure -2.5627e+05 1.0773e+05 -70813 -42569 v TurbVisc 4.7842e-21 0.012407 0.00016005 1.9802e-05 v CourantNb 2.0092e-08 0.011754 0.00016786 4.9273e-06 v FourierNb 1.2425e-07 0.046993 0.00014593 2.6786e-07 v total_pressure -1.5495e+05 2.0905e+05 30512 58756 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0745 0.099336 0.0028341 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2322e-07 0.0523 0.00031379 5.1952e-06 INSTANT 0.875707000E-01 TIME STEP NUMBER 55905 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283090032E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.787715595E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.46938E-02 0.21122E+01 Friction velocity uk : 0.46938E-02 0.21122E+01 Dimensionless distance yplus : 0.45480E-02 0.20740E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.425541309e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29457E+08 1 0.17994E-09 0.24685E+02 0.19325E+04 c Velocity[X] 0.12761E+02 c Velocity[Y] 0.11924E+02 c Velocity[Z] 0.14169E-05 c Pressure 0.12494E-03 67 0.82129E-04 0.13375E-02 0.14147E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -21.907 34.262 5.6109 8.0043 v Velocity[Y] -24.348 25.679 -0.14385 -0.0012858 v Velocity[Z] -2.9999 3.0103 2.7472e-06 -5.3875e-08 v ǁVelocityǁ 0.00057994 34.352 7.5142 8.0731 v Pressure -2.573e+05 1.0684e+05 -71770 -43129 v TurbVisc 5.1089e-21 0.012426 0.00016011 1.9834e-05 v CourantNb 2.5163e-08 0.011754 0.00016786 4.9273e-06 v FourierNb 1.2425e-07 0.046988 0.00014594 2.6808e-07 v total_pressure -1.5598e+05 2.0816e+05 29555 58196 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.074 0.099328 0.0028338 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2322e-07 0.052295 0.0003138 5.1954e-06 INSTANT 0.875708000E-01 TIME STEP NUMBER 55906 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283083810E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.787476522E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11923E-01 0.21118E+01 Friction velocity uk : 0.11923E-01 0.21118E+01 Dimensionless distance yplus : 0.11552E-01 0.20736E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.406702145e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29457E+08 1 0.17992E-09 0.24685E+02 0.19325E+04 c Velocity[X] 0.12764E+02 c Velocity[Y] 0.11921E+02 c Velocity[Z] 0.14080E-05 c Pressure 0.12192E-03 188 0.95443E-04 0.13044E-02 0.13456E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -21.918 34.277 5.6108 8.0041 v Velocity[Y] -24.361 25.69 -0.14385 -0.0012913 v Velocity[Z] -2.9997 3.0105 2.7465e-06 -5.3875e-08 v ǁVelocityǁ 0.00054629 34.367 7.5158 8.0731 v Pressure -2.583e+05 1.0595e+05 -72683 -43625 v TurbVisc 5.6552e-21 0.012445 0.00016016 1.987e-05 v CourantNb 1.9235e-08 0.011754 0.00016786 4.9273e-06 v FourierNb 1.2425e-07 0.046984 0.00014594 2.6832e-07 v total_pressure -1.5698e+05 2.0728e+05 28642 57700 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0736 0.099321 0.0028335 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2322e-07 0.052289 0.0003138 5.1957e-06 INSTANT 0.875709000E-01 TIME STEP NUMBER 55907 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283077296E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.787231275E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.14855E-01 0.21113E+01 Friction velocity uk : 0.14855E-01 0.21113E+01 Dimensionless distance yplus : 0.14901E-01 0.20731E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.382230069e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29456E+08 1 0.17991E-09 0.24677E+02 0.19321E+04 c Velocity[X] 0.12767E+02 c Velocity[Y] 0.11910E+02 c Velocity[Z] 0.14007E-05 c Pressure 0.11902E-03 77 0.80894E-04 0.12726E-02 0.12564E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -21.929 34.292 5.6107 8.004 v Velocity[Y] -24.374 25.7 -0.14385 -0.0012983 v Velocity[Z] -2.9995 3.0107 2.7457e-06 -5.3875e-08 v ǁVelocityǁ 0.00051643 34.382 7.5173 8.0731 v Pressure -2.5926e+05 1.0513e+05 -73557 -44186 v TurbVisc 6.0947e-21 0.012464 0.00016021 1.9902e-05 v CourantNb 4.9788e-08 0.011754 0.00016786 4.9273e-06 v FourierNb 1.2425e-07 0.046979 0.00014594 2.6855e-07 v total_pressure -1.5794e+05 2.0645e+05 27768 57139 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0731 0.099312 0.0028331 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2323e-07 0.052284 0.0003138 5.1959e-06 INSTANT 0.875710000E-01 TIME STEP NUMBER 55908 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283070845E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.786979397E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.84462E-02 0.21108E+01 Friction velocity uk : 0.84462E-02 0.21108E+01 Dimensionless distance yplus : 0.84721E-02 0.20726E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.352814502e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29455E+08 1 0.17989E-09 0.24679E+02 0.19322E+04 c Velocity[X] 0.12770E+02 c Velocity[Y] 0.11909E+02 c Velocity[Z] 0.13952E-05 c Pressure 0.11330E-03 9 0.55226E-04 0.12107E-02 0.87591E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -21.94 34.307 5.6106 8.0039 v Velocity[Y] -24.386 25.71 -0.14384 -0.0013062 v Velocity[Z] -2.9994 3.0109 2.745e-06 -5.3875e-08 v ǁVelocityǁ 0.00048872 34.397 7.5188 8.0731 v Pressure -2.6015e+05 1.0435e+05 -74369 -44590 v TurbVisc 6.1987e-21 0.012484 0.00016027 1.9936e-05 v CourantNb 2.9811e-08 0.011753 0.00016786 4.9273e-06 v FourierNb 1.2425e-07 0.046974 0.00014595 2.6878e-07 v total_pressure -1.5882e+05 2.0567e+05 26956 56735 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0726 0.099302 0.0028328 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2323e-07 0.052278 0.00031381 5.1961e-06 INSTANT 0.875711000E-01 TIME STEP NUMBER 55909 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283064331E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.786720847E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.47093E-02 0.21103E+01 Friction velocity uk : 0.47093E-02 0.21103E+01 Dimensionless distance yplus : 0.45659E-02 0.20722E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.311384019e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29455E+08 1 0.17987E-09 0.24676E+02 0.19320E+04 c Velocity[X] 0.12772E+02 c Velocity[Y] 0.11904E+02 c Velocity[Z] 0.13855E-05 c Pressure 0.11096E-03 167 0.76434E-04 0.11850E-02 0.12051E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -21.951 34.322 5.6105 8.0037 v Velocity[Y] -24.399 25.721 -0.14384 -0.0013122 v Velocity[Z] -2.9992 3.0111 2.7442e-06 -5.3875e-08 v ǁVelocityǁ 0.00046943 34.412 7.5204 8.0731 v Pressure -2.6103e+05 1.0358e+05 -75150 -45066 v TurbVisc 6.6805e-21 0.012503 0.00016032 1.9972e-05 v CourantNb 2.7256e-08 0.011753 0.00016786 4.9273e-06 v FourierNb 1.2425e-07 0.046969 0.00014595 2.6902e-07 v total_pressure -1.5971e+05 2.0491e+05 26175 56259 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0722 0.099292 0.0028324 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2323e-07 0.052273 0.00031381 5.1964e-06 INSTANT 0.875712000E-01 TIME STEP NUMBER 55910 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283057675E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.786455306E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.61894E-02 0.21099E+01 Friction velocity uk : 0.61894E-02 0.21099E+01 Dimensionless distance yplus : 0.61364E-02 0.20717E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.276554292e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29454E+08 1 0.17985E-09 0.24675E+02 0.19320E+04 c Velocity[X] 0.12775E+02 c Velocity[Y] 0.11900E+02 c Velocity[Z] 0.13810E-05 c Pressure 0.10786E-03 53 0.81927E-04 0.11512E-02 0.12019E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -21.962 34.336 5.6103 8.0036 v Velocity[Y] -24.411 25.731 -0.14384 -0.0013203 v Velocity[Z] -2.999 3.0113 2.7435e-06 -5.3875e-08 v ǁVelocityǁ 0.00045273 34.427 7.5219 8.073 v Pressure -2.6183e+05 1.029e+05 -75903 -45529 v TurbVisc 7.5357e-21 0.012522 0.00016038 2.0005e-05 v CourantNb 4.6278e-08 0.011753 0.00016786 4.9274e-06 v FourierNb 1.2425e-07 0.046964 0.00014595 2.6925e-07 v total_pressure -1.6051e+05 2.0422e+05 25422 55796 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0717 0.09928 0.002832 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2323e-07 0.052267 0.00031381 5.1966e-06 INSTANT 0.875713000E-01 TIME STEP NUMBER 55911 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283051104E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.786186858E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.32246E-02 0.21094E+01 Friction velocity uk : 0.32246E-02 0.21094E+01 Dimensionless distance yplus : 0.31880E-02 0.20713E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.222744596e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29454E+08 1 0.17983E-09 0.24673E+02 0.19319E+04 c Velocity[X] 0.12776E+02 c Velocity[Y] 0.11897E+02 c Velocity[Z] 0.13702E-05 c Pressure 0.10521E-03 230 0.95305E-04 0.11223E-02 0.11477E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -21.974 34.351 5.6102 8.0035 v Velocity[Y] -24.424 25.741 -0.14384 -0.0013261 v Velocity[Z] -2.9988 3.0115 2.7427e-06 -5.3875e-08 v ǁVelocityǁ 0.00044103 34.442 7.5234 8.073 v Pressure -2.6262e+05 1.0222e+05 -76607 -45919 v TurbVisc 7.5911e-21 0.012541 0.00016043 2.004e-05 v CourantNb 6.5092e-08 0.011753 0.00016786 4.9274e-06 v FourierNb 1.2425e-07 0.046959 0.00014595 2.6949e-07 v total_pressure -1.6129e+05 2.0354e+05 24718 55406 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0713 0.099272 0.0028317 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2323e-07 0.052262 0.00031382 5.1969e-06 INSTANT 0.875714000E-01 TIME STEP NUMBER 55912 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283044256E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.785913343E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.41373E-02 0.21090E+01 Friction velocity uk : 0.41373E-02 0.21090E+01 Dimensionless distance yplus : 0.40225E-02 0.20708E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.167268153e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29453E+08 1 0.17981E-09 0.24663E+02 0.19315E+04 c Velocity[X] 0.12778E+02 c Velocity[Y] 0.11886E+02 c Velocity[Z] 0.13602E-05 c Pressure 0.10274E-03 605 0.80890E-04 0.10954E-02 0.88845E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -21.985 34.366 5.6101 8.0033 v Velocity[Y] -24.436 25.751 -0.14383 -0.0013332 v Velocity[Z] -2.9986 3.0117 2.7419e-06 -5.3875e-08 v ǁVelocityǁ 0.00043347 34.456 7.5249 8.073 v Pressure -2.6333e+05 1.0163e+05 -77250 -46293 v TurbVisc 7.9806e-21 0.012561 0.00016048 2.0073e-05 v CourantNb 6.9258e-08 0.011753 0.00016786 4.9274e-06 v FourierNb 1.2425e-07 0.046954 0.00014596 2.6972e-07 v total_pressure -1.62e+05 2.0295e+05 24075 55032 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0708 0.099294 0.0028316 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2323e-07 0.052257 0.00031382 5.1971e-06 INSTANT 0.875715000E-01 TIME STEP NUMBER 55913 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283037510E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.785634918E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.52066E-02 0.21085E+01 Friction velocity uk : 0.52066E-02 0.21085E+01 Dimensionless distance yplus : 0.50712E-02 0.20704E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.109610727e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29452E+08 1 0.17979E-09 0.24663E+02 0.19315E+04 c Velocity[X] 0.12779E+02 c Velocity[Y] 0.11884E+02 c Velocity[Z] 0.13556E-05 c Pressure 0.97030E-04 9 0.55168E-04 0.10339E-02 0.74476E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -21.996 34.38 5.61 8.0032 v Velocity[Y] -24.449 25.761 -0.14384 -0.0013418 v Velocity[Z] -2.9985 3.0119 2.7412e-06 -5.3875e-08 v ǁVelocityǁ 0.00043014 34.471 7.5265 8.073 v Pressure -2.6401e+05 1.0106e+05 -77857 -46633 v TurbVisc 8.2964e-21 0.01258 0.00016053 2.0107e-05 v CourantNb 5.9428e-08 0.011752 0.00016787 4.9274e-06 v FourierNb 1.2425e-07 0.046949 0.00014596 2.6995e-07 v total_pressure -1.6268e+05 2.0239e+05 23468 54692 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0704 0.099317 0.0028316 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2323e-07 0.052251 0.00031383 5.1973e-06 INSTANT 0.875716000E-01 TIME STEP NUMBER 55914 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283030695E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.785350470E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.42252E-02 0.21081E+01 Friction velocity uk : 0.42252E-02 0.21081E+01 Dimensionless distance yplus : 0.41153E-02 0.20699E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.038357779e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29452E+08 1 0.17977E-09 0.24659E+02 0.19312E+04 c Velocity[X] 0.12780E+02 c Velocity[Y] 0.11879E+02 c Velocity[Z] 0.13487E-05 c Pressure 0.95380E-04 166 0.77036E-04 0.10157E-02 0.98560E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -22.007 34.394 5.6099 8.0031 v Velocity[Y] -24.461 25.771 -0.14384 -0.0013481 v Velocity[Z] -2.9983 3.0121 2.7404e-06 -5.3875e-08 v ǁVelocityǁ 0.0004296 34.486 7.528 8.073 v Pressure -2.6466e+05 1.0051e+05 -78428 -46978 v TurbVisc 9.0148e-21 0.012599 0.00016058 2.0143e-05 v CourantNb 5.0461e-08 0.011752 0.00016787 4.9274e-06 v FourierNb 1.2425e-07 0.046944 0.00014596 2.702e-07 v total_pressure -1.6334e+05 2.0184e+05 22897 54347 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0699 0.099339 0.0028317 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2323e-07 0.052246 0.00031383 5.1976e-06 INSTANT 0.875717000E-01 TIME STEP NUMBER 55915 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283023758E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.785060424E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10283E-01 0.21076E+01 Friction velocity uk : 0.10283E-01 0.21076E+01 Dimensionless distance yplus : 0.10015E-01 0.20695E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -9.940264373e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29451E+08 1 0.17975E-09 0.24656E+02 0.19311E+04 c Velocity[X] 0.12781E+02 c Velocity[Y] 0.11874E+02 c Velocity[Z] 0.13427E-05 c Pressure 0.92890E-04 65 0.82347E-04 0.98862E-03 0.97489E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -22.017 34.409 5.6098 8.0029 v Velocity[Y] -24.473 25.78 -0.14384 -0.0013565 v Velocity[Z] -2.9981 3.0123 2.7397e-06 -5.3875e-08 v ǁVelocityǁ 0.00043085 34.5 7.5295 8.073 v Pressure -2.6523e+05 1.0005e+05 -78951 -47301 v TurbVisc 9.6172e-21 0.012618 0.00016064 2.0176e-05 v CourantNb 4.011e-08 0.011752 0.00016787 4.9274e-06 v FourierNb 1.2425e-07 0.04694 0.00014597 2.7042e-07 v total_pressure -1.6391e+05 2.0137e+05 22374 54024 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0695 0.099367 0.0028318 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2323e-07 0.052241 0.00031383 5.1978e-06 INSTANT 0.875718000E-01 TIME STEP NUMBER 55916 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283016932E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.784769305E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.30730E-02 0.21072E+01 Friction velocity uk : 0.30730E-02 0.21072E+01 Dimensionless distance yplus : 0.29989E-02 0.20691E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -9.212008173e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29451E+08 1 0.17973E-09 0.24652E+02 0.19309E+04 c Velocity[X] 0.12781E+02 c Velocity[Y] 0.11871E+02 c Velocity[Z] 0.13346E-05 c Pressure 0.90988E-04 295 0.95956E-04 0.96782E-03 0.98447E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -22.028 34.423 5.6097 8.0028 v Velocity[Y] -24.486 25.79 -0.14384 -0.0013626 v Velocity[Z] -2.9979 3.0125 2.7389e-06 -5.3875e-08 v ǁVelocityǁ 0.00043427 34.515 7.5311 8.0729 v Pressure -2.6578e+05 99591 -79431 -47554 v TurbVisc 1.1103e-20 0.012637 0.00016069 2.0212e-05 v CourantNb 3.1834e-08 0.011752 0.00016787 4.9274e-06 v FourierNb 1.2425e-07 0.046935 0.00014597 2.7067e-07 v total_pressure -1.6445e+05 2.0092e+05 21894 53771 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0691 0.099389 0.0028319 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2323e-07 0.052236 0.00031384 5.198e-06 INSTANT 0.875719000E-01 TIME STEP NUMBER 55917 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283009864E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.784473323E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.39962E-02 0.21068E+01 Friction velocity uk : 0.39962E-02 0.21068E+01 Dimensionless distance yplus : 0.38999E-02 0.20687E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -8.536904176e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29450E+08 1 0.17971E-09 0.24640E+02 0.19305E+04 c Velocity[X] 0.12781E+02 c Velocity[Y] 0.11859E+02 c Velocity[Z] 0.13273E-05 c Pressure 0.89376E-04 96 0.81264E-04 0.95014E-03 0.76679E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -22.039 34.437 5.6096 8.0026 v Velocity[Y] -24.498 25.8 -0.14384 -0.0013705 v Velocity[Z] -2.9977 3.0127 2.7381e-06 -5.3875e-08 v ǁVelocityǁ 0.00043629 34.529 7.5326 8.0729 v Pressure -2.6627e+05 99207 -79864 -47854 v TurbVisc 1.0341e-20 0.012657 0.00016074 2.0245e-05 v CourantNb 2.4258e-08 0.011752 0.00016787 4.9274e-06 v FourierNb 1.2425e-07 0.04693 0.00014597 2.709e-07 v total_pressure -1.6494e+05 2.0053e+05 21461 53471 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0687 0.09941 0.0028319 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2323e-07 0.05223 0.00031384 5.1983e-06 INSTANT 0.875720000E-01 TIME STEP NUMBER 55918 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283002876E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.784174105E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.83785E-02 0.21063E+01 Friction velocity uk : 0.83785E-02 0.21063E+01 Dimensionless distance yplus : 0.83350E-02 0.20682E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -7.902606054e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29449E+08 1 0.17969E-09 0.24638E+02 0.19303E+04 c Velocity[X] 0.12781E+02 c Velocity[Y] 0.11857E+02 c Velocity[Z] 0.13300E-05 c Pressure 0.84073E-04 7 0.55394E-04 0.89325E-03 0.43592E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -22.05 34.452 5.6095 8.0025 v Velocity[Y] -24.51 25.809 -0.14384 -0.0013791 v Velocity[Z] -2.9976 3.0129 2.7374e-06 -5.3875e-08 v ǁVelocityǁ 0.00043572 34.544 7.5341 8.0729 v Pressure -2.6669e+05 98875 -80215 -48006 v TurbVisc 1.0558e-20 0.012676 0.00016079 2.028e-05 v CourantNb 1.7398e-08 0.011751 0.00016787 4.9274e-06 v FourierNb 1.2425e-07 0.046925 0.00014597 2.7113e-07 v total_pressure -1.6536e+05 2.002e+05 21110 53319 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0682 0.099432 0.0028321 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2324e-07 0.052225 0.00031385 5.1985e-06 INSTANT 0.875721000E-01 TIME STEP NUMBER 55919 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282995903E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.783870580E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.62940E-02 0.21059E+01 Friction velocity uk : 0.62940E-02 0.21059E+01 Dimensionless distance yplus : 0.62613E-02 0.20678E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -7.195993616e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29449E+08 1 0.17967E-09 0.24631E+02 0.19301E+04 c Velocity[X] 0.12780E+02 c Velocity[Y] 0.11851E+02 c Velocity[Z] 0.13246E-05 c Pressure 0.83570E-04 270 0.77296E-04 0.88740E-03 0.84857E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -22.061 34.466 5.6094 8.0024 v Velocity[Y] -24.522 25.818 -0.14385 -0.0013858 v Velocity[Z] -2.9974 3.0131 2.7366e-06 -5.3875e-08 v ǁVelocityǁ 0.00043024 34.558 7.5357 8.0729 v Pressure -2.6711e+05 98574 -80602 -48269 v TurbVisc 6.2002e-21 0.012695 0.00016084 2.0315e-05 v CourantNb 1.0676e-08 0.011751 0.00016787 4.9274e-06 v FourierNb 1.2425e-07 0.04692 0.00014598 2.7138e-07 v total_pressure -1.6578e+05 1.999e+05 20723 53056 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0678 0.099453 0.0028322 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2324e-07 0.05222 0.00031385 5.1988e-06 INSTANT 0.875722000E-01 TIME STEP NUMBER 55920 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282988766E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.783560496E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11191E-01 0.21055E+01 Friction velocity uk : 0.11191E-01 0.21055E+01 Dimensionless distance yplus : 0.11133E-01 0.20674E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -6.724874713e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29448E+08 1 0.17965E-09 0.24626E+02 0.19299E+04 c Velocity[X] 0.12780E+02 c Velocity[Y] 0.11847E+02 c Velocity[Z] 0.13096E-05 c Pressure 0.82213E-04 380 0.82701E-04 0.87250E-03 0.84163E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -22.071 34.48 5.6093 8.0022 v Velocity[Y] -24.534 25.828 -0.14385 -0.0013949 v Velocity[Z] -2.9972 3.0133 2.7359e-06 -5.3875e-08 v ǁVelocityǁ 0.00042927 34.572 7.5372 8.0729 v Pressure -2.6744e+05 98326 -80882 -48461 v TurbVisc 1.3607e-20 0.012714 0.00016089 2.0349e-05 v CourantNb 4.6107e-09 0.011751 0.00016787 4.9274e-06 v FourierNb 1.2425e-07 0.046916 0.00014598 2.7161e-07 v total_pressure -1.6612e+05 1.9965e+05 20443 52864 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0674 0.099473 0.0028323 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2324e-07 0.052215 0.00031385 5.199e-06 INSTANT 0.875723000E-01 TIME STEP NUMBER 55921 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282981775E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.783253783E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.18859E-01 0.21051E+01 Friction velocity uk : 0.18859E-01 0.21051E+01 Dimensionless distance yplus : 0.18761E-01 0.20670E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -6.092079401e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29447E+08 1 0.17963E-09 0.24620E+02 0.19296E+04 c Velocity[X] 0.12777E+02 c Velocity[Y] 0.11843E+02 c Velocity[Z] 0.13029E-05 c Pressure 0.81596E-04 123 0.96028E-04 0.86547E-03 0.89261E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -22.082 34.494 5.6093 8.0021 v Velocity[Y] -24.546 25.837 -0.14386 -0.0014012 v Velocity[Z] -2.997 3.0135 2.7351e-06 -5.3875e-08 v ǁVelocityǁ 0.000429 34.586 7.5387 8.0729 v Pressure -2.6773e+05 98133 -81109 -48516 v TurbVisc 1.273e-20 0.012733 0.00016094 2.0385e-05 v CourantNb 1.1148e-09 0.011751 0.00016788 4.9274e-06 v FourierNb 1.2425e-07 0.046911 0.00014598 2.7186e-07 v total_pressure -1.664e+05 1.9946e+05 20216 52809 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.067 0.099496 0.0028325 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2324e-07 0.05221 0.00031386 5.1992e-06 INSTANT 0.875724000E-01 TIME STEP NUMBER 55922 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282974586E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.782942269E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19183E-01 0.21047E+01 Friction velocity uk : 0.19183E-01 0.21047E+01 Dimensionless distance yplus : 0.18608E-01 0.20666E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -5.549107277e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29447E+08 1 0.17961E-09 0.24607E+02 0.19290E+04 c Velocity[X] 0.12776E+02 c Velocity[Y] 0.11831E+02 c Velocity[Z] 0.12970E-05 c Pressure 0.81336E-04 82 0.81428E-04 0.86223E-03 0.64987E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -22.092 34.508 5.6092 8.0019 v Velocity[Y] -24.558 25.846 -0.14387 -0.0014093 v Velocity[Z] -2.9968 3.0137 2.7344e-06 -5.3875e-08 v ǁVelocityǁ 0.00042914 34.601 7.5403 8.0728 v Pressure -2.6799e+05 97983 -81328 -48728 v TurbVisc 1.1216e-20 0.012752 0.00016099 2.0418e-05 v CourantNb 5.4278e-09 0.011751 0.00016788 4.9274e-06 v FourierNb 1.2425e-07 0.046907 0.00014599 2.7208e-07 v total_pressure -1.6666e+05 1.9931e+05 19997 52597 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0666 0.099517 0.0028326 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2324e-07 0.052205 0.00031386 5.1995e-06 INSTANT 0.875725000E-01 TIME STEP NUMBER 55923 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282967490E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.782626990E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.18496E-01 0.21043E+01 Friction velocity uk : 0.18496E-01 0.21043E+01 Dimensionless distance yplus : 0.17942E-01 0.20662E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -5.063837591e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29446E+08 1 0.17959E-09 0.24602E+02 0.19289E+04 c Velocity[X] 0.12774E+02 c Velocity[Y] 0.11829E+02 c Velocity[Z] 0.12955E-05 c Pressure 0.77119E-04 6 0.55837E-04 0.81707E-03 0.33759E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -22.103 34.522 5.6091 8.0018 v Velocity[Y] -24.57 25.855 -0.14387 -0.0014183 v Velocity[Z] -2.9966 3.0139 2.7336e-06 -5.3876e-08 v ǁVelocityǁ 0.000429 34.615 7.5418 8.0728 v Pressure -2.6817e+05 97903 -81442 -48773 v TurbVisc 1.2556e-20 0.012772 0.00016104 2.0453e-05 v CourantNb 9.5811e-09 0.01175 0.00016788 4.9274e-06 v FourierNb 1.2425e-07 0.046902 0.00014599 2.7232e-07 v total_pressure -1.6685e+05 1.9923e+05 19883 52552 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0662 0.099536 0.0028327 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2324e-07 0.0522 0.00031387 5.1997e-06 INSTANT 0.875726000E-01 TIME STEP NUMBER 55924 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282960437E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.782309424E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.18015E-01 0.21039E+01 Friction velocity uk : 0.18015E-01 0.21039E+01 Dimensionless distance yplus : 0.17475E-01 0.20658E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -4.604593166e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29446E+08 1 0.17958E-09 0.24594E+02 0.19285E+04 c Velocity[X] 0.12771E+02 c Velocity[Y] 0.11823E+02 c Velocity[Z] 0.12890E-05 c Pressure 0.78320E-04 53 0.77763E-04 0.82933E-03 0.70596E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -22.113 34.536 5.609 8.0016 v Velocity[Y] -24.582 25.864 -0.14388 -0.0014254 v Velocity[Z] -2.9965 3.0141 2.7329e-06 -5.3876e-08 v ǁVelocityǁ 0.00042977 34.629 7.5434 8.0728 v Pressure -2.6834e+05 97843 -81600 -48853 v TurbVisc 1.3184e-20 0.012791 0.00016109 2.0489e-05 v CourantNb 1.4299e-08 0.01175 0.00016788 4.9274e-06 v FourierNb 1.2425e-07 0.046897 0.00014599 2.7257e-07 v total_pressure -1.6702e+05 1.9917e+05 19725 52472 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0658 0.099555 0.0028329 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2324e-07 0.052194 0.00031387 5.1999e-06 INSTANT 0.875727000E-01 TIME STEP NUMBER 55925 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282953220E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.781986136E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.17509E-01 0.21035E+01 Friction velocity uk : 0.17509E-01 0.21035E+01 Dimensionless distance yplus : 0.16984E-01 0.20654E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -4.256422120e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29445E+08 1 0.17956E-09 0.24587E+02 0.19282E+04 c Velocity[X] 0.12769E+02 c Velocity[Y] 0.11818E+02 c Velocity[Z] 0.12812E-05 c Pressure 0.78518E-04 471 0.83111E-04 0.83097E-03 0.78861E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -22.124 34.55 5.6089 8.0015 v Velocity[Y] -24.594 25.873 -0.14389 -0.0014349 v Velocity[Z] -2.9963 3.0143 2.7321e-06 -5.3876e-08 v ǁVelocityǁ 0.00043018 34.643 7.5449 8.0728 v Pressure -2.6845e+05 97851 -81654 -48960 v TurbVisc 1.3633e-20 0.01281 0.00016113 2.0523e-05 v CourantNb 1.6434e-08 0.01175 0.00016788 4.9274e-06 v FourierNb 1.2425e-07 0.046893 0.00014599 2.728e-07 v total_pressure -1.6712e+05 1.9918e+05 19671 52365 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0654 0.099569 0.002833 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2325e-07 0.05219 0.00031388 5.2002e-06 INSTANT 0.875728000E-01 TIME STEP NUMBER 55926 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282946169E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.781667084E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15692E-01 0.21031E+01 Friction velocity uk : 0.15692E-01 0.21031E+01 Dimensionless distance yplus : 0.15662E-01 0.20651E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -3.927555209e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29444E+08 1 0.17954E-09 0.24579E+02 0.19279E+04 c Velocity[X] 0.12765E+02 c Velocity[Y] 0.11814E+02 c Velocity[Z] 0.12735E-05 c Pressure 0.79562E-04 38 0.96707E-04 0.84155E-03 0.91070E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -22.134 34.563 5.6089 8.0013 v Velocity[Y] -24.605 25.882 -0.1439 -0.0014415 v Velocity[Z] -2.9961 3.0145 2.7314e-06 -5.3876e-08 v ǁVelocityǁ 0.00043035 34.657 7.5464 8.0727 v Pressure -2.685e+05 97909 -81651 -48890 v TurbVisc 1.6064e-20 0.012829 0.00016118 2.0559e-05 v CourantNb 1.9565e-08 0.01175 0.00016788 4.9274e-06 v FourierNb 1.2425e-07 0.046888 0.000146 2.7305e-07 v total_pressure -1.6717e+05 1.9923e+05 19674 52435 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0651 0.099584 0.0028331 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2325e-07 0.052185 0.00031388 5.2004e-06 INSTANT 0.875729000E-01 TIME STEP NUMBER 55927 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282938953E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.781344444E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10642E-01 0.21027E+01 Friction velocity uk : 0.10642E-01 0.21027E+01 Dimensionless distance yplus : 0.10621E-01 0.20647E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -3.664832203e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29444E+08 1 0.17952E-09 0.24563E+02 0.19272E+04 c Velocity[X] 0.12762E+02 c Velocity[Y] 0.11801E+02 c Velocity[Z] 0.12663E-05 c Pressure 0.80977E-04 127 0.81794E-04 0.85604E-03 0.53040E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -22.144 34.577 5.6088 8.0012 v Velocity[Y] -24.617 25.891 -0.14391 -0.00145 v Velocity[Z] -2.9959 3.0147 2.7306e-06 -5.3876e-08 v ǁVelocityǁ 0.00043028 34.671 7.548 8.0727 v Pressure -2.6851e+05 98024 -81623 -48935 v TurbVisc 1.4421e-20 0.012848 0.00016123 2.0592e-05 v CourantNb 2.2316e-08 0.011749 0.00016789 4.9274e-06 v FourierNb 1.2425e-07 0.046884 0.000146 2.7328e-07 v total_pressure -1.6718e+05 1.9935e+05 19702 52390 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0647 0.099597 0.0028332 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2325e-07 0.05218 0.00031388 5.2007e-06 INSTANT 0.875730000E-01 TIME STEP NUMBER 55928 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282931851E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.781019915E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.35158E-02 0.21024E+01 Friction velocity uk : 0.35158E-02 0.21024E+01 Dimensionless distance yplus : 0.35089E-02 0.20643E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -3.479750224e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29443E+08 1 0.17950E-09 0.24558E+02 0.19270E+04 c Velocity[X] 0.12759E+02 c Velocity[Y] 0.11798E+02 c Velocity[Z] 0.12677E-05 c Pressure 0.78384E-04 7 0.55504E-04 0.82818E-03 0.31910E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -22.155 34.591 5.6087 8.0011 v Velocity[Y] -24.629 25.9 -0.14392 -0.0014593 v Velocity[Z] -2.9957 3.0149 2.7299e-06 -5.3876e-08 v ǁVelocityǁ 0.00043074 34.684 7.5495 8.0727 v Pressure -2.6848e+05 98181 -81581 -48932 v TurbVisc 1.4473e-20 0.012868 0.00016128 2.0627e-05 v CourantNb 2.4816e-08 0.011749 0.00016789 4.9274e-06 v FourierNb 1.2425e-07 0.04688 0.000146 2.7352e-07 v total_pressure -1.6716e+05 1.9951e+05 19744 52393 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0643 0.099609 0.0028334 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2325e-07 0.052175 0.00031389 5.2009e-06 INSTANT 0.875731000E-01 TIME STEP NUMBER 55929 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282924801E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.780693711E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.66303E-02 0.21020E+01 Friction velocity uk : 0.66303E-02 0.21020E+01 Dimensionless distance yplus : 0.66173E-02 0.20640E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -3.293011740e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29442E+08 1 0.17948E-09 0.24547E+02 0.19265E+04 c Velocity[X] 0.12754E+02 c Velocity[Y] 0.11793E+02 c Velocity[Z] 0.12569E-05 c Pressure 0.81204E-04 43 0.77723E-04 0.85751E-03 0.74974E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -22.165 34.604 5.6087 8.0009 v Velocity[Y] -24.64 25.909 -0.14393 -0.0014668 v Velocity[Z] -2.9955 3.0151 2.7291e-06 -5.3876e-08 v ǁVelocityǁ 0.00042975 34.698 7.551 8.0727 v Pressure -2.6838e+05 98410 -81381 -48782 v TurbVisc 9.4961e-23 0.012887 0.00016132 2.0664e-05 v CourantNb 2.5991e-08 0.011749 0.00016789 4.9274e-06 v FourierNb 1.2425e-07 0.046875 0.000146 2.7376e-07 v total_pressure -1.6706e+05 1.9973e+05 19944 52543 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.064 0.099621 0.0028334 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2325e-07 0.052171 0.00031389 5.2012e-06 INSTANT 0.875732000E-01 TIME STEP NUMBER 55930 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282917627E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.780369920E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.93888E-02 0.21017E+01 Friction velocity uk : 0.93888E-02 0.21017E+01 Dimensionless distance yplus : 0.92203E-02 0.20636E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -3.342919920e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29442E+08 1 0.17946E-09 0.24538E+02 0.19262E+04 c Velocity[X] 0.12750E+02 c Velocity[Y] 0.11787E+02 c Velocity[Z] 0.12501E-05 c Pressure 0.83016E-04 474 0.82899E-04 0.87616E-03 0.75097E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -22.175 34.618 5.6086 8.0008 v Velocity[Y] -24.652 25.917 -0.14394 -0.0014767 v Velocity[Z] -2.9954 3.0153 2.7283e-06 -5.3876e-08 v ǁVelocityǁ 0.00042899 34.712 7.5526 8.0727 v Pressure -2.6827e+05 98669 -81241 -48755 v TurbVisc 1.2752e-20 0.012906 0.00016137 2.0697e-05 v CourantNb 2.9509e-08 0.011749 0.00016789 4.9274e-06 v FourierNb 1.2425e-07 0.046871 0.000146 2.74e-07 v total_pressure -1.6694e+05 1.9999e+05 20084 52570 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0636 0.099639 0.0028336 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2326e-07 0.052166 0.0003139 5.2014e-06 INSTANT 0.875733000E-01 TIME STEP NUMBER 55931 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282910637E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.780038418E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.49899E-02 0.21013E+01 Friction velocity uk : 0.49899E-02 0.21013E+01 Dimensionless distance yplus : 0.49946E-02 0.20633E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -3.314973219e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29441E+08 1 0.17944E-09 0.24528E+02 0.19258E+04 c Velocity[X] 0.12745E+02 c Velocity[Y] 0.11784E+02 c Velocity[Z] 0.12412E-05 c Pressure 0.85531E-04 183 0.96619E-04 0.90221E-03 0.97865E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -22.185 34.631 5.6085 8.0006 v Velocity[Y] -24.663 25.926 -0.14395 -0.0014836 v Velocity[Z] -2.9952 3.0155 2.7276e-06 -5.3876e-08 v ǁVelocityǁ 0.00042858 34.726 7.5541 8.0727 v Pressure -2.6808e+05 98988 -81013 -48565 v TurbVisc 1.3328e-20 0.012925 0.00016142 2.0734e-05 v CourantNb 3.156e-08 0.011748 0.00016789 4.9274e-06 v FourierNb 1.2425e-07 0.046867 0.00014601 2.7425e-07 v total_pressure -1.6676e+05 2.0031e+05 20312 52760 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0633 0.099656 0.0028337 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2326e-07 0.052161 0.0003139 5.2016e-06 INSTANT 0.875734000E-01 TIME STEP NUMBER 55932 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282903505E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.779709114E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.31031E-02 0.21010E+01 Friction velocity uk : 0.31031E-02 0.21010E+01 Dimensionless distance yplus : 0.30474E-02 0.20630E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -3.371008861e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29441E+08 1 0.17942E-09 0.24511E+02 0.19251E+04 c Velocity[X] 0.12740E+02 c Velocity[Y] 0.11771E+02 c Velocity[Z] 0.12343E-05 c Pressure 0.88321E-04 74 0.81640E-04 0.93114E-03 0.55931E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -22.195 34.645 5.6085 8.0005 v Velocity[Y] -24.674 25.935 -0.14396 -0.0014926 v Velocity[Z] -2.995 3.0157 2.7268e-06 -5.3876e-08 v ǁVelocityǁ 0.00042805 34.739 7.5556 8.0726 v Pressure -2.6788e+05 99348 -80769 -48528 v TurbVisc 1.3629e-20 0.012944 0.00016147 2.0768e-05 v CourantNb 3.3683e-08 0.011748 0.00016789 4.9274e-06 v FourierNb 1.2425e-07 0.046862 0.00014601 2.7448e-07 v total_pressure -1.6656e+05 2.0067e+05 20556 52797 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.063 0.099673 0.0028338 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2326e-07 0.052157 0.0003139 5.2019e-06 INSTANT 0.875735000E-01 TIME STEP NUMBER 55933 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282896482E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.779379794E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.33057E-02 0.21007E+01 Friction velocity uk : 0.33057E-02 0.21007E+01 Dimensionless distance yplus : 0.32464E-02 0.20627E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -3.494384044e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29440E+08 1 0.17941E-09 0.24503E+02 0.19247E+04 c Velocity[X] 0.12736E+02 c Velocity[Y] 0.11767E+02 c Velocity[Z] 0.12334E-05 c Pressure 0.87386E-04 7 0.55419E-04 0.92078E-03 0.38275E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -22.205 34.658 5.6084 8.0003 v Velocity[Y] -24.685 25.943 -0.14397 -0.0015025 v Velocity[Z] -2.9948 3.0159 2.7261e-06 -5.3876e-08 v ǁVelocityǁ 0.00042829 34.753 7.5571 8.0726 v Pressure -2.6763e+05 99767 -80488 -48419 v TurbVisc 1.3796e-20 0.012964 0.00016151 2.0803e-05 v CourantNb 3.5929e-08 0.011748 0.0001679 4.9274e-06 v FourierNb 1.2425e-07 0.046858 0.00014601 2.7472e-07 v total_pressure -1.6631e+05 2.0109e+05 20837 52906 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0627 0.099691 0.0028339 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2326e-07 0.052152 0.00031391 5.2021e-06 INSTANT 0.875736000E-01 TIME STEP NUMBER 55934 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282889552E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.779051015E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.53913E-02 0.21004E+01 Friction velocity uk : 0.53913E-02 0.21004E+01 Dimensionless distance yplus : 0.52734E-02 0.20624E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -3.667508282e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29439E+08 1 0.17939E-09 0.24491E+02 0.19242E+04 c Velocity[X] 0.12728E+02 c Velocity[Y] 0.11762E+02 c Velocity[Z] 0.12236E-05 c Pressure 0.91265E-04 43 0.77888E-04 0.96113E-03 0.10457E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -22.215 34.672 5.6083 8.0002 v Velocity[Y] -24.697 25.952 -0.14398 -0.0015102 v Velocity[Z] -2.9946 3.0161 2.7253e-06 -5.3876e-08 v ǁVelocityǁ 0.00042766 34.766 7.5587 8.0726 v Pressure -2.673e+05 1.0026e+05 -80055 -48042 v TurbVisc 1.7145e-20 0.012983 0.00016156 2.0839e-05 v CourantNb 3.8293e-08 0.011748 0.0001679 4.9274e-06 v FourierNb 1.2425e-07 0.046854 0.00014601 2.7497e-07 v total_pressure -1.6597e+05 2.0158e+05 21270 53283 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0624 0.099706 0.0028339 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2327e-07 0.052148 0.00031391 5.2024e-06 INSTANT 0.875737000E-01 TIME STEP NUMBER 55935 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282882517E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.778724931E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.33190E-02 0.21000E+01 Friction velocity uk : 0.33190E-02 0.21000E+01 Dimensionless distance yplus : 0.32464E-02 0.20620E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -3.915668863e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29439E+08 1 0.17937E-09 0.24481E+02 0.19238E+04 c Velocity[X] 0.12724E+02 c Velocity[Y] 0.11757E+02 c Velocity[Z] 0.12175E-05 c Pressure 0.94223E-04 321 0.83174E-04 0.99176E-03 0.81710E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -22.225 34.685 5.6082 8.0001 v Velocity[Y] -24.708 25.96 -0.14399 -0.0015204 v Velocity[Z] -2.9944 3.0163 2.7246e-06 -5.3876e-08 v ǁVelocityǁ 0.00042756 34.78 7.5602 8.0726 v Pressure -2.6696e+05 1.0077e+05 -79688 -47925 v TurbVisc 1.4736e-20 0.013002 0.0001616 2.0874e-05 v CourantNb 4.0564e-08 0.011747 0.0001679 4.9274e-06 v FourierNb 1.2425e-07 0.04685 0.00014602 2.752e-07 v total_pressure -1.6564e+05 2.021e+05 21637 53400 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.062 0.099725 0.002834 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2327e-07 0.052144 0.00031392 5.2026e-06 INSTANT 0.875738000E-01 TIME STEP NUMBER 55936 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282875685E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.778393148E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15670E-02 0.20997E+01 Friction velocity uk : 0.15670E-02 0.20997E+01 Dimensionless distance yplus : 0.15327E-02 0.20617E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -4.169842976e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29438E+08 1 0.17935E-09 0.24470E+02 0.19234E+04 c Velocity[X] 0.12717E+02 c Velocity[Y] 0.11753E+02 c Velocity[Z] 0.12087E-05 c Pressure 0.97673E-04 32 0.97108E-04 0.10275E-02 0.11180E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -22.234 34.698 5.6082 7.9999 v Velocity[Y] -24.719 25.969 -0.144 -0.0015277 v Velocity[Z] -2.9943 3.0165 2.7238e-06 -5.3876e-08 v ǁVelocityǁ 0.00042756 34.793 7.5617 8.0726 v Pressure -2.6657e+05 1.0134e+05 -79233 -47611 v TurbVisc 1.616e-20 0.013021 0.00016165 2.091e-05 v CourantNb 4.3237e-08 0.011747 0.0001679 4.9274e-06 v FourierNb 1.2425e-07 0.046846 0.00014602 2.7545e-07 v total_pressure -1.6524e+05 2.0266e+05 22092 53714 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0617 0.099741 0.002834 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2327e-07 0.052139 0.00031392 5.2029e-06 INSTANT 0.875739000E-01 TIME STEP NUMBER 55937 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282868733E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.778064160E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.32207E-02 0.20994E+01 Friction velocity uk : 0.32207E-02 0.20994E+01 Dimensionless distance yplus : 0.31502E-02 0.20614E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -4.507114458e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29438E+08 1 0.17934E-09 0.24450E+02 0.19226E+04 c Velocity[X] 0.12710E+02 c Velocity[Y] 0.11740E+02 c Velocity[Z] 0.11999E-05 c Pressure 0.10128E-03 633 0.82494E-04 0.10649E-02 0.68898E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -22.244 34.711 5.6081 7.9998 v Velocity[Y] -24.73 25.977 -0.14401 -0.0015369 v Velocity[Z] -2.9941 3.0167 2.7231e-06 -5.3876e-08 v ǁVelocityǁ 0.00042779 34.807 7.5632 8.0726 v Pressure -2.6613e+05 1.0197e+05 -78744 -47402 v TurbVisc 1.6297e-20 0.01304 0.0001617 2.0944e-05 v CourantNb 4.387e-08 0.011747 0.0001679 4.9274e-06 v FourierNb 1.2425e-07 0.046842 0.00014602 2.7569e-07 v total_pressure -1.6481e+05 2.0329e+05 22581 53923 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0614 0.099755 0.002834 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2328e-07 0.052135 0.00031392 5.2031e-06 INSTANT 0.875740000E-01 TIME STEP NUMBER 55938 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282861923E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.777736984E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19995E-02 0.20991E+01 Friction velocity uk : 0.19995E-02 0.20991E+01 Dimensionless distance yplus : 0.19557E-02 0.20611E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -4.839767411e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29437E+08 1 0.17932E-09 0.24442E+02 0.19222E+04 c Velocity[X] 0.12705E+02 c Velocity[Y] 0.11737E+02 c Velocity[Z] 0.11961E-05 c Pressure 0.10155E-03 9 0.56647E-04 0.10671E-02 0.47995E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -22.254 34.724 5.608 7.9996 v Velocity[Y] -24.741 25.986 -0.14403 -0.0015474 v Velocity[Z] -2.9939 3.0169 2.7223e-06 -5.3876e-08 v ǁVelocityǁ 0.00042696 34.82 7.5648 8.0725 v Pressure -2.657e+05 1.0261e+05 -78251 -47242 v TurbVisc 1.7228e-20 0.013059 0.00016174 2.098e-05 v CourantNb 4.0612e-08 0.011746 0.0001679 4.9274e-06 v FourierNb 1.2425e-07 0.046838 0.00014602 2.7593e-07 v total_pressure -1.6438e+05 2.0393e+05 23074 54083 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0611 0.09977 0.002834 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2328e-07 0.052131 0.00031393 5.2033e-06 INSTANT 0.875741000E-01 TIME STEP NUMBER 55939 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282855203E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.777410410E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.23083E-02 0.20988E+01 Friction velocity uk : 0.23083E-02 0.20988E+01 Dimensionless distance yplus : 0.22578E-02 0.20609E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -5.240514146e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29436E+08 1 0.17930E-09 0.24428E+02 0.19216E+04 c Velocity[X] 0.12696E+02 c Velocity[Y] 0.11732E+02 c Velocity[Z] 0.11905E-05 c Pressure 0.10593E-03 59 0.78861E-04 0.11126E-02 0.13129E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -22.263 34.738 5.608 7.9995 v Velocity[Y] -24.752 25.994 -0.14404 -0.0015554 v Velocity[Z] -2.9937 3.0171 2.7216e-06 -5.3876e-08 v ǁVelocityǁ 0.00042853 34.833 7.5663 8.0725 v Pressure -2.6514e+05 1.0335e+05 -77610 -46709 v TurbVisc 1.5554e-20 0.013079 0.00016179 2.1016e-05 v CourantNb 3.653e-08 0.011746 0.00016791 4.9274e-06 v FourierNb 1.2425e-07 0.046834 0.00014603 2.7618e-07 v total_pressure -1.6381e+05 2.0467e+05 23715 54616 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0609 0.099783 0.002834 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2328e-07 0.052127 0.00031393 5.2036e-06 INSTANT 0.875742000E-01 TIME STEP NUMBER 55940 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282848407E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.777088431E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.69730E-02 0.20985E+01 Friction velocity uk : 0.69730E-02 0.20985E+01 Dimensionless distance yplus : 0.68204E-02 0.20605E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -5.573856768e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29436E+08 1 0.17929E-09 0.24416E+02 0.19212E+04 c Velocity[X] 0.12690E+02 c Velocity[Y] 0.11726E+02 c Velocity[Z] 0.11854E-05 c Pressure 0.10946E-03 262 0.84219E-04 0.11490E-02 0.96577E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -22.273 34.751 5.6079 7.9994 v Velocity[Y] -24.763 26.002 -0.14405 -0.0015658 v Velocity[Z] -2.9935 3.0173 2.7208e-06 -5.3876e-08 v ǁVelocityǁ 0.00042881 34.847 7.5678 8.0725 v Pressure -2.6458e+05 1.0412e+05 -76998 -46427 v TurbVisc 1.4255e-20 0.013098 0.00016183 2.1051e-05 v CourantNb 3.3446e-08 0.011746 0.00016791 4.9274e-06 v FourierNb 1.2425e-07 0.046829 0.00014603 2.7642e-07 v total_pressure -1.6326e+05 2.0544e+05 24327 54898 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0605 0.099801 0.002834 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2329e-07 0.052122 0.00031394 5.2038e-06 INSTANT 0.875743000E-01 TIME STEP NUMBER 55941 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282841848E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.776763538E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10448E-01 0.20982E+01 Friction velocity uk : 0.10448E-01 0.20982E+01 Dimensionless distance yplus : 0.10058E-01 0.20602E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -5.990447029e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29435E+08 1 0.17927E-09 0.24404E+02 0.19207E+04 c Velocity[X] 0.12682E+02 c Velocity[Y] 0.11722E+02 c Velocity[Z] 0.11771E-05 c Pressure 0.11336E-03 107 0.98275E-04 0.11893E-02 0.12175E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -22.282 34.764 5.6078 7.9992 v Velocity[Y] -24.774 26.011 -0.14406 -0.0015737 v Velocity[Z] -2.9933 3.0175 2.7201e-06 -5.3876e-08 v ǁVelocityǁ 0.00042888 34.86 7.5693 8.0725 v Pressure -2.64e+05 1.049e+05 -76339 -46049 v TurbVisc 1.446e-20 0.013117 0.00016188 2.1088e-05 v CourantNb 2.9177e-08 0.011746 0.00016791 4.9274e-06 v FourierNb 1.2425e-07 0.046825 0.00014603 2.7667e-07 v total_pressure -1.6268e+05 2.0623e+05 24986 55276 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0602 0.099815 0.0028339 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2329e-07 0.052117 0.00031394 5.2041e-06 INSTANT 0.875744000E-01 TIME STEP NUMBER 55942 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282835160E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.776441284E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.39901E-02 0.20979E+01 Friction velocity uk : 0.39901E-02 0.20979E+01 Dimensionless distance yplus : 0.38413E-02 0.20599E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -6.425479656e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29435E+08 1 0.17926E-09 0.24384E+02 0.19198E+04 c Velocity[X] 0.12674E+02 c Velocity[Y] 0.11709E+02 c Velocity[Z] 0.11705E-05 c Pressure 0.11729E-03 510 0.83466E-04 0.12300E-02 0.88274E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -22.292 34.777 5.6078 7.9991 v Velocity[Y] -24.784 26.019 -0.14407 -0.0015834 v Velocity[Z] -2.9931 3.0177 2.7193e-06 -5.3876e-08 v ǁVelocityǁ 0.00042872 34.873 7.5708 8.0725 v Pressure -2.6337e+05 1.0576e+05 -75635 -45718 v TurbVisc 1.6234e-20 0.013136 0.00016192 2.1122e-05 v CourantNb 2.4627e-08 0.011745 0.00016791 4.9274e-06 v FourierNb 1.2425e-07 0.046821 0.00014603 2.769e-07 v total_pressure -1.6204e+05 2.0709e+05 25690 55607 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0599 0.099829 0.0028339 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.233e-07 0.052113 0.00031394 5.2043e-06 INSTANT 0.875745000E-01 TIME STEP NUMBER 55943 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282828639E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.776123144E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.91254E-02 0.20975E+01 Friction velocity uk : 0.91254E-02 0.20975E+01 Dimensionless distance yplus : 0.87852E-02 0.20596E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -6.825880820e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29434E+08 1 0.17924E-09 0.24374E+02 0.19194E+04 c Velocity[X] 0.12668E+02 c Velocity[Y] 0.11706E+02 c Velocity[Z] 0.11668E-05 c Pressure 0.11820E-03 9 0.56769E-04 0.12389E-02 0.70903E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -22.301 34.79 5.6077 7.999 v Velocity[Y] -24.795 26.028 -0.14408 -0.001594 v Velocity[Z] -2.9929 3.0179 2.7186e-06 -5.3876e-08 v ǁVelocityǁ 0.00042799 34.886 7.5723 8.0725 v Pressure -2.6271e+05 1.0665e+05 -74900 -45395 v TurbVisc 1.8482e-20 0.013155 0.00016197 2.1157e-05 v CourantNb 2.1692e-08 0.011745 0.00016791 4.9274e-06 v FourierNb 1.2425e-07 0.046817 0.00014604 2.7715e-07 v total_pressure -1.6138e+05 2.0797e+05 26425 55930 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0596 0.099843 0.0028338 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.233e-07 0.052108 0.00031395 5.2046e-06 INSTANT 0.875746000E-01 TIME STEP NUMBER 55944 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282822268E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.775807958E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.40197E-02 0.20972E+01 Friction velocity uk : 0.40197E-02 0.20972E+01 Dimensionless distance yplus : 0.38997E-02 0.20593E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -7.297775091e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29433E+08 1 0.17923E-09 0.24359E+02 0.19188E+04 c Velocity[X] 0.12658E+02 c Velocity[Y] 0.11701E+02 c Velocity[Z] 0.11623E-05 c Pressure 0.12275E-03 53 0.79125E-04 0.12859E-02 0.15607E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -22.311 34.803 5.6076 7.9988 v Velocity[Y] -24.806 26.036 -0.14409 -0.0016024 v Velocity[Z] -2.9928 3.0181 2.7179e-06 -5.3876e-08 v ǁVelocityǁ 0.00042784 34.899 7.5738 8.0725 v Pressure -2.6195e+05 1.0762e+05 -74069 -44746 v TurbVisc 1.5248e-20 0.013174 0.00016201 2.1194e-05 v CourantNb 2.1889e-08 0.011745 0.00016791 4.9274e-06 v FourierNb 1.2425e-07 0.046813 0.00014604 2.774e-07 v total_pressure -1.6062e+05 2.0894e+05 27256 56579 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0593 0.099856 0.0028337 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2331e-07 0.052104 0.00031395 5.2048e-06 INSTANT 0.875747000E-01 TIME STEP NUMBER 55945 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282815799E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.775496600E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.41315E-02 0.20969E+01 Friction velocity uk : 0.41315E-02 0.20969E+01 Dimensionless distance yplus : 0.40082E-02 0.20590E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -7.561313585e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29433E+08 1 0.17921E-09 0.24347E+02 0.19183E+04 c Velocity[X] 0.12651E+02 c Velocity[Y] 0.11696E+02 c Velocity[Z] 0.11551E-05 c Pressure 0.12642E-03 529 0.84555E-04 0.13236E-02 0.11514E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -22.32 34.816 5.6075 7.9987 v Velocity[Y] -24.817 26.044 -0.14409 -0.0016134 v Velocity[Z] -2.9926 3.0183 2.7171e-06 -5.3876e-08 v ǁVelocityǁ 0.000427 34.912 7.5753 8.0725 v Pressure -2.612e+05 1.086e+05 -73236 -44353 v TurbVisc 1.8661e-20 0.013194 0.00016206 2.1229e-05 v CourantNb 2.2182e-08 0.011745 0.00016791 4.9275e-06 v FourierNb 1.2425e-07 0.046808 0.00014604 2.7764e-07 v total_pressure -1.5988e+05 2.0993e+05 28089 56972 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.059 0.099872 0.0028336 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2331e-07 0.052099 0.00031395 5.2051e-06 INSTANT 0.875748000E-01 TIME STEP NUMBER 55946 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282809592E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.775186326E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.32647E-02 0.20966E+01 Friction velocity uk : 0.32647E-02 0.20966E+01 Dimensionless distance yplus : 0.31672E-02 0.20586E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -7.992765947e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29432E+08 1 0.17920E-09 0.24334E+02 0.19178E+04 c Velocity[X] 0.12642E+02 c Velocity[Y] 0.11692E+02 c Velocity[Z] 0.11500E-05 c Pressure 0.13043E-03 33 0.98685E-04 0.13648E-02 0.14963E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -22.329 34.829 5.6074 7.9986 v Velocity[Y] -24.827 26.053 -0.1441 -0.0016214 v Velocity[Z] -2.9924 3.0185 2.7164e-06 -5.3876e-08 v ǁVelocityǁ 0.00042639 34.925 7.5768 8.0725 v Pressure -2.604e+05 1.0962e+05 -72361 -43823 v TurbVisc 1.9257e-20 0.013213 0.0001621 2.1266e-05 v CourantNb 2.2459e-08 0.011744 0.00016792 4.9275e-06 v FourierNb 1.2425e-07 0.046803 0.00014604 2.7789e-07 v total_pressure -1.5908e+05 2.1094e+05 28964 57502 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0586 0.099888 0.0028335 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2332e-07 0.052094 0.00031396 5.2053e-06 INSTANT 0.875749000E-01 TIME STEP NUMBER 55947 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282803296E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.774878617E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.42837E-02 0.20962E+01 Friction velocity uk : 0.42837E-02 0.20962E+01 Dimensionless distance yplus : 0.41558E-02 0.20583E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -8.372164199e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29432E+08 1 0.17919E-09 0.24313E+02 0.19169E+04 c Velocity[X] 0.12634E+02 c Velocity[Y] 0.11679E+02 c Velocity[Z] 0.11470E-05 c Pressure 0.13441E-03 857 0.83833E-04 0.14058E-02 0.11331E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -22.338 34.841 5.6073 7.9985 v Velocity[Y] -24.838 26.061 -0.14411 -0.0016312 v Velocity[Z] -2.9922 3.0187 2.7156e-06 -5.3876e-08 v ǁVelocityǁ 0.00042616 34.939 7.5783 8.0725 v Pressure -2.5956e+05 1.107e+05 -71443 -43361 v TurbVisc 1.9449e-20 0.013232 0.00016215 2.1301e-05 v CourantNb 2.546e-08 0.011744 0.00016792 4.9275e-06 v FourierNb 1.2425e-07 0.046799 0.00014604 2.7813e-07 v total_pressure -1.5823e+05 2.1202e+05 29882 57964 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0583 0.099905 0.0028334 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2332e-07 0.052089 0.00031396 5.2056e-06 INSTANT 0.875750000E-01 TIME STEP NUMBER 55948 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282797180E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.774576747E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.99387E-02 0.20958E+01 Friction velocity uk : 0.99387E-02 0.20958E+01 Dimensionless distance yplus : 0.96420E-02 0.20579E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -8.701578720e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29431E+08 1 0.17917E-09 0.24303E+02 0.19165E+04 c Velocity[X] 0.12627E+02 c Velocity[Y] 0.11676E+02 c Velocity[Z] 0.11458E-05 c Pressure 0.13570E-03 9 0.57576E-04 0.14186E-02 0.86783E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -22.348 34.854 5.6073 7.9983 v Velocity[Y] -24.848 26.069 -0.14412 -0.0016425 v Velocity[Z] -2.992 3.0189 2.7149e-06 -5.3876e-08 v ǁVelocityǁ 0.00042624 34.952 7.5798 8.0725 v Pressure -2.5873e+05 1.1177e+05 -70516 -42978 v TurbVisc 1.8652e-20 0.013251 0.00016219 2.1337e-05 v CourantNb 1.3873e-08 0.011744 0.00016792 4.9275e-06 v FourierNb 1.2425e-07 0.046794 0.00014605 2.7837e-07 v total_pressure -1.574e+05 2.1309e+05 30809 58347 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0579 0.099922 0.0028333 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2333e-07 0.052084 0.00031397 5.2058e-06 INSTANT 0.875751000E-01 TIME STEP NUMBER 55949 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282791229E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.774278665E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.14117E-01 0.20955E+01 Friction velocity uk : 0.14117E-01 0.20955E+01 Dimensionless distance yplus : 0.13678E-01 0.20576E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -9.054260227e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29431E+08 1 0.17916E-09 0.24288E+02 0.19159E+04 c Velocity[X] 0.12616E+02 c Velocity[Y] 0.11672E+02 c Velocity[Z] 0.11415E-05 c Pressure 0.14013E-03 160 0.79881E-04 0.14640E-02 0.19727E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -22.357 34.867 5.6072 7.9982 v Velocity[Y] -24.859 26.078 -0.14412 -0.001651 v Velocity[Z] -2.9918 3.0191 2.7141e-06 -5.3877e-08 v ǁVelocityǁ 0.00042747 34.965 7.5813 8.0725 v Pressure -2.5774e+05 1.1296e+05 -69478 -42156 v TurbVisc 1.8066e-20 0.01327 0.00016223 2.1373e-05 v CourantNb 8.4652e-10 0.011744 0.00016792 4.9275e-06 v FourierNb 1.2425e-07 0.046789 0.00014605 2.7863e-07 v total_pressure -1.5641e+05 2.1429e+05 31847 59169 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0576 0.09994 0.0028333 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2334e-07 0.052079 0.00031397 5.2061e-06 INSTANT 0.875752000E-01 TIME STEP NUMBER 55950 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282785201E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.773986757E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.93048E-02 0.20951E+01 Friction velocity uk : 0.93048E-02 0.20951E+01 Dimensionless distance yplus : 0.90259E-02 0.20572E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -9.230193662e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29430E+08 1 0.17915E-09 0.24275E+02 0.19154E+04 c Velocity[X] 0.12609E+02 c Velocity[Y] 0.11667E+02 c Velocity[Z] 0.11380E-05 c Pressure 0.14378E-03 508 0.85359E-04 0.15014E-02 0.13196E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -22.366 34.88 5.6071 7.9981 v Velocity[Y] -24.87 26.086 -0.14413 -0.0016625 v Velocity[Z] -2.9916 3.0193 2.7134e-06 -5.3877e-08 v ǁVelocityǁ 0.00043162 34.978 7.5828 8.0725 v Pressure -2.5681e+05 1.1414e+05 -68453 -41720 v TurbVisc 1.3728e-20 0.013289 0.00016228 2.1409e-05 v CourantNb 1.0782e-08 0.011743 0.00016792 4.9275e-06 v FourierNb 1.2425e-07 0.046784 0.00014605 2.7887e-07 v total_pressure -1.5549e+05 2.1546e+05 32872 59605 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0572 0.099957 0.0028332 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2334e-07 0.052074 0.00031397 5.2064e-06 INSTANT 0.875753000E-01 TIME STEP NUMBER 55951 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282779416E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.773697263E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.29478E-02 0.20947E+01 Friction velocity uk : 0.29478E-02 0.20947E+01 Dimensionless distance yplus : 0.28869E-02 0.20568E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -9.521312216e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29430E+08 1 0.17913E-09 0.24263E+02 0.19148E+04 c Velocity[X] 0.12599E+02 c Velocity[Y] 0.11663E+02 c Velocity[Z] 0.11339E-05 c Pressure 0.14767E-03 33 0.99740E-04 0.15413E-02 0.18270E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -22.375 34.893 5.607 7.998 v Velocity[Y] -24.88 26.094 -0.14413 -0.0016708 v Velocity[Z] -2.9914 3.0195 2.7126e-06 -5.3877e-08 v ǁVelocityǁ 0.00043814 34.991 7.5843 8.0725 v Pressure -2.558e+05 1.1535e+05 -67375 -41042 v TurbVisc 2.1933e-20 0.013309 0.00016232 2.1446e-05 v CourantNb 2.6005e-08 0.011743 0.00016792 4.9275e-06 v FourierNb 1.2425e-07 0.046779 0.00014605 2.7912e-07 v total_pressure -1.5448e+05 2.1668e+05 33950 60283 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0568 0.099974 0.0028331 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2335e-07 0.052068 0.00031398 5.2066e-06 INSTANT 0.875754000E-01 TIME STEP NUMBER 55952 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282773594E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.773411844E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.73427E-02 0.20943E+01 Friction velocity uk : 0.73427E-02 0.20943E+01 Dimensionless distance yplus : 0.71909E-02 0.20564E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -9.753433761e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29429E+08 1 0.17912E-09 0.24241E+02 0.19139E+04 c Velocity[X] 0.12590E+02 c Velocity[Y] 0.11651E+02 c Velocity[Z] 0.11296E-05 c Pressure 0.15153E-03 794 0.84641E-04 0.15807E-02 0.14228E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -22.384 34.906 5.6069 7.9979 v Velocity[Y] -24.89 26.103 -0.14414 -0.0016811 v Velocity[Z] -2.9912 3.0197 2.7119e-06 -5.3877e-08 v ǁVelocityǁ 0.00044849 35.004 7.5858 8.0725 v Pressure -2.5475e+05 1.1663e+05 -66261 -40461 v TurbVisc 1.8988e-20 0.013328 0.00016237 2.1481e-05 v CourantNb 4.1904e-08 0.011743 0.00016792 4.9275e-06 v FourierNb 1.2425e-07 0.046774 0.00014606 2.7936e-07 v total_pressure -1.5343e+05 2.1795e+05 35064 60864 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0564 0.099995 0.002833 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2336e-07 0.052063 0.00031398 5.2069e-06 INSTANT 0.875755000E-01 TIME STEP NUMBER 55953 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282767967E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.773134229E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12520E-01 0.20938E+01 Friction velocity uk : 0.12520E-01 0.20938E+01 Dimensionless distance yplus : 0.12120E-01 0.20560E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -9.927011977e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29429E+08 1 0.17911E-09 0.24231E+02 0.19135E+04 c Velocity[X] 0.12583E+02 c Velocity[Y] 0.11648E+02 c Velocity[Z] 0.11315E-05 c Pressure 0.15290E-03 9 0.58687E-04 0.15942E-02 0.10896E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -22.393 34.919 5.6068 7.9977 v Velocity[Y] -24.901 26.111 -0.14414 -0.0016927 v Velocity[Z] -2.9911 3.0199 2.7111e-06 -5.3877e-08 v ǁVelocityǁ 0.00046068 35.017 7.5873 8.0725 v Pressure -2.5372e+05 1.1789e+05 -65145 -39988 v TurbVisc 1.6289e-20 0.013347 0.00016241 2.1517e-05 v CourantNb 5.8524e-08 0.011743 0.00016792 4.9275e-06 v FourierNb 1.2425e-07 0.046769 0.00014606 2.7961e-07 v total_pressure -1.524e+05 2.1921e+05 36180 61337 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.056 0.10002 0.002833 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2336e-07 0.052057 0.00031398 5.2071e-06 INSTANT 0.875756000E-01 TIME STEP NUMBER 55954 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282762526E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.772861746E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11795E-01 0.20934E+01 Friction velocity uk : 0.11795E-01 0.20934E+01 Dimensionless distance yplus : 0.11418E-01 0.20555E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.009632656e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29428E+08 1 0.17910E-09 0.24216E+02 0.19129E+04 c Velocity[X] 0.12572E+02 c Velocity[Y] 0.11644E+02 c Velocity[Z] 0.11278E-05 c Pressure 0.15709E-03 34 0.80586E-04 0.16370E-02 0.23588E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -22.402 34.932 5.6067 7.9976 v Velocity[Y] -24.911 26.119 -0.14414 -0.0017016 v Velocity[Z] -2.9909 3.0201 2.7104e-06 -5.3877e-08 v ǁVelocityǁ 0.0004812 35.03 7.5887 8.0725 v Pressure -2.5253e+05 1.1927e+05 -63920 -39039 v TurbVisc 1.2158e-20 0.013366 0.00016246 2.1554e-05 v CourantNb 7.5411e-08 0.011742 0.00016793 4.9275e-06 v FourierNb 1.2425e-07 0.046764 0.00014606 2.7986e-07 v total_pressure -1.512e+05 2.2059e+05 37405 62286 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0555 0.10004 0.0028329 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2337e-07 0.052051 0.00031399 5.2074e-06 INSTANT 0.875757000E-01 TIME STEP NUMBER 55955 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282757008E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.772596894E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12750E-01 0.20929E+01 Friction velocity uk : 0.12750E-01 0.20929E+01 Dimensionless distance yplus : 0.12367E-01 0.20551E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.011877800e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29428E+08 1 0.17909E-09 0.24204E+02 0.19124E+04 c Velocity[X] 0.12565E+02 c Velocity[Y] 0.11640E+02 c Velocity[Z] 0.11226E-05 c Pressure 0.16055E-03 414 0.86127E-04 0.16722E-02 0.15908E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -22.411 34.945 5.6066 7.9975 v Velocity[Y] -24.922 26.127 -0.14414 -0.0017133 v Velocity[Z] -2.9907 3.0203 2.7096e-06 -5.3877e-08 v ǁVelocityǁ 0.00050562 35.043 7.5902 8.0725 v Pressure -2.5139e+05 1.2063e+05 -62701 -38482 v TurbVisc 1.1991e-20 0.013385 0.0001625 2.1589e-05 v CourantNb 8.7055e-08 0.011742 0.00016793 4.9275e-06 v FourierNb 1.2425e-07 0.046758 0.00014607 2.801e-07 v total_pressure -1.5007e+05 2.2196e+05 38624 62843 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0551 0.10006 0.0028328 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2338e-07 0.052045 0.00031399 5.2076e-06 INSTANT 0.875758000E-01 TIME STEP NUMBER 55956 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282751763E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.772335797E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.38799E-02 0.20924E+01 Friction velocity uk : 0.38799E-02 0.20924E+01 Dimensionless distance yplus : 0.38047E-02 0.20546E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.025099994e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29427E+08 1 0.17908E-09 0.24185E+02 0.19116E+04 c Velocity[X] 0.12555E+02 c Velocity[Y] 0.11629E+02 c Velocity[Z] 0.11238E-05 c Pressure 0.16424E-03 72 0.75164E-04 0.17098E-02 0.17722E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -22.419 34.958 5.6065 7.9974 v Velocity[Y] -24.932 26.135 -0.14415 -0.0017235 v Velocity[Z] -2.9905 3.0205 2.7089e-06 -5.3877e-08 v ǁVelocityǁ 0.00053425 35.057 7.5917 8.0726 v Pressure -2.5018e+05 1.2202e+05 -61450 -37746 v TurbVisc 7.2118e-22 0.013404 0.00016254 2.1627e-05 v CourantNb 5.3001e-08 0.011742 0.00016793 4.9275e-06 v FourierNb 1.2425e-07 0.046752 0.00014607 2.8036e-07 v total_pressure -1.4886e+05 2.2335e+05 39875 63579 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0546 0.10008 0.0028327 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2339e-07 0.052039 0.000314 5.2079e-06 INSTANT 0.875759000E-01 TIME STEP NUMBER 55957 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282746552E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.772078928E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.73438E-02 0.20919E+01 Friction velocity uk : 0.73438E-02 0.20919E+01 Dimensionless distance yplus : 0.72016E-02 0.20541E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.028138751e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29427E+08 1 0.17907E-09 0.24174E+02 0.19112E+04 c Velocity[X] 0.12548E+02 c Velocity[Y] 0.11627E+02 c Velocity[Z] 0.11311E-05 c Pressure 0.16595E-03 9 0.55177E-04 0.17267E-02 0.14964E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -22.428 34.971 5.6064 7.9973 v Velocity[Y] -24.942 26.144 -0.14415 -0.0017331 v Velocity[Z] -2.9903 3.0207 2.7082e-06 -5.3877e-08 v ǁVelocityǁ 0.0005599 35.07 7.5932 8.0726 v Pressure -2.4898e+05 1.2343e+05 -60168 -37113 v TurbVisc 4.5687e-21 0.013423 0.00016259 2.1663e-05 v CourantNb 2.7259e-08 0.011742 0.00016793 4.9276e-06 v FourierNb 1.2425e-07 0.046746 0.00014607 2.8061e-07 v total_pressure -1.4765e+05 2.2475e+05 41157 64212 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0541 0.1001 0.0028327 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.234e-07 0.052032 0.000314 5.2082e-06 INSTANT 0.875760000E-01 TIME STEP NUMBER 55958 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282741483E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.771831521E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.64787E-02 0.20914E+01 Friction velocity uk : 0.64787E-02 0.20914E+01 Dimensionless distance yplus : 0.63295E-02 0.20536E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.030827548e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29426E+08 1 0.17906E-09 0.24158E+02 0.19105E+04 c Velocity[X] 0.12538E+02 c Velocity[Y] 0.11619E+02 c Velocity[Z] 0.11259E-05 c Pressure 0.16975E-03 135 0.96971E-04 0.17653E-02 0.19712E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -22.437 34.984 5.6063 7.9972 v Velocity[Y] -24.953 26.152 -0.14415 -0.0017432 v Velocity[Z] -2.9901 3.0209 2.7074e-06 -5.3877e-08 v ǁVelocityǁ 0.00059688 35.083 7.5947 8.0726 v Pressure -2.4766e+05 1.2491e+05 -58860 -36299 v TurbVisc 3.1361e-21 0.013443 0.00016263 2.1698e-05 v CourantNb 4.0778e-08 0.011741 0.00016793 4.9276e-06 v FourierNb 1.2425e-07 0.046741 0.00014607 2.8085e-07 v total_pressure -1.4634e+05 2.2624e+05 42465 65026 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0536 0.10013 0.0028326 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2341e-07 0.052026 0.000314 5.2084e-06 INSTANT 0.875761000E-01 TIME STEP NUMBER 55959 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282736529E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.771591876E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.42462E-02 0.20909E+01 Friction velocity uk : 0.42462E-02 0.20909E+01 Dimensionless distance yplus : 0.41484E-02 0.20531E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.022676674e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29426E+08 1 0.17905E-09 0.24144E+02 0.19099E+04 c Velocity[X] 0.12530E+02 c Velocity[Y] 0.11614E+02 c Velocity[Z] 0.11169E-05 c Pressure 0.17251E-03 22 0.80408E-04 0.17930E-02 0.17596E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -22.446 34.997 5.6062 7.9971 v Velocity[Y] -24.963 26.16 -0.14415 -0.001754 v Velocity[Z] -2.9899 3.0211 2.7067e-06 -5.3877e-08 v ǁVelocityǁ 0.0006 35.096 7.5961 8.0726 v Pressure -2.4638e+05 1.264e+05 -57489 -35564 v TurbVisc 1.0308e-20 0.013462 0.00016267 2.1735e-05 v CourantNb 8.4015e-08 0.011741 0.00016793 4.9276e-06 v FourierNb 1.2425e-07 0.046734 0.00014608 2.811e-07 v total_pressure -1.4506e+05 2.2773e+05 43836 65761 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0531 0.10015 0.0028326 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2342e-07 0.052019 0.00031401 5.2087e-06 INSTANT 0.875762000E-01 TIME STEP NUMBER 55960 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282731695E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.771360728E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.97139E-02 0.20904E+01 Friction velocity uk : 0.97139E-02 0.20904E+01 Dimensionless distance yplus : 0.94903E-02 0.20526E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.021496978e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29426E+08 1 0.17904E-09 0.24134E+02 0.19095E+04 c Velocity[X] 0.12523E+02 c Velocity[Y] 0.11612E+02 c Velocity[Z] 0.11264E-05 c Pressure 0.17508E-03 9 0.52363E-04 0.18189E-02 0.17211E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -22.455 35.01 5.6061 7.997 v Velocity[Y] -24.973 26.168 -0.14415 -0.0017661 v Velocity[Z] -2.9897 3.0212 2.7059e-06 -5.3877e-08 v ǁVelocityǁ 0.00059877 35.11 7.5976 8.0727 v Pressure -2.4506e+05 1.2793e+05 -56085 -34856 v TurbVisc 2.5186e-21 0.013481 0.00016272 2.1771e-05 v CourantNb 1.0299e-07 0.011741 0.00016793 4.9276e-06 v FourierNb 1.2425e-07 0.046728 0.00014608 2.8135e-07 v total_pressure -1.4374e+05 2.2925e+05 45240 66469 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0526 0.10017 0.0028325 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2343e-07 0.052012 0.00031401 5.2089e-06 INSTANT 0.875763000E-01 TIME STEP NUMBER 55961 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282727058E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.771133956E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.78706E-02 0.20899E+01 Friction velocity uk : 0.78706E-02 0.20899E+01 Dimensionless distance yplus : 0.76468E-02 0.20521E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.008721217e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29425E+08 1 0.17903E-09 0.24118E+02 0.19088E+04 c Velocity[X] 0.12513E+02 c Velocity[Y] 0.11605E+02 c Velocity[Z] 0.11232E-05 c Pressure 0.17873E-03 203 0.96145E-04 0.18558E-02 0.23197E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -22.463 35.023 5.606 7.9969 v Velocity[Y] -24.983 26.176 -0.14415 -0.0017769 v Velocity[Z] -2.9895 3.0214 2.7052e-06 -5.3877e-08 v ǁVelocityǁ 0.00058641 35.123 7.5991 8.0727 v Pressure -2.4363e+05 1.295e+05 -54690 -33940 v TurbVisc 3.345e-21 0.0135 0.00016276 2.1808e-05 v CourantNb 9.9368e-08 0.011741 0.00016793 4.9276e-06 v FourierNb 1.2425e-07 0.046722 0.00014608 2.816e-07 v total_pressure -1.423e+05 2.3082e+05 46635 67385 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0521 0.1002 0.0028325 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2344e-07 0.052006 0.00031402 5.2092e-06 INSTANT 0.875764000E-01 TIME STEP NUMBER 55962 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282722467E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.770914195E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.42975E-02 0.20894E+01 Friction velocity uk : 0.42975E-02 0.20894E+01 Dimensionless distance yplus : 0.41753E-02 0.20516E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -9.974353943e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29425E+08 1 0.17902E-09 0.24105E+02 0.19082E+04 c Velocity[X] 0.12505E+02 c Velocity[Y] 0.11600E+02 c Velocity[Z] 0.11135E-05 c Pressure 0.18133E-03 236 0.81696E-04 0.18818E-02 0.21157E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -22.472 35.037 5.6059 7.9968 v Velocity[Y] -24.993 26.184 -0.14415 -0.0017876 v Velocity[Z] -2.9893 3.0216 2.7044e-06 -5.3877e-08 v ǁVelocityǁ 0.00058302 35.136 7.6006 8.0727 v Pressure -2.4222e+05 1.3107e+05 -53204 -33087 v TurbVisc 6.5355e-21 0.013519 0.00016281 2.1845e-05 v CourantNb 9.5922e-08 0.01174 0.00016793 4.9276e-06 v FourierNb 1.2425e-07 0.046716 0.00014609 2.8186e-07 v total_pressure -1.4089e+05 2.324e+05 48121 68238 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0516 0.10022 0.0028324 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2345e-07 0.051999 0.00031402 5.2095e-06 INSTANT 0.875765000E-01 TIME STEP NUMBER 55963 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282718027E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.770704834E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.37469E-02 0.20888E+01 Friction velocity uk : 0.37469E-02 0.20888E+01 Dimensionless distance yplus : 0.36404E-02 0.20510E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -9.835068305e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29424E+08 1 0.17901E-09 0.24096E+02 0.19079E+04 c Velocity[X] 0.12498E+02 c Velocity[Y] 0.11598E+02 c Velocity[Z] 0.11138E-05 c Pressure 0.18376E-03 10 0.55484E-04 0.19061E-02 0.19483E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -22.481 35.05 5.6058 7.9967 v Velocity[Y] -25.003 26.193 -0.14414 -0.0017978 v Velocity[Z] -2.9892 3.0218 2.7037e-06 -5.3877e-08 v ǁVelocityǁ 0.00057404 35.15 7.6021 8.0728 v Pressure -2.4078e+05 1.3266e+05 -51722 -32327 v TurbVisc 2.394e-20 0.013538 0.00016285 2.1882e-05 v CourantNb 9.2419e-08 0.01174 0.00016793 4.9277e-06 v FourierNb 1.2425e-07 0.04671 0.00014609 2.8211e-07 v total_pressure -1.3946e+05 2.3399e+05 49603 68998 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.051 0.10024 0.0028323 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2346e-07 0.051992 0.00031402 5.2098e-06 INSTANT 0.875766000E-01 TIME STEP NUMBER 55964 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282713716E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.770498954E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.26226E-02 0.20883E+01 Friction velocity uk : 0.26226E-02 0.20883E+01 Dimensionless distance yplus : 0.25301E-02 0.20505E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -9.704936382e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29424E+08 1 0.17900E-09 0.24083E+02 0.19073E+04 c Velocity[X] 0.12490E+02 c Velocity[Y] 0.11593E+02 c Velocity[Z] 0.11124E-05 c Pressure 0.18716E-03 88 0.75185E-04 0.19404E-02 0.24319E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -22.489 35.063 5.6057 7.9966 v Velocity[Y] -25.013 26.201 -0.14414 -0.0018096 v Velocity[Z] -2.989 3.022 2.703e-06 -5.3877e-08 v ǁVelocityǁ 0.00057173 35.163 7.6035 8.0728 v Pressure -2.3925e+05 1.3431e+05 -50247 -31475 v TurbVisc 7.7173e-21 0.013558 0.00016289 2.1918e-05 v CourantNb 8.8824e-08 0.01174 0.00016794 4.9277e-06 v FourierNb 1.2425e-07 0.046704 0.00014609 2.8235e-07 v total_pressure -1.3792e+05 2.3564e+05 51078 69850 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0505 0.10027 0.0028323 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2347e-07 0.051985 0.00031403 5.21e-06 INSTANT 0.875767000E-01 TIME STEP NUMBER 55965 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282709548E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.770303642E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.54083E-02 0.20878E+01 Friction velocity uk : 0.54083E-02 0.20878E+01 Dimensionless distance yplus : 0.52626E-02 0.20500E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -9.466613382e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29424E+08 1 0.17899E-09 0.24073E+02 0.19069E+04 c Velocity[X] 0.12482E+02 c Velocity[Y] 0.11591E+02 c Velocity[Z] 0.11119E-05 c Pressure 0.18990E-03 61 0.79910E-04 0.19678E-02 0.25345E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -22.498 35.076 5.6056 7.9966 v Velocity[Y] -25.023 26.209 -0.14414 -0.0018198 v Velocity[Z] -2.9888 3.0222 2.7022e-06 -5.3877e-08 v ǁVelocityǁ 0.00058352 35.176 7.605 8.0728 v Pressure -2.3774e+05 1.3595e+05 -48686 -30583 v TurbVisc 1.8331e-21 0.013577 0.00016294 2.1955e-05 v CourantNb 8.5797e-08 0.01174 0.00016794 4.9277e-06 v FourierNb 1.2425e-07 0.046697 0.0001461 2.8261e-07 v total_pressure -1.3641e+05 2.3728e+05 52639 70742 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.05 0.1003 0.0028324 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2348e-07 0.051978 0.00031403 5.2103e-06 INSTANT 0.875768000E-01 TIME STEP NUMBER 55966 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282705423E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.770114481E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.39309E-02 0.20872E+01 Friction velocity uk : 0.39309E-02 0.20872E+01 Dimensionless distance yplus : 0.37844E-02 0.20495E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -9.297176113e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29423E+08 1 0.17899E-09 0.24063E+02 0.19065E+04 c Velocity[X] 0.12476E+02 c Velocity[Y] 0.11587E+02 c Velocity[Z] 0.11113E-05 c Pressure 0.19275E-03 263 0.92609E-04 0.19963E-02 0.24876E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -22.507 35.09 5.6055 7.9965 v Velocity[Y] -25.033 26.217 -0.14414 -0.0018322 v Velocity[Z] -2.9886 3.0224 2.7015e-06 -5.3877e-08 v ǁVelocityǁ 0.00058592 35.19 7.6065 8.0729 v Pressure -2.3616e+05 1.3764e+05 -47126 -29735 v TurbVisc 1.5182e-21 0.013596 0.00016298 2.1991e-05 v CourantNb 8.2487e-08 0.011739 0.00016794 4.9277e-06 v FourierNb 1.2425e-07 0.046691 0.0001461 2.8285e-07 v total_pressure -1.3483e+05 2.3897e+05 54199 71590 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0495 0.10033 0.0028326 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2349e-07 0.051971 0.00031404 5.2106e-06 INSTANT 0.875769000E-01 TIME STEP NUMBER 55967 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282701665E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.769933124E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.47050E-02 0.20867E+01 Friction velocity uk : 0.47050E-02 0.20867E+01 Dimensionless distance yplus : 0.45297E-02 0.20490E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -9.065125721e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29423E+08 1 0.17898E-09 0.24046E+02 0.19057E+04 c Velocity[X] 0.12468E+02 c Velocity[Y] 0.11578E+02 c Velocity[Z] 0.11088E-05 c Pressure 0.19553E-03 81 0.78556E-04 0.20240E-02 0.25762E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -22.515 35.103 5.6054 7.9964 v Velocity[Y] -25.043 26.225 -0.14414 -0.0018433 v Velocity[Z] -2.9884 3.0226 2.7007e-06 -5.3877e-08 v ǁVelocityǁ 0.00061699 35.203 7.608 8.0729 v Pressure -2.3456e+05 1.3933e+05 -45537 -28822 v TurbVisc 5.2329e-21 0.013615 0.00016303 2.2029e-05 v CourantNb 7.9315e-08 0.011739 0.00016794 4.9277e-06 v FourierNb 1.2425e-07 0.046685 0.0001461 2.8311e-07 v total_pressure -1.3324e+05 2.4066e+05 55788 72503 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.049 0.10037 0.0028328 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.235e-07 0.051965 0.00031404 5.2108e-06 INSTANT 0.875770000E-01 TIME STEP NUMBER 55968 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282697903E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.769761274E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.81801E-02 0.20862E+01 Friction velocity uk : 0.81801E-02 0.20862E+01 Dimensionless distance yplus : 0.78753E-02 0.20485E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -8.828531241e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29423E+08 1 0.17897E-09 0.24039E+02 0.19054E+04 c Velocity[X] 0.12462E+02 c Velocity[Y] 0.11577E+02 c Velocity[Z] 0.11074E-05 c Pressure 0.19651E-03 10 0.56816E-04 0.20331E-02 0.22542E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -22.524 35.116 5.6053 7.9963 v Velocity[Y] -25.053 26.233 -0.14413 -0.0018538 v Velocity[Z] -2.9882 3.0228 2.7e-06 -5.3877e-08 v ǁVelocityǁ 0.00068508 35.217 7.6094 8.073 v Pressure -2.3297e+05 1.4101e+05 -43939 -28010 v TurbVisc 1.3344e-21 0.013634 0.00016307 2.2066e-05 v CourantNb 7.6244e-08 0.011739 0.00016794 4.9278e-06 v FourierNb 1.2425e-07 0.046679 0.00014611 2.8336e-07 v total_pressure -1.3164e+05 2.4234e+05 57386 73315 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0485 0.1004 0.002833 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2352e-07 0.051958 0.00031404 5.2111e-06 INSTANT 0.875771000E-01 TIME STEP NUMBER 55969 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282694342E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.769598041E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.66439E-02 0.20857E+01 Friction velocity uk : 0.66439E-02 0.20857E+01 Dimensionless distance yplus : 0.64499E-02 0.20479E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -8.465356177e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29422E+08 1 0.17896E-09 0.24025E+02 0.19048E+04 c Velocity[X] 0.12455E+02 c Velocity[Y] 0.11570E+02 c Velocity[Z] 0.11055E-05 c Pressure 0.19932E-03 119 0.99598E-04 0.20612E-02 0.28561E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -22.532 35.13 5.6052 7.9962 v Velocity[Y] -25.063 26.241 -0.14413 -0.0018648 v Velocity[Z] -2.988 3.023 2.6993e-06 -5.3877e-08 v ǁVelocityǁ 0.00076389 35.23 7.6109 8.073 v Pressure -2.3124e+05 1.4278e+05 -42317 -27026 v TurbVisc 2.7747e-21 0.013653 0.00016311 2.2102e-05 v CourantNb 7.2984e-08 0.011739 0.00016794 4.9278e-06 v FourierNb 1.2425e-07 0.046673 0.00014611 2.8361e-07 v total_pressure -1.2991e+05 2.441e+05 59008 74299 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0479 0.10043 0.0028332 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2353e-07 0.051951 0.00031405 5.2114e-06 INSTANT 0.875772000E-01 TIME STEP NUMBER 55970 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282690885E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.769445739E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.29523E-02 0.20852E+01 Friction velocity uk : 0.29523E-02 0.20852E+01 Dimensionless distance yplus : 0.29037E-02 0.20475E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -8.270535540e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29422E+08 1 0.17896E-09 0.24015E+02 0.19044E+04 c Velocity[X] 0.12449E+02 c Velocity[Y] 0.11566E+02 c Velocity[Z] 0.11024E-05 c Pressure 0.20130E-03 35 0.82664E-04 0.20805E-02 0.26059E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -22.541 35.143 5.6052 7.9962 v Velocity[Y] -25.073 26.249 -0.14413 -0.0018765 v Velocity[Z] -2.9878 3.0232 2.6985e-06 -5.3877e-08 v ǁVelocityǁ 0.00086245 35.244 7.6124 8.0731 v Pressure -2.2957e+05 1.4453e+05 -40638 -26118 v TurbVisc 1.6506e-21 0.013672 0.00016316 2.2138e-05 v CourantNb 4.0568e-08 0.011738 0.00016794 4.9278e-06 v FourierNb 1.2425e-07 0.046667 0.00014611 2.8386e-07 v total_pressure -1.2824e+05 2.4585e+05 60687 75207 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0475 0.10045 0.0028333 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2354e-07 0.051945 0.00031405 5.2117e-06 INSTANT 0.875773000E-01 TIME STEP NUMBER 55971 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282687586E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.769297870E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.46224E-02 0.20847E+01 Friction velocity uk : 0.46224E-02 0.20847E+01 Dimensionless distance yplus : 0.44486E-02 0.20470E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -7.956107610e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29422E+08 1 0.17895E-09 0.24010E+02 0.19041E+04 c Velocity[X] 0.12444E+02 c Velocity[Y] 0.11565E+02 c Velocity[Z] 0.11029E-05 c Pressure 0.20296E-03 10 0.55103E-04 0.20966E-02 0.25798E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -22.549 35.156 5.6051 7.9961 v Velocity[Y] -25.083 26.258 -0.14413 -0.0018896 v Velocity[Z] -2.9876 3.0234 2.6978e-06 -5.3877e-08 v ǁVelocityǁ 0.00097451 35.258 7.6139 8.0732 v Pressure -2.2787e+05 1.463e+05 -38940 -25231 v TurbVisc 1.1095e-21 0.013691 0.0001632 2.2175e-05 v CourantNb 4.9177e-08 0.011738 0.00016794 4.9278e-06 v FourierNb 1.2425e-07 0.046661 0.00014612 2.8411e-07 v total_pressure -1.2655e+05 2.4762e+05 62385 76094 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.047 0.10049 0.0028336 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2356e-07 0.051938 0.00031406 5.212e-06 INSTANT 0.875774000E-01 TIME STEP NUMBER 55972 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282684525E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.769156690E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10503E-01 0.20842E+01 Friction velocity uk : 0.10503E-01 0.20842E+01 Dimensionless distance yplus : 0.10108E-01 0.20465E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -7.498710786e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29421E+08 1 0.17895E-09 0.23997E+02 0.19036E+04 c Velocity[X] 0.12438E+02 c Velocity[Y] 0.11559E+02 c Velocity[Z] 0.11074E-05 c Pressure 0.20553E-03 31 0.99392E-04 0.21221E-02 0.31821E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -22.558 35.17 5.605 7.996 v Velocity[Y] -25.093 26.266 -0.14413 -0.0019014 v Velocity[Z] -2.9874 3.0236 2.697e-06 -5.3877e-08 v ǁVelocityǁ 0.0010735 35.271 7.6154 8.0732 v Pressure -2.2606e+05 1.4811e+05 -37259 -24194 v TurbVisc 2.7015e-21 0.013711 0.00016325 2.2213e-05 v CourantNb 6.4684e-08 0.011738 0.00016794 4.9279e-06 v FourierNb 1.2425e-07 0.046655 0.00014612 2.8437e-07 v total_pressure -1.2474e+05 2.4943e+05 64066 77131 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0465 0.10052 0.0028338 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2357e-07 0.051932 0.00031406 5.2122e-06 INSTANT 0.875775000E-01 TIME STEP NUMBER 55973 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282681502E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.769026669E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.75847E-02 0.20838E+01 Friction velocity uk : 0.75847E-02 0.20838E+01 Dimensionless distance yplus : 0.72994E-02 0.20461E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -7.294954671e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29421E+08 1 0.17894E-09 0.23988E+02 0.19032E+04 c Velocity[X] 0.12433E+02 c Velocity[Y] 0.11556E+02 c Velocity[Z] 0.11035E-05 c Pressure 0.20722E-03 79 0.84605E-04 0.21385E-02 0.31463E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -22.566 35.183 5.6049 7.996 v Velocity[Y] -25.103 26.274 -0.14413 -0.001913 v Velocity[Z] -2.9872 3.0238 2.6963e-06 -5.3877e-08 v ǁVelocityǁ 0.0011866 35.285 7.6169 8.0733 v Pressure -2.2429e+05 1.4991e+05 -35509 -23147 v TurbVisc 2.6874e-21 0.01373 0.00016329 2.225e-05 v CourantNb 6.2811e-08 0.011738 0.00016794 4.9279e-06 v FourierNb 1.2425e-07 0.046649 0.00014612 2.8463e-07 v total_pressure -1.2296e+05 2.5124e+05 65816 78178 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0461 0.10055 0.002834 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2359e-07 0.051926 0.00031406 5.2125e-06 INSTANT 0.875776000E-01 TIME STEP NUMBER 55974 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282678680E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.768903483E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.96438E-02 0.20834E+01 Friction velocity uk : 0.96438E-02 0.20834E+01 Dimensionless distance yplus : 0.92811E-02 0.20457E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -6.952493201e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29421E+08 1 0.17894E-09 0.23985E+02 0.19030E+04 c Velocity[X] 0.12429E+02 c Velocity[Y] 0.11556E+02 c Velocity[Z] 0.10987E-05 c Pressure 0.20859E-03 10 0.58178E-04 0.21515E-02 0.28254E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -22.575 35.197 5.6049 7.9959 v Velocity[Y] -25.112 26.282 -0.14413 -0.0019241 v Velocity[Z] -2.987 3.024 2.6956e-06 -5.3877e-08 v ǁVelocityǁ 0.0012592 35.299 7.6183 8.0733 v Pressure -2.2252e+05 1.517e+05 -33754 -22240 v TurbVisc 2.3229e-21 0.013749 0.00016334 2.2287e-05 v CourantNb 6.0269e-08 0.011737 0.00016795 4.9279e-06 v FourierNb 1.2425e-07 0.046644 0.00014612 2.8488e-07 v total_pressure -1.2119e+05 2.5303e+05 67571 79085 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0457 0.10057 0.0028342 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.236e-07 0.05192 0.00031407 5.2128e-06 INSTANT 0.875777000E-01 TIME STEP NUMBER 55975 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282676000E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.768788241E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12657E-01 0.20830E+01 Friction velocity uk : 0.12657E-01 0.20830E+01 Dimensionless distance yplus : 0.12182E-01 0.20453E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -6.314001007e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29421E+08 1 0.17893E-09 0.23976E+02 0.19027E+04 c Velocity[X] 0.12424E+02 c Velocity[Y] 0.11553E+02 c Velocity[Z] 0.11003E-05 c Pressure 0.21086E-03 155 0.77571E-04 0.21738E-02 0.33843E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -22.583 35.21 5.6048 7.9959 v Velocity[Y] -25.122 26.291 -0.14413 -0.001937 v Velocity[Z] -2.9868 3.0242 2.6948e-06 -5.3878e-08 v ǁVelocityǁ 0.0013015 35.312 7.6198 8.0734 v Pressure -2.2064e+05 1.5356e+05 -32029 -21261 v TurbVisc 2.4444e-21 0.013768 0.00016338 2.2324e-05 v CourantNb 5.7763e-08 0.011737 0.00016795 4.928e-06 v FourierNb 1.2425e-07 0.046639 0.00014613 2.8513e-07 v total_pressure -1.1931e+05 2.5489e+05 69296 80064 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0453 0.10059 0.0028344 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2362e-07 0.051914 0.00031407 5.2131e-06 INSTANT 0.875778000E-01 TIME STEP NUMBER 55976 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282673468E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.768685057E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.85688E-02 0.20826E+01 Friction velocity uk : 0.85688E-02 0.20826E+01 Dimensionless distance yplus : 0.82468E-02 0.20450E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -6.114692212e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29421E+08 1 0.17893E-09 0.23971E+02 0.19024E+04 c Velocity[X] 0.12420E+02 c Velocity[Y] 0.11552E+02 c Velocity[Z] 0.10976E-05 c Pressure 0.21255E-03 67 0.82721E-04 0.21901E-02 0.36527E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -22.592 35.224 5.6047 7.9958 v Velocity[Y] -25.132 26.299 -0.14412 -0.0019479 v Velocity[Z] -2.9866 3.0244 2.6941e-06 -5.3878e-08 v ǁVelocityǁ 0.0013195 35.326 7.6213 8.0735 v Pressure -2.1881e+05 1.5539e+05 -30219 -20188 v TurbVisc 2.522e-21 0.013787 0.00016343 2.2361e-05 v CourantNb 5.6198e-08 0.011737 0.00016795 4.928e-06 v FourierNb 1.2425e-07 0.046634 0.00014613 2.8539e-07 v total_pressure -1.1748e+05 2.5672e+05 71106 81137 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.045 0.10061 0.0028345 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2363e-07 0.051909 0.00031408 5.2134e-06 INSTANT 0.875779000E-01 TIME STEP NUMBER 55977 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282671035E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.768586859E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.23065E-02 0.20823E+01 Friction velocity uk : 0.23065E-02 0.20823E+01 Dimensionless distance yplus : 0.22198E-02 0.20446E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -5.651587353e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29420E+08 1 0.17892E-09 0.23967E+02 0.19022E+04 c Velocity[X] 0.12417E+02 c Velocity[Y] 0.11550E+02 c Velocity[Z] 0.10935E-05 c Pressure 0.21427E-03 236 0.95739E-04 0.22067E-02 0.32263E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -22.6 35.237 5.6047 7.9958 v Velocity[Y] -25.141 26.307 -0.14413 -0.0019616 v Velocity[Z] -2.9864 3.0245 2.6933e-06 -5.3878e-08 v ǁVelocityǁ 0.0013338 35.34 7.6228 8.0736 v Pressure -2.1695e+05 1.5725e+05 -28450 -19309 v TurbVisc 2.6857e-21 0.013806 0.00016347 2.2398e-05 v CourantNb 5.4216e-08 0.011736 0.00016795 4.928e-06 v FourierNb 1.2425e-07 0.046629 0.00014613 2.8564e-07 v total_pressure -1.1563e+05 2.5857e+05 72875 82016 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0446 0.10063 0.0028346 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2365e-07 0.051904 0.00031408 5.2137e-06 INSTANT 0.875780000E-01 TIME STEP NUMBER 55978 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282668939E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.768497806E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.48678E-02 0.20820E+01 Friction velocity uk : 0.48678E-02 0.20820E+01 Dimensionless distance yplus : 0.46847E-02 0.20443E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -5.201105955e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29420E+08 1 0.17892E-09 0.23954E+02 0.19016E+04 c Velocity[X] 0.12413E+02 c Velocity[Y] 0.11541E+02 c Velocity[Z] 0.10925E-05 c Pressure 0.21587E-03 120 0.81699E-04 0.22220E-02 0.37710E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -22.609 35.251 5.6046 7.9957 v Velocity[Y] -25.151 26.316 -0.14413 -0.0019738 v Velocity[Z] -2.9862 3.0247 2.6926e-06 -5.3878e-08 v ǁVelocityǁ 0.0013452 35.353 7.6243 8.0737 v Pressure -2.1505e+05 1.5911e+05 -26631 -18207 v TurbVisc 4.8494e-21 0.013825 0.00016352 2.2436e-05 v CourantNb 5.2487e-08 0.011736 0.00016795 4.9281e-06 v FourierNb 1.2425e-07 0.046624 0.00014613 2.859e-07 v total_pressure -1.1373e+05 2.6044e+05 74694 83118 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0443 0.10065 0.0028347 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2367e-07 0.051899 0.00031408 5.214e-06 INSTANT 0.875781000E-01 TIME STEP NUMBER 55979 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282666891E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.768419793E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.46247E-02 0.20817E+01 Friction velocity uk : 0.46247E-02 0.20817E+01 Dimensionless distance yplus : 0.44508E-02 0.20440E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -4.729449966e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29420E+08 1 0.17892E-09 0.23953E+02 0.19016E+04 c Velocity[X] 0.12411E+02 c Velocity[Y] 0.11542E+02 c Velocity[Z] 0.10936E-05 c Pressure 0.21571E-03 10 0.59818E-04 0.22192E-02 0.31110E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -22.617 35.264 5.6046 7.9957 v Velocity[Y] -25.161 26.324 -0.14413 -0.0019853 v Velocity[Z] -2.986 3.0249 2.6919e-06 -5.3878e-08 v ǁVelocityǁ 0.0013323 35.367 7.6258 8.0737 v Pressure -2.132e+05 1.6094e+05 -24827 -17292 v TurbVisc 3.3543e-21 0.013844 0.00016356 2.2473e-05 v CourantNb 5.0926e-08 0.011736 0.00016795 4.9281e-06 v FourierNb 1.2425e-07 0.046619 0.00014614 2.8615e-07 v total_pressure -1.1187e+05 2.6227e+05 76498 84033 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.044 0.10066 0.0028348 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2368e-07 0.051894 0.00031409 5.2143e-06 INSTANT 0.875782000E-01 TIME STEP NUMBER 55980 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282665064E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.768351360E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.58407E-02 0.20814E+01 Friction velocity uk : 0.58407E-02 0.20814E+01 Dimensionless distance yplus : 0.56210E-02 0.20437E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -4.126290857e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29420E+08 1 0.17891E-09 0.23948E+02 0.19013E+04 c Velocity[X] 0.12408E+02 c Velocity[Y] 0.11540E+02 c Velocity[Z] 0.10950E-05 c Pressure 0.21732E-03 147 0.77503E-04 0.22347E-02 0.40727E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -22.626 35.278 5.6046 7.9957 v Velocity[Y] -25.17 26.333 -0.14413 -0.0019987 v Velocity[Z] -2.9859 3.0251 2.6911e-06 -5.3878e-08 v ǁVelocityǁ 0.0013148 35.381 7.6273 8.0738 v Pressure -2.1121e+05 1.6288e+05 -22999 -16207 v TurbVisc 3.8431e-21 0.013864 0.00016361 2.251e-05 v CourantNb 4.9181e-08 0.011735 0.00016795 4.9282e-06 v FourierNb 1.2425e-07 0.046615 0.00014614 2.864e-07 v total_pressure -1.0989e+05 2.642e+05 78326 85118 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0437 0.10068 0.0028349 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.237e-07 0.051889 0.00031409 5.2146e-06 INSTANT 0.875783000E-01 TIME STEP NUMBER 55981 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282663344E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.768294335E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.68580E-02 0.20812E+01 Friction velocity uk : 0.68580E-02 0.20812E+01 Dimensionless distance yplus : 0.66001E-02 0.20435E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -3.757773683e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29420E+08 1 0.17891E-09 0.23946E+02 0.19012E+04 c Velocity[X] 0.12406E+02 c Velocity[Y] 0.11540E+02 c Velocity[Z] 0.10933E-05 c Pressure 0.21849E-03 61 0.83450E-04 0.22456E-02 0.42074E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -22.634 35.292 5.6045 7.9956 v Velocity[Y] -25.18 26.341 -0.14413 -0.0020101 v Velocity[Z] -2.9857 3.0253 2.6904e-06 -5.3878e-08 v ǁVelocityǁ 0.0012983 35.395 7.6288 8.0739 v Pressure -2.093e+05 1.6476e+05 -21115 -15075 v TurbVisc 4.2208e-21 0.013883 0.00016365 2.2548e-05 v CourantNb 4.8478e-08 0.011735 0.00016795 4.9282e-06 v FourierNb 1.2425e-07 0.04661 0.00014614 2.8666e-07 v total_pressure -1.0798e+05 2.6609e+05 80210 86250 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0435 0.10069 0.0028349 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2372e-07 0.051885 0.00031409 5.2149e-06 INSTANT 0.875784000E-01 TIME STEP NUMBER 55982 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282661732E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.768239656E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.94295E-02 0.20810E+01 Friction velocity uk : 0.94295E-02 0.20810E+01 Dimensionless distance yplus : 0.90748E-02 0.20433E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -3.235375690e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29420E+08 1 0.17891E-09 0.23944E+02 0.19011E+04 c Velocity[X] 0.12405E+02 c Velocity[Y] 0.11539E+02 c Velocity[Z] 0.10912E-05 c Pressure 0.21967E-03 236 0.96315E-04 0.22565E-02 0.36394E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -22.642 35.305 5.6045 7.9956 v Velocity[Y] -25.19 26.35 -0.14414 -0.0020243 v Velocity[Z] -2.9855 3.0255 2.6897e-06 -5.3878e-08 v ǁVelocityǁ 0.0012859 35.408 7.6303 8.074 v Pressure -2.0738e+05 1.6666e+05 -19286 -14168 v TurbVisc 4.4459e-21 0.013902 0.0001637 2.2584e-05 v CourantNb 4.7372e-08 0.011735 0.00016796 4.9282e-06 v FourierNb 1.2425e-07 0.046606 0.00014614 2.8691e-07 v total_pressure -1.0605e+05 2.6798e+05 82039 87157 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0433 0.1007 0.002835 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2374e-07 0.051881 0.0003141 5.2152e-06 INSTANT 0.875785000E-01 TIME STEP NUMBER 55983 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282660456E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.768193096E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10744E-01 0.20808E+01 Friction velocity uk : 0.10744E-01 0.20808E+01 Dimensionless distance yplus : 0.10340E-01 0.20431E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -2.695401003e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29419E+08 1 0.17890E-09 0.23935E+02 0.19006E+04 c Velocity[X] 0.12404E+02 c Velocity[Y] 0.11531E+02 c Velocity[Z] 0.10909E-05 c Pressure 0.22069E-03 132 0.82125E-04 0.22658E-02 0.42499E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -22.651 35.319 5.6045 7.9956 v Velocity[Y] -25.199 26.359 -0.14414 -0.002037 v Velocity[Z] -2.9853 3.0257 2.6889e-06 -5.3878e-08 v ǁVelocityǁ 0.001278 35.422 7.6319 8.0741 v Pressure -2.0541e+05 1.6856e+05 -17409 -13027 v TurbVisc 9.9226e-21 0.013921 0.00016375 2.2623e-05 v CourantNb 4.6529e-08 0.011734 0.00016796 4.9283e-06 v FourierNb 1.2425e-07 0.046602 0.00014614 2.8718e-07 v total_pressure -1.0409e+05 2.6988e+05 83916 88298 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0431 0.1007 0.002835 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2376e-07 0.051877 0.0003141 5.2155e-06 INSTANT 0.875786000E-01 TIME STEP NUMBER 55984 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282659235E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.768159032E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10702E-01 0.20806E+01 Friction velocity uk : 0.10702E-01 0.20806E+01 Dimensionless distance yplus : 0.10300E-01 0.20430E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -2.147072695e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29419E+08 1 0.17890E-09 0.23937E+02 0.19007E+04 c Velocity[X] 0.12404E+02 c Velocity[Y] 0.11533E+02 c Velocity[Z] 0.10943E-05 c Pressure 0.21996E-03 10 0.60567E-04 0.22571E-02 0.34921E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -22.659 35.332 5.6045 7.9955 v Velocity[Y] -25.209 26.367 -0.14414 -0.002049 v Velocity[Z] -2.9851 3.0259 2.6882e-06 -5.3878e-08 v ǁVelocityǁ 0.0012781 35.436 7.6334 8.0742 v Pressure -2.0351e+05 1.7049e+05 -15551 -12080 v TurbVisc 5.8605e-21 0.01394 0.00016379 2.266e-05 v CourantNb 4.5884e-08 0.011734 0.00016796 4.9283e-06 v FourierNb 1.2425e-07 0.046599 0.00014615 2.8743e-07 v total_pressure -1.0218e+05 2.7181e+05 85774 89245 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.043 0.10071 0.0028351 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2378e-07 0.051873 0.00031411 5.2158e-06 INSTANT 0.875787000E-01 TIME STEP NUMBER 55985 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282658245E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.768135687E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10139E-01 0.20804E+01 Friction velocity uk : 0.10139E-01 0.20804E+01 Dimensionless distance yplus : 0.97580E-02 0.20428E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.474666873e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29419E+08 1 0.17890E-09 0.23935E+02 0.19005E+04 c Velocity[X] 0.12404E+02 c Velocity[Y] 0.11531E+02 c Velocity[Z] 0.10954E-05 c Pressure 0.22101E-03 191 0.77876E-04 0.22668E-02 0.44895E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -22.668 35.346 5.6045 7.9955 v Velocity[Y] -25.219 26.376 -0.14415 -0.002063 v Velocity[Z] -2.9849 3.0261 2.6874e-06 -5.3878e-08 v ǁVelocityǁ 0.0012768 35.45 7.6349 8.0743 v Pressure -2.0158e+05 1.7255e+05 -13682 -10975 v TurbVisc 4.7789e-21 0.013959 0.00016384 2.2697e-05 v CourantNb 4.4988e-08 0.011734 0.00016796 4.9284e-06 v FourierNb 1.2425e-07 0.046595 0.00014615 2.8768e-07 v total_pressure -1.0025e+05 2.7388e+05 87643 90350 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0428 0.10072 0.0028351 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.238e-07 0.05187 0.00031411 5.2161e-06 INSTANT 0.875788000E-01 TIME STEP NUMBER 55986 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282657361E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.768124494E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.93290E-02 0.20803E+01 Friction velocity uk : 0.93290E-02 0.20803E+01 Dimensionless distance yplus : 0.89781E-02 0.20427E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.007709365e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29419E+08 1 0.17889E-09 0.23936E+02 0.19005E+04 c Velocity[X] 0.12404E+02 c Velocity[Y] 0.11532E+02 c Velocity[Z] 0.10938E-05 c Pressure 0.22158E-03 29 0.84316E-04 0.22715E-02 0.46097E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -22.676 35.36 5.6045 7.9955 v Velocity[Y] -25.228 26.385 -0.14415 -0.0020748 v Velocity[Z] -2.9847 3.0263 2.6867e-06 -5.3878e-08 v ǁVelocityǁ 0.00128 35.464 7.6364 8.0744 v Pressure -1.9985e+05 1.7456e+05 -11758 -9822.2 v TurbVisc 5.7429e-21 0.013978 0.00016389 2.2735e-05 v CourantNb 4.5344e-08 0.011733 0.00016796 4.9284e-06 v FourierNb 1.2425e-07 0.046592 0.00014615 2.8795e-07 v total_pressure -98528 2.7589e+05 89567 91503 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0427 0.10072 0.0028351 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2382e-07 0.051867 0.00031411 5.2164e-06 INSTANT 0.875789000E-01 TIME STEP NUMBER 55987 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282656586E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.768117176E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.90187E-02 0.20802E+01 Friction velocity uk : 0.90187E-02 0.20802E+01 Dimensionless distance yplus : 0.86795E-02 0.20426E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -4.363714055e-03 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29419E+08 1 0.17889E-09 0.23938E+02 0.19005E+04 c Velocity[X] 0.12406E+02 c Velocity[Y] 0.11533E+02 c Velocity[Z] 0.10940E-05 c Pressure 0.22219E-03 229 0.97419E-04 0.22766E-02 0.40004E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -22.684 35.373 5.6045 7.9955 v Velocity[Y] -25.238 26.394 -0.14416 -0.0020896 v Velocity[Z] -2.9845 3.0265 2.686e-06 -5.3878e-08 v ǁVelocityǁ 0.001288 35.477 7.6379 8.0746 v Pressure -1.9811e+05 1.7657e+05 -9891.3 -8888.8 v TurbVisc 8.7597e-21 0.013997 0.00016394 2.2772e-05 v CourantNb 4.52e-08 0.011733 0.00016797 4.9285e-06 v FourierNb 1.2425e-07 0.046589 0.00014615 2.882e-07 v total_pressure -96789 2.779e+05 91434 92436 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0426 0.10072 0.0028351 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2384e-07 0.051863 0.00031412 5.2167e-06 INSTANT 0.875790000E-01 TIME STEP NUMBER 55988 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282656158E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.768117966E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.90471E-02 0.20802E+01 Friction velocity uk : 0.90471E-02 0.20802E+01 Dimensionless distance yplus : 0.87068E-02 0.20425E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.571483366e-03 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29419E+08 1 0.17889E-09 0.23932E+02 0.19002E+04 c Velocity[X] 0.12406E+02 c Velocity[Y] 0.11525E+02 c Velocity[Z] 0.10954E-05 c Pressure 0.22267E-03 128 0.82930E-04 0.22802E-02 0.45971E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -22.693 35.387 5.6045 7.9955 v Velocity[Y] -25.247 26.403 -0.14417 -0.0021027 v Velocity[Z] -2.9843 3.0267 2.6852e-06 -5.3878e-08 v ǁVelocityǁ 0.0012845 35.491 7.6395 8.0747 v Pressure -1.9637e+05 1.786e+05 -7984.6 -7730 v TurbVisc 1.1992e-20 0.014016 0.00016398 2.281e-05 v CourantNb 4.5343e-08 0.011733 0.00016797 4.9286e-06 v FourierNb 1.2425e-07 0.046585 0.00014615 2.8846e-07 v total_pressure -95044 2.7992e+05 93340 93595 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0425 0.10071 0.002835 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2386e-07 0.051861 0.00031412 5.217e-06 INSTANT 0.875791000E-01 TIME STEP NUMBER 55989 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282655784E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.768131287E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.94076E-02 0.20801E+01 Friction velocity uk : 0.94076E-02 0.20801E+01 Dimensionless distance yplus : 0.90538E-02 0.20425E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 7.291107925e-03 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29419E+08 1 0.17889E-09 0.23938E+02 0.19004E+04 c Velocity[X] 0.12409E+02 c Velocity[Y] 0.11529E+02 c Velocity[Z] 0.11004E-05 c Pressure 0.22134E-03 10 0.61134E-04 0.22656E-02 0.37416E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -22.701 35.401 5.6045 7.9955 v Velocity[Y] -25.257 26.412 -0.14418 -0.0021153 v Velocity[Z] -2.9841 3.0268 2.6845e-06 -5.3878e-08 v ǁVelocityǁ 0.0012454 35.505 7.641 8.0748 v Pressure -1.9467e+05 1.8058e+05 -6102.3 -6772 v TurbVisc 1.1239e-20 0.014036 0.00016403 2.2848e-05 v CourantNb 4.5688e-08 0.011732 0.00016797 4.9286e-06 v FourierNb 1.2425e-07 0.046582 0.00014615 2.8872e-07 v total_pressure -93348 2.8191e+05 95223 94553 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0425 0.10071 0.002835 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2388e-07 0.051858 0.00031412 5.2173e-06 INSTANT 0.875792000E-01 TIME STEP NUMBER 55990 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282655644E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.768155558E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10228E-01 0.20801E+01 Friction velocity uk : 0.10228E-01 0.20801E+01 Dimensionless distance yplus : 0.98430E-02 0.20424E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.415777486e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29419E+08 1 0.17889E-09 0.23939E+02 0.19004E+04 c Velocity[X] 0.12411E+02 c Velocity[Y] 0.11528E+02 c Velocity[Z] 0.11037E-05 c Pressure 0.22186E-03 274 0.79006E-04 0.22697E-02 0.47659E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -22.71 35.415 5.6045 7.9955 v Velocity[Y] -25.267 26.421 -0.14418 -0.0021298 v Velocity[Z] -2.9839 3.027 2.6838e-06 -5.3878e-08 v ǁVelocityǁ 0.0012475 35.519 7.6425 8.0749 v Pressure -1.9286e+05 1.8267e+05 -4218.1 -5657.1 v TurbVisc 6.1167e-21 0.014055 0.00016408 2.2885e-05 v CourantNb 4.5751e-08 0.011732 0.00016797 4.9287e-06 v FourierNb 1.2425e-07 0.04658 0.00014615 2.8897e-07 v total_pressure -91534 2.84e+05 97107 95668 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0424 0.10071 0.002835 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.239e-07 0.051855 0.00031413 5.2177e-06 INSTANT 0.875793000E-01 TIME STEP NUMBER 55991 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282655609E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.768191955E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11148E-01 0.20801E+01 Friction velocity uk : 0.11148E-01 0.20801E+01 Dimensionless distance yplus : 0.10729E-01 0.20424E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.894648579e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29419E+08 1 0.17889E-09 0.23943E+02 0.19005E+04 c Velocity[X] 0.12414E+02 c Velocity[Y] 0.11529E+02 c Velocity[Z] 0.11023E-05 c Pressure 0.22186E-03 34 0.85329E-04 0.22685E-02 0.48649E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -22.718 35.429 5.6045 7.9955 v Velocity[Y] -25.276 26.43 -0.14419 -0.0021422 v Velocity[Z] -2.9837 3.0272 2.683e-06 -5.3878e-08 v ǁVelocityǁ 0.0012276 35.533 7.6441 8.0751 v Pressure -1.9112e+05 1.8478e+05 -2279.6 -4490.6 v TurbVisc 1.437e-20 0.014074 0.00016413 2.2923e-05 v CourantNb 4.7118e-08 0.011732 0.00016798 4.9287e-06 v FourierNb 1.2425e-07 0.046577 0.00014615 2.8923e-07 v total_pressure -89794 2.861e+05 99045 96834 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0424 0.1007 0.0028349 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2392e-07 0.051853 0.00031413 5.218e-06 INSTANT 0.875794000E-01 TIME STEP NUMBER 55992 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282655686E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.768233297E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11000E-01 0.20801E+01 Friction velocity uk : 0.11000E-01 0.20801E+01 Dimensionless distance yplus : 0.10587E-01 0.20425E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 2.439500617e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29419E+08 1 0.17889E-09 0.23949E+02 0.19007E+04 c Velocity[X] 0.12418E+02 c Velocity[Y] 0.11531E+02 c Velocity[Z] 0.11050E-05 c Pressure 0.22193E-03 1563 0.98551E-04 0.22680E-02 0.41386E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -22.726 35.442 5.6046 7.9955 v Velocity[Y] -25.286 26.439 -0.1442 -0.0021577 v Velocity[Z] -2.9835 3.0274 2.6823e-06 -5.3878e-08 v ǁVelocityǁ 0.0012055 35.547 7.6456 8.0752 v Pressure -1.8937e+05 1.8687e+05 -409.55 -3567 v TurbVisc 7.5064e-21 0.014093 0.00016418 2.296e-05 v CourantNb 4.7944e-08 0.011731 0.00016798 4.9288e-06 v FourierNb 1.2425e-07 0.046574 0.00014616 2.8949e-07 v total_pressure -88046 2.8819e+05 1.0092e+05 97758 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0425 0.10069 0.0028348 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2395e-07 0.051851 0.00031413 5.2183e-06 INSTANT 0.875795000E-01 TIME STEP NUMBER 55993 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282656106E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.768282773E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.91634E-02 0.20801E+01 Friction velocity uk : 0.91634E-02 0.20801E+01 Dimensionless distance yplus : 0.88187E-02 0.20425E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 2.995022500e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29419E+08 1 0.17889E-09 0.23945E+02 0.19005E+04 c Velocity[X] 0.12421E+02 c Velocity[Y] 0.11524E+02 c Velocity[Z] 0.11077E-05 c Pressure 0.22184E-03 128 0.83938E-04 0.22659E-02 0.48175E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -22.735 35.456 5.6046 7.9955 v Velocity[Y] -25.296 26.448 -0.14421 -0.0021712 v Velocity[Z] -2.9833 3.0276 2.6816e-06 -5.3878e-08 v ǁVelocityǁ 0.0011856 35.561 7.6472 8.0753 v Pressure -1.8759e+05 1.89e+05 1507.6 -2385 v TurbVisc 1.9552e-21 0.014112 0.00016422 2.2999e-05 v CourantNb 4.905e-08 0.011731 0.00016798 4.9289e-06 v FourierNb 1.2425e-07 0.046572 0.00014616 2.8975e-07 v total_pressure -86269 2.9033e+05 1.0283e+05 98940 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0425 0.10068 0.0028348 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2397e-07 0.051848 0.00031414 5.2186e-06 INSTANT 0.875796000E-01 TIME STEP NUMBER 55994 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282656592E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.768345518E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.34894E-02 0.20801E+01 Friction velocity uk : 0.34894E-02 0.20801E+01 Dimensionless distance yplus : 0.34320E-02 0.20425E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 3.523953025e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29419E+08 1 0.17889E-09 0.23955E+02 0.19008E+04 c Velocity[X] 0.12426E+02 c Velocity[Y] 0.11529E+02 c Velocity[Z] 0.11143E-05 c Pressure 0.21994E-03 10 0.61741E-04 0.22453E-02 0.37704E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -22.743 35.47 5.6046 7.9955 v Velocity[Y] -25.305 26.457 -0.14422 -0.0021842 v Velocity[Z] -2.9831 3.0278 2.6808e-06 -5.3878e-08 v ǁVelocityǁ 0.001143 35.575 7.6487 8.0755 v Pressure -1.8589e+05 1.9104e+05 3382.8 -1439.7 v TurbVisc 4.2496e-21 0.014131 0.00016427 2.3036e-05 v CourantNb 5.0301e-08 0.01173 0.00016798 4.9289e-06 v FourierNb 1.2425e-07 0.046569 0.00014616 2.9001e-07 v total_pressure -84568 2.9236e+05 1.0471e+05 99885 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0425 0.10066 0.0028346 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2399e-07 0.051846 0.00031414 5.2189e-06 INSTANT 0.875797000E-01 TIME STEP NUMBER 55995 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282657302E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.768419025E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.34396E-02 0.20801E+01 Friction velocity uk : 0.34396E-02 0.20801E+01 Dimensionless distance yplus : 0.33104E-02 0.20425E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 4.111286587e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29419E+08 1 0.17888E-09 0.23959E+02 0.19009E+04 c Velocity[X] 0.12430E+02 c Velocity[Y] 0.11529E+02 c Velocity[Z] 0.11193E-05 c Pressure 0.21992E-03 523 0.79856E-04 0.22440E-02 0.48159E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -22.751 35.484 5.6047 7.9955 v Velocity[Y] -25.315 26.466 -0.14423 -0.0021995 v Velocity[Z] -2.9829 3.028 2.6801e-06 -5.3878e-08 v ǁVelocityǁ 0.0011409 35.589 7.6502 8.0756 v Pressure -1.8408e+05 1.9321e+05 5259.5 -328.54 v TurbVisc 1.1565e-20 0.01415 0.00016432 2.3074e-05 v CourantNb 5.1262e-08 0.01173 0.00016799 4.929e-06 v FourierNb 1.2425e-07 0.046567 0.00014616 2.9026e-07 v total_pressure -82753 2.9453e+05 1.0658e+05 1.01e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0425 0.10066 0.0028346 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2402e-07 0.051844 0.00031415 5.2193e-06 INSTANT 0.875798000E-01 TIME STEP NUMBER 55996 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282658118E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.768505173E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.45964E-02 0.20802E+01 Friction velocity uk : 0.45964E-02 0.20802E+01 Dimensionless distance yplus : 0.44235E-02 0.20426E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 4.539938016e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29420E+08 1 0.17888E-09 0.23967E+02 0.19012E+04 c Velocity[X] 0.12436E+02 c Velocity[Y] 0.11531E+02 c Velocity[Z] 0.11189E-05 c Pressure 0.21938E-03 35 0.86150E-04 0.22373E-02 0.48329E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -22.76 35.498 5.6047 7.9955 v Velocity[Y] -25.325 26.476 -0.14425 -0.0022122 v Velocity[Z] -2.9827 3.0282 2.6794e-06 -5.3878e-08 v ǁVelocityǁ 0.0011182 35.603 7.6518 8.0758 v Pressure -1.8232e+05 1.9527e+05 7179.3 827.04 v TurbVisc 1.6466e-20 0.014169 0.00016437 2.3112e-05 v CourantNb 5.3494e-08 0.01173 0.00016799 4.9291e-06 v FourierNb 1.2425e-07 0.046564 0.00014616 2.9053e-07 v total_pressure -80998 2.966e+05 1.085e+05 1.0215e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0426 0.10064 0.0028346 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2404e-07 0.051842 0.00031415 5.2196e-06 INSTANT 0.875799000E-01 TIME STEP NUMBER 55997 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282659049E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.768596449E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.47763E-02 0.20803E+01 Friction velocity uk : 0.47763E-02 0.20803E+01 Dimensionless distance yplus : 0.45967E-02 0.20427E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 4.966732240e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29420E+08 1 0.17888E-09 0.23976E+02 0.19015E+04 c Velocity[X] 0.12442E+02 c Velocity[Y] 0.11534E+02 c Velocity[Z] 0.11227E-05 c Pressure 0.21891E-03 160 0.99554E-04 0.22313E-02 0.41099E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -22.768 35.512 5.6048 7.9956 v Velocity[Y] -25.334 26.485 -0.14426 -0.002228 v Velocity[Z] -2.9825 3.0284 2.6786e-06 -5.3878e-08 v ǁVelocityǁ 0.0010653 35.618 7.6534 8.0759 v Pressure -1.8057e+05 1.9733e+05 9032.6 1749 v TurbVisc 2.0866e-20 0.014188 0.00016442 2.3149e-05 v CourantNb 5.5132e-08 0.011729 0.00016799 4.9291e-06 v FourierNb 1.2425e-07 0.046562 0.00014616 2.9078e-07 v total_pressure -79243 2.9865e+05 1.1036e+05 1.0307e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0427 0.10063 0.0028346 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2407e-07 0.051841 0.00031415 5.2199e-06 INSTANT 0.875800000E-01 TIME STEP NUMBER 55998 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282660331E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.768696573E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.69726E-02 0.20804E+01 Friction velocity uk : 0.69726E-02 0.20804E+01 Dimensionless distance yplus : 0.67103E-02 0.20427E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 5.399381514e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29420E+08 1 0.17889E-09 0.23976E+02 0.19014E+04 c Velocity[X] 0.12448E+02 c Velocity[Y] 0.11528E+02 c Velocity[Z] 0.11270E-05 c Pressure 0.21830E-03 170 0.84875E-04 0.22240E-02 0.45943E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -22.776 35.526 5.6048 7.9956 v Velocity[Y] -25.344 26.494 -0.14427 -0.0022423 v Velocity[Z] -2.9823 3.0286 2.6779e-06 -5.3878e-08 v ǁVelocityǁ 0.00095405 35.632 7.6549 8.0761 v Pressure -1.7881e+05 1.994e+05 10922 2895.4 v TurbVisc 1.8091e-20 0.014207 0.00016447 2.3188e-05 v CourantNb 5.6976e-08 0.011729 0.000168 4.9292e-06 v FourierNb 1.2425e-07 0.04656 0.00014616 2.9105e-07 v total_pressure -77483 3.0072e+05 1.1225e+05 1.0422e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0427 0.10062 0.0028346 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2409e-07 0.051839 0.00031416 5.2203e-06 INSTANT 0.875801000E-01 TIME STEP NUMBER 55999 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282661655E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.768810014E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.78036E-02 0.20804E+01 Friction velocity uk : 0.78036E-02 0.20804E+01 Dimensionless distance yplus : 0.75934E-02 0.20428E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 5.756199750e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29420E+08 1 0.17889E-09 0.23989E+02 0.19019E+04 c Velocity[X] 0.12455E+02 c Velocity[Y] 0.11533E+02 c Velocity[Z] 0.11328E-05 c Pressure 0.21579E-03 10 0.62039E-04 0.21973E-02 0.36565E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -22.785 35.54 5.6049 7.9956 v Velocity[Y] -25.354 26.504 -0.14428 -0.0022558 v Velocity[Z] -2.9821 3.0287 2.6772e-06 -5.3878e-08 v ǁVelocityǁ 0.0008547 35.646 7.6565 8.0762 v Pressure -1.771e+05 2.0139e+05 12768 3835.2 v TurbVisc 2.4847e-20 0.014226 0.00016452 2.3226e-05 v CourantNb 5.8976e-08 0.011729 0.000168 4.9293e-06 v FourierNb 1.2425e-07 0.046558 0.00014616 2.9131e-07 v total_pressure -75776 3.0271e+05 1.1409e+05 1.0516e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0428 0.1006 0.0028345 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2412e-07 0.051837 0.00031416 5.2206e-06 INSTANT 0.875802000E-01 TIME STEP NUMBER 56000 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282663210E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.768934270E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.42404E-02 0.20805E+01 Friction velocity uk : 0.42404E-02 0.20805E+01 Dimensionless distance yplus : 0.41262E-02 0.20429E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 6.171884209e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29420E+08 1 0.17888E-09 0.23996E+02 0.19021E+04 c Velocity[X] 0.12462E+02 c Velocity[Y] 0.11534E+02 c Velocity[Z] 0.11372E-05 c Pressure 0.21527E-03 349 0.80473E-04 0.21908E-02 0.45629E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -22.793 35.554 5.6049 7.9956 v Velocity[Y] -25.363 26.513 -0.1443 -0.0022715 v Velocity[Z] -2.9819 3.0289 2.6765e-06 -5.3879e-08 v ǁVelocityǁ 0.00074802 35.66 7.658 8.0764 v Pressure -1.7529e+05 2.0349e+05 14607 4921.6 v TurbVisc 1.3668e-20 0.014245 0.00016457 2.3263e-05 v CourantNb 6.058e-08 0.011728 0.000168 4.9294e-06 v FourierNb 1.2425e-07 0.046555 0.00014616 2.9156e-07 v total_pressure -73966 3.0482e+05 1.1593e+05 1.0625e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0429 0.10058 0.0028345 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2415e-07 0.051835 0.00031416 5.2209e-06 INSTANT 0.875803000E-01 TIME STEP NUMBER 56001 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282664871E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.769071733E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.33676E-02 0.20806E+01 Friction velocity uk : 0.33676E-02 0.20806E+01 Dimensionless distance yplus : 0.32719E-02 0.20430E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 6.455899695e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29420E+08 1 0.17889E-09 0.24008E+02 0.19025E+04 c Velocity[X] 0.12471E+02 c Velocity[Y] 0.11537E+02 c Velocity[Z] 0.11385E-05 c Pressure 0.21420E-03 38 0.86706E-04 0.21788E-02 0.45495E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -22.801 35.568 5.605 7.9957 v Velocity[Y] -25.373 26.523 -0.14431 -0.0022849 v Velocity[Z] -2.9817 3.0291 2.6757e-06 -5.3879e-08 v ǁVelocityǁ 0.00066763 35.675 7.6596 8.0765 v Pressure -1.7355e+05 2.055e+05 16488 6053.3 v TurbVisc 2.2482e-20 0.014265 0.00016462 2.3302e-05 v CourantNb 6.339e-08 0.011728 0.000168 4.9295e-06 v FourierNb 1.2425e-07 0.046553 0.00014616 2.9183e-07 v total_pressure -72223 3.0682e+05 1.1781e+05 1.0738e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.043 0.10057 0.0028344 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2417e-07 0.051834 0.00031417 5.2213e-06 INSTANT 0.875804000E-01 TIME STEP NUMBER 56002 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282666641E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.769214124E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.39237E-02 0.20807E+01 Friction velocity uk : 0.39237E-02 0.20807E+01 Dimensionless distance yplus : 0.38252E-02 0.20431E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 6.684655542e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29420E+08 1 0.17889E-09 0.24012E+02 0.19026E+04 c Velocity[X] 0.12478E+02 c Velocity[Y] 0.11534E+02 c Velocity[Z] 0.11425E-05 c Pressure 0.21321E-03 989 0.75038E-04 0.21675E-02 0.36327E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -22.81 35.583 5.6051 7.9957 v Velocity[Y] -25.383 26.532 -0.14432 -0.0023001 v Velocity[Z] -2.9815 3.0293 2.675e-06 -5.3879e-08 v ǁVelocityǁ 0.00060961 35.689 7.6612 8.0767 v Pressure -1.7181e+05 2.0748e+05 18299 6981.3 v TurbVisc 2.8184e-20 0.014284 0.00016468 2.3339e-05 v CourantNb 6.5579e-08 0.011728 0.00016801 4.9295e-06 v FourierNb 1.2425e-07 0.046551 0.00014616 2.9208e-07 v total_pressure -70488 3.088e+05 1.1962e+05 1.0831e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0431 0.10055 0.0028345 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.242e-07 0.051832 0.00031417 5.2216e-06 INSTANT 0.875805000E-01 TIME STEP NUMBER 56003 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282668654E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.769365528E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.52470E-02 0.20808E+01 Friction velocity uk : 0.52470E-02 0.20808E+01 Dimensionless distance yplus : 0.50514E-02 0.20432E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 6.899959413e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29421E+08 1 0.17889E-09 0.24027E+02 0.19031E+04 c Velocity[X] 0.12487E+02 c Velocity[Y] 0.11540E+02 c Velocity[Z] 0.11490E-05 c Pressure 0.21052E-03 10 0.56661E-04 0.21391E-02 0.32811E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -22.818 35.597 5.6051 7.9958 v Velocity[Y] -25.392 26.542 -0.14434 -0.0023161 v Velocity[Z] -2.9813 3.0295 2.6743e-06 -5.3879e-08 v ǁVelocityǁ 0.00059098 35.704 7.6627 8.0769 v Pressure -1.7011e+05 2.0941e+05 20101 7884.4 v TurbVisc 2.8881e-20 0.014303 0.00016473 2.3378e-05 v CourantNb 6.7892e-08 0.011727 0.00016801 4.9296e-06 v FourierNb 1.2425e-07 0.046549 0.00014616 2.9235e-07 v total_pressure -68790 3.1073e+05 1.2143e+05 1.0921e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0432 0.10055 0.0028347 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2423e-07 0.05183 0.00031418 5.222e-06 INSTANT 0.875806000E-01 TIME STEP NUMBER 56004 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282670991E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.769530070E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11974E-01 0.20809E+01 Friction velocity uk : 0.11974E-01 0.20809E+01 Dimensionless distance yplus : 0.11523E-01 0.20432E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 7.113150120e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29421E+08 1 0.17889E-09 0.24034E+02 0.19033E+04 c Velocity[X] 0.12496E+02 c Velocity[Y] 0.11539E+02 c Velocity[Z] 0.11549E-05 c Pressure 0.20942E-03 48 0.95657E-04 0.21268E-02 0.42348E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -22.826 35.611 5.6052 7.9958 v Velocity[Y] -25.402 26.552 -0.14435 -0.0023312 v Velocity[Z] -2.9811 3.0297 2.6735e-06 -5.3879e-08 v ǁVelocityǁ 0.00058697 35.718 7.6643 8.077 v Pressure -1.6834e+05 2.1144e+05 21892 9011.4 v TurbVisc 1.9513e-20 0.014322 0.00016478 2.3416e-05 v CourantNb 2.6337e-08 0.011727 0.00016802 4.9297e-06 v FourierNb 1.2425e-07 0.046547 0.00014617 2.9261e-07 v total_pressure -67013 3.1276e+05 1.2322e+05 1.1034e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0432 0.10055 0.002835 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2426e-07 0.051829 0.00031418 5.2223e-06 INSTANT 0.875807000E-01 TIME STEP NUMBER 56005 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282673305E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.769709377E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.40966E-02 0.20810E+01 Friction velocity uk : 0.40966E-02 0.20810E+01 Dimensionless distance yplus : 0.40022E-02 0.20434E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 7.202832092e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29421E+08 1 0.17889E-09 0.24046E+02 0.19037E+04 c Velocity[X] 0.12505E+02 c Velocity[Y] 0.11540E+02 c Velocity[Z] 0.11558E-05 c Pressure 0.20756E-03 251 0.80048E-04 0.21068E-02 0.39053E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -22.835 35.626 5.6053 7.9958 v Velocity[Y] -25.412 26.562 -0.14436 -0.0023462 v Velocity[Z] -2.9809 3.0299 2.6728e-06 -5.3879e-08 v ǁVelocityǁ 0.00058018 35.733 7.6659 8.0772 v Pressure -1.6661e+05 2.1338e+05 23729 10105 v TurbVisc 5.8973e-21 0.014341 0.00016483 2.3455e-05 v CourantNb 7.2719e-08 0.011726 0.00016802 4.9298e-06 v FourierNb 1.2425e-07 0.046545 0.00014617 2.9288e-07 v total_pressure -65285 3.1471e+05 1.2505e+05 1.1143e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0434 0.10054 0.0028352 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2429e-07 0.051827 0.00031418 5.2227e-06 INSTANT 0.875808000E-01 TIME STEP NUMBER 56006 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282675803E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.769895733E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.57752E-02 0.20811E+01 Friction velocity uk : 0.57752E-02 0.20811E+01 Dimensionless distance yplus : 0.55579E-02 0.20435E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 7.383233371e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29421E+08 1 0.17889E-09 0.24062E+02 0.19043E+04 c Velocity[X] 0.12516E+02 c Velocity[Y] 0.11547E+02 c Velocity[Z] 0.11624E-05 c Pressure 0.20545E-03 10 0.54407E-04 0.20843E-02 0.33097E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -22.843 35.64 5.6053 7.9959 v Velocity[Y] -25.422 26.571 -0.14438 -0.0023607 v Velocity[Z] -2.9807 3.0301 2.6721e-06 -5.3879e-08 v ǁVelocityǁ 0.00057666 35.747 7.6674 8.0774 v Pressure -1.6492e+05 2.1527e+05 25512 11038 v TurbVisc 1.4559e-20 0.01436 0.00016488 2.3493e-05 v CourantNb 5.902e-08 0.011726 0.00016802 4.9299e-06 v FourierNb 1.2425e-07 0.046542 0.00014617 2.9314e-07 v total_pressure -63592 3.1659e+05 1.2684e+05 1.1236e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0435 0.10054 0.0028355 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2431e-07 0.051825 0.00031419 5.223e-06 INSTANT 0.875809000E-01 TIME STEP NUMBER 56007 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282678464E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.770088983E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.82825E-02 0.20812E+01 Friction velocity uk : 0.82825E-02 0.20812E+01 Dimensionless distance yplus : 0.79710E-02 0.20435E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 7.353542056e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29422E+08 1 0.17889E-09 0.24072E+02 0.19046E+04 c Velocity[X] 0.12526E+02 c Velocity[Y] 0.11546E+02 c Velocity[Z] 0.11684E-05 c Pressure 0.20417E-03 124 0.97052E-04 0.20702E-02 0.36193E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -22.851 35.655 5.6054 7.996 v Velocity[Y] -25.431 26.581 -0.14439 -0.0023755 v Velocity[Z] -2.9805 3.0303 2.6714e-06 -5.3879e-08 v ǁVelocityǁ 0.00059213 35.762 7.669 8.0776 v Pressure -1.632e+05 2.1722e+05 27224 12040 v TurbVisc 3.0664e-22 0.014379 0.00016494 2.3531e-05 v CourantNb 2.9417e-08 0.011726 0.00016803 4.93e-06 v FourierNb 1.2425e-07 0.04654 0.00014617 2.934e-07 v total_pressure -61873 3.1855e+05 1.2855e+05 1.1336e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0435 0.10054 0.0028357 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2434e-07 0.051823 0.00031419 5.2234e-06 INSTANT 0.875810000E-01 TIME STEP NUMBER 56008 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282681254E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.770295831E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12409E-01 0.20813E+01 Friction velocity uk : 0.12409E-01 0.20813E+01 Dimensionless distance yplus : 0.11942E-01 0.20437E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 7.364911277e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29422E+08 1 0.17889E-09 0.24085E+02 0.19051E+04 c Velocity[X] 0.12536E+02 c Velocity[Y] 0.11549E+02 c Velocity[Z] 0.11693E-05 c Pressure 0.20198E-03 34 0.81315E-04 0.20469E-02 0.31782E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -22.859 35.669 5.6055 7.996 v Velocity[Y] -25.441 26.591 -0.1444 -0.0023912 v Velocity[Z] -2.9803 3.0305 2.6706e-06 -5.3879e-08 v ǁVelocityǁ 0.00058852 35.777 7.6706 8.0778 v Pressure -1.6152e+05 2.1907e+05 28978 12970 v TurbVisc 1.5108e-20 0.014398 0.00016499 2.3569e-05 v CourantNb 3.3045e-09 0.011725 0.00016803 4.93e-06 v FourierNb 1.2425e-07 0.046538 0.00014617 2.9366e-07 v total_pressure -60195 3.2039e+05 1.303e+05 1.143e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0437 0.10053 0.0028359 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2437e-07 0.051822 0.0003142 5.2237e-06 INSTANT 0.875811000E-01 TIME STEP NUMBER 56009 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282684226E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.770512210E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15642E-02 0.20814E+01 Friction velocity uk : 0.15642E-02 0.20814E+01 Dimensionless distance yplus : 0.15300E-02 0.20438E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 7.311459252e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29422E+08 1 0.17890E-09 0.24103E+02 0.19057E+04 c Velocity[X] 0.12547E+02 c Velocity[Y] 0.11556E+02 c Velocity[Z] 0.11749E-05 c Pressure 0.19947E-03 10 0.54941E-04 0.20204E-02 0.30066E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -22.868 35.684 5.6055 7.9961 v Velocity[Y] -25.451 26.601 -0.14442 -0.0024082 v Velocity[Z] -2.9801 3.0306 2.6699e-06 -5.3879e-08 v ǁVelocityǁ 0.00061468 35.791 7.6722 8.078 v Pressure -1.5988e+05 2.2089e+05 30715 13864 v TurbVisc 2.2266e-20 0.014417 0.00016504 2.3608e-05 v CourantNb 2.9794e-08 0.011725 0.00016803 4.9301e-06 v FourierNb 1.2425e-07 0.046536 0.00014617 2.9392e-07 v total_pressure -58552 3.2221e+05 1.3204e+05 1.1519e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0438 0.10052 0.002836 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.244e-07 0.05182 0.0003142 5.2241e-06 INSTANT 0.875812000E-01 TIME STEP NUMBER 56010 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282687439E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.770737828E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.70458E-02 0.20815E+01 Friction velocity uk : 0.70458E-02 0.20815E+01 Dimensionless distance yplus : 0.69001E-02 0.20438E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 7.310167955e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29422E+08 1 0.17890E-09 0.24114E+02 0.19061E+04 c Velocity[X] 0.12559E+02 c Velocity[Y] 0.11555E+02 c Velocity[Z] 0.11855E-05 c Pressure 0.19792E-03 28 0.98151E-04 0.20036E-02 0.35452E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -22.876 35.698 5.6056 7.9961 v Velocity[Y] -25.461 26.611 -0.14443 -0.0024239 v Velocity[Z] -2.9799 3.0308 2.6692e-06 -5.3879e-08 v ǁVelocityǁ 0.00060246 35.806 7.6737 8.0782 v Pressure -1.5826e+05 2.2278e+05 32389 14907 v TurbVisc 2.5901e-20 0.014436 0.0001651 2.3647e-05 v CourantNb 2.9343e-08 0.011724 0.00016804 4.9302e-06 v FourierNb 1.2425e-07 0.046533 0.00014617 2.9419e-07 v total_pressure -56938 3.2411e+05 1.3371e+05 1.1623e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0438 0.10051 0.0028362 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2443e-07 0.051818 0.00031421 5.2244e-06 INSTANT 0.875813000E-01 TIME STEP NUMBER 56011 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282690696E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.770976358E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.53648E-02 0.20816E+01 Friction velocity uk : 0.53648E-02 0.20816E+01 Dimensionless distance yplus : 0.52046E-02 0.20440E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 7.155383510e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29423E+08 1 0.17890E-09 0.24129E+02 0.19066E+04 c Velocity[X] 0.12571E+02 c Velocity[Y] 0.11558E+02 c Velocity[Z] 0.11868E-05 c Pressure 0.19544E-03 76 0.83210E-04 0.19775E-02 0.32637E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -22.884 35.713 5.6057 7.9962 v Velocity[Y] -25.471 26.622 -0.14444 -0.0024395 v Velocity[Z] -2.9797 3.031 2.6685e-06 -5.3879e-08 v ǁVelocityǁ 0.00060606 35.821 7.6753 8.0784 v Pressure -1.5667e+05 2.2459e+05 34096 15923 v TurbVisc 1.846e-20 0.014455 0.00016515 2.3686e-05 v CourantNb 4.185e-08 0.011724 0.00016804 4.9303e-06 v FourierNb 1.2425e-07 0.046531 0.00014617 2.9446e-07 v total_pressure -55345 3.2591e+05 1.3542e+05 1.1725e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.044 0.10051 0.0028364 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2447e-07 0.051816 0.00031421 5.2248e-06 INSTANT 0.875814000E-01 TIME STEP NUMBER 56012 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282694145E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.771222824E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.86873E-02 0.20817E+01 Friction velocity uk : 0.86873E-02 0.20817E+01 Dimensionless distance yplus : 0.84280E-02 0.20441E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 6.979577358e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29423E+08 1 0.17890E-09 0.24149E+02 0.19073E+04 c Velocity[X] 0.12583E+02 c Velocity[Y] 0.11566E+02 c Velocity[Z] 0.11868E-05 c Pressure 0.19265E-03 10 0.56669E-04 0.19482E-02 0.27440E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -22.892 35.728 5.6057 7.9963 v Velocity[Y] -25.48 26.632 -0.14445 -0.0024546 v Velocity[Z] -2.9795 3.0312 2.6677e-06 -5.3879e-08 v ǁVelocityǁ 0.00059139 35.836 7.6769 8.0786 v Pressure -1.5515e+05 2.2633e+05 35765 16771 v TurbVisc 2.7228e-20 0.014474 0.00016521 2.3725e-05 v CourantNb 3.8333e-08 0.011724 0.00016804 4.9304e-06 v FourierNb 1.2425e-07 0.046529 0.00014617 2.9472e-07 v total_pressure -53827 3.2766e+05 1.3709e+05 1.181e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0441 0.10051 0.0028367 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.245e-07 0.051815 0.00031421 5.2251e-06 INSTANT 0.875815000E-01 TIME STEP NUMBER 56013 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282697721E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.771477963E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15406E-01 0.20818E+01 Friction velocity uk : 0.15406E-01 0.20818E+01 Dimensionless distance yplus : 0.14956E-01 0.20441E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 6.946771778e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29423E+08 1 0.17890E-09 0.24164E+02 0.19078E+04 c Velocity[X] 0.12595E+02 c Velocity[Y] 0.11569E+02 c Velocity[Z] 0.11934E-05 c Pressure 0.19087E-03 145 0.76033E-04 0.19292E-02 0.31623E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -22.901 35.743 5.6058 7.9963 v Velocity[Y] -25.49 26.642 -0.14447 -0.0024715 v Velocity[Z] -2.9793 3.0314 2.667e-06 -5.3879e-08 v ǁVelocityǁ 0.00060031 35.851 7.6785 8.0788 v Pressure -1.5357e+05 2.2814e+05 37365 17684 v TurbVisc 3.3597e-20 0.014493 0.00016526 2.3763e-05 v CourantNb 2.5653e-08 0.011723 0.00016804 4.9305e-06 v FourierNb 1.2425e-07 0.046526 0.00014617 2.9498e-07 v total_pressure -52247 3.2947e+05 1.3869e+05 1.1901e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0441 0.10051 0.0028369 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2453e-07 0.051812 0.00031422 5.2255e-06 INSTANT 0.875816000E-01 TIME STEP NUMBER 56014 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282701452E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.771746542E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.23311E-02 0.20819E+01 Friction velocity uk : 0.23311E-02 0.20819E+01 Dimensionless distance yplus : 0.22749E-02 0.20442E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 6.713880105e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29424E+08 1 0.17891E-09 0.24182E+02 0.19085E+04 c Velocity[X] 0.12609E+02 c Velocity[Y] 0.11573E+02 c Velocity[Z] 0.11956E-05 c Pressure 0.18846E-03 416 0.80947E-04 0.19038E-02 0.32963E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -22.909 35.758 5.6059 7.9964 v Velocity[Y] -25.5 26.653 -0.14448 -0.0024863 v Velocity[Z] -2.9791 3.0316 2.6663e-06 -5.3879e-08 v ǁVelocityǁ 0.0006357 35.866 7.68 8.079 v Pressure -1.5205e+05 2.2987e+05 39020 18686 v TurbVisc 2.2678e-20 0.014512 0.00016532 2.3802e-05 v CourantNb 1.3725e-08 0.011723 0.00016805 4.9306e-06 v FourierNb 1.2425e-07 0.046524 0.00014617 2.9525e-07 v total_pressure -50723 3.312e+05 1.4034e+05 1.2001e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0442 0.10051 0.0028371 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2456e-07 0.051811 0.00031422 5.2258e-06 INSTANT 0.875817000E-01 TIME STEP NUMBER 56015 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282705250E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.772020844E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.68722E-02 0.20820E+01 Friction velocity uk : 0.68722E-02 0.20820E+01 Dimensionless distance yplus : 0.67065E-02 0.20443E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 6.458883587e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29424E+08 1 0.17891E-09 0.24201E+02 0.19091E+04 c Velocity[X] 0.12621E+02 c Velocity[Y] 0.11580E+02 c Velocity[Z] 0.11989E-05 c Pressure 0.18619E-03 163 0.93596E-04 0.18798E-02 0.25217E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -22.917 35.772 5.606 7.9965 v Velocity[Y] -25.51 26.663 -0.14449 -0.002504 v Velocity[Z] -2.9788 3.0318 2.6656e-06 -5.3879e-08 v ǁVelocityǁ 0.00062927 35.881 7.6816 8.0792 v Pressure -1.5059e+05 2.3154e+05 40556 19386 v TurbVisc 3.614e-20 0.014531 0.00016537 2.384e-05 v CourantNb 2.7242e-09 0.011723 0.00016805 4.9307e-06 v FourierNb 1.2425e-07 0.046521 0.00014618 2.9552e-07 v total_pressure -49265 3.3286e+05 1.4188e+05 1.2071e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0443 0.1005 0.0028373 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.246e-07 0.051809 0.00031423 5.2262e-06 INSTANT 0.875818000E-01 TIME STEP NUMBER 56016 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282709384E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.772304960E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10622E-01 0.20821E+01 Friction velocity uk : 0.10622E-01 0.20821E+01 Dimensionless distance yplus : 0.10346E-01 0.20444E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 6.251858015e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29424E+08 1 0.17891E-09 0.24212E+02 0.19095E+04 c Velocity[X] 0.12635E+02 c Velocity[Y] 0.11577E+02 c Velocity[Z] 0.12017E-05 c Pressure 0.18374E-03 102 0.79440E-04 0.18541E-02 0.30362E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -22.926 35.787 5.606 7.9966 v Velocity[Y] -25.52 26.674 -0.1445 -0.0025202 v Velocity[Z] -2.9786 3.032 2.6648e-06 -5.3879e-08 v ǁVelocityǁ 0.00060322 35.896 7.6832 8.0794 v Pressure -1.491e+05 2.3324e+05 42144 20371 v TurbVisc 1.5359e-20 0.01455 0.00016543 2.388e-05 v CourantNb 1.033e-08 0.011722 0.00016805 4.9308e-06 v FourierNb 1.2425e-07 0.046519 0.00014618 2.9579e-07 v total_pressure -47778 3.3457e+05 1.4347e+05 1.217e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0444 0.1005 0.0028374 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2463e-07 0.051807 0.00031423 5.2266e-06 INSTANT 0.875819000E-01 TIME STEP NUMBER 56017 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282713532E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.772603100E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.36892E-02 0.20822E+01 Friction velocity uk : 0.36892E-02 0.20822E+01 Dimensionless distance yplus : 0.35932E-02 0.20445E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 5.999706711e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29425E+08 1 0.17892E-09 0.24234E+02 0.19103E+04 c Velocity[X] 0.12648E+02 c Velocity[Y] 0.11586E+02 c Velocity[Z] 0.12237E-05 c Pressure 0.17932E-03 9 0.57113E-04 0.18086E-02 0.22007E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -22.934 35.802 5.6061 7.9967 v Velocity[Y] -25.53 26.684 -0.14451 -0.0025358 v Velocity[Z] -2.9784 3.0321 2.6641e-06 -5.3879e-08 v ǁVelocityǁ 0.00056908 35.911 7.6848 8.0796 v Pressure -1.4771e+05 2.3484e+05 43655 21109 v TurbVisc 2.3413e-20 0.014569 0.00016548 2.3919e-05 v CourantNb 2.0302e-08 0.011722 0.00016806 4.9309e-06 v FourierNb 1.2425e-07 0.046516 0.00014618 2.9606e-07 v total_pressure -46386 3.3616e+05 1.4498e+05 1.2243e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0445 0.1005 0.0028375 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2466e-07 0.051805 0.00031423 5.2269e-06 INSTANT 0.875820000E-01 TIME STEP NUMBER 56018 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282717853E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.772910361E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.25292E-02 0.20822E+01 Friction velocity uk : 0.25292E-02 0.20822E+01 Dimensionless distance yplus : 0.24591E-02 0.20446E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 5.755721483e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29425E+08 1 0.17892E-09 0.24251E+02 0.19109E+04 c Velocity[X] 0.12662E+02 c Velocity[Y] 0.11589E+02 c Velocity[Z] 0.12201E-05 c Pressure 0.17709E-03 384 0.75163E-04 0.17851E-02 0.29176E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -22.942 35.818 5.6061 7.9968 v Velocity[Y] -25.54 26.695 -0.14452 -0.0025532 v Velocity[Z] -2.9782 3.0323 2.6634e-06 -5.3879e-08 v ǁVelocityǁ 0.00053834 35.927 7.6864 8.0798 v Pressure -1.4624e+05 2.3654e+05 45161 22029 v TurbVisc 1.2322e-20 0.014588 0.00016554 2.3958e-05 v CourantNb 2.8616e-08 0.011721 0.00016806 4.931e-06 v FourierNb 1.2425e-07 0.046513 0.00014618 2.9632e-07 v total_pressure -44915 3.3787e+05 1.4649e+05 1.2335e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0446 0.1005 0.0028377 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.247e-07 0.051802 0.00031424 5.2273e-06 INSTANT 0.875821000E-01 TIME STEP NUMBER 56019 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282722308E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.773228977E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.36666E-02 0.20823E+01 Friction velocity uk : 0.36666E-02 0.20823E+01 Dimensionless distance yplus : 0.35649E-02 0.20446E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 5.604574716e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29426E+08 1 0.17892E-09 0.24272E+02 0.19116E+04 c Velocity[X] 0.12677E+02 c Velocity[Y] 0.11595E+02 c Velocity[Z] 0.12147E-05 c Pressure 0.17426E-03 83 0.80562E-04 0.17556E-02 0.26765E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -22.951 35.833 5.6062 7.9968 v Velocity[Y] -25.55 26.706 -0.14453 -0.0025688 v Velocity[Z] -2.978 3.0325 2.6627e-06 -5.3879e-08 v ǁVelocityǁ 0.00049802 35.942 7.6879 8.08 v Pressure -1.4486e+05 2.381e+05 46658 22886 v TurbVisc 3.0685e-20 0.014607 0.0001656 2.3997e-05 v CourantNb 3.8319e-08 0.011721 0.00016806 4.9311e-06 v FourierNb 1.2425e-07 0.04651 0.00014618 2.9659e-07 v total_pressure -43538 3.3943e+05 1.4798e+05 1.2421e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0446 0.10049 0.0028377 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2473e-07 0.0518 0.00031424 5.2277e-06 INSTANT 0.875822000E-01 TIME STEP NUMBER 56020 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282726779E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.773552664E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.49113E-02 0.20824E+01 Friction velocity uk : 0.49113E-02 0.20824E+01 Dimensionless distance yplus : 0.47750E-02 0.20447E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 5.311529984e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29426E+08 1 0.17893E-09 0.24292E+02 0.19123E+04 c Velocity[X] 0.12691E+02 c Velocity[Y] 0.11602E+02 c Velocity[Z] 0.12203E-05 c Pressure 0.17158E-03 262 0.93031E-04 0.17276E-02 0.24561E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -22.959 35.848 5.6063 7.9969 v Velocity[Y] -25.56 26.716 -0.14454 -0.0025868 v Velocity[Z] -2.9778 3.0327 2.662e-06 -5.3879e-08 v ǁVelocityǁ 0.00047097 35.957 7.6895 8.0803 v Pressure -1.4349e+05 2.3968e+05 48105 23660 v TurbVisc 3.1344e-20 0.014626 0.00016566 2.4036e-05 v CourantNb 4.6075e-08 0.011721 0.00016807 4.9312e-06 v FourierNb 1.2425e-07 0.046508 0.00014618 2.9686e-07 v total_pressure -42163 3.4101e+05 1.4943e+05 1.2498e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0447 0.10049 0.0028379 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2477e-07 0.051798 0.00031425 5.228e-06 INSTANT 0.875823000E-01 TIME STEP NUMBER 56021 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282731618E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.773884949E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.37159E-02 0.20824E+01 Friction velocity uk : 0.37159E-02 0.20824E+01 Dimensionless distance yplus : 0.36492E-02 0.20448E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 5.062273408e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29426E+08 1 0.17893E-09 0.24305E+02 0.19127E+04 c Velocity[X] 0.12705E+02 c Velocity[Y] 0.11600E+02 c Velocity[Z] 0.12277E-05 c Pressure 0.16886E-03 160 0.78894E-04 0.16993E-02 0.23496E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -22.967 35.863 5.6063 7.997 v Velocity[Y] -25.57 26.727 -0.14454 -0.0026035 v Velocity[Z] -2.9776 3.0329 2.6612e-06 -5.3879e-08 v ǁVelocityǁ 0.00045767 35.973 7.6911 8.0805 v Pressure -1.4218e+05 2.412e+05 49520 24472 v TurbVisc 2.4337e-20 0.014645 0.00016571 2.4076e-05 v CourantNb 5.3334e-08 0.01172 0.00016807 4.9313e-06 v FourierNb 1.2425e-07 0.046505 0.00014618 2.9713e-07 v total_pressure -40850 3.4252e+05 1.5084e+05 1.258e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0448 0.10049 0.0028379 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.248e-07 0.051795 0.00031425 5.2284e-06 INSTANT 0.875824000E-01 TIME STEP NUMBER 56022 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282736430E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.774227919E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.37589E-02 0.20825E+01 Friction velocity uk : 0.37589E-02 0.20825E+01 Dimensionless distance yplus : 0.36914E-02 0.20448E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 4.836880221e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29427E+08 1 0.17894E-09 0.24329E+02 0.19136E+04 c Velocity[X] 0.12720E+02 c Velocity[Y] 0.11609E+02 c Velocity[Z] 0.12423E-05 c Pressure 0.16391E-03 9 0.56154E-04 0.16486E-02 0.18615E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -22.976 35.879 5.6064 7.9971 v Velocity[Y] -25.58 26.738 -0.14455 -0.0026196 v Velocity[Z] -2.9774 3.0331 2.6605e-06 -5.3879e-08 v ǁVelocityǁ 0.00046005 35.988 7.6927 8.0807 v Pressure -1.4096e+05 2.4265e+05 50889 25144 v TurbVisc 3.0696e-20 0.014664 0.00016577 2.4115e-05 v CourantNb 6.0136e-08 0.01172 0.00016807 4.9314e-06 v FourierNb 1.2425e-07 0.046502 0.00014618 2.974e-07 v total_pressure -39635 3.4397e+05 1.5221e+05 1.2647e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0448 0.10049 0.0028381 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2484e-07 0.051793 0.00031425 5.2288e-06 INSTANT 0.875825000E-01 TIME STEP NUMBER 56023 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282741399E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.774581294E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.81437E-02 0.20825E+01 Friction velocity uk : 0.81437E-02 0.20825E+01 Dimensionless distance yplus : 0.78957E-02 0.20449E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 4.623492538e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29427E+08 1 0.17894E-09 0.24345E+02 0.19141E+04 c Velocity[X] 0.12735E+02 c Velocity[Y] 0.11610E+02 c Velocity[Z] 0.12451E-05 c Pressure 0.16140E-03 121 0.99796E-04 0.16225E-02 0.22994E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -22.984 35.894 5.6065 7.9972 v Velocity[Y] -25.59 26.749 -0.14456 -0.0026362 v Velocity[Z] -2.9772 3.0333 2.6598e-06 -5.3879e-08 v ǁVelocityǁ 0.00046558 36.004 7.6942 8.081 v Pressure -1.397e+05 2.4418e+05 52232 25978 v TurbVisc 1.423e-20 0.014683 0.00016583 2.4154e-05 v CourantNb 6.5691e-08 0.011719 0.00016807 4.9315e-06 v FourierNb 1.2425e-07 0.046499 0.00014619 2.9767e-07 v total_pressure -38372 3.4551e+05 1.5356e+05 1.273e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0449 0.10049 0.0028382 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2487e-07 0.051791 0.00031426 5.2292e-06 INSTANT 0.875826000E-01 TIME STEP NUMBER 56024 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282746483E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.774945534E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.45622E-02 0.20826E+01 Friction velocity uk : 0.45622E-02 0.20826E+01 Dimensionless distance yplus : 0.44233E-02 0.20449E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 4.499708670e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29428E+08 1 0.17895E-09 0.24364E+02 0.19148E+04 c Velocity[X] 0.12749E+02 c Velocity[Y] 0.11615E+02 c Velocity[Z] 0.12416E-05 c Pressure 0.15775E-03 34 0.82814E-04 0.15849E-02 0.18687E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -22.993 35.909 5.6065 7.9973 v Velocity[Y] -25.6 26.76 -0.14456 -0.0026536 v Velocity[Z] -2.977 3.0335 2.6591e-06 -5.388e-08 v ǁVelocityǁ 0.00045406 36.019 7.6958 8.0812 v Pressure -1.385e+05 2.4558e+05 53565 26682 v TurbVisc 3.5477e-20 0.014702 0.00016589 2.4194e-05 v CourantNb 7.294e-08 0.011719 0.00016808 4.9316e-06 v FourierNb 1.2425e-07 0.046496 0.00014619 2.9794e-07 v total_pressure -37178 3.4691e+05 1.5489e+05 1.2801e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0449 0.10049 0.0028383 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2491e-07 0.051788 0.00031426 5.2295e-06 INSTANT 0.875827000E-01 TIME STEP NUMBER 56025 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282751684E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.775317422E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.32882E-02 0.20826E+01 Friction velocity uk : 0.32882E-02 0.20826E+01 Dimensionless distance yplus : 0.31881E-02 0.20450E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 4.317601054e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29428E+08 1 0.17895E-09 0.24389E+02 0.19157E+04 c Velocity[X] 0.12764E+02 c Velocity[Y] 0.11625E+02 c Velocity[Z] 0.12535E-05 c Pressure 0.15381E-03 9 0.53386E-04 0.15445E-02 0.16977E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -23.001 35.925 5.6066 7.9974 v Velocity[Y] -25.61 26.772 -0.14457 -0.0026723 v Velocity[Z] -2.9768 3.0336 2.6584e-06 -5.388e-08 v ǁVelocityǁ 0.0004408 36.035 7.6974 8.0814 v Pressure -1.3735e+05 2.4695e+05 54863 27324 v TurbVisc 2.3567e-20 0.014721 0.00016595 2.4234e-05 v CourantNb 7.8444e-08 0.011719 0.00016808 4.9317e-06 v FourierNb 1.2425e-07 0.046493 0.00014619 2.9821e-07 v total_pressure -36020 3.4827e+05 1.5619e+05 1.2865e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.045 0.10049 0.0028385 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2495e-07 0.051785 0.00031427 5.2299e-06 INSTANT 0.875828000E-01 TIME STEP NUMBER 56026 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282757074E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.775695667E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.60352E-02 0.20826E+01 Friction velocity uk : 0.60352E-02 0.20826E+01 Dimensionless distance yplus : 0.58514E-02 0.20450E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 4.187329464e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29429E+08 1 0.17896E-09 0.24406E+02 0.19163E+04 c Velocity[X] 0.12780E+02 c Velocity[Y] 0.11626E+02 c Velocity[Z] 0.12575E-05 c Pressure 0.15130E-03 28 0.99264E-04 0.15185E-02 0.21765E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -23.01 35.94 5.6066 7.9975 v Velocity[Y] -25.62 26.783 -0.14457 -0.0026898 v Velocity[Z] -2.9766 3.0338 2.6576e-06 -5.388e-08 v ǁVelocityǁ 0.000435 36.051 7.699 8.0817 v Pressure -1.362e+05 2.4837e+05 56107 28147 v TurbVisc 1.7e-20 0.01474 0.00016601 2.4274e-05 v CourantNb 8.3247e-08 0.011718 0.00016808 4.9318e-06 v FourierNb 1.2425e-07 0.04649 0.00014619 2.9849e-07 v total_pressure -34878 3.497e+05 1.5743e+05 1.2947e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.045 0.10049 0.0028386 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2499e-07 0.051783 0.00031427 5.2303e-06 INSTANT 0.875829000E-01 TIME STEP NUMBER 56027 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282762495E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.776082670E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.80414E-02 0.20827E+01 Friction velocity uk : 0.80414E-02 0.20827E+01 Dimensionless distance yplus : 0.78065E-02 0.20450E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 4.062637696e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29429E+08 1 0.17896E-09 0.24426E+02 0.19170E+04 c Velocity[X] 0.12795E+02 c Velocity[Y] 0.11631E+02 c Velocity[Z] 0.12567E-05 c Pressure 0.14753E-03 221 0.84667E-04 0.14798E-02 0.17945E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -23.018 35.956 5.6067 7.9977 v Velocity[Y] -25.631 26.794 -0.14458 -0.0027072 v Velocity[Z] -2.9764 3.034 2.6569e-06 -5.388e-08 v ǁVelocityǁ 0.00043161 36.066 7.7006 8.0819 v Pressure -1.3512e+05 2.4969e+05 57336 28860 v TurbVisc 1.6357e-20 0.014759 0.00016607 2.4314e-05 v CourantNb 8.7996e-08 0.011718 0.00016808 4.9319e-06 v FourierNb 1.2425e-07 0.046486 0.00014619 2.9876e-07 v total_pressure -33795 3.5102e+05 1.5866e+05 1.3018e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.045 0.1005 0.0028388 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2502e-07 0.05178 0.00031428 5.2307e-06 INSTANT 0.875830000E-01 TIME STEP NUMBER 56028 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282768037E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.776479189E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.45993E-02 0.20827E+01 Friction velocity uk : 0.45993E-02 0.20827E+01 Dimensionless distance yplus : 0.46036E-02 0.20450E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 4.038563833e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29430E+08 1 0.17897E-09 0.24451E+02 0.19179E+04 c Velocity[X] 0.12811E+02 c Velocity[Y] 0.11641E+02 c Velocity[Z] 0.12707E-05 c Pressure 0.14345E-03 9 0.56259E-04 0.14381E-02 0.15181E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -23.027 35.972 5.6067 7.9978 v Velocity[Y] -25.641 26.806 -0.14458 -0.0027239 v Velocity[Z] -2.9762 3.0342 2.6562e-06 -5.388e-08 v ǁVelocityǁ 0.0004248 36.082 7.7021 8.0821 v Pressure -1.341e+05 2.5096e+05 58525 29447 v TurbVisc 1.6661e-20 0.014778 0.00016613 2.4353e-05 v CourantNb 8.2996e-08 0.011717 0.00016809 4.932e-06 v FourierNb 1.2425e-07 0.046483 0.00014619 2.9903e-07 v total_pressure -32774 3.5228e+05 1.5985e+05 1.3077e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.045 0.10049 0.0028389 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2506e-07 0.051777 0.00031428 5.2311e-06 INSTANT 0.875831000E-01 TIME STEP NUMBER 56029 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282773664E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.776882146E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.69284E-02 0.20827E+01 Friction velocity uk : 0.69284E-02 0.20827E+01 Dimensionless distance yplus : 0.67260E-02 0.20450E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 3.908169204e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29430E+08 1 0.17897E-09 0.24471E+02 0.19186E+04 c Velocity[X] 0.12826E+02 c Velocity[Y] 0.11646E+02 c Velocity[Z] 0.12773E-05 c Pressure 0.14098E-03 175 0.77788E-04 0.14125E-02 0.18701E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -23.035 35.988 5.6068 7.9979 v Velocity[Y] -25.651 26.817 -0.14459 -0.0027425 v Velocity[Z] -2.976 3.0344 2.6555e-06 -5.388e-08 v ǁVelocityǁ 0.00042364 36.098 7.7037 8.0824 v Pressure -1.3307e+05 2.5226e+05 59642 30090 v TurbVisc 1.3688e-20 0.014797 0.00016619 2.4393e-05 v CourantNb 7.9437e-08 0.011717 0.00016809 4.9321e-06 v FourierNb 1.2425e-07 0.04648 0.0001462 2.993e-07 v total_pressure -31745 3.5359e+05 1.6097e+05 1.3142e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.045 0.10049 0.002839 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.251e-07 0.051774 0.00031428 5.2314e-06 INSTANT 0.875832000E-01 TIME STEP NUMBER 56030 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282779454E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.777293748E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.69386E-02 0.20827E+01 Friction velocity uk : 0.69386E-02 0.20827E+01 Dimensionless distance yplus : 0.67360E-02 0.20451E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 3.943009528e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29431E+08 1 0.17898E-09 0.24495E+02 0.19194E+04 c Velocity[X] 0.12842E+02 c Velocity[Y] 0.11653E+02 c Velocity[Z] 0.12780E-05 c Pressure 0.13757E-03 416 0.82860E-04 0.13776E-02 0.19426E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -23.044 36.003 5.6069 7.998 v Velocity[Y] -25.662 26.828 -0.14459 -0.0027591 v Velocity[Z] -2.9758 3.0346 2.6548e-06 -5.388e-08 v ǁVelocityǁ 0.00042156 36.114 7.7053 8.0826 v Pressure -1.321e+05 2.5348e+05 60781 30779 v TurbVisc 5.2244e-20 0.014816 0.00016625 2.4433e-05 v CourantNb 7.4193e-08 0.011717 0.00016809 4.9322e-06 v FourierNb 1.2425e-07 0.046476 0.0001462 2.9958e-07 v total_pressure -30778 3.548e+05 1.6211e+05 1.321e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0451 0.1005 0.0028391 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2514e-07 0.051771 0.00031429 5.2318e-06 INSTANT 0.875833000E-01 TIME STEP NUMBER 56031 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282785223E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.777713814E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.62716E-02 0.20827E+01 Friction velocity uk : 0.62716E-02 0.20827E+01 Dimensionless distance yplus : 0.60884E-02 0.20451E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 3.898415493e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29431E+08 1 0.17899E-09 0.24518E+02 0.19202E+04 c Velocity[X] 0.12856E+02 c Velocity[Y] 0.11662E+02 c Velocity[Z] 0.12828E-05 c Pressure 0.13459E-03 462 0.96456E-04 0.13470E-02 0.15501E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -23.053 36.019 5.6069 7.9981 v Velocity[Y] -25.672 26.84 -0.14459 -0.0027789 v Velocity[Z] -2.9756 3.0348 2.654e-06 -5.388e-08 v ǁVelocityǁ 0.00042017 36.13 7.7069 8.0829 v Pressure -1.3123e+05 2.5462e+05 61807 31196 v TurbVisc 5.382e-20 0.014835 0.00016631 2.4473e-05 v CourantNb 6.9755e-08 0.011716 0.00016809 4.9324e-06 v FourierNb 1.2425e-07 0.046473 0.0001462 2.9985e-07 v total_pressure -29901 3.5594e+05 1.6313e+05 1.3252e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0451 0.1005 0.0028392 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2518e-07 0.051768 0.00031429 5.2322e-06 INSTANT 0.875834000E-01 TIME STEP NUMBER 56032 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282791278E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.778139193E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.54019E-02 0.20828E+01 Friction velocity uk : 0.54019E-02 0.20828E+01 Dimensionless distance yplus : 0.52441E-02 0.20451E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 3.930597108e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29432E+08 1 0.17900E-09 0.24531E+02 0.19207E+04 c Velocity[X] 0.12872E+02 c Velocity[Y] 0.11660E+02 c Velocity[Z] 0.12924E-05 c Pressure 0.13158E-03 490 0.81851E-04 0.13161E-02 0.17838E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -23.061 36.035 5.607 7.9982 v Velocity[Y] -25.682 26.852 -0.1446 -0.0027968 v Velocity[Z] -2.9753 3.0349 2.6533e-06 -5.388e-08 v ǁVelocityǁ 0.00041934 36.146 7.7085 8.0831 v Pressure -1.3031e+05 2.558e+05 62864 31887 v TurbVisc 4.2848e-20 0.014854 0.00016637 2.4514e-05 v CourantNb 6.5289e-08 0.011716 0.0001681 4.9325e-06 v FourierNb 1.2425e-07 0.04647 0.0001462 3.0013e-07 v total_pressure -28988 3.5713e+05 1.6419e+05 1.3321e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0451 0.1005 0.0028393 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2522e-07 0.051765 0.0003143 5.2326e-06 INSTANT 0.875835000E-01 TIME STEP NUMBER 56033 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282797305E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.778574872E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.42136E-02 0.20828E+01 Friction velocity uk : 0.42136E-02 0.20828E+01 Dimensionless distance yplus : 0.40905E-02 0.20451E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 3.989415713e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29433E+08 1 0.17900E-09 0.24557E+02 0.19216E+04 c Velocity[X] 0.12887E+02 c Velocity[Y] 0.11670E+02 c Velocity[Z] 0.13025E-05 c Pressure 0.12564E-03 9 0.56579E-04 0.12560E-02 0.12088E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -23.07 36.051 5.607 7.9983 v Velocity[Y] -25.693 26.863 -0.1446 -0.0028138 v Velocity[Z] -2.9751 3.0351 2.6526e-06 -5.388e-08 v ǁVelocityǁ 0.0004185 36.163 7.7101 8.0834 v Pressure -1.2952e+05 2.5688e+05 63850 32370 v TurbVisc 4.7917e-20 0.014873 0.00016643 2.4554e-05 v CourantNb 6.0594e-08 0.011716 0.0001681 4.9326e-06 v FourierNb 1.2425e-07 0.046466 0.0001462 3.0041e-07 v total_pressure -28195 3.5821e+05 1.6518e+05 1.3369e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0451 0.1005 0.0028395 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2526e-07 0.051762 0.0003143 5.233e-06 INSTANT 0.875836000E-01 TIME STEP NUMBER 56034 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282803442E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.779016841E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.28020E-02 0.20828E+01 Friction velocity uk : 0.28020E-02 0.20828E+01 Dimensionless distance yplus : 0.27201E-02 0.20451E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 4.089563293e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29433E+08 1 0.17901E-09 0.24578E+02 0.19223E+04 c Velocity[X] 0.12902E+02 c Velocity[Y] 0.11676E+02 c Velocity[Z] 0.13085E-05 c Pressure 0.12325E-03 251 0.77876E-04 0.12314E-02 0.16357E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -23.079 36.068 5.6071 7.9985 v Velocity[Y] -25.703 26.875 -0.1446 -0.0028332 v Velocity[Z] -2.9749 3.0353 2.6519e-06 -5.388e-08 v ǁVelocityǁ 0.00041846 36.179 7.7117 8.0837 v Pressure -1.2867e+05 2.5803e+05 64793 32937 v TurbVisc 5.8428e-20 0.014892 0.0001665 2.4594e-05 v CourantNb 5.6239e-08 0.011715 0.0001681 4.9327e-06 v FourierNb 1.2425e-07 0.046463 0.0001462 3.0068e-07 v total_pressure -27344 3.5935e+05 1.6612e+05 1.3426e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0451 0.10051 0.0028396 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.253e-07 0.051759 0.00031431 5.2334e-06 INSTANT 0.875837000E-01 TIME STEP NUMBER 56035 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282809712E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.779465070E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.48819E-02 0.20828E+01 Friction velocity uk : 0.48819E-02 0.20828E+01 Dimensionless distance yplus : 0.47393E-02 0.20451E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 4.202923081e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29434E+08 1 0.17902E-09 0.24601E+02 0.19232E+04 c Velocity[X] 0.12918E+02 c Velocity[Y] 0.11683E+02 c Velocity[Z] 0.13182E-05 c Pressure 0.11995E-03 65 0.83598E-04 0.11978E-02 0.15155E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -23.088 36.084 5.6071 7.9986 v Velocity[Y] -25.714 26.887 -0.1446 -0.0028505 v Velocity[Z] -2.9747 3.0355 2.6512e-06 -5.388e-08 v ǁVelocityǁ 0.00041825 36.195 7.7133 8.0839 v Pressure -1.2795e+05 2.5902e+05 65711 33439 v TurbVisc 5.4531e-20 0.014911 0.00016656 2.4634e-05 v CourantNb 5.0563e-08 0.011715 0.00016811 4.9328e-06 v FourierNb 1.2425e-07 0.046459 0.00014621 3.0096e-07 v total_pressure -26626 3.6035e+05 1.6704e+05 1.3476e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0451 0.10052 0.0028398 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2534e-07 0.051756 0.00031431 5.2338e-06 INSTANT 0.875838000E-01 TIME STEP NUMBER 56036 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282815910E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.779918619E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.66213E-02 0.20828E+01 Friction velocity uk : 0.66213E-02 0.20828E+01 Dimensionless distance yplus : 0.64279E-02 0.20451E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 4.327787023e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29434E+08 1 0.17903E-09 0.24624E+02 0.19240E+04 c Velocity[X] 0.12932E+02 c Velocity[Y] 0.11692E+02 c Velocity[Z] 0.13203E-05 c Pressure 0.11708E-03 187 0.97043E-04 0.11685E-02 0.14797E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -23.097 36.1 5.6072 7.9987 v Velocity[Y] -25.724 26.899 -0.1446 -0.0028704 v Velocity[Z] -2.9745 3.0357 2.6505e-06 -5.388e-08 v ǁVelocityǁ 0.00041821 36.212 7.7149 8.0842 v Pressure -1.2721e+05 2.6004e+05 66585 33889 v TurbVisc 5.2459e-20 0.01493 0.00016662 2.4674e-05 v CourantNb 4.524e-08 0.011714 0.00016811 4.9329e-06 v FourierNb 1.2425e-07 0.046456 0.00014621 3.0123e-07 v total_pressure -25883 3.6136e+05 1.6791e+05 1.3521e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0451 0.10054 0.00284 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2538e-07 0.051753 0.00031432 5.2342e-06 INSTANT 0.875839000E-01 TIME STEP NUMBER 56037 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282822425E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.780377098E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.81614E-02 0.20828E+01 Friction velocity uk : 0.81614E-02 0.20828E+01 Dimensionless distance yplus : 0.79230E-02 0.20451E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 4.469755763e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29435E+08 1 0.17904E-09 0.24638E+02 0.19244E+04 c Velocity[X] 0.12947E+02 c Velocity[Y] 0.11690E+02 c Velocity[Z] 0.13272E-05 c Pressure 0.11436E-03 91 0.82239E-04 0.11408E-02 0.13389E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -23.106 36.116 5.6073 7.9989 v Velocity[Y] -25.735 26.91 -0.14461 -0.002889 v Velocity[Z] -2.9743 3.0359 2.6498e-06 -5.388e-08 v ǁVelocityǁ 0.00041807 36.228 7.7165 8.0844 v Pressure -1.2656e+05 2.6101e+05 67420 34404 v TurbVisc 5.6763e-20 0.014949 0.00016669 2.4715e-05 v CourantNb 4.0744e-08 0.011714 0.00016811 4.933e-06 v FourierNb 1.2425e-07 0.046452 0.00014621 3.0151e-07 v total_pressure -25230 3.6233e+05 1.6874e+05 1.3573e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0451 0.10055 0.0028403 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2542e-07 0.051749 0.00031432 5.2345e-06 INSTANT 0.875840000E-01 TIME STEP NUMBER 56038 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282828868E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.780842165E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.95819E-02 0.20828E+01 Friction velocity uk : 0.95819E-02 0.20828E+01 Dimensionless distance yplus : 0.93020E-02 0.20451E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 4.663993026e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29435E+08 1 0.17905E-09 0.24663E+02 0.19253E+04 c Velocity[X] 0.12962E+02 c Velocity[Y] 0.11701E+02 c Velocity[Z] 0.13357E-05 c Pressure 0.10814E-03 9 0.56376E-04 0.10781E-02 0.88158E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -23.115 36.133 5.6073 7.999 v Velocity[Y] -25.746 26.922 -0.14461 -0.0029068 v Velocity[Z] -2.9741 3.0361 2.649e-06 -5.388e-08 v ǁVelocityǁ 0.00041794 36.245 7.7181 8.0847 v Pressure -1.2598e+05 2.6189e+05 68191 34746 v TurbVisc 5.802e-20 0.014968 0.00016675 2.4756e-05 v CourantNb 4.0804e-08 0.011714 0.00016811 4.9332e-06 v FourierNb 1.2425e-07 0.046449 0.00014621 3.0179e-07 v total_pressure -24655 3.6322e+05 1.6952e+05 1.3607e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0451 0.10056 0.0028405 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2546e-07 0.051746 0.00031433 5.2349e-06 INSTANT 0.875841000E-01 TIME STEP NUMBER 56039 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282835374E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.781313544E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11050E-01 0.20828E+01 Friction velocity uk : 0.11050E-01 0.20828E+01 Dimensionless distance yplus : 0.10727E-01 0.20452E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 4.918729898e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29436E+08 1 0.17905E-09 0.24683E+02 0.19260E+04 c Velocity[X] 0.12976E+02 c Velocity[Y] 0.11707E+02 c Velocity[Z] 0.13446E-05 c Pressure 0.10616E-03 167 0.78122E-04 0.10577E-02 0.13365E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -23.124 36.149 5.6074 7.9991 v Velocity[Y] -25.756 26.934 -0.14461 -0.0029268 v Velocity[Z] -2.9739 3.0362 2.6483e-06 -5.388e-08 v ǁVelocityǁ 0.00041793 36.261 7.7197 8.085 v Pressure -1.2536e+05 2.6283e+05 68935 35193 v TurbVisc 6.2522e-20 0.014987 0.00016681 2.4796e-05 v CourantNb 4.1006e-08 0.011713 0.00016812 4.9333e-06 v FourierNb 1.2425e-07 0.046445 0.00014621 3.0207e-07 v total_pressure -24033 3.6415e+05 1.7026e+05 1.3652e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0452 0.10057 0.0028407 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.255e-07 0.051744 0.00031433 5.2353e-06 INSTANT 0.875842000E-01 TIME STEP NUMBER 56040 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282842032E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.781790675E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12355E-01 0.20829E+01 Friction velocity uk : 0.12355E-01 0.20829E+01 Dimensionless distance yplus : 0.11994E-01 0.20452E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 5.094583786e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29437E+08 1 0.17906E-09 0.24706E+02 0.19268E+04 c Velocity[X] 0.12992E+02 c Velocity[Y] 0.11715E+02 c Velocity[Z] 0.13555E-05 c Pressure 0.10316E-03 43 0.83779E-04 0.10273E-02 0.13073E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -23.133 36.166 5.6075 7.9992 v Velocity[Y] -25.767 26.946 -0.14461 -0.0029448 v Velocity[Z] -2.9737 3.0364 2.6476e-06 -5.388e-08 v ǁVelocityǁ 0.00041786 36.278 7.7213 8.0852 v Pressure -1.2485e+05 2.6365e+05 69649 35601 v TurbVisc 5.7607e-20 0.015006 0.00016688 2.4837e-05 v CourantNb 4.1002e-08 0.011713 0.00016812 4.9334e-06 v FourierNb 1.2425e-07 0.046442 0.00014622 3.0235e-07 v total_pressure -23521 3.6497e+05 1.7097e+05 1.3693e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0452 0.10058 0.002841 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2555e-07 0.05174 0.00031433 5.2357e-06 INSTANT 0.875843000E-01 TIME STEP NUMBER 56041 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282848592E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.782272693E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13660E-01 0.20829E+01 Friction velocity uk : 0.13660E-01 0.20829E+01 Dimensionless distance yplus : 0.13261E-01 0.20452E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 5.350147063e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29437E+08 1 0.17907E-09 0.24729E+02 0.19276E+04 c Velocity[X] 0.13005E+02 c Velocity[Y] 0.11724E+02 c Velocity[Z] 0.13577E-05 c Pressure 0.10075E-03 396 0.97485E-04 0.10027E-02 0.12727E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -23.142 36.182 5.6076 7.9994 v Velocity[Y] -25.778 26.958 -0.14461 -0.0029655 v Velocity[Z] -2.9735 3.0366 2.6469e-06 -5.388e-08 v ǁVelocityǁ 0.00041785 36.295 7.7229 8.0855 v Pressure -1.2433e+05 2.6446e+05 70308 35922 v TurbVisc 5.9042e-20 0.015025 0.00016694 2.4877e-05 v CourantNb 4.1137e-08 0.011712 0.00016812 4.9335e-06 v FourierNb 1.2425e-07 0.046438 0.00014622 3.0263e-07 v total_pressure -23006 3.6579e+05 1.7163e+05 1.3725e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0452 0.10059 0.0028412 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2559e-07 0.051738 0.00031434 5.2361e-06 INSTANT 0.875844000E-01 TIME STEP NUMBER 56042 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282855435E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.782757843E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.14918E-01 0.20830E+01 Friction velocity uk : 0.14918E-01 0.20830E+01 Dimensionless distance yplus : 0.14482E-01 0.20453E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 5.615685556e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29438E+08 1 0.17909E-09 0.24742E+02 0.19280E+04 c Velocity[X] 0.13019E+02 c Velocity[Y] 0.11722E+02 c Velocity[Z] 0.13641E-05 c Pressure 0.98577E-04 98 0.82766E-04 0.98052E-03 0.10689E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -23.151 36.199 5.6076 7.9995 v Velocity[Y] -25.788 26.97 -0.14462 -0.0029845 v Velocity[Z] -2.9733 3.0368 2.6462e-06 -5.388e-08 v ǁVelocityǁ 0.00041778 36.311 7.7245 8.0858 v Pressure -1.239e+05 2.6523e+05 70930 36313 v TurbVisc 4.8389e-20 0.015044 0.00016701 2.4919e-05 v CourantNb 4.1277e-08 0.011712 0.00016813 4.9336e-06 v FourierNb 1.2425e-07 0.046435 0.00014622 3.0291e-07 v total_pressure -22570 3.6656e+05 1.7225e+05 1.3764e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0453 0.1006 0.0028414 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2563e-07 0.051735 0.00031434 5.2365e-06 INSTANT 0.875845000E-01 TIME STEP NUMBER 56043 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282862206E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.783247754E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10792E-01 0.20830E+01 Friction velocity uk : 0.10792E-01 0.20830E+01 Dimensionless distance yplus : 0.10456E-01 0.20453E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 5.887965308e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29438E+08 1 0.17910E-09 0.24767E+02 0.19289E+04 c Velocity[X] 0.13033E+02 c Velocity[Y] 0.11733E+02 c Velocity[Z] 0.13821E-05 c Pressure 0.92332E-04 15 0.57366E-04 0.91788E-03 0.65233E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -23.161 36.216 5.6077 7.9997 v Velocity[Y] -25.799 26.983 -0.14462 -0.0030029 v Velocity[Z] -2.973 3.037 2.6455e-06 -5.388e-08 v ǁVelocityǁ 0.00041685 36.328 7.7261 8.086 v Pressure -1.2355e+05 2.6591e+05 71480 36539 v TurbVisc 5.5257e-20 0.015063 0.00016707 2.496e-05 v CourantNb 4.3651e-08 0.011712 0.00016813 4.9337e-06 v FourierNb 1.2425e-07 0.046432 0.00014622 3.0319e-07 v total_pressure -22221 3.6724e+05 1.728e+05 1.3786e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0453 0.10061 0.0028416 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2568e-07 0.051732 0.00031435 5.2369e-06 INSTANT 0.875846000E-01 TIME STEP NUMBER 56044 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282869008E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.783742433E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.48291E-02 0.20831E+01 Friction velocity uk : 0.48291E-02 0.20831E+01 Dimensionless distance yplus : 0.46791E-02 0.20454E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 6.254734775e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29439E+08 1 0.17911E-09 0.24786E+02 0.19296E+04 c Velocity[X] 0.13047E+02 c Velocity[Y] 0.11740E+02 c Velocity[Z] 0.13846E-05 c Pressure 0.91184E-04 561 0.79252E-04 0.90595E-03 0.11134E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -23.17 36.232 5.6078 7.9998 v Velocity[Y] -25.81 26.995 -0.14462 -0.0030239 v Velocity[Z] -2.9728 3.0372 2.6448e-06 -5.388e-08 v ǁVelocityǁ 0.00041764 36.345 7.7277 8.0863 v Pressure -1.2316e+05 2.6664e+05 72019 36846 v TurbVisc 5.3393e-21 0.015082 0.00016714 2.5e-05 v CourantNb 5.162e-08 0.011711 0.00016813 4.9339e-06 v FourierNb 1.2425e-07 0.046429 0.00014622 3.0347e-07 v total_pressure -21830 3.6796e+05 1.7334e+05 1.3817e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0454 0.10061 0.0028418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2572e-07 0.05173 0.00031435 5.2373e-06 INSTANT 0.875847000E-01 TIME STEP NUMBER 56045 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282875940E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.784242310E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.28659E-02 0.20832E+01 Friction velocity uk : 0.28659E-02 0.20832E+01 Dimensionless distance yplus : 0.28331E-02 0.20455E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 6.449021206e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29440E+08 1 0.17912E-09 0.24808E+02 0.19303E+04 c Velocity[X] 0.13061E+02 c Velocity[Y] 0.11747E+02 c Velocity[Z] 0.13874E-05 c Pressure 0.88932E-04 382 0.85101E-04 0.88307E-03 0.12179E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -23.179 36.249 5.6079 7.9999 v Velocity[Y] -25.821 27.007 -0.14463 -0.0030419 v Velocity[Z] -2.9726 3.0374 2.6441e-06 -5.388e-08 v ǁVelocityǁ 0.00041753 36.362 7.7293 8.0866 v Pressure -1.2283e+05 2.6728e+05 72522 37189 v TurbVisc 5.0219e-20 0.015101 0.0001672 2.5042e-05 v CourantNb 6.1689e-08 0.011711 0.00016814 4.934e-06 v FourierNb 1.2425e-07 0.046425 0.00014622 3.0375e-07 v total_pressure -21509 3.6861e+05 1.7385e+05 1.3851e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0455 0.10061 0.002842 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2576e-07 0.051727 0.00031436 5.2377e-06 INSTANT 0.875848000E-01 TIME STEP NUMBER 56046 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282882790E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.784743949E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.51038E-02 0.20833E+01 Friction velocity uk : 0.51038E-02 0.20833E+01 Dimensionless distance yplus : 0.50280E-02 0.20456E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 6.799000848e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29440E+08 1 0.17913E-09 0.24830E+02 0.19311E+04 c Velocity[X] 0.13073E+02 c Velocity[Y] 0.11757E+02 c Velocity[Z] 0.13934E-05 c Pressure 0.87433E-04 123 0.98910E-04 0.86768E-03 0.11384E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -23.188 36.266 5.608 8.0001 v Velocity[Y] -25.832 27.019 -0.14463 -0.0030635 v Velocity[Z] -2.9724 3.0375 2.6433e-06 -5.388e-08 v ǁVelocityǁ 0.00041759 36.379 7.731 8.0869 v Pressure -1.2259e+05 2.6783e+05 72928 37275 v TurbVisc 5.4704e-20 0.015119 0.00016727 2.5083e-05 v CourantNb 7.1328e-08 0.01171 0.00016814 4.9341e-06 v FourierNb 1.2425e-07 0.046422 0.00014622 3.0403e-07 v total_pressure -21270 3.6916e+05 1.7425e+05 1.386e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0456 0.10063 0.0028424 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2581e-07 0.051724 0.00031436 5.2381e-06 INSTANT 0.875849000E-01 TIME STEP NUMBER 56047 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282889854E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.785247830E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.54320E-02 0.20834E+01 Friction velocity uk : 0.54320E-02 0.20834E+01 Dimensionless distance yplus : 0.54500E-02 0.20457E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 7.129704881e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29441E+08 1 0.17914E-09 0.24841E+02 0.19314E+04 c Velocity[X] 0.13086E+02 c Velocity[Y] 0.11755E+02 c Velocity[Z] 0.13999E-05 c Pressure 0.86240E-04 172 0.84215E-04 0.85536E-03 0.93831E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -23.198 36.283 5.608 8.0002 v Velocity[Y] -25.843 27.032 -0.14464 -0.0030833 v Velocity[Z] -2.9722 3.0377 2.6426e-06 -5.388e-08 v ǁVelocityǁ 0.00041739 36.396 7.7326 8.0871 v Pressure -1.2237e+05 2.6841e+05 73346 37592 v TurbVisc 3.4183e-20 0.015138 0.00016734 2.5124e-05 v CourantNb 8.1437e-08 0.01171 0.00016814 4.9342e-06 v FourierNb 1.2425e-07 0.046419 0.00014623 3.0432e-07 v total_pressure -21041 3.6973e+05 1.7467e+05 1.3892e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0457 0.10066 0.0028429 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2585e-07 0.051722 0.00031437 5.2386e-06 INSTANT 0.875850000E-01 TIME STEP NUMBER 56048 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282896837E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.785756664E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11081E-01 0.20835E+01 Friction velocity uk : 0.11081E-01 0.20835E+01 Dimensionless distance yplus : 0.11118E-01 0.20459E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 7.455074061e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29442E+08 1 0.17916E-09 0.24865E+02 0.19323E+04 c Velocity[X] 0.13099E+02 c Velocity[Y] 0.11766E+02 c Velocity[Z] 0.14123E-05 c Pressure 0.80323E-04 7 0.58083E-04 0.79621E-03 0.47213E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -23.207 36.3 5.6081 8.0003 v Velocity[Y] -25.854 27.044 -0.14464 -0.0031024 v Velocity[Z] -2.972 3.0379 2.6419e-06 -5.388e-08 v ǁVelocityǁ 0.0004172 36.413 7.7342 8.0874 v Pressure -1.2224e+05 2.6888e+05 73652 37693 v TurbVisc 5.9178e-20 0.015157 0.0001674 2.5166e-05 v CourantNb 8.5075e-08 0.01171 0.00016815 4.9344e-06 v FourierNb 1.2425e-07 0.046417 0.00014623 3.046e-07 v total_pressure -20914 3.702e+05 1.7498e+05 1.3902e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0459 0.10068 0.0028434 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.259e-07 0.05172 0.00031437 5.239e-06 INSTANT 0.875851000E-01 TIME STEP NUMBER 56049 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282903819E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.786268101E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12110E-01 0.20837E+01 Friction velocity uk : 0.12110E-01 0.20837E+01 Dimensionless distance yplus : 0.11747E-01 0.20460E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 7.883692400e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29442E+08 1 0.17917E-09 0.24884E+02 0.19329E+04 c Velocity[X] 0.13111E+02 c Velocity[Y] 0.11773E+02 c Velocity[Z] 0.14139E-05 c Pressure 0.80527E-04 68 0.80487E-04 0.79778E-03 0.94357E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -23.217 36.316 5.6082 8.0005 v Velocity[Y] -25.865 27.057 -0.14465 -0.0031237 v Velocity[Z] -2.9718 3.0381 2.6412e-06 -5.3881e-08 v ǁVelocityǁ 0.00041766 36.43 7.7359 8.0877 v Pressure -1.2206e+05 2.6938e+05 74003 37872 v TurbVisc 6.1515e-20 0.015176 0.00016747 2.5207e-05 v CourantNb 8.6588e-08 0.011709 0.00016815 4.9345e-06 v FourierNb 1.2425e-07 0.046414 0.00014623 3.0489e-07 v total_pressure -20738 3.707e+05 1.7533e+05 1.392e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.046 0.10071 0.0028439 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2594e-07 0.051718 0.00031438 5.2394e-06 INSTANT 0.875852000E-01 TIME STEP NUMBER 56050 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282910960E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.786785358E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.94353E-02 0.20839E+01 Friction velocity uk : 0.94353E-02 0.20839E+01 Dimensionless distance yplus : 0.90835E-02 0.20462E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 8.076536658e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29443E+08 1 0.17918E-09 0.24904E+02 0.19336E+04 c Velocity[X] 0.13124E+02 c Velocity[Y] 0.11780E+02 c Velocity[Z] 0.14188E-05 c Pressure 0.79523E-04 379 0.86535E-04 0.78738E-03 0.10459E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -23.226 36.333 5.6083 8.0006 v Velocity[Y] -25.876 27.069 -0.14465 -0.0031427 v Velocity[Z] -2.9716 3.0383 2.6405e-06 -5.3881e-08 v ǁVelocityǁ 0.00041869 36.447 7.7375 8.088 v Pressure -1.2198e+05 2.6979e+05 74264 38083 v TurbVisc 5.3221e-20 0.015195 0.00016754 2.5249e-05 v CourantNb 8.2206e-08 0.011709 0.00016815 4.9346e-06 v FourierNb 1.2425e-07 0.046411 0.00014623 3.0517e-07 v total_pressure -20653 3.7112e+05 1.7559e+05 1.3941e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0462 0.10073 0.0028444 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2599e-07 0.051716 0.00031438 5.2398e-06 INSTANT 0.875853000E-01 TIME STEP NUMBER 56051 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282917961E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.787300112E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.44196E-02 0.20840E+01 Friction velocity uk : 0.44196E-02 0.20840E+01 Dimensionless distance yplus : 0.42548E-02 0.20464E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 8.471460918e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29444E+08 1 0.17920E-09 0.24916E+02 0.19340E+04 c Velocity[X] 0.13134E+02 c Velocity[Y] 0.11782E+02 c Velocity[Z] 0.14205E-05 c Pressure 0.79406E-04 54 0.75175E-04 0.78577E-03 0.59254E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -23.236 36.35 5.6084 8.0008 v Velocity[Y] -25.887 27.082 -0.14466 -0.0031637 v Velocity[Z] -2.9713 3.0385 2.6398e-06 -5.3881e-08 v ǁVelocityǁ 0.00042072 36.464 7.7391 8.0882 v Pressure -1.2197e+05 2.7012e+05 74442 38063 v TurbVisc 5.5844e-20 0.015214 0.00016761 2.529e-05 v CourantNb 8.1532e-08 0.011708 0.00016816 4.9347e-06 v FourierNb 1.2425e-07 0.046409 0.00014623 3.0545e-07 v total_pressure -20645 3.7144e+05 1.7577e+05 1.3939e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0464 0.10075 0.0028448 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2603e-07 0.051714 0.00031439 5.2402e-06 INSTANT 0.875854000E-01 TIME STEP NUMBER 56052 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282925074E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.787817120E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.32025E-02 0.20843E+01 Friction velocity uk : 0.32025E-02 0.20843E+01 Dimensionless distance yplus : 0.31663E-02 0.20466E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 8.837963334e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29444E+08 1 0.17921E-09 0.24939E+02 0.19347E+04 c Velocity[X] 0.13146E+02 c Velocity[Y] 0.11793E+02 c Velocity[Z] 0.14273E-05 c Pressure 0.75154E-04 7 0.52293E-04 0.74326E-03 0.37385E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -23.245 36.367 5.6085 8.0009 v Velocity[Y] -25.898 27.094 -0.14467 -0.0031855 v Velocity[Z] -2.9711 3.0386 2.6391e-06 -5.3881e-08 v ǁVelocityǁ 0.00042119 36.481 7.7408 8.0885 v Pressure -1.2198e+05 2.7042e+05 74572 38093 v TurbVisc 6.3142e-20 0.015233 0.00016768 2.5331e-05 v CourantNb 8.0394e-08 0.011708 0.00016816 4.9349e-06 v FourierNb 1.2425e-07 0.046406 0.00014623 3.0574e-07 v total_pressure -20660 3.7175e+05 1.759e+05 1.3942e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0466 0.10077 0.0028452 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2608e-07 0.051713 0.00031439 5.2406e-06 INSTANT 0.875855000E-01 TIME STEP NUMBER 56053 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282932255E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.788338197E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.89488E-02 0.20845E+01 Friction velocity uk : 0.89488E-02 0.20845E+01 Dimensionless distance yplus : 0.86305E-02 0.20468E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 9.272174259e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29445E+08 1 0.17923E-09 0.24953E+02 0.19352E+04 c Velocity[X] 0.13158E+02 c Velocity[Y] 0.11795E+02 c Velocity[Z] 0.14318E-05 c Pressure 0.76340E-04 83 0.97065E-04 0.75456E-03 0.53712E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -23.255 36.384 5.6087 8.0011 v Velocity[Y] -25.909 27.107 -0.14468 -0.0032065 v Velocity[Z] -2.9709 3.0388 2.6384e-06 -5.3881e-08 v ǁVelocityǁ 0.0004238 36.498 7.7424 8.0888 v Pressure -1.2198e+05 2.7074e+05 74778 38302 v TurbVisc 6.1042e-20 0.015252 0.00016774 2.5374e-05 v CourantNb 7.9436e-08 0.011708 0.00016816 4.935e-06 v FourierNb 1.2425e-07 0.046404 0.00014623 3.0603e-07 v total_pressure -20655 3.7206e+05 1.761e+05 1.3963e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0468 0.10079 0.0028456 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2612e-07 0.051711 0.0003144 5.241e-06 INSTANT 0.875856000E-01 TIME STEP NUMBER 56054 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282939426E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.788864562E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.34294E-02 0.20847E+01 Friction velocity uk : 0.34294E-02 0.20847E+01 Dimensionless distance yplus : 0.33074E-02 0.20470E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 9.468119862e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29446E+08 1 0.17924E-09 0.24970E+02 0.19357E+04 c Velocity[X] 0.13169E+02 c Velocity[Y] 0.11801E+02 c Velocity[Z] 0.14368E-05 c Pressure 0.75633E-04 46 0.81031E-04 0.74714E-03 0.23149E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -23.264 36.401 5.6088 8.0012 v Velocity[Y] -25.92 27.12 -0.14468 -0.0032273 v Velocity[Z] -2.9707 3.039 2.6377e-06 -5.3881e-08 v ǁVelocityǁ 0.00041903 36.516 7.7441 8.0891 v Pressure -1.2211e+05 2.7093e+05 74813 38288 v TurbVisc 6.5698e-20 0.015271 0.00016781 2.5416e-05 v CourantNb 7.7634e-08 0.011707 0.00016817 4.9351e-06 v FourierNb 1.2425e-07 0.046402 0.00014623 3.0632e-07 v total_pressure -20781 3.7226e+05 1.7614e+05 1.3961e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.047 0.10081 0.002846 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2617e-07 0.05171 0.0003144 5.2414e-06 INSTANT 0.875857000E-01 TIME STEP NUMBER 56055 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282946552E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.789384839E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.43189E-02 0.20850E+01 Friction velocity uk : 0.43189E-02 0.20850E+01 Dimensionless distance yplus : 0.41653E-02 0.20473E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 9.902518366e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29446E+08 1 0.17926E-09 0.24991E+02 0.19365E+04 c Velocity[X] 0.13180E+02 c Velocity[Y] 0.11811E+02 c Velocity[Z] 0.14445E-05 c Pressure 0.74722E-04 6 0.51039E-04 0.73771E-03 0.35223E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -23.274 36.418 5.6089 8.0013 v Velocity[Y] -25.931 27.132 -0.14469 -0.0032475 v Velocity[Z] -2.9705 3.0392 2.637e-06 -5.3881e-08 v ǁVelocityǁ 0.00041711 36.533 7.7457 8.0893 v Pressure -1.2224e+05 2.7109e+05 74824 38263 v TurbVisc 6.5415e-20 0.01529 0.00016788 2.5457e-05 v CourantNb 7.6693e-08 0.011707 0.00016817 4.9352e-06 v FourierNb 1.2425e-07 0.0464 0.00014624 3.066e-07 v total_pressure -20917 3.7241e+05 1.7615e+05 1.3959e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0473 0.10083 0.0028464 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2622e-07 0.051709 0.00031441 5.2418e-06 INSTANT 0.875858000E-01 TIME STEP NUMBER 56056 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282953639E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.789910254E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.31481E-02 0.20852E+01 Friction velocity uk : 0.31481E-02 0.20852E+01 Dimensionless distance yplus : 0.30361E-02 0.20475E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.017583762e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29447E+08 1 0.17927E-09 0.25004E+02 0.19369E+04 c Velocity[X] 0.13189E+02 c Velocity[Y] 0.11814E+02 c Velocity[Z] 0.14477E-05 c Pressure 0.77006E-04 350 0.97525E-04 0.75982E-03 0.27412E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -23.284 36.435 5.609 8.0015 v Velocity[Y] -25.942 27.145 -0.1447 -0.0032683 v Velocity[Z] -2.9703 3.0394 2.6363e-06 -5.3881e-08 v ǁVelocityǁ 0.00041677 36.55 7.7474 8.0896 v Pressure -1.2244e+05 2.7122e+05 74829 38214 v TurbVisc 6.4809e-20 0.015308 0.00016795 2.5499e-05 v CourantNb 7.5255e-08 0.011706 0.00016817 4.9354e-06 v FourierNb 1.2425e-07 0.046398 0.00014624 3.0689e-07 v total_pressure -21116 3.7255e+05 1.7615e+05 1.3954e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0475 0.10085 0.0028468 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2626e-07 0.051708 0.00031441 5.2423e-06 INSTANT 0.875859000E-01 TIME STEP NUMBER 56057 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282960775E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.790437470E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.34132E-02 0.20855E+01 Friction velocity uk : 0.34132E-02 0.20855E+01 Dimensionless distance yplus : 0.33109E-02 0.20478E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.059598454e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29447E+08 1 0.17929E-09 0.25020E+02 0.19374E+04 c Velocity[X] 0.13199E+02 c Velocity[Y] 0.11821E+02 c Velocity[Z] 0.14514E-05 c Pressure 0.77305E-04 35 0.82481E-04 0.76233E-03 0.31437E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -23.293 36.452 5.6091 8.0016 v Velocity[Y] -25.954 27.158 -0.14472 -0.0032901 v Velocity[Z] -2.9701 3.0396 2.6356e-06 -5.3881e-08 v ǁVelocityǁ 0.00042004 36.567 7.749 8.0899 v Pressure -1.2266e+05 2.7127e+05 74745 38128 v TurbVisc 5.7528e-20 0.015327 0.00016802 2.5541e-05 v CourantNb 7.3696e-08 0.011706 0.00016818 4.9355e-06 v FourierNb 1.2425e-07 0.046396 0.00014624 3.0718e-07 v total_pressure -21339 3.7259e+05 1.7607e+05 1.3945e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0478 0.10088 0.0028474 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2631e-07 0.051707 0.00031442 5.2427e-06 INSTANT 0.875860000E-01 TIME STEP NUMBER 56058 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282967918E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.790962908E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.85332E-02 0.20858E+01 Friction velocity uk : 0.85332E-02 0.20858E+01 Dimensionless distance yplus : 0.82297E-02 0.20481E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.085379722e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29448E+08 1 0.17931E-09 0.25039E+02 0.19381E+04 c Velocity[X] 0.13209E+02 c Velocity[Y] 0.11831E+02 c Velocity[Z] 0.14635E-05 c Pressure 0.77390E-04 7 0.52944E-04 0.76273E-03 0.36956E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -23.303 36.469 5.6093 8.0018 v Velocity[Y] -25.965 27.171 -0.14473 -0.0033127 v Velocity[Z] -2.9699 3.0397 2.6349e-06 -5.3881e-08 v ǁVelocityǁ 0.0004316 36.584 7.7507 8.0902 v Pressure -1.2291e+05 2.713e+05 74665 38095 v TurbVisc 6.6985e-20 0.015346 0.00016809 2.5583e-05 v CourantNb 7.2495e-08 0.011705 0.00016818 4.9356e-06 v FourierNb 1.2425e-07 0.046394 0.00014624 3.0747e-07 v total_pressure -21580 3.7263e+05 1.7599e+05 1.3942e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0481 0.10091 0.0028478 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2636e-07 0.051706 0.00031442 5.2431e-06 INSTANT 0.875861000E-01 TIME STEP NUMBER 56059 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282975131E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.791490626E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11478E-01 0.20861E+01 Friction velocity uk : 0.11478E-01 0.20861E+01 Dimensionless distance yplus : 0.11069E-01 0.20484E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.114957937e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29449E+08 1 0.17932E-09 0.25055E+02 0.19386E+04 c Velocity[X] 0.13218E+02 c Velocity[Y] 0.11836E+02 c Velocity[Z] 0.14637E-05 c Pressure 0.80669E-04 49 0.75730E-04 0.79457E-03 0.83201E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -23.313 36.486 5.6094 8.0019 v Velocity[Y] -25.976 27.184 -0.14474 -0.0033334 v Velocity[Z] -2.9696 3.0399 2.6342e-06 -5.3881e-08 v ǁVelocityǁ 0.0004423 36.601 7.7524 8.0905 v Pressure -1.2326e+05 2.7123e+05 74436 37946 v TurbVisc 5.2435e-20 0.015365 0.00016816 2.5626e-05 v CourantNb 7.0291e-08 0.011705 0.00016819 4.9358e-06 v FourierNb 1.2425e-07 0.046392 0.00014624 3.0776e-07 v total_pressure -21932 3.7256e+05 1.7576e+05 1.3927e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0484 0.10093 0.0028483 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2641e-07 0.051705 0.00031443 5.2435e-06 INSTANT 0.875862000E-01 TIME STEP NUMBER 56060 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282982152E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.792015751E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.66030E-02 0.20864E+01 Friction velocity uk : 0.66030E-02 0.20864E+01 Dimensionless distance yplus : 0.66091E-02 0.20487E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.156457635e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29449E+08 1 0.17934E-09 0.25072E+02 0.19391E+04 c Velocity[X] 0.13227E+02 c Velocity[Y] 0.11845E+02 c Velocity[Z] 0.14640E-05 c Pressure 0.82715E-04 30 0.80109E-04 0.81426E-03 0.90504E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -23.322 36.503 5.6095 8.0021 v Velocity[Y] -25.988 27.197 -0.14475 -0.0033563 v Velocity[Z] -2.9694 3.0401 2.6334e-06 -5.3881e-08 v ǁVelocityǁ 0.00046334 36.619 7.754 8.0907 v Pressure -1.2359e+05 2.7116e+05 74258 37798 v TurbVisc 3.6728e-20 0.015384 0.00016823 2.5668e-05 v CourantNb 6.2066e-08 0.011704 0.00016819 4.9359e-06 v FourierNb 1.2425e-07 0.04639 0.00014624 3.0805e-07 v total_pressure -22268 3.7248e+05 1.7558e+05 1.3912e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0487 0.10095 0.0028486 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2645e-07 0.051704 0.00031443 5.2439e-06 INSTANT 0.875863000E-01 TIME STEP NUMBER 56061 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282989356E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.792547516E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.29007E-02 0.20868E+01 Friction velocity uk : 0.29007E-02 0.20868E+01 Dimensionless distance yplus : 0.28660E-02 0.20490E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.180973224e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29450E+08 1 0.17936E-09 0.25088E+02 0.19397E+04 c Velocity[X] 0.13236E+02 c Velocity[Y] 0.11851E+02 c Velocity[Z] 0.14699E-05 c Pressure 0.85538E-04 77 0.93222E-04 0.84156E-03 0.10109E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -23.332 36.52 5.6096 8.0022 v Velocity[Y] -25.999 27.21 -0.14477 -0.0033771 v Velocity[Z] -2.9692 3.0403 2.6327e-06 -5.3881e-08 v ǁVelocityǁ 0.00049024 36.636 7.7557 8.091 v Pressure -1.2401e+05 2.7101e+05 74008 37671 v TurbVisc 5.8044e-20 0.015403 0.0001683 2.5711e-05 v CourantNb 3.3386e-08 0.011704 0.00016819 4.936e-06 v FourierNb 1.2425e-07 0.046388 0.00014624 3.0834e-07 v total_pressure -22680 3.7234e+05 1.7533e+05 1.39e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.049 0.10097 0.002849 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.265e-07 0.051703 0.00031444 5.2443e-06 INSTANT 0.875864000E-01 TIME STEP NUMBER 56062 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282996326E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.793076360E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11736E-01 0.20871E+01 Friction velocity uk : 0.11736E-01 0.20871E+01 Dimensionless distance yplus : 0.11361E-01 0.20494E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.209153790e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29451E+08 1 0.17938E-09 0.25095E+02 0.19398E+04 c Velocity[X] 0.13243E+02 c Velocity[Y] 0.11852E+02 c Velocity[Z] 0.14748E-05 c Pressure 0.88587E-04 67 0.78970E-04 0.87104E-03 0.77349E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -23.342 36.537 5.6098 8.0023 v Velocity[Y] -26.011 27.223 -0.14478 -0.0033993 v Velocity[Z] -2.969 3.0405 2.632e-06 -5.3881e-08 v ǁVelocityǁ 0.0005236 36.653 7.7574 8.0913 v Pressure -1.2445e+05 2.7081e+05 73696 37421 v TurbVisc 7.6333e-20 0.015422 0.00016837 2.5753e-05 v CourantNb 4.3245e-08 0.011704 0.0001682 4.9361e-06 v FourierNb 1.2425e-07 0.046387 0.00014624 3.0863e-07 v total_pressure -23121 3.7213e+05 1.7502e+05 1.3875e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0494 0.101 0.0028494 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2655e-07 0.051703 0.00031444 5.2448e-06 INSTANT 0.875865000E-01 TIME STEP NUMBER 56063 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283003405E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.793605082E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10316E-01 0.20874E+01 Friction velocity uk : 0.10316E-01 0.20874E+01 Dimensionless distance yplus : 0.99862E-02 0.20497E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.234422839e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29451E+08 1 0.17939E-09 0.25113E+02 0.19405E+04 c Velocity[X] 0.13251E+02 c Velocity[Y] 0.11862E+02 c Velocity[Z] 0.14830E-05 c Pressure 0.87706E-04 7 0.53726E-04 0.86188E-03 0.48193E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -23.352 36.554 5.6099 8.0025 v Velocity[Y] -26.022 27.236 -0.14479 -0.0034227 v Velocity[Z] -2.9688 3.0407 2.6313e-06 -5.3881e-08 v ǁVelocityǁ 0.00057898 36.67 7.7591 8.0916 v Pressure -1.2489e+05 2.7059e+05 73389 37282 v TurbVisc 7.8207e-20 0.01544 0.00016844 2.5795e-05 v CourantNb 5.9391e-08 0.011703 0.0001682 4.9363e-06 v FourierNb 1.2425e-07 0.046385 0.00014624 3.0892e-07 v total_pressure -23568 3.7192e+05 1.7471e+05 1.3861e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0497 0.10102 0.0028497 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.266e-07 0.051702 0.00031445 5.2452e-06 INSTANT 0.875866000E-01 TIME STEP NUMBER 56064 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283010500E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.794133726E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10846E-01 0.20878E+01 Friction velocity uk : 0.10846E-01 0.20878E+01 Dimensionless distance yplus : 0.10500E-01 0.20500E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.260933932e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29452E+08 1 0.17941E-09 0.25127E+02 0.19409E+04 c Velocity[X] 0.13260E+02 c Velocity[Y] 0.11867E+02 c Velocity[Z] 0.14868E-05 c Pressure 0.91907E-04 57 0.75232E-04 0.90263E-03 0.98317E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -23.362 36.571 5.61 8.0026 v Velocity[Y] -26.034 27.249 -0.14481 -0.0034441 v Velocity[Z] -2.9686 3.0408 2.6306e-06 -5.3881e-08 v ǁVelocityǁ 0.00060878 36.687 7.7607 8.0919 v Pressure -1.2545e+05 2.7026e+05 72956 37007 v TurbVisc 4.4464e-20 0.015459 0.00016851 2.5838e-05 v CourantNb 5.537e-08 0.011703 0.00016821 4.9364e-06 v FourierNb 1.2425e-07 0.046383 0.00014624 3.0922e-07 v total_pressure -24126 3.7158e+05 1.7428e+05 1.3833e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.05 0.10104 0.00285 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2665e-07 0.051701 0.00031445 5.2456e-06 INSTANT 0.875867000E-01 TIME STEP NUMBER 56065 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283017412E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.794659137E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.93268E-03 0.20881E+01 Friction velocity uk : 0.93268E-03 0.20881E+01 Dimensionless distance yplus : 0.90273E-03 0.20504E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.276617852e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29453E+08 1 0.17943E-09 0.25142E+02 0.19414E+04 c Velocity[X] 0.13266E+02 c Velocity[Y] 0.11876E+02 c Velocity[Z] 0.14848E-05 c Pressure 0.95075E-04 65 0.80361E-04 0.93319E-03 0.10868E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -23.372 36.589 5.6102 8.0028 v Velocity[Y] -26.045 27.262 -0.14482 -0.0034678 v Velocity[Z] -2.9683 3.041 2.6299e-06 -5.3881e-08 v ǁVelocityǁ 0.00065734 36.705 7.7624 8.0921 v Pressure -1.26e+05 2.6991e+05 72527 36708 v TurbVisc 8.0055e-20 0.015478 0.00016858 2.5881e-05 v CourantNb 5.1901e-08 0.011702 0.00016821 4.9365e-06 v FourierNb 1.2425e-07 0.046381 0.00014624 3.0951e-07 v total_pressure -24677 3.7124e+05 1.7385e+05 1.3803e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0504 0.10105 0.0028502 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2669e-07 0.051701 0.00031446 5.246e-06 INSTANT 0.875868000E-01 TIME STEP NUMBER 56066 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283024467E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.795187471E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.69241E-02 0.20885E+01 Friction velocity uk : 0.69241E-02 0.20885E+01 Dimensionless distance yplus : 0.68191E-02 0.20507E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.297756701e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29453E+08 1 0.17945E-09 0.25156E+02 0.19418E+04 c Velocity[X] 0.13274E+02 c Velocity[Y] 0.11882E+02 c Velocity[Z] 0.14897E-05 c Pressure 0.98784E-04 113 0.93631E-04 0.96903E-03 0.11283E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -23.382 36.606 5.6103 8.0029 v Velocity[Y] -26.057 27.276 -0.14484 -0.0034892 v Velocity[Z] -2.9681 3.0412 2.6292e-06 -5.3881e-08 v ǁVelocityǁ 0.00070954 36.722 7.7641 8.0924 v Pressure -1.2664e+05 2.695e+05 72048 36461 v TurbVisc 8.273e-20 0.015497 0.00016866 2.5924e-05 v CourantNb 4.7526e-08 0.011702 0.00016822 4.9366e-06 v FourierNb 1.2425e-07 0.04638 0.00014625 3.0981e-07 v total_pressure -25313 3.7083e+05 1.7337e+05 1.3779e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0507 0.10106 0.0028506 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2674e-07 0.0517 0.00031446 5.2465e-06 INSTANT 0.875869000E-01 TIME STEP NUMBER 56067 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283031277E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.795714086E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.44345E-02 0.20888E+01 Friction velocity uk : 0.44345E-02 0.20888E+01 Dimensionless distance yplus : 0.42900E-02 0.20510E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.313985463e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29454E+08 1 0.17947E-09 0.25161E+02 0.19419E+04 c Velocity[X] 0.13279E+02 c Velocity[Y] 0.11882E+02 c Velocity[Z] 0.14947E-05 c Pressure 0.10263E-03 87 0.79523E-04 0.10062E-02 0.10405E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -23.392 36.623 5.6104 8.003 v Velocity[Y] -26.068 27.289 -0.14486 -0.0035122 v Velocity[Z] -2.9679 3.0414 2.6285e-06 -5.3881e-08 v ǁVelocityǁ 0.00076534 36.739 7.7658 8.0927 v Pressure -1.2728e+05 2.6903e+05 71504 36059 v TurbVisc 8.6117e-20 0.015516 0.00016873 2.5966e-05 v CourantNb 4.3881e-08 0.011701 0.00016822 4.9368e-06 v FourierNb 1.2425e-07 0.046378 0.00014625 3.101e-07 v total_pressure -25955 3.7035e+05 1.7283e+05 1.3738e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.051 0.10108 0.0028509 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2679e-07 0.051699 0.00031447 5.2469e-06 INSTANT 0.875870000E-01 TIME STEP NUMBER 56068 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283038169E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.796239280E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.67303E-02 0.20892E+01 Friction velocity uk : 0.67303E-02 0.20892E+01 Dimensionless distance yplus : 0.64753E-02 0.20514E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.325721703e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29455E+08 1 0.17949E-09 0.25178E+02 0.19425E+04 c Velocity[X] 0.13286E+02 c Velocity[Y] 0.11892E+02 c Velocity[Z] 0.15041E-05 c Pressure 0.10297E-03 12 0.54988E-04 0.10089E-02 0.66791E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -23.402 36.64 5.6106 8.0032 v Velocity[Y] -26.08 27.302 -0.14487 -0.0035364 v Velocity[Z] -2.9677 3.0416 2.6278e-06 -5.3881e-08 v ǁVelocityǁ 0.00083104 36.756 7.7674 8.093 v Pressure -1.2793e+05 2.6856e+05 70957 35801 v TurbVisc 8.7351e-20 0.015534 0.0001688 2.6009e-05 v CourantNb 4.8426e-08 0.011701 0.00016822 4.9369e-06 v FourierNb 1.2425e-07 0.046376 0.00014625 3.1039e-07 v total_pressure -26603 3.6988e+05 1.7228e+05 1.3713e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0514 0.10111 0.0028514 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2684e-07 0.051698 0.00031447 5.2473e-06 INSTANT 0.875871000E-01 TIME STEP NUMBER 56069 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283045041E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.796763176E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.33838E-02 0.20895E+01 Friction velocity uk : 0.33838E-02 0.20895E+01 Dimensionless distance yplus : 0.32556E-02 0.20517E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.333371818e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29455E+08 1 0.17951E-09 0.25189E+02 0.19428E+04 c Velocity[X] 0.13292E+02 c Velocity[Y] 0.11897E+02 c Velocity[Z] 0.15082E-05 c Pressure 0.10765E-03 238 0.76027E-04 0.10541E-02 0.12177E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -23.412 36.657 5.6107 8.0033 v Velocity[Y] -26.092 27.315 -0.14489 -0.0035584 v Velocity[Z] -2.9675 3.0417 2.6271e-06 -5.3881e-08 v ǁVelocityǁ 0.00088217 36.773 7.7691 8.0932 v Pressure -1.287e+05 2.6794e+05 70321 35387 v TurbVisc 2.2144e-21 0.015553 0.00016887 2.6053e-05 v CourantNb 5.2392e-08 0.0117 0.00016823 4.937e-06 v FourierNb 1.2425e-07 0.046374 0.00014625 3.1069e-07 v total_pressure -27375 3.6927e+05 1.7165e+05 1.3671e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0517 0.10113 0.0028519 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2689e-07 0.051697 0.00031448 5.2477e-06 INSTANT 0.875872000E-01 TIME STEP NUMBER 56070 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283051743E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.797283633E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.79329E-02 0.20898E+01 Friction velocity uk : 0.79329E-02 0.20898E+01 Dimensionless distance yplus : 0.76323E-02 0.20520E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.338383849e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29456E+08 1 0.17953E-09 0.25202E+02 0.19432E+04 c Velocity[X] 0.13297E+02 c Velocity[Y] 0.11905E+02 c Velocity[Z] 0.15105E-05 c Pressure 0.11136E-03 63 0.81216E-04 0.10898E-02 0.12461E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -23.422 36.674 5.6108 8.0034 v Velocity[Y] -26.104 27.329 -0.14491 -0.0035829 v Velocity[Z] -2.9673 3.0419 2.6264e-06 -5.3881e-08 v ǁVelocityǁ 0.00094125 36.791 7.7708 8.0935 v Pressure -1.2944e+05 2.6736e+05 69665 34994 v TurbVisc 7.9148e-21 0.015572 0.00016894 2.6096e-05 v CourantNb 4.4522e-08 0.0117 0.00016823 4.9372e-06 v FourierNb 1.2425e-07 0.046372 0.00014625 3.1098e-07 v total_pressure -28114 3.6869e+05 1.7099e+05 1.3632e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.052 0.10115 0.0028524 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2694e-07 0.051697 0.00031448 5.2481e-06 INSTANT 0.875873000E-01 TIME STEP NUMBER 56071 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283058567E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.797805157E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.59535E-02 0.20901E+01 Friction velocity uk : 0.59535E-02 0.20901E+01 Dimensionless distance yplus : 0.58451E-02 0.20523E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.339359804e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29456E+08 1 0.17955E-09 0.25214E+02 0.19436E+04 c Velocity[X] 0.13304E+02 c Velocity[Y] 0.11911E+02 c Velocity[Z] 0.15158E-05 c Pressure 0.11545E-03 229 0.94775E-04 0.11292E-02 0.13662E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -23.432 36.691 5.611 8.0036 v Velocity[Y] -26.115 27.342 -0.14492 -0.003605 v Velocity[Z] -2.967 3.0421 2.6257e-06 -5.3881e-08 v ǁVelocityǁ 0.0010011 36.808 7.7725 8.0938 v Pressure -1.3029e+05 2.6667e+05 68950 34576 v TurbVisc 4.4803e-20 0.015591 0.00016902 2.6139e-05 v CourantNb 4.5215e-08 0.011699 0.00016824 4.9373e-06 v FourierNb 1.2425e-07 0.04637 0.00014625 3.1128e-07 v total_pressure -28962 3.6799e+05 1.7027e+05 1.359e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0523 0.10116 0.0028529 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2699e-07 0.051696 0.00031449 5.2486e-06 INSTANT 0.875874000E-01 TIME STEP NUMBER 56072 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283065103E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.798323822E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15711E-01 0.20904E+01 Friction velocity uk : 0.15711E-01 0.20904E+01 Dimensionless distance yplus : 0.15116E-01 0.20526E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.336256281e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29457E+08 1 0.17957E-09 0.25218E+02 0.19436E+04 c Velocity[X] 0.13308E+02 c Velocity[Y] 0.11910E+02 c Velocity[Z] 0.15196E-05 c Pressure 0.11965E-03 142 0.80441E-04 0.11696E-02 0.11939E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -23.442 36.708 5.6111 8.0037 v Velocity[Y] -26.127 27.355 -0.14494 -0.0036287 v Velocity[Z] -2.9668 3.0423 2.625e-06 -5.3881e-08 v ǁVelocityǁ 0.0010601 36.825 7.7742 8.0941 v Pressure -1.3112e+05 2.6597e+05 68203 34107 v TurbVisc 7.3135e-20 0.01561 0.00016909 2.6182e-05 v CourantNb 4.1787e-08 0.011699 0.00016824 4.9374e-06 v FourierNb 1.2425e-07 0.046368 0.00014625 3.1158e-07 v total_pressure -29790 3.6729e+05 1.6953e+05 1.3543e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0526 0.10119 0.0028535 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2704e-07 0.051694 0.00031449 5.249e-06 INSTANT 0.875875000E-01 TIME STEP NUMBER 56073 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283071728E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.798840401E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.17064E-01 0.20907E+01 Friction velocity uk : 0.17064E-01 0.20907E+01 Dimensionless distance yplus : 0.16566E-01 0.20529E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.328766577e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29458E+08 1 0.17960E-09 0.25232E+02 0.19441E+04 c Velocity[X] 0.13313E+02 c Velocity[Y] 0.11919E+02 c Velocity[Z] 0.15256E-05 c Pressure 0.12063E-03 9 0.55299E-04 0.11784E-02 0.98560E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -23.452 36.725 5.6112 8.0038 v Velocity[Y] -26.139 27.368 -0.14496 -0.0036536 v Velocity[Z] -2.9666 3.0425 2.6243e-06 -5.3882e-08 v ǁVelocityǁ 0.0011162 36.842 7.7759 8.0943 v Pressure -1.3196e+05 2.6522e+05 67419 33693 v TurbVisc 1.0044e-19 0.015628 0.00016916 2.6226e-05 v CourantNb 3.8445e-08 0.011698 0.00016824 4.9375e-06 v FourierNb 1.2425e-07 0.046366 0.00014625 3.1188e-07 v total_pressure -30631 3.6655e+05 1.6874e+05 1.3502e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0529 0.10121 0.002854 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2709e-07 0.051693 0.0003145 5.2494e-06 INSTANT 0.875876000E-01 TIME STEP NUMBER 56074 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283078278E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.799353805E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12351E-01 0.20910E+01 Friction velocity uk : 0.12351E-01 0.20910E+01 Dimensionless distance yplus : 0.11990E-01 0.20532E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.310751324e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29458E+08 1 0.17962E-09 0.25241E+02 0.19443E+04 c Velocity[X] 0.13318E+02 c Velocity[Y] 0.11924E+02 c Velocity[Z] 0.15277E-05 c Pressure 0.12541E-03 90 0.76478E-04 0.12245E-02 0.14363E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -23.462 36.742 5.6114 8.004 v Velocity[Y] -26.151 27.382 -0.14497 -0.0036764 v Velocity[Z] -2.9664 3.0427 2.6236e-06 -5.3882e-08 v ǁVelocityǁ 0.001174 36.86 7.7775 8.0946 v Pressure -1.3293e+05 2.6437e+05 66588 33185 v TurbVisc 5.9225e-20 0.015647 0.00016924 2.627e-05 v CourantNb 4.179e-08 0.011698 0.00016825 4.9377e-06 v FourierNb 1.2425e-07 0.046363 0.00014625 3.1218e-07 v total_pressure -31601 3.657e+05 1.6791e+05 1.3451e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0532 0.10123 0.0028545 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2714e-07 0.051692 0.0003145 5.2498e-06 INSTANT 0.875877000E-01 TIME STEP NUMBER 56075 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283084690E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.799863452E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11104E-01 0.20913E+01 Friction velocity uk : 0.11104E-01 0.20913E+01 Dimensionless distance yplus : 0.10779E-01 0.20534E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.299700770e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29459E+08 1 0.17964E-09 0.25253E+02 0.19447E+04 c Velocity[X] 0.13321E+02 c Velocity[Y] 0.11932E+02 c Velocity[Z] 0.15323E-05 c Pressure 0.12925E-03 65 0.82028E-04 0.12611E-02 0.16134E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -23.472 36.759 5.6115 8.0041 v Velocity[Y] -26.163 27.395 -0.14499 -0.0037016 v Velocity[Z] -2.9662 3.0428 2.623e-06 -5.3882e-08 v ǁVelocityǁ 0.0012281 36.877 7.7792 8.0949 v Pressure -1.3387e+05 2.6352e+05 65691 32603 v TurbVisc 1.0745e-19 0.015666 0.00016931 2.6313e-05 v CourantNb 4.0129e-08 0.011697 0.00016825 4.9378e-06 v FourierNb 1.2425e-07 0.046361 0.00014626 3.1247e-07 v total_pressure -32549 3.6484e+05 1.6702e+05 1.3393e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0534 0.10125 0.002855 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2719e-07 0.05169 0.00031451 5.2503e-06 INSTANT 0.875878000E-01 TIME STEP NUMBER 56076 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283091168E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.800371328E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.57210E-02 0.20915E+01 Friction velocity uk : 0.57210E-02 0.20915E+01 Dimensionless distance yplus : 0.56010E-02 0.20537E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.275858751e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29459E+08 1 0.17966E-09 0.25263E+02 0.19450E+04 c Velocity[X] 0.13326E+02 c Velocity[Y] 0.11937E+02 c Velocity[Z] 0.15373E-05 c Pressure 0.13344E-03 233 0.95641E-04 0.13013E-02 0.15709E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -23.482 36.776 5.6116 8.0042 v Velocity[Y] -26.175 27.408 -0.14501 -0.0037244 v Velocity[Z] -2.966 3.043 2.6223e-06 -5.3882e-08 v ǁVelocityǁ 0.0012815 36.894 7.7809 8.0951 v Pressure -1.3491e+05 2.6259e+05 64769 32090 v TurbVisc 1.1258e-19 0.015685 0.00016938 2.6357e-05 v CourantNb 4.3539e-08 0.011697 0.00016826 4.9379e-06 v FourierNb 1.2425e-07 0.046358 0.00014626 3.1278e-07 v total_pressure -33583 3.6391e+05 1.6609e+05 1.3342e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0537 0.10126 0.0028554 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2724e-07 0.051688 0.00031451 5.2507e-06 INSTANT 0.875879000E-01 TIME STEP NUMBER 56077 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283097348E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.800877078E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.16187E-01 0.20917E+01 Friction velocity uk : 0.16187E-01 0.20917E+01 Dimensionless distance yplus : 0.15727E-01 0.20539E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.249803972e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29460E+08 1 0.17969E-09 0.25264E+02 0.19449E+04 c Velocity[X] 0.13328E+02 c Velocity[Y] 0.11936E+02 c Velocity[Z] 0.15389E-05 c Pressure 0.13766E-03 77 0.81164E-04 0.13416E-02 0.14807E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -23.492 36.794 5.6117 8.0044 v Velocity[Y] -26.187 27.422 -0.14502 -0.0037489 v Velocity[Z] -2.9657 3.0432 2.6216e-06 -5.3882e-08 v ǁVelocityǁ 0.0013299 36.911 7.7826 8.0954 v Pressure -1.3592e+05 2.6165e+05 63812 31503 v TurbVisc 1.1571e-19 0.015704 0.00016946 2.64e-05 v CourantNb 4.5322e-08 0.011696 0.00016826 4.938e-06 v FourierNb 1.2425e-07 0.046355 0.00014626 3.1307e-07 v total_pressure -34596 3.6297e+05 1.6514e+05 1.3283e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0539 0.10128 0.0028559 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2729e-07 0.051687 0.00031452 5.2511e-06 INSTANT 0.875880000E-01 TIME STEP NUMBER 56078 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283103597E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.801379143E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10089E-01 0.20919E+01 Friction velocity uk : 0.10089E-01 0.20919E+01 Dimensionless distance yplus : 0.98023E-02 0.20541E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.219001804e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29460E+08 1 0.17971E-09 0.25277E+02 0.19453E+04 c Velocity[X] 0.13332E+02 c Velocity[Y] 0.11945E+02 c Velocity[Z] 0.15495E-05 c Pressure 0.13895E-03 9 0.56231E-04 0.13534E-02 0.12607E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -23.502 36.811 5.6118 8.0045 v Velocity[Y] -26.199 27.435 -0.14504 -0.0037745 v Velocity[Z] -2.9655 3.0434 2.6209e-06 -5.3882e-08 v ǁVelocityǁ 0.0013686 36.929 7.7843 8.0957 v Pressure -1.3695e+05 2.607e+05 62821 30979 v TurbVisc 1.192e-19 0.015722 0.00016953 2.6444e-05 v CourantNb 4.6146e-08 0.011696 0.00016827 4.9381e-06 v FourierNb 1.2425e-07 0.046352 0.00014626 3.1337e-07 v total_pressure -35622 3.6203e+05 1.6415e+05 1.323e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0541 0.1013 0.0028563 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2734e-07 0.051685 0.00031453 5.2515e-06 INSTANT 0.875881000E-01 TIME STEP NUMBER 56079 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283109754E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.801876746E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.55327E-02 0.20921E+01 Friction velocity uk : 0.55327E-02 0.20921E+01 Dimensionless distance yplus : 0.48848E-02 0.20543E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.172069093e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29461E+08 1 0.17973E-09 0.25285E+02 0.19455E+04 c Velocity[X] 0.13336E+02 c Velocity[Y] 0.11949E+02 c Velocity[Z] 0.15496E-05 c Pressure 0.14358E-03 166 0.77074E-04 0.13977E-02 0.17787E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -23.513 36.828 5.6119 8.0046 v Velocity[Y] -26.211 27.448 -0.14506 -0.003798 v Velocity[Z] -2.9653 3.0436 2.6202e-06 -5.3882e-08 v ǁVelocityǁ 0.0014193 36.946 7.7859 8.0959 v Pressure -1.3811e+05 2.5962e+05 61784 30334 v TurbVisc 6.5647e-20 0.015741 0.0001696 2.6488e-05 v CourantNb 5.2048e-08 0.011696 0.00016827 4.9383e-06 v FourierNb 1.2425e-07 0.046349 0.00014626 3.1368e-07 v total_pressure -36785 3.6095e+05 1.6311e+05 1.3166e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0543 0.10132 0.0028568 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2739e-07 0.051682 0.00031453 5.2519e-06 INSTANT 0.875882000E-01 TIME STEP NUMBER 56080 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283115757E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.802369317E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.14256E-01 0.20923E+01 Friction velocity uk : 0.14256E-01 0.20923E+01 Dimensionless distance yplus : 0.13851E-01 0.20545E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.145762869e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29462E+08 1 0.17976E-09 0.25294E+02 0.19458E+04 c Velocity[X] 0.13338E+02 c Velocity[Y] 0.11956E+02 c Velocity[Z] 0.15524E-05 c Pressure 0.14736E-03 62 0.82445E-04 0.14337E-02 0.18740E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -23.523 36.845 5.612 8.0047 v Velocity[Y] -26.223 27.462 -0.14507 -0.0038239 v Velocity[Z] -2.9651 3.0437 2.6195e-06 -5.3882e-08 v ǁVelocityǁ 0.0014585 36.963 7.7876 8.0962 v Pressure -1.3923e+05 2.5861e+05 60689 29664 v TurbVisc 6.3364e-20 0.01576 0.00016968 2.6532e-05 v CourantNb 5.207e-08 0.011695 0.00016827 4.9384e-06 v FourierNb 1.2425e-07 0.046346 0.00014626 3.1398e-07 v total_pressure -37906 3.5994e+05 1.6201e+05 1.3099e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0545 0.10136 0.0028573 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2744e-07 0.05168 0.00031454 5.2524e-06 INSTANT 0.875883000E-01 TIME STEP NUMBER 56081 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283121820E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.802859530E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.65685E-02 0.20925E+01 Friction velocity uk : 0.65685E-02 0.20925E+01 Dimensionless distance yplus : 0.64147E-02 0.20546E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.096740676e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29462E+08 1 0.17978E-09 0.25303E+02 0.19461E+04 c Velocity[X] 0.13342E+02 c Velocity[Y] 0.11961E+02 c Velocity[Z] 0.15558E-05 c Pressure 0.15140E-03 342 0.96283E-04 0.14721E-02 0.18762E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -23.533 36.862 5.6121 8.0048 v Velocity[Y] -26.235 27.475 -0.14509 -0.0038474 v Velocity[Z] -2.9649 3.0439 2.6188e-06 -5.3882e-08 v ǁVelocityǁ 0.0014952 36.981 7.7893 8.0964 v Pressure -1.4045e+05 2.5751e+05 59564 29026 v TurbVisc 7.0991e-20 0.015779 0.00016975 2.6576e-05 v CourantNb 4.2282e-08 0.011695 0.00016828 4.9385e-06 v FourierNb 1.2425e-07 0.046343 0.00014627 3.1428e-07 v total_pressure -39123 3.5884e+05 1.6089e+05 1.3035e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0546 0.10139 0.0028577 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2749e-07 0.051678 0.00031454 5.2528e-06 INSTANT 0.875884000E-01 TIME STEP NUMBER 56082 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283127554E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.803346101E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.42805E-02 0.20926E+01 Friction velocity uk : 0.42805E-02 0.20926E+01 Dimensionless distance yplus : 0.41802E-02 0.20548E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.047013646e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29463E+08 1 0.17980E-09 0.25302E+02 0.19459E+04 c Velocity[X] 0.13343E+02 c Velocity[Y] 0.11959E+02 c Velocity[Z] 0.15556E-05 c Pressure 0.15544E-03 79 0.81665E-04 0.15105E-02 0.18371E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -23.543 36.879 5.6122 8.005 v Velocity[Y] -26.247 27.488 -0.1451 -0.0038727 v Velocity[Z] -2.9646 3.0441 2.6181e-06 -5.3882e-08 v ǁVelocityǁ 0.0015274 36.998 7.791 8.0967 v Pressure -1.4165e+05 2.5638e+05 58408 28315 v TurbVisc 7.2602e-20 0.015797 0.00016982 2.662e-05 v CourantNb 2.7341e-08 0.011694 0.00016828 4.9386e-06 v FourierNb 1.2425e-07 0.046339 0.00014627 3.1458e-07 v total_pressure -40326 3.5771e+05 1.5973e+05 1.2964e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0548 0.10142 0.0028581 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2754e-07 0.051675 0.00031455 5.2532e-06 INSTANT 0.875885000E-01 TIME STEP NUMBER 56083 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283133339E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.803827604E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13457E-01 0.20928E+01 Friction velocity uk : 0.13457E-01 0.20928E+01 Dimensionless distance yplus : 0.13142E-01 0.20549E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 9.973726336e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29463E+08 1 0.17983E-09 0.25314E+02 0.19463E+04 c Velocity[X] 0.13346E+02 c Velocity[Y] 0.11968E+02 c Velocity[Z] 0.15678E-05 c Pressure 0.15681E-03 9 0.57319E-04 0.15229E-02 0.15352E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -23.554 36.896 5.6123 8.0051 v Velocity[Y] -26.259 27.501 -0.14512 -0.003899 v Velocity[Z] -2.9644 3.0443 2.6174e-06 -5.3882e-08 v ǁVelocityǁ 0.0015462 37.015 7.7927 8.097 v Pressure -1.4285e+05 2.5529e+05 57225 27700 v TurbVisc 7.2654e-20 0.015816 0.0001699 2.6664e-05 v CourantNb 1.2166e-08 0.011694 0.00016829 4.9387e-06 v FourierNb 1.2425e-07 0.046336 0.00014627 3.1489e-07 v total_pressure -41523 3.5661e+05 1.5855e+05 1.2902e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0549 0.10145 0.0028586 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2759e-07 0.051672 0.00031456 5.2536e-06 INSTANT 0.875886000E-01 TIME STEP NUMBER 56084 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283139015E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.804302954E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.17462E-01 0.20929E+01 Friction velocity uk : 0.17462E-01 0.20929E+01 Dimensionless distance yplus : 0.16889E-01 0.20550E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 9.280461017e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29464E+08 1 0.17985E-09 0.25320E+02 0.19464E+04 c Velocity[X] 0.13348E+02 c Velocity[Y] 0.11972E+02 c Velocity[Z] 0.15647E-05 c Pressure 0.16117E-03 174 0.77346E-04 0.15643E-02 0.21673E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -23.564 36.914 5.6124 8.0052 v Velocity[Y] -26.271 27.515 -0.14513 -0.0039232 v Velocity[Z] -2.9642 3.0445 2.6167e-06 -5.3882e-08 v ǁVelocityǁ 0.0015807 37.033 7.7943 8.0972 v Pressure -1.4419e+05 2.5398e+05 55997 26924 v TurbVisc 1.2662e-19 0.015835 0.00016997 2.6709e-05 v CourantNb 2.472e-08 0.011693 0.00016829 4.9389e-06 v FourierNb 1.2425e-07 0.046332 0.00014627 3.1519e-07 v total_pressure -42870 3.5531e+05 1.5732e+05 1.2825e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.055 0.10148 0.002859 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2764e-07 0.051669 0.00031456 5.254e-06 INSTANT 0.875887000E-01 TIME STEP NUMBER 56085 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283144530E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.804772359E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.17229E-01 0.20930E+01 Friction velocity uk : 0.17229E-01 0.20930E+01 Dimensionless distance yplus : 0.16739E-01 0.20551E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 8.861067108e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29464E+08 1 0.17988E-09 0.25328E+02 0.19467E+04 c Velocity[X] 0.13350E+02 c Velocity[Y] 0.11978E+02 c Velocity[Z] 0.15654E-05 c Pressure 0.16473E-03 51 0.82837E-04 0.15979E-02 0.21973E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -23.574 36.931 5.6125 8.0053 v Velocity[Y] -26.284 27.528 -0.14514 -0.0039499 v Velocity[Z] -2.964 3.0446 2.616e-06 -5.3882e-08 v ǁVelocityǁ 0.0016009 37.05 7.796 8.0975 v Pressure -1.4549e+05 2.5278e+05 54711 26152 v TurbVisc 5.3844e-20 0.015854 0.00017004 2.6753e-05 v CourantNb 2.488e-08 0.011693 0.00016829 4.939e-06 v FourierNb 1.2425e-07 0.046328 0.00014628 3.155e-07 v total_pressure -44164 3.5411e+05 1.5604e+05 1.2748e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0551 0.10151 0.0028594 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.277e-07 0.051666 0.00031457 5.2545e-06 INSTANT 0.875888000E-01 TIME STEP NUMBER 56086 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283150083E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.805238203E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.65480E-02 0.20931E+01 Friction velocity uk : 0.65480E-02 0.20931E+01 Dimensionless distance yplus : 0.65308E-02 0.20552E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 8.212167680e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29465E+08 1 0.17990E-09 0.25335E+02 0.19468E+04 c Velocity[X] 0.13352E+02 c Velocity[Y] 0.11983E+02 c Velocity[Z] 0.15658E-05 c Pressure 0.16851E-03 298 0.96431E-04 0.16336E-02 0.22004E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -23.585 36.948 5.6126 8.0054 v Velocity[Y] -26.296 27.541 -0.14516 -0.0039741 v Velocity[Z] -2.9638 3.0448 2.6153e-06 -5.3882e-08 v ǁVelocityǁ 0.0016183 37.067 7.7977 8.0977 v Pressure -1.4688e+05 2.5148e+05 53402 25407 v TurbVisc 5.1693e-20 0.015872 0.00017012 2.6798e-05 v CourantNb 2.1216e-08 0.011692 0.0001683 4.9391e-06 v FourierNb 1.2425e-07 0.046324 0.00014628 3.158e-07 v total_pressure -45559 3.5281e+05 1.5473e+05 1.2673e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0552 0.10153 0.0028597 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2775e-07 0.051662 0.00031457 5.2549e-06 INSTANT 0.875889000E-01 TIME STEP NUMBER 56087 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283155289E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.805699681E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.63260E-02 0.20931E+01 Friction velocity uk : 0.63260E-02 0.20931E+01 Dimensionless distance yplus : 0.63094E-02 0.20553E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 7.583856235e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29465E+08 1 0.17992E-09 0.25333E+02 0.19467E+04 c Velocity[X] 0.13353E+02 c Velocity[Y] 0.11981E+02 c Velocity[Z] 0.15676E-05 c Pressure 0.17226E-03 101 0.81773E-04 0.16690E-02 0.21839E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -23.595 36.965 5.6127 8.0055 v Velocity[Y] -26.308 27.554 -0.14517 -0.0040001 v Velocity[Z] -2.9635 3.045 2.6146e-06 -5.3882e-08 v ǁVelocityǁ 0.0016325 37.085 7.7993 8.098 v Pressure -1.4825e+05 2.5018e+05 52067 24595 v TurbVisc 5.5162e-20 0.015891 0.00017019 2.6842e-05 v CourantNb 2.3631e-08 0.011692 0.0001683 4.9392e-06 v FourierNb 1.2425e-07 0.04632 0.00014628 3.1611e-07 v total_pressure -46923 3.515e+05 1.5339e+05 1.2592e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0553 0.10155 0.0028601 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.278e-07 0.051659 0.00031458 5.2553e-06 INSTANT 0.875890000E-01 TIME STEP NUMBER 56088 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283160531E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.806154558E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13306E-01 0.20932E+01 Friction velocity uk : 0.13306E-01 0.20932E+01 Dimensionless distance yplus : 0.12983E-01 0.20553E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 6.943720860e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29466E+08 1 0.17995E-09 0.25344E+02 0.19470E+04 c Velocity[X] 0.13355E+02 c Velocity[Y] 0.11989E+02 c Velocity[Z] 0.15831E-05 c Pressure 0.17354E-03 9 0.58251E-04 0.16804E-02 0.18748E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -23.605 36.982 5.6127 8.0056 v Velocity[Y] -26.32 27.568 -0.14518 -0.0040271 v Velocity[Z] -2.9633 3.0452 2.6139e-06 -5.3882e-08 v ǁVelocityǁ 0.0016277 37.102 7.801 8.0982 v Pressure -1.4962e+05 2.4889e+05 50704 23878 v TurbVisc 6.0076e-20 0.01591 0.00017027 2.6887e-05 v CourantNb 3.3427e-08 0.011691 0.0001683 4.9393e-06 v FourierNb 1.2425e-07 0.046316 0.00014628 3.1641e-07 v total_pressure -48292 3.5021e+05 1.5203e+05 1.252e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0553 0.10158 0.0028605 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2785e-07 0.051655 0.00031459 5.2557e-06 INSTANT 0.875891000E-01 TIME STEP NUMBER 56089 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283165635E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.806601854E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12535E-01 0.20932E+01 Friction velocity uk : 0.12535E-01 0.20932E+01 Dimensionless distance yplus : 0.12179E-01 0.20553E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 6.176022510e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29466E+08 1 0.17997E-09 0.25349E+02 0.19471E+04 c Velocity[X] 0.13357E+02 c Velocity[Y] 0.11992E+02 c Velocity[Z] 0.15760E-05 c Pressure 0.17754E-03 162 0.77396E-04 0.17181E-02 0.25367E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -23.616 37 5.6128 8.0057 v Velocity[Y] -26.332 27.581 -0.14519 -0.0040521 v Velocity[Z] -2.9631 3.0454 2.6133e-06 -5.3882e-08 v ǁVelocityǁ 0.0016486 37.119 7.8027 8.0984 v Pressure -1.5113e+05 2.4742e+05 49307 23008 v TurbVisc 1.4347e-19 0.015928 0.00017034 2.6932e-05 v CourantNb 3.1858e-08 0.011691 0.00016831 4.9394e-06 v FourierNb 1.2425e-07 0.046312 0.00014629 3.1672e-07 v total_pressure -49803 3.4875e+05 1.5063e+05 1.2433e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0553 0.10161 0.0028608 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.279e-07 0.051651 0.00031459 5.2561e-06 INSTANT 0.875892000E-01 TIME STEP NUMBER 56090 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283170592E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.807042309E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.96602E-02 0.20932E+01 Friction velocity uk : 0.96602E-02 0.20932E+01 Dimensionless distance yplus : 0.94123E-02 0.20553E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 5.672912560e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29467E+08 1 0.18000E-09 0.25356E+02 0.19473E+04 c Velocity[X] 0.13357E+02 c Velocity[Y] 0.11999E+02 c Velocity[Z] 0.15699E-05 c Pressure 0.18077E-03 402 0.83062E-04 0.17483E-02 0.27576E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -23.626 37.017 5.6129 8.0058 v Velocity[Y] -26.345 27.594 -0.1452 -0.0040798 v Velocity[Z] -2.9629 3.0455 2.6126e-06 -5.3882e-08 v ǁVelocityǁ 0.001652 37.137 7.8043 8.0987 v Pressure -1.5263e+05 2.46e+05 47825 22060 v TurbVisc 1.5984e-19 0.015947 0.00017042 2.6976e-05 v CourantNb 2.4904e-08 0.011691 0.00016831 4.9395e-06 v FourierNb 1.2425e-07 0.046307 0.00014629 3.1703e-07 v total_pressure -51300 3.4733e+05 1.4915e+05 1.2338e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0553 0.10163 0.0028611 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2795e-07 0.051648 0.0003146 5.2565e-06 INSTANT 0.875893000E-01 TIME STEP NUMBER 56091 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283175535E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.807477399E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.35349E-02 0.20932E+01 Friction velocity uk : 0.35349E-02 0.20932E+01 Dimensionless distance yplus : 0.34442E-02 0.20553E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 5.007767386e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29467E+08 1 0.18002E-09 0.25362E+02 0.19474E+04 c Velocity[X] 0.13360E+02 c Velocity[Y] 0.12002E+02 c Velocity[Z] 0.15674E-05 c Pressure 0.18426E-03 223 0.96652E-04 0.17811E-02 0.23047E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -23.636 37.034 5.6129 8.0059 v Velocity[Y] -26.357 27.607 -0.14521 -0.0041045 v Velocity[Z] -2.9627 3.0457 2.6119e-06 -5.3882e-08 v ǁVelocityǁ 0.0016532 37.154 7.806 8.0989 v Pressure -1.5412e+05 2.446e+05 46391 21352 v TurbVisc 1.5518e-19 0.015966 0.00017049 2.7022e-05 v CourantNb 2.5037e-08 0.01169 0.00016831 4.9396e-06 v FourierNb 1.2425e-07 0.046303 0.00014629 3.1734e-07 v total_pressure -52793 3.4593e+05 1.4772e+05 1.2268e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0553 0.10165 0.0028613 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.28e-07 0.051644 0.00031461 5.257e-06 INSTANT 0.875894000E-01 TIME STEP NUMBER 56092 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283180159E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.807909091E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.49397E-02 0.20932E+01 Friction velocity uk : 0.49397E-02 0.20932E+01 Dimensionless distance yplus : 0.48130E-02 0.20553E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 4.351044349e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29467E+08 1 0.18005E-09 0.25359E+02 0.19472E+04 c Velocity[X] 0.13360E+02 c Velocity[Y] 0.11999E+02 c Velocity[Z] 0.15670E-05 c Pressure 0.18757E-03 119 0.82162E-04 0.18121E-02 0.27121E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -23.647 37.051 5.613 8.006 v Velocity[Y] -26.369 27.62 -0.14522 -0.0041312 v Velocity[Z] -2.9624 3.0459 2.6112e-06 -5.3882e-08 v ǁVelocityǁ 0.0016487 37.171 7.8076 8.0992 v Pressure -1.5567e+05 2.4311e+05 44873 20391 v TurbVisc 1.4108e-19 0.015984 0.00017056 2.7066e-05 v CourantNb 2.5351e-08 0.01169 0.00016832 4.9397e-06 v FourierNb 1.2425e-07 0.046298 0.00014629 3.1764e-07 v total_pressure -54346 3.4444e+05 1.462e+05 1.2172e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0553 0.10167 0.0028616 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2806e-07 0.051639 0.00031461 5.2574e-06 INSTANT 0.875895000E-01 TIME STEP NUMBER 56093 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283184785E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.808330083E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.38898E-02 0.20932E+01 Friction velocity uk : 0.38898E-02 0.20932E+01 Dimensionless distance yplus : 0.37900E-02 0.20553E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 3.753377754e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29468E+08 1 0.18007E-09 0.25368E+02 0.19475E+04 c Velocity[X] 0.13361E+02 c Velocity[Y] 0.12007E+02 c Velocity[Z] 0.15743E-05 c Pressure 0.18866E-03 10 0.59050E-04 0.18215E-02 0.22570E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -23.657 37.068 5.613 8.0061 v Velocity[Y] -26.382 27.634 -0.14523 -0.0041589 v Velocity[Z] -2.9622 3.0461 2.6105e-06 -5.3882e-08 v ǁVelocityǁ 0.0016243 37.189 7.8093 8.0994 v Pressure -1.572e+05 2.4167e+05 43350 19576 v TurbVisc 1.463e-19 0.016003 0.00017064 2.7111e-05 v CourantNb 2.4424e-08 0.011689 0.00016832 4.9398e-06 v FourierNb 1.2425e-07 0.046293 0.0001463 3.1795e-07 v total_pressure -55874 3.4299e+05 1.4468e+05 1.209e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0553 0.10169 0.0028618 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2811e-07 0.051635 0.00031462 5.2578e-06 INSTANT 0.875896000E-01 TIME STEP NUMBER 56094 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283189245E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.808743569E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.90059E-02 0.20931E+01 Friction velocity uk : 0.90059E-02 0.20931E+01 Dimensionless distance yplus : 0.87748E-02 0.20553E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 3.066978529e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29468E+08 1 0.18010E-09 0.25373E+02 0.19476E+04 c Velocity[X] 0.13363E+02 c Velocity[Y] 0.12010E+02 c Velocity[Z] 0.15694E-05 c Pressure 0.19222E-03 450 0.77990E-04 0.18548E-02 0.29295E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -23.668 37.085 5.6131 8.0062 v Velocity[Y] -26.394 27.647 -0.14524 -0.0041847 v Velocity[Z] -2.962 3.0462 2.6098e-06 -5.3882e-08 v ǁVelocityǁ 0.0016343 37.206 7.8109 8.0996 v Pressure -1.5887e+05 2.4004e+05 41803 18626 v TurbVisc 1.6437e-19 0.016022 0.00017071 2.7157e-05 v CourantNb 2.6685e-08 0.011689 0.00016832 4.9399e-06 v FourierNb 1.2425e-07 0.046288 0.0001463 3.1826e-07 v total_pressure -57545 3.4137e+05 1.4313e+05 1.1995e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0553 0.10171 0.002862 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2816e-07 0.051631 0.00031462 5.2582e-06 INSTANT 0.875897000E-01 TIME STEP NUMBER 56095 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283193568E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.809147811E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10552E-01 0.20931E+01 Friction velocity uk : 0.10552E-01 0.20931E+01 Dimensionless distance yplus : 0.10281E-01 0.20552E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 2.553422766e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29469E+08 1 0.18012E-09 0.25379E+02 0.19477E+04 c Velocity[X] 0.13363E+02 c Velocity[Y] 0.12016E+02 c Velocity[Z] 0.15668E-05 c Pressure 0.19511E-03 92 0.83609E-04 0.18815E-02 0.31176E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -23.678 37.102 5.6131 8.0062 v Velocity[Y] -26.406 27.66 -0.14524 -0.004213 v Velocity[Z] -2.9618 3.0464 2.6091e-06 -5.3882e-08 v ǁVelocityǁ 0.0016229 37.223 7.8126 8.0998 v Pressure -1.605e+05 2.385e+05 40176 17606 v TurbVisc 1.7024e-19 0.016041 0.00017079 2.7201e-05 v CourantNb 2.7837e-08 0.011688 0.00016833 4.94e-06 v FourierNb 1.2425e-07 0.046283 0.0001463 3.1857e-07 v total_pressure -59178 3.3982e+05 1.415e+05 1.1893e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0552 0.10173 0.0028623 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2821e-07 0.051626 0.00031463 5.2586e-06 INSTANT 0.875898000E-01 TIME STEP NUMBER 56096 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283197848E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.809548064E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12344E-01 0.20930E+01 Friction velocity uk : 0.12344E-01 0.20930E+01 Dimensionless distance yplus : 0.11993E-01 0.20551E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 2.034004371e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29469E+08 1 0.18014E-09 0.25385E+02 0.19479E+04 c Velocity[X] 0.13366E+02 c Velocity[Y] 0.12019E+02 c Velocity[Z] 0.15630E-05 c Pressure 0.19815E-03 191 0.97068E-04 0.19097E-02 0.27316E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -23.689 37.12 5.6131 8.0063 v Velocity[Y] -26.419 27.673 -0.14525 -0.0042385 v Velocity[Z] -2.9615 3.0466 2.6084e-06 -5.3883e-08 v ǁVelocityǁ 0.0016094 37.24 7.8142 8.1001 v Pressure -1.6218e+05 2.3694e+05 38581 16789 v TurbVisc 1.7768e-19 0.016059 0.00017086 2.7247e-05 v CourantNb 2.9579e-08 0.011688 0.00016833 4.9401e-06 v FourierNb 1.2425e-07 0.046278 0.00014631 3.1889e-07 v total_pressure -60853 3.3826e+05 1.3991e+05 1.1811e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0551 0.10174 0.0028624 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2826e-07 0.051621 0.00031464 5.259e-06 INSTANT 0.875899000E-01 TIME STEP NUMBER 56097 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283201809E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.809942620E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13193E-01 0.20929E+01 Friction velocity uk : 0.13193E-01 0.20929E+01 Dimensionless distance yplus : 0.12818E-01 0.20551E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.528843594e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29469E+08 1 0.18017E-09 0.25381E+02 0.19476E+04 c Velocity[X] 0.13365E+02 c Velocity[Y] 0.12016E+02 c Velocity[Z] 0.15636E-05 c Pressure 0.20107E-03 112 0.82662E-04 0.19367E-02 0.31646E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -23.699 37.137 5.6132 8.0064 v Velocity[Y] -26.431 27.686 -0.14526 -0.004266 v Velocity[Z] -2.9613 3.0468 2.6077e-06 -5.3883e-08 v ǁVelocityǁ 0.0015949 37.258 7.8159 8.1003 v Pressure -1.6387e+05 2.353e+05 36923 15730 v TurbVisc 1.7823e-19 0.016078 0.00017093 2.7292e-05 v CourantNb 2.9966e-08 0.011688 0.00016833 4.9402e-06 v FourierNb 1.2425e-07 0.046273 0.00014631 3.1919e-07 v total_pressure -62549 3.3663e+05 1.3825e+05 1.1705e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0551 0.10176 0.0028626 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2831e-07 0.051617 0.00031464 5.2594e-06 INSTANT 0.875900000E-01 TIME STEP NUMBER 56098 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283205746E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.810326757E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13464E-01 0.20928E+01 Friction velocity uk : 0.13464E-01 0.20928E+01 Dimensionless distance yplus : 0.13019E-01 0.20550E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.059626046e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29470E+08 1 0.18019E-09 0.25390E+02 0.19479E+04 c Velocity[X] 0.13367E+02 c Velocity[Y] 0.12023E+02 c Velocity[Z] 0.15684E-05 c Pressure 0.20184E-03 10 0.60009E-04 0.19430E-02 0.25641E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -23.71 37.154 5.6132 8.0065 v Velocity[Y] -26.444 27.699 -0.14527 -0.0042946 v Velocity[Z] -2.9611 3.047 2.6071e-06 -5.3883e-08 v ǁVelocityǁ 0.0015584 37.275 7.8175 8.1005 v Pressure -1.6554e+05 2.3375e+05 35266 14859 v TurbVisc 1.7764e-19 0.016097 0.00017101 2.7337e-05 v CourantNb 3.0339e-08 0.011687 0.00016833 4.9403e-06 v FourierNb 1.2425e-07 0.046268 0.00014631 3.195e-07 v total_pressure -64213 3.3507e+05 1.3659e+05 1.1618e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.055 0.10177 0.0028628 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2837e-07 0.051612 0.00031465 5.2598e-06 INSTANT 0.875901000E-01 TIME STEP NUMBER 56099 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283209504E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.810701943E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12541E-01 0.20927E+01 Friction velocity uk : 0.12541E-01 0.20927E+01 Dimensionless distance yplus : 0.12127E-01 0.20549E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 5.814626610e-03 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29470E+08 1 0.18022E-09 0.25394E+02 0.19480E+04 c Velocity[X] 0.13369E+02 c Velocity[Y] 0.12025E+02 c Velocity[Z] 0.15619E-05 c Pressure 0.20492E-03 376 0.78563E-04 0.19715E-02 0.33488E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -23.721 37.171 5.6132 8.0066 v Velocity[Y] -26.456 27.712 -0.14527 -0.0043211 v Velocity[Z] -2.9609 3.0471 2.6064e-06 -5.3883e-08 v ǁVelocityǁ 0.0015596 37.292 7.8192 8.1007 v Pressure -1.6736e+05 2.3199e+05 33586 13831 v TurbVisc 1.7398e-19 0.016115 0.00017108 2.7383e-05 v CourantNb 3.0821e-08 0.011687 0.00016834 4.9404e-06 v FourierNb 1.2425e-07 0.046262 0.00014632 3.1982e-07 v total_pressure -66030 3.3332e+05 1.3491e+05 1.1516e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0549 0.10178 0.0028629 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2842e-07 0.051607 0.00031465 5.2602e-06 INSTANT 0.875902000E-01 TIME STEP NUMBER 56100 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283213123E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.811066810E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12380E-01 0.20926E+01 Friction velocity uk : 0.12380E-01 0.20926E+01 Dimensionless distance yplus : 0.11971E-01 0.20548E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 2.286193886e-03 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29470E+08 1 0.18024E-09 0.25400E+02 0.19481E+04 c Velocity[X] 0.13369E+02 c Velocity[Y] 0.12031E+02 c Velocity[Z] 0.15570E-05 c Pressure 0.20738E-03 66 0.84412E-04 0.19940E-02 0.35421E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -23.731 37.188 5.6132 8.0066 v Velocity[Y] -26.468 27.725 -0.14528 -0.0043502 v Velocity[Z] -2.9606 3.0473 2.6057e-06 -5.3883e-08 v ǁVelocityǁ 0.0015392 37.309 7.8208 8.1009 v Pressure -1.6913e+05 2.3033e+05 31828 12733 v TurbVisc 1.5402e-19 0.016134 0.00017116 2.7428e-05 v CourantNb 3.0956e-08 0.011686 0.00016834 4.9405e-06 v FourierNb 1.2425e-07 0.046257 0.00014632 3.2013e-07 v total_pressure -67804 3.3166e+05 1.3315e+05 1.1406e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0548 0.1018 0.002863 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2847e-07 0.051602 0.00031466 5.2606e-06 INSTANT 0.875903000E-01 TIME STEP NUMBER 56101 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283216686E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.811427851E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12162E-01 0.20925E+01 Friction velocity uk : 0.12162E-01 0.20925E+01 Dimensionless distance yplus : 0.11760E-01 0.20546E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -6.105989538e-04 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29471E+08 1 0.18026E-09 0.25405E+02 0.19482E+04 c Velocity[X] 0.13372E+02 c Velocity[Y] 0.12033E+02 c Velocity[Z] 0.15546E-05 c Pressure 0.20996E-03 123 0.98055E-04 0.20177E-02 0.30832E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -23.742 37.205 5.6133 8.0067 v Velocity[Y] -26.481 27.738 -0.14528 -0.0043765 v Velocity[Z] -2.9604 3.0475 2.605e-06 -5.3883e-08 v ǁVelocityǁ 0.00152 37.326 7.8225 8.1012 v Pressure -1.7094e+05 2.2865e+05 30113 11851 v TurbVisc 1.8886e-19 0.016152 0.00017123 2.7474e-05 v CourantNb 3.125e-08 0.011686 0.00016834 4.9406e-06 v FourierNb 1.2425e-07 0.046251 0.00014632 3.2044e-07 v total_pressure -69612 3.2998e+05 1.3144e+05 1.1318e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0546 0.10181 0.0028631 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2852e-07 0.051596 0.00031467 5.2611e-06 INSTANT 0.875904000E-01 TIME STEP NUMBER 56102 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283219911E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.811782211E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12098E-01 0.20924E+01 Friction velocity uk : 0.12098E-01 0.20924E+01 Dimensionless distance yplus : 0.11698E-01 0.20545E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -3.451328978e-03 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29471E+08 1 0.18028E-09 0.25401E+02 0.19480E+04 c Velocity[X] 0.13372E+02 c Velocity[Y] 0.12029E+02 c Velocity[Z] 0.15517E-05 c Pressure 0.21240E-03 123 0.83546E-04 0.20399E-02 0.35681E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -23.752 37.222 5.6133 8.0068 v Velocity[Y] -26.493 27.751 -0.14529 -0.0044047 v Velocity[Z] -2.9602 3.0477 2.6043e-06 -5.3883e-08 v ǁVelocityǁ 0.0014963 37.344 7.8241 8.1014 v Pressure -1.7277e+05 2.2692e+05 28328 10722 v TurbVisc 1.8921e-19 0.016171 0.0001713 2.752e-05 v CourantNb 3.1487e-08 0.011685 0.00016834 4.9407e-06 v FourierNb 1.2425e-07 0.046246 0.00014633 3.2075e-07 v total_pressure -71445 3.2825e+05 1.2965e+05 1.1205e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0545 0.10182 0.0028632 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2857e-07 0.051591 0.00031467 5.2615e-06 INSTANT 0.875905000E-01 TIME STEP NUMBER 56103 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283223110E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.812124881E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10905E-01 0.20922E+01 Friction velocity uk : 0.10905E-01 0.20922E+01 Dimensionless distance yplus : 0.10876E-01 0.20544E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -5.543030066e-03 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29471E+08 1 0.18031E-09 0.25410E+02 0.19482E+04 c Velocity[X] 0.13373E+02 c Velocity[Y] 0.12036E+02 c Velocity[Z] 0.15586E-05 c Pressure 0.21276E-03 10 0.60915E-04 0.20421E-02 0.29167E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -23.763 37.239 5.6133 8.0068 v Velocity[Y] -26.506 27.764 -0.14529 -0.0044341 v Velocity[Z] -2.96 3.0479 2.6036e-06 -5.3883e-08 v ǁVelocityǁ 0.0014518 37.361 7.8258 8.1016 v Pressure -1.7456e+05 2.2526e+05 26561 9783.3 v TurbVisc 1.898e-19 0.01619 0.00017138 2.7565e-05 v CourantNb 3.1637e-08 0.011685 0.00016835 4.9408e-06 v FourierNb 1.2425e-07 0.04624 0.00014633 3.2107e-07 v total_pressure -73231 3.2659e+05 1.2789e+05 1.1111e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0544 0.10183 0.0028633 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2863e-07 0.051586 0.00031468 5.2619e-06 INSTANT 0.875906000E-01 TIME STEP NUMBER 56104 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283226105E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.812458696E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.61628E-02 0.20921E+01 Friction velocity uk : 0.61628E-02 0.20921E+01 Dimensionless distance yplus : 0.61467E-02 0.20543E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -7.987534767e-03 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29472E+08 1 0.18033E-09 0.25413E+02 0.19483E+04 c Velocity[X] 0.13376E+02 c Velocity[Y] 0.12038E+02 c Velocity[Z] 0.15503E-05 c Pressure 0.21532E-03 494 0.79273E-04 0.20655E-02 0.37063E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -23.774 37.256 5.6133 8.0069 v Velocity[Y] -26.518 27.777 -0.1453 -0.0044614 v Velocity[Z] -2.9597 3.048 2.6029e-06 -5.3883e-08 v ǁVelocityǁ 0.0014492 37.378 7.8274 8.1018 v Pressure -1.7651e+05 2.2343e+05 24768 8703.1 v TurbVisc 1.881e-19 0.016208 0.00017145 2.7612e-05 v CourantNb 3.1825e-08 0.011685 0.00016835 4.9409e-06 v FourierNb 1.2425e-07 0.046234 0.00014633 3.2139e-07 v total_pressure -75185 3.2476e+05 1.2609e+05 1.1003e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0543 0.10183 0.0028633 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2868e-07 0.05158 0.00031468 5.2623e-06 INSTANT 0.875907000E-01 TIME STEP NUMBER 56105 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283228978E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.812780467E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.46756E-02 0.20919E+01 Friction velocity uk : 0.46756E-02 0.20919E+01 Dimensionless distance yplus : 0.46634E-02 0.20541E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -8.810140897e-03 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29472E+08 1 0.18035E-09 0.25419E+02 0.19485E+04 c Velocity[X] 0.13377E+02 c Velocity[Y] 0.12043E+02 c Velocity[Z] 0.15444E-05 c Pressure 0.21731E-03 66 0.85171E-04 0.20834E-02 0.39284E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -23.784 37.272 5.6133 8.0069 v Velocity[Y] -26.531 27.79 -0.1453 -0.0044914 v Velocity[Z] -2.9595 3.0482 2.6023e-06 -5.3883e-08 v ǁVelocityǁ 0.0014259 37.395 7.829 8.102 v Pressure -1.7839e+05 2.2173e+05 22909 7536.3 v TurbVisc 1.9678e-19 0.016227 0.00017152 2.7657e-05 v CourantNb 3.1745e-08 0.011684 0.00016835 4.941e-06 v FourierNb 1.2425e-07 0.046228 0.00014634 3.217e-07 v total_pressure -77068 3.2305e+05 1.2423e+05 1.0886e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0541 0.10184 0.0028634 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2873e-07 0.051575 0.00031469 5.2627e-06 INSTANT 0.875908000E-01 TIME STEP NUMBER 56106 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283231766E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.813099533E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12350E-01 0.20918E+01 Friction velocity uk : 0.12350E-01 0.20918E+01 Dimensionless distance yplus : 0.12318E-01 0.20539E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -9.499117558e-03 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29472E+08 1 0.18037E-09 0.25425E+02 0.19486E+04 c Velocity[X] 0.13379E+02 c Velocity[Y] 0.12045E+02 c Velocity[Z] 0.15432E-05 c Pressure 0.21936E-03 159 0.98901E-04 0.21019E-02 0.33991E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -23.795 37.289 5.6133 8.007 v Velocity[Y] -26.543 27.803 -0.14531 -0.0045185 v Velocity[Z] -2.9593 3.0484 2.6016e-06 -5.3883e-08 v ǁVelocityǁ 0.0014034 37.412 7.8307 8.1022 v Pressure -1.8032e+05 2.2001e+05 21091 6597.6 v TurbVisc 1.9031e-19 0.016246 0.0001716 2.7704e-05 v CourantNb 2.8533e-08 0.011684 0.00016835 4.9411e-06 v FourierNb 1.2425e-07 0.046223 0.00014634 3.2202e-07 v total_pressure -78996 3.2133e+05 1.2242e+05 1.0792e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0539 0.10186 0.0028635 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2878e-07 0.051569 0.0003147 5.2631e-06 INSTANT 0.875909000E-01 TIME STEP NUMBER 56107 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283234212E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.813409998E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.14240E-01 0.20916E+01 Friction velocity uk : 0.14240E-01 0.20916E+01 Dimensionless distance yplus : 0.13770E-01 0.20537E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -9.716512834e-03 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29472E+08 1 0.18040E-09 0.25420E+02 0.19483E+04 c Velocity[X] 0.13380E+02 c Velocity[Y] 0.12040E+02 c Velocity[Z] 0.15397E-05 c Pressure 0.22129E-03 121 0.84140E-04 0.21191E-02 0.38771E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -23.806 37.306 5.6133 8.007 v Velocity[Y] -26.556 27.815 -0.14531 -0.0045475 v Velocity[Z] -2.9591 3.0486 2.6009e-06 -5.3883e-08 v ǁVelocityǁ 0.0013779 37.429 7.8323 8.1024 v Pressure -1.8226e+05 2.1824e+05 19213 5420 v TurbVisc 1.9245e-19 0.016264 0.00017167 2.7749e-05 v CourantNb 2.8581e-08 0.011683 0.00016836 4.9411e-06 v FourierNb 1.2425e-07 0.046217 0.00014635 3.2233e-07 v total_pressure -80938 3.1957e+05 1.2054e+05 1.0675e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0537 0.10187 0.0028636 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2883e-07 0.051563 0.0003147 5.2635e-06 INSTANT 0.875910000E-01 TIME STEP NUMBER 56108 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283236623E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.813708636E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13835E-01 0.20914E+01 Friction velocity uk : 0.13835E-01 0.20914E+01 Dimensionless distance yplus : 0.13480E-01 0.20536E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -9.378113326e-03 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29472E+08 1 0.18042E-09 0.25429E+02 0.19486E+04 c Velocity[X] 0.13382E+02 c Velocity[Y] 0.12047E+02 c Velocity[Z] 0.15473E-05 c Pressure 0.22113E-03 10 0.61830E-04 0.21164E-02 0.32062E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -23.816 37.323 5.6133 8.0071 v Velocity[Y] -26.568 27.828 -0.14532 -0.0045778 v Velocity[Z] -2.9588 3.0487 2.6002e-06 -5.3883e-08 v ǁVelocityǁ 0.0013306 37.446 7.8339 8.1025 v Pressure -1.8416e+05 2.1653e+05 17356 4426.3 v TurbVisc 1.9405e-19 0.016283 0.00017174 2.7795e-05 v CourantNb 2.8547e-08 0.011683 0.00016836 4.9412e-06 v FourierNb 1.2425e-07 0.046211 0.00014635 3.2265e-07 v total_pressure -82831 3.1786e+05 1.1868e+05 1.0575e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0536 0.10188 0.0028637 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2889e-07 0.051558 0.00031471 5.2639e-06 INSTANT 0.875911000E-01 TIME STEP NUMBER 56109 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283238818E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.813997639E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.14153E-01 0.20912E+01 Friction velocity uk : 0.14153E-01 0.20912E+01 Dimensionless distance yplus : 0.13790E-01 0.20534E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -9.027259678e-03 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29473E+08 1 0.18044E-09 0.25433E+02 0.19487E+04 c Velocity[X] 0.13386E+02 c Velocity[Y] 0.12047E+02 c Velocity[Z] 0.15383E-05 c Pressure 0.22314E-03 426 0.79951E-04 0.21343E-02 0.39943E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -23.827 37.34 5.6134 8.0071 v Velocity[Y] -26.581 27.841 -0.14532 -0.0046057 v Velocity[Z] -2.9586 3.0489 2.5995e-06 -5.3883e-08 v ǁVelocityǁ 0.0013294 37.463 7.8356 8.1027 v Pressure -1.862e+05 2.1467e+05 15477 3301.6 v TurbVisc 1.9147e-19 0.016301 0.00017182 2.7842e-05 v CourantNb 2.819e-08 0.011682 0.00016836 4.9413e-06 v FourierNb 1.2425e-07 0.046205 0.00014635 3.2297e-07 v total_pressure -84876 3.16e+05 1.168e+05 1.0463e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0534 0.10189 0.0028638 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2894e-07 0.051552 0.00031471 5.2643e-06 INSTANT 0.875912000E-01 TIME STEP NUMBER 56110 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283240895E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.814273646E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11506E-01 0.20910E+01 Friction velocity uk : 0.11506E-01 0.20910E+01 Dimensionless distance yplus : 0.11211E-01 0.20532E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -8.644083516e-03 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29473E+08 1 0.18046E-09 0.25439E+02 0.19488E+04 c Velocity[X] 0.13387E+02 c Velocity[Y] 0.12052E+02 c Velocity[Z] 0.15315E-05 c Pressure 0.22460E-03 38 0.86005E-04 0.21471E-02 0.41995E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -23.838 37.356 5.6134 8.0072 v Velocity[Y] -26.593 27.853 -0.14533 -0.0046367 v Velocity[Z] -2.9584 3.0491 2.5988e-06 -5.3883e-08 v ǁVelocityǁ 0.0013062 37.479 7.8372 8.1029 v Pressure -1.8819e+05 2.129e+05 13539 2087.1 v TurbVisc 1.9944e-19 0.01632 0.00017189 2.7888e-05 v CourantNb 3.051e-08 0.011682 0.00016836 4.9414e-06 v FourierNb 1.2425e-07 0.046198 0.00014636 3.2328e-07 v total_pressure -86870 3.1423e+05 1.1486e+05 1.0341e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0532 0.1019 0.0028639 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2899e-07 0.051546 0.00031472 5.2647e-06 INSTANT 0.875913000E-01 TIME STEP NUMBER 56111 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283242871E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.814547352E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.99212E-02 0.20908E+01 Friction velocity uk : 0.99212E-02 0.20908E+01 Dimensionless distance yplus : 0.96666E-02 0.20530E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -6.778750981e-03 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29473E+08 1 0.18048E-09 0.25445E+02 0.19490E+04 c Velocity[X] 0.13391E+02 c Velocity[Y] 0.12054E+02 c Velocity[Z] 0.15303E-05 c Pressure 0.22610E-03 159 0.99816E-04 0.21602E-02 0.36158E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -23.849 37.373 5.6134 8.0072 v Velocity[Y] -26.606 27.866 -0.14534 -0.0046646 v Velocity[Z] -2.9582 3.0493 2.5982e-06 -5.3883e-08 v ǁVelocityǁ 0.0012849 37.496 7.8388 8.1031 v Pressure -1.9021e+05 2.111e+05 11647 1107.7 v TurbVisc 1.9746e-19 0.016339 0.00017196 2.7935e-05 v CourantNb 3.0469e-08 0.011682 0.00016837 4.9415e-06 v FourierNb 1.2425e-07 0.046192 0.00014636 3.236e-07 v total_pressure -88881 3.1242e+05 1.1297e+05 1.0243e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.053 0.10191 0.002864 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2904e-07 0.05154 0.00031473 5.2651e-06 INSTANT 0.875914000E-01 TIME STEP NUMBER 56112 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283244498E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.814811359E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.75663E-02 0.20906E+01 Friction velocity uk : 0.75663E-02 0.20906E+01 Dimensionless distance yplus : 0.73721E-02 0.20528E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -5.169234993e-03 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29473E+08 1 0.18050E-09 0.25440E+02 0.19487E+04 c Velocity[X] 0.13392E+02 c Velocity[Y] 0.12048E+02 c Velocity[Z] 0.15253E-05 c Pressure 0.22747E-03 139 0.84843E-04 0.21720E-02 0.40823E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -23.859 37.389 5.6134 8.0072 v Velocity[Y] -26.618 27.878 -0.14534 -0.0046945 v Velocity[Z] -2.9579 3.0494 2.5975e-06 -5.3883e-08 v ǁVelocityǁ 0.0012612 37.513 7.8405 8.1033 v Pressure -1.9223e+05 2.0926e+05 9699.9 -111.64 v TurbVisc 1.9711e-19 0.016357 0.00017204 2.7981e-05 v CourantNb 3.0352e-08 0.011681 0.00016837 4.9415e-06 v FourierNb 1.2425e-07 0.046186 0.00014636 3.2392e-07 v total_pressure -90906 3.1059e+05 1.1102e+05 1.0121e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0528 0.10192 0.0028642 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.291e-07 0.051534 0.00031473 5.2655e-06 INSTANT 0.875915000E-01 TIME STEP NUMBER 56113 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283246088E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.815062901E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.47520E-02 0.20904E+01 Friction velocity uk : 0.47520E-02 0.20904E+01 Dimensionless distance yplus : 0.46301E-02 0.20526E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -3.199690096e-03 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29473E+08 1 0.18052E-09 0.25450E+02 0.19490E+04 c Velocity[X] 0.13395E+02 c Velocity[Y] 0.12055E+02 c Velocity[Z] 0.15323E-05 c Pressure 0.22675E-03 10 0.62536E-04 0.21639E-02 0.33476E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -23.87 37.406 5.6134 8.0072 v Velocity[Y] -26.631 27.891 -0.14535 -0.0047256 v Velocity[Z] -2.9577 3.0496 2.5968e-06 -5.3883e-08 v ǁVelocityǁ 0.0012162 37.53 7.8421 8.1034 v Pressure -1.942e+05 2.0749e+05 7780.9 -1137.7 v TurbVisc 1.9884e-19 0.016376 0.00017211 2.8027e-05 v CourantNb 3.0925e-08 0.011681 0.00016837 4.9416e-06 v FourierNb 1.2425e-07 0.04618 0.00014637 3.2424e-07 v total_pressure -92872 3.0882e+05 1.0911e+05 1.0019e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0526 0.10193 0.0028643 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2915e-07 0.051528 0.00031474 5.2658e-06 INSTANT 0.875916000E-01 TIME STEP NUMBER 56114 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283247451E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.815304208E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.51474E-02 0.20902E+01 Friction velocity uk : 0.51474E-02 0.20902E+01 Dimensionless distance yplus : 0.50153E-02 0.20524E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.198707967e-03 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29473E+08 1 0.18054E-09 0.25454E+02 0.19491E+04 c Velocity[X] 0.13399E+02 c Velocity[Y] 0.12055E+02 c Velocity[Z] 0.15237E-05 c Pressure 0.22818E-03 200 0.80660E-04 0.21763E-02 0.41219E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -23.881 37.423 5.6134 8.0073 v Velocity[Y] -26.643 27.903 -0.14536 -0.0047546 v Velocity[Z] -2.9575 3.0498 2.5961e-06 -5.3883e-08 v ǁVelocityǁ 0.001218 37.546 7.8438 8.1036 v Pressure -1.9632e+05 2.0558e+05 5842.8 -2297.3 v TurbVisc 1.9556e-19 0.016394 0.00017218 2.8074e-05 v CourantNb 3.0741e-08 0.01168 0.00016837 4.9417e-06 v FourierNb 1.2425e-07 0.046174 0.00014637 3.2456e-07 v total_pressure -94998 3.069e+05 1.0717e+05 99028 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0524 0.10194 0.0028644 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.292e-07 0.051522 0.00031474 5.2662e-06 INSTANT 0.875917000E-01 TIME STEP NUMBER 56115 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283248694E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.815531569E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.36489E-02 0.20900E+01 Friction velocity uk : 0.36489E-02 0.20900E+01 Dimensionless distance yplus : 0.35553E-02 0.20522E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 3.656593487e-06 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29474E+08 1 0.18056E-09 0.25461E+02 0.19493E+04 c Velocity[X] 0.13402E+02 c Velocity[Y] 0.12059E+02 c Velocity[Z] 0.15155E-05 c Pressure 0.22907E-03 29 0.86881E-04 0.21835E-02 0.42941E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -23.892 37.439 5.6134 8.0073 v Velocity[Y] -26.656 27.915 -0.14537 -0.0047863 v Velocity[Z] -2.9573 3.05 2.5954e-06 -5.3883e-08 v ǁVelocityǁ 0.0011988 37.563 7.8454 8.1038 v Pressure -1.9837e+05 2.0374e+05 3851.7 -3545.6 v TurbVisc 2.0443e-19 0.016413 0.00017225 2.812e-05 v CourantNb 2.5078e-08 0.01168 0.00016838 4.9418e-06 v FourierNb 1.2425e-07 0.046167 0.00014638 3.2488e-07 v total_pressure -97040 3.0507e+05 1.0518e+05 97779 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0522 0.10195 0.0028645 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2925e-07 0.051516 0.00031475 5.2666e-06 INSTANT 0.875918000E-01 TIME STEP NUMBER 56116 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283249836E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.815756729E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.51542E-02 0.20898E+01 Friction velocity uk : 0.51542E-02 0.20898E+01 Dimensionless distance yplus : 0.50220E-02 0.20520E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 2.841701222e-03 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29474E+08 1 0.18058E-09 0.25458E+02 0.19491E+04 c Velocity[X] 0.13405E+02 c Velocity[Y] 0.12053E+02 c Velocity[Z] 0.15117E-05 c Pressure 0.23000E-03 139 0.75398E-04 0.21911E-02 0.34078E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -23.902 37.455 5.6134 8.0073 v Velocity[Y] -26.668 27.928 -0.14537 -0.0048164 v Velocity[Z] -2.957 3.0501 2.5948e-06 -5.3883e-08 v ǁVelocityǁ 0.0011811 37.58 7.847 8.1039 v Pressure -2.0043e+05 2.019e+05 1913.6 -4562.2 v TurbVisc 1.9953e-19 0.016432 0.00017232 2.8168e-05 v CourantNb 2.4616e-08 0.011679 0.00016838 4.9418e-06 v FourierNb 1.2425e-07 0.046161 0.00014638 3.252e-07 v total_pressure -99101 3.0322e+05 1.0324e+05 96763 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.052 0.10196 0.0028647 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2931e-07 0.05151 0.00031476 5.267e-06 INSTANT 0.875919000E-01 TIME STEP NUMBER 56117 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283250731E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.815971264E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.48531E-02 0.20896E+01 Friction velocity uk : 0.48531E-02 0.20896E+01 Dimensionless distance yplus : 0.47286E-02 0.20518E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 5.235687853e-03 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29474E+08 1 0.18059E-09 0.25466E+02 0.19494E+04 c Velocity[X] 0.13409E+02 c Velocity[Y] 0.12058E+02 c Velocity[Z] 0.15177E-05 c Pressure 0.22912E-03 10 0.59634E-04 0.21815E-02 0.33364E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -23.913 37.472 5.6134 8.0073 v Velocity[Y] -26.681 27.94 -0.14538 -0.004846 v Velocity[Z] -2.9568 3.0503 2.5941e-06 -5.3883e-08 v ǁVelocityǁ 0.0011393 37.596 7.8487 8.1041 v Pressure -2.0244e+05 2.001e+05 -48.069 -5624 v TurbVisc 1.9909e-19 0.01645 0.0001724 2.8214e-05 v CourantNb 2.3042e-08 0.011679 0.00016838 4.9419e-06 v FourierNb 1.2425e-07 0.046155 0.00014638 3.2552e-07 v total_pressure -1.0112e+05 3.0142e+05 1.0128e+05 95701 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0518 0.10198 0.0028649 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2936e-07 0.051503 0.00031476 5.2674e-06 INSTANT 0.875920000E-01 TIME STEP NUMBER 56118 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283251282E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.816172640E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.45521E-02 0.20894E+01 Friction velocity uk : 0.45521E-02 0.20894E+01 Dimensionless distance yplus : 0.44353E-02 0.20516E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 7.704865116e-03 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29474E+08 1 0.18061E-09 0.25468E+02 0.19494E+04 c Velocity[X] 0.13413E+02 c Velocity[Y] 0.12055E+02 c Velocity[Z] 0.15152E-05 c Pressure 0.22993E-03 31 0.96188E-04 0.21879E-02 0.41005E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -23.924 37.488 5.6134 8.0073 v Velocity[Y] -26.693 27.952 -0.14539 -0.0048766 v Velocity[Z] -2.9566 3.0505 2.5934e-06 -5.3883e-08 v ǁVelocityǁ 0.0011373 37.613 7.8503 8.1043 v Pressure -2.0458e+05 1.9819e+05 -2011.3 -6874.1 v TurbVisc 1.9928e-19 0.016469 0.00017247 2.8261e-05 v CourantNb 2.3871e-08 0.011678 0.00016838 4.942e-06 v FourierNb 1.2425e-07 0.046148 0.00014639 3.2584e-07 v total_pressure -1.0326e+05 2.9952e+05 99314 94451 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0516 0.10199 0.002865 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2941e-07 0.051497 0.00031477 5.2678e-06 INSTANT 0.875921000E-01 TIME STEP NUMBER 56119 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283251855E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.816359095E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.27154E-02 0.20891E+01 Friction velocity uk : 0.27154E-02 0.20891E+01 Dimensionless distance yplus : 0.26458E-02 0.20514E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 9.187901505e-03 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29474E+08 1 0.18063E-09 0.25472E+02 0.19494E+04 c Velocity[X] 0.13417E+02 c Velocity[Y] 0.12055E+02 c Velocity[Z] 0.15070E-05 c Pressure 0.22994E-03 246 0.80352E-04 0.21868E-02 0.39196E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -23.935 37.504 5.6134 8.0073 v Velocity[Y] -26.706 27.964 -0.1454 -0.0049078 v Velocity[Z] -2.9563 3.0507 2.5927e-06 -5.3884e-08 v ǁVelocityǁ 0.0011293 37.629 7.8519 8.1044 v Pressure -2.0668e+05 1.9627e+05 -4025.1 -8120.3 v TurbVisc 1.3997e-19 0.016487 0.00017254 2.8308e-05 v CourantNb 1.5998e-08 0.011678 0.00016839 4.942e-06 v FourierNb 1.2425e-07 0.046142 0.00014639 3.2616e-07 v total_pressure -1.0535e+05 2.976e+05 97300 93205 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0514 0.102 0.0028652 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2946e-07 0.051491 0.00031478 5.2682e-06 INSTANT 0.875922000E-01 TIME STEP NUMBER 56120 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283252238E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.816539727E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.30993E-02 0.20889E+01 Friction velocity uk : 0.30993E-02 0.20889E+01 Dimensionless distance yplus : 0.30198E-02 0.20511E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.080872882e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29474E+08 1 0.18064E-09 0.25482E+02 0.19497E+04 c Velocity[X] 0.13421E+02 c Velocity[Y] 0.12060E+02 c Velocity[Z] 0.15050E-05 c Pressure 0.22966E-03 10 0.55831E-04 0.21829E-02 0.34331E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -23.946 37.521 5.6134 8.0073 v Velocity[Y] -26.718 27.976 -0.14541 -0.00494 v Velocity[Z] -2.9561 3.0508 2.592e-06 -5.3884e-08 v ǁVelocityǁ 0.0010921 37.645 7.8536 8.1046 v Pressure -2.0874e+05 1.9446e+05 -6020.7 -9215.9 v TurbVisc 2.268e-19 0.016506 0.00017261 2.8355e-05 v CourantNb 1.2804e-08 0.011677 0.00016839 4.9421e-06 v FourierNb 1.2425e-07 0.046135 0.00014639 3.2648e-07 v total_pressure -1.0741e+05 2.9578e+05 95304 92109 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0511 0.10201 0.0028654 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2951e-07 0.051485 0.00031478 5.2686e-06 INSTANT 0.875923000E-01 TIME STEP NUMBER 56121 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283252447E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.816711927E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.30200E-02 0.20887E+01 Friction velocity uk : 0.30200E-02 0.20887E+01 Dimensionless distance yplus : 0.29425E-02 0.20510E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.349190420e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29474E+08 1 0.18066E-09 0.25483E+02 0.19497E+04 c Velocity[X] 0.13426E+02 c Velocity[Y] 0.12057E+02 c Velocity[Z] 0.14976E-05 c Pressure 0.23023E-03 327 0.97152E-04 0.21871E-02 0.36625E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -23.956 37.537 5.6134 8.0073 v Velocity[Y] -26.731 27.988 -0.14542 -0.0049718 v Velocity[Z] -2.9559 3.051 2.5914e-06 -5.3884e-08 v ǁVelocityǁ 0.0011027 37.662 7.8552 8.1047 v Pressure -2.1084e+05 1.9258e+05 -7950.5 -10355 v TurbVisc 1.9622e-19 0.016524 0.00017268 2.8402e-05 v CourantNb 1.295e-08 0.011677 0.00016839 4.9422e-06 v FourierNb 1.2425e-07 0.046129 0.0001464 3.2681e-07 v total_pressure -1.0951e+05 2.9391e+05 93374 90970 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.051 0.10203 0.0028656 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2957e-07 0.051479 0.00031479 5.269e-06 INSTANT 0.875924000E-01 TIME STEP NUMBER 56122 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283252518E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.816869849E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.77090E-02 0.20885E+01 Friction velocity uk : 0.77090E-02 0.20885E+01 Dimensionless distance yplus : 0.75112E-02 0.20507E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.466298612e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29474E+08 1 0.18068E-09 0.25488E+02 0.19498E+04 c Velocity[X] 0.13431E+02 c Velocity[Y] 0.12057E+02 c Velocity[Z] 0.14887E-05 c Pressure 0.22987E-03 30 0.81861E-04 0.21824E-02 0.34393E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -23.967 37.553 5.6134 8.0073 v Velocity[Y] -26.743 27.999 -0.14544 -0.0050031 v Velocity[Z] -2.9557 3.0512 2.5907e-06 -5.3884e-08 v ǁVelocityǁ 0.0010889 37.678 7.8569 8.1049 v Pressure -2.1292e+05 1.9075e+05 -9952.7 -11482 v TurbVisc 9.4897e-22 0.016543 0.00017275 2.8449e-05 v CourantNb 1.0671e-08 0.011676 0.0001684 4.9422e-06 v FourierNb 1.2425e-07 0.046123 0.0001464 3.2713e-07 v total_pressure -1.1159e+05 2.9207e+05 91372 89843 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0507 0.10204 0.0028659 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2962e-07 0.051473 0.0003148 5.2694e-06 INSTANT 0.875925000E-01 TIME STEP NUMBER 56123 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283252387E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.817018583E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.84423E-02 0.20883E+01 Friction velocity uk : 0.84423E-02 0.20883E+01 Dimensionless distance yplus : 0.82257E-02 0.20505E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.634628060e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29474E+08 1 0.18069E-09 0.25497E+02 0.19501E+04 c Velocity[X] 0.13436E+02 c Velocity[Y] 0.12061E+02 c Velocity[Z] 0.14925E-05 c Pressure 0.22917E-03 10 0.58336E-04 0.21746E-02 0.32704E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -23.978 37.569 5.6134 8.0073 v Velocity[Y] -26.756 28.011 -0.14545 -0.0050335 v Velocity[Z] -2.9554 3.0514 2.59e-06 -5.3884e-08 v ǁVelocityǁ 0.0010577 37.694 7.8585 8.105 v Pressure -2.1501e+05 1.889e+05 -11955 -12570 v TurbVisc 8.7541e-20 0.016561 0.00017282 2.8496e-05 v CourantNb 9.4699e-09 0.011676 0.0001684 4.9423e-06 v FourierNb 1.2425e-07 0.046116 0.00014641 3.2745e-07 v total_pressure -1.1368e+05 2.9023e+05 89370 88755 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0505 0.10205 0.0028661 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2967e-07 0.051467 0.0003148 5.2698e-06 INSTANT 0.875926000E-01 TIME STEP NUMBER 56124 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283251997E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.817157120E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.70569E-02 0.20881E+01 Friction velocity uk : 0.70569E-02 0.20881E+01 Dimensionless distance yplus : 0.68758E-02 0.20503E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.720614345e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29474E+08 1 0.18071E-09 0.25500E+02 0.19502E+04 c Velocity[X] 0.13442E+02 c Velocity[Y] 0.12058E+02 c Velocity[Z] 0.14885E-05 c Pressure 0.22943E-03 25 0.99356E-04 0.21758E-02 0.38058E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -23.989 37.585 5.6134 8.0073 v Velocity[Y] -26.768 28.023 -0.14546 -0.0050653 v Velocity[Z] -2.9552 3.0515 2.5893e-06 -5.3884e-08 v ǁVelocityǁ 0.0010642 37.71 7.8601 8.1051 v Pressure -2.1711e+05 1.8705e+05 -13901 -13809 v TurbVisc 9.975e-20 0.01658 0.00017289 2.8543e-05 v CourantNb 1.0384e-08 0.011676 0.0001684 4.9424e-06 v FourierNb 1.2425e-07 0.04611 0.00014641 3.2777e-07 v total_pressure -1.1578e+05 2.8838e+05 87424 87516 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0503 0.10207 0.0028663 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2972e-07 0.051461 0.00031481 5.2701e-06 INSTANT 0.875927000E-01 TIME STEP NUMBER 56125 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283251550E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.817282152E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.90898E-02 0.20879E+01 Friction velocity uk : 0.90898E-02 0.20879E+01 Dimensionless distance yplus : 0.88566E-02 0.20501E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.778364225e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29474E+08 1 0.18072E-09 0.25504E+02 0.19503E+04 c Velocity[X] 0.13447E+02 c Velocity[Y] 0.12058E+02 c Velocity[Z] 0.14782E-05 c Pressure 0.22872E-03 153 0.84165E-04 0.21679E-02 0.35945E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -23.999 37.601 5.6134 8.0073 v Velocity[Y] -26.78 28.034 -0.14547 -0.0050976 v Velocity[Z] -2.955 3.0517 2.5886e-06 -5.3884e-08 v ǁVelocityǁ 0.0010635 37.726 7.8618 8.1053 v Pressure -2.1921e+05 1.852e+05 -15905 -15042 v TurbVisc 1.2316e-19 0.016598 0.00017296 2.8591e-05 v CourantNb 1.1379e-08 0.011675 0.0001684 4.9424e-06 v FourierNb 1.2425e-07 0.046104 0.00014641 3.281e-07 v total_pressure -1.1788e+05 2.8652e+05 85420 86283 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0501 0.10208 0.0028665 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2978e-07 0.051454 0.00031482 5.2705e-06 INSTANT 0.875928000E-01 TIME STEP NUMBER 56126 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283250895E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.817397846E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11027E-01 0.20877E+01 Friction velocity uk : 0.11027E-01 0.20877E+01 Dimensionless distance yplus : 0.10744E-01 0.20499E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.870036445e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29474E+08 1 0.18073E-09 0.25515E+02 0.19506E+04 c Velocity[X] 0.13452E+02 c Velocity[Y] 0.12063E+02 c Velocity[Z] 0.14762E-05 c Pressure 0.22769E-03 10 0.58767E-04 0.21570E-02 0.31473E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -24.01 37.617 5.6134 8.0073 v Velocity[Y] -26.793 28.046 -0.14549 -0.0051309 v Velocity[Z] -2.9547 3.0519 2.588e-06 -5.3884e-08 v ǁVelocityǁ 0.0010322 37.742 7.8634 8.1054 v Pressure -2.2123e+05 1.8342e+05 -17904 -16120 v TurbVisc 1.0505e-19 0.016617 0.00017303 2.8638e-05 v CourantNb 1.1568e-08 0.011675 0.00016841 4.9425e-06 v FourierNb 1.2425e-07 0.046097 0.00014642 3.2842e-07 v total_pressure -1.1991e+05 2.8474e+05 83421 85205 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0499 0.1021 0.0028667 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2983e-07 0.051448 0.00031482 5.2709e-06 INSTANT 0.875929000E-01 TIME STEP NUMBER 56127 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283250087E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.817503974E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.83230E-02 0.20875E+01 Friction velocity uk : 0.83230E-02 0.20875E+01 Dimensionless distance yplus : 0.81095E-02 0.20498E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.858168091e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29474E+08 1 0.18075E-09 0.25520E+02 0.19508E+04 c Velocity[X] 0.13459E+02 c Velocity[Y] 0.12061E+02 c Velocity[Z] 0.14686E-05 c Pressure 0.22767E-03 155 0.76784E-04 0.21556E-02 0.35013E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -24.021 37.632 5.6134 8.0073 v Velocity[Y] -26.805 28.057 -0.1455 -0.0051623 v Velocity[Z] -2.9545 3.0521 2.5873e-06 -5.3884e-08 v ǁVelocityǁ 0.0010503 37.758 7.865 8.1055 v Pressure -2.2335e+05 1.8155e+05 -19821 -17241 v TurbVisc 1.6473e-19 0.016635 0.0001731 2.8686e-05 v CourantNb 1.475e-08 0.011674 0.00016841 4.9425e-06 v FourierNb 1.2425e-07 0.046091 0.00014642 3.2875e-07 v total_pressure -1.2202e+05 2.8287e+05 81504 84084 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0498 0.10211 0.0028669 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2988e-07 0.051442 0.00031483 5.2713e-06 INSTANT 0.875930000E-01 TIME STEP NUMBER 56128 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283249116E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.817596618E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10815E-01 0.20873E+01 Friction velocity uk : 0.10815E-01 0.20873E+01 Dimensionless distance yplus : 0.10537E-01 0.20495E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.835374568e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29474E+08 1 0.18076E-09 0.25529E+02 0.19510E+04 c Velocity[X] 0.13465E+02 c Velocity[Y] 0.12064E+02 c Velocity[Z] 0.14590E-05 c Pressure 0.22698E-03 173 0.81730E-04 0.21478E-02 0.36722E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -24.032 37.648 5.6134 8.0073 v Velocity[Y] -26.817 28.069 -0.14552 -0.0051962 v Velocity[Z] -2.9543 3.0522 2.5866e-06 -5.3884e-08 v ǁVelocityǁ 0.0010449 37.774 7.8667 8.1057 v Pressure -2.254e+05 1.7974e+05 -21826 -18479 v TurbVisc 1.7642e-19 0.016654 0.00017317 2.8733e-05 v CourantNb 1.1305e-08 0.011674 0.00016841 4.9426e-06 v FourierNb 1.2425e-07 0.046085 0.00014642 3.2907e-07 v total_pressure -1.2408e+05 2.8106e+05 79499 82846 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0495 0.10213 0.0028671 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2993e-07 0.051436 0.00031484 5.2717e-06 INSTANT 0.875931000E-01 TIME STEP NUMBER 56129 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283248046E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.817681438E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10791E-01 0.20871E+01 Friction velocity uk : 0.10791E-01 0.20871E+01 Dimensionless distance yplus : 0.10514E-01 0.20494E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.839237670e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29474E+08 1 0.18077E-09 0.25536E+02 0.19512E+04 c Velocity[X] 0.13471E+02 c Velocity[Y] 0.12065E+02 c Velocity[Z] 0.14506E-05 c Pressure 0.22639E-03 555 0.94892E-04 0.21410E-02 0.30578E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -24.042 37.664 5.6134 8.0072 v Velocity[Y] -26.829 28.08 -0.14553 -0.0052275 v Velocity[Z] -2.954 3.0524 2.5859e-06 -5.3884e-08 v ǁVelocityǁ 0.001039 37.79 7.8683 8.1058 v Pressure -2.2744e+05 1.7795e+05 -23750 -19468 v TurbVisc 1.3069e-19 0.016672 0.00017324 2.8781e-05 v CourantNb 1.1667e-08 0.011673 0.00016841 4.9426e-06 v FourierNb 1.2425e-07 0.046078 0.00014643 3.294e-07 v total_pressure -1.2611e+05 2.7927e+05 77575 81857 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0494 0.10214 0.0028673 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2999e-07 0.05143 0.00031484 5.2721e-06 INSTANT 0.875932000E-01 TIME STEP NUMBER 56130 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283246617E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.817755168E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10512E-01 0.20869E+01 Friction velocity uk : 0.10512E-01 0.20869E+01 Dimensionless distance yplus : 0.10242E-01 0.20492E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.782413210e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29473E+08 1 0.18078E-09 0.25535E+02 0.19511E+04 c Velocity[X] 0.13477E+02 c Velocity[Y] 0.12057E+02 c Velocity[Z] 0.14456E-05 c Pressure 0.22563E-03 113 0.80581E-04 0.21327E-02 0.34739E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -24.053 37.679 5.6134 8.0072 v Velocity[Y] -26.842 28.091 -0.14555 -0.0052607 v Velocity[Z] -2.9538 3.0526 2.5853e-06 -5.3884e-08 v ǁVelocityǁ 0.0010356 37.806 7.8699 8.1059 v Pressure -2.2949e+05 1.7614e+05 -25713 -20711 v TurbVisc 7.6336e-20 0.016691 0.00017331 2.8828e-05 v CourantNb 1.4145e-08 0.011673 0.00016842 4.9427e-06 v FourierNb 1.2425e-07 0.046072 0.00014643 3.2973e-07 v total_pressure -1.2816e+05 2.7747e+05 75612 80614 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0492 0.10216 0.0028675 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.3004e-07 0.051424 0.00031485 5.2724e-06 INSTANT 0.875933000E-01 TIME STEP NUMBER 56131 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283245142E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.817814628E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10527E-01 0.20867E+01 Friction velocity uk : 0.10527E-01 0.20867E+01 Dimensionless distance yplus : 0.10256E-01 0.20490E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.656664260e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29473E+08 1 0.18079E-09 0.25546E+02 0.19515E+04 c Velocity[X] 0.13483E+02 c Velocity[Y] 0.12062E+02 c Velocity[Z] 0.14494E-05 c Pressure 0.22296E-03 10 0.59771E-04 0.21063E-02 0.27434E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -24.064 37.695 5.6134 8.0072 v Velocity[Y] -26.854 28.102 -0.14557 -0.005295 v Velocity[Z] -2.9536 3.0528 2.5846e-06 -5.3884e-08 v ǁVelocityǁ 0.0010087 37.821 7.8716 8.106 v Pressure -2.3145e+05 1.7443e+05 -27636 -21731 v TurbVisc 1.475e-19 0.016709 0.00017338 2.8876e-05 v CourantNb 1.8624e-08 0.011672 0.00016842 4.9428e-06 v FourierNb 1.2425e-07 0.046066 0.00014643 3.3005e-07 v total_pressure -1.3012e+05 2.7575e+05 73689 79594 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.049 0.10217 0.0028677 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.3009e-07 0.051418 0.00031486 5.2728e-06 INSTANT 0.875934000E-01 TIME STEP NUMBER 56132 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283243449E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.817862367E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.81061E-02 0.20866E+01 Friction velocity uk : 0.81061E-02 0.20866E+01 Dimensionless distance yplus : 0.78981E-02 0.20488E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.483726077e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29473E+08 1 0.18080E-09 0.25552E+02 0.19517E+04 c Velocity[X] 0.13492E+02 c Velocity[Y] 0.12060E+02 c Velocity[Z] 0.14381E-05 c Pressure 0.22232E-03 278 0.76442E-04 0.20990E-02 0.33289E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -24.074 37.71 5.6134 8.0071 v Velocity[Y] -26.866 28.114 -0.14559 -0.0053273 v Velocity[Z] -2.9533 3.0529 2.5839e-06 -5.3884e-08 v ǁVelocityǁ 0.0010277 37.837 7.8732 8.1061 v Pressure -2.3353e+05 1.7259e+05 -29548 -22893 v TurbVisc 1.647e-19 0.016728 0.00017344 2.8924e-05 v CourantNb 1.3398e-08 0.011672 0.00016842 4.9428e-06 v FourierNb 1.2425e-07 0.046059 0.00014644 3.3038e-07 v total_pressure -1.3221e+05 2.7391e+05 71777 78432 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0488 0.10219 0.0028678 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.3009e-07 0.051412 0.00031486 5.2732e-06 INSTANT 0.875935000E-01 TIME STEP NUMBER 56133 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283241637E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.817896919E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.99503E-02 0.20864E+01 Friction velocity uk : 0.99503E-02 0.20864E+01 Dimensionless distance yplus : 0.96950E-02 0.20486E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.278563009e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29473E+08 1 0.18081E-09 0.25561E+02 0.19519E+04 c Velocity[X] 0.13499E+02 c Velocity[Y] 0.12062E+02 c Velocity[Z] 0.14286E-05 c Pressure 0.22113E-03 68 0.81906E-04 0.20867E-02 0.33268E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -24.085 37.725 5.6134 8.0071 v Velocity[Y] -26.878 28.125 -0.1456 -0.0053623 v Velocity[Z] -2.9531 3.0531 2.5832e-06 -5.3884e-08 v ǁVelocityǁ 0.0010237 37.852 7.8748 8.1062 v Pressure -2.3553e+05 1.7084e+05 -31503 -24107 v TurbVisc 1.4753e-19 0.016746 0.00017351 2.8971e-05 v CourantNb 1.4827e-08 0.011671 0.00016843 4.9429e-06 v FourierNb 1.2425e-07 0.046053 0.00014644 3.3071e-07 v total_pressure -1.342e+05 2.7216e+05 69822 77218 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0486 0.1022 0.002868 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.3008e-07 0.051406 0.00031487 5.2736e-06 INSTANT 0.875936000E-01 TIME STEP NUMBER 56134 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283239734E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.817927158E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.90764E-02 0.20862E+01 Friction velocity uk : 0.90764E-02 0.20862E+01 Dimensionless distance yplus : 0.87768E-02 0.20485E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.142611288e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29473E+08 1 0.18082E-09 0.25569E+02 0.19522E+04 c Velocity[X] 0.13506E+02 c Velocity[Y] 0.12063E+02 c Velocity[Z] 0.14209E-05 c Pressure 0.22003E-03 257 0.94911E-04 0.20751E-02 0.27969E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -24.095 37.74 5.6134 8.007 v Velocity[Y] -26.89 28.136 -0.14562 -0.0053944 v Velocity[Z] -2.9529 3.0533 2.5826e-06 -5.3884e-08 v ǁVelocityǁ 0.0010199 37.868 7.8764 8.1063 v Pressure -2.3751e+05 1.6909e+05 -33383 -25084 v TurbVisc 1.7979e-19 0.016765 0.00017358 2.9019e-05 v CourantNb 1.4313e-08 0.011671 0.00016843 4.9429e-06 v FourierNb 1.2425e-07 0.046046 0.00014645 3.3104e-07 v total_pressure -1.3619e+05 2.7042e+05 67942 76241 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0485 0.10222 0.0028682 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.3007e-07 0.051399 0.00031487 5.2739e-06 INSTANT 0.875937000E-01 TIME STEP NUMBER 56135 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283237483E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.817947632E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.71631E-02 0.20860E+01 Friction velocity uk : 0.71631E-02 0.20860E+01 Dimensionless distance yplus : 0.69266E-02 0.20483E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 9.060820380e-03 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29473E+08 1 0.18083E-09 0.25567E+02 0.19521E+04 c Velocity[X] 0.13513E+02 c Velocity[Y] 0.12055E+02 c Velocity[Z] 0.14135E-05 c Pressure 0.21878E-03 123 0.80868E-04 0.20623E-02 0.30859E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -24.106 37.756 5.6134 8.007 v Velocity[Y] -26.902 28.147 -0.14564 -0.0054286 v Velocity[Z] -2.9527 3.0535 2.5819e-06 -5.3884e-08 v ǁVelocityǁ 0.0010156 37.883 7.8781 8.1064 v Pressure -2.3948e+05 1.6737e+05 -35285 -26285 v TurbVisc 1.858e-19 0.016783 0.00017365 2.9067e-05 v CourantNb 2.2833e-08 0.01167 0.00016843 4.9429e-06 v FourierNb 1.2425e-07 0.04604 0.00014645 3.3136e-07 v total_pressure -1.3816e+05 2.6869e+05 66040 75040 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0483 0.10223 0.0028683 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.3005e-07 0.051393 0.00031488 5.2743e-06 INSTANT 0.875938000E-01 TIME STEP NUMBER 56136 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283235189E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.817954090E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.45649E-02 0.20858E+01 Friction velocity uk : 0.45649E-02 0.20858E+01 Dimensionless distance yplus : 0.44142E-02 0.20481E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 6.614019256e-03 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29472E+08 1 0.18083E-09 0.25579E+02 0.19525E+04 c Velocity[X] 0.13520E+02 c Velocity[Y] 0.12059E+02 c Velocity[Z] 0.14149E-05 c Pressure 0.21551E-03 10 0.59573E-04 0.20303E-02 0.24434E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -24.116 37.771 5.6134 8.0069 v Velocity[Y] -26.915 28.157 -0.14566 -0.0054638 v Velocity[Z] -2.9524 3.0536 2.5812e-06 -5.3884e-08 v ǁVelocityǁ 0.00098873 37.898 7.8797 8.1065 v Pressure -2.4137e+05 1.6573e+05 -37146 -27275 v TurbVisc 1.9639e-19 0.016802 0.00017371 2.9115e-05 v CourantNb 2.1339e-08 0.01167 0.00016844 4.943e-06 v FourierNb 1.2425e-07 0.046033 0.00014645 3.3169e-07 v total_pressure -1.4004e+05 2.6705e+05 64179 74050 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0481 0.10225 0.0028684 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.3004e-07 0.051387 0.00031489 5.2747e-06 INSTANT 0.875939000E-01 TIME STEP NUMBER 56137 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283232688E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.817948005E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.22634E-02 0.20856E+01 Friction velocity uk : 0.22634E-02 0.20856E+01 Dimensionless distance yplus : 0.21887E-02 0.20479E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 3.009758585e-03 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29472E+08 1 0.18084E-09 0.25586E+02 0.19527E+04 c Velocity[X] 0.13529E+02 c Velocity[Y] 0.12057E+02 c Velocity[Z] 0.14044E-05 c Pressure 0.21437E-03 149 0.76735E-04 0.20185E-02 0.29512E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -24.127 37.786 5.6134 8.0069 v Velocity[Y] -26.927 28.168 -0.14568 -0.0054971 v Velocity[Z] -2.9522 3.0538 2.5805e-06 -5.3884e-08 v ǁVelocityǁ 0.001005 37.913 7.8813 8.1066 v Pressure -2.4337e+05 1.6397e+05 -38988 -28393 v TurbVisc 1.9397e-19 0.01682 0.00017378 2.9163e-05 v CourantNb 2.0293e-08 0.011669 0.00016844 4.943e-06 v FourierNb 1.2425e-07 0.046027 0.00014646 3.3202e-07 v total_pressure -1.4204e+05 2.653e+05 62337 72932 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0479 0.10226 0.0028685 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.3003e-07 0.051381 0.00031489 5.2751e-06 INSTANT 0.875940000E-01 TIME STEP NUMBER 56138 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283230063E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.817928334E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.18507E-02 0.20854E+01 Friction velocity uk : 0.18507E-02 0.20854E+01 Dimensionless distance yplus : 0.17896E-02 0.20477E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 2.208620408e-04 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29472E+08 1 0.18085E-09 0.25595E+02 0.19530E+04 c Velocity[X] 0.13537E+02 c Velocity[Y] 0.12058E+02 c Velocity[Z] 0.13948E-05 c Pressure 0.21267E-03 66 0.82199E-04 0.20014E-02 0.29759E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -24.137 37.8 5.6134 8.0068 v Velocity[Y] -26.939 28.179 -0.1457 -0.005533 v Velocity[Z] -2.952 3.054 2.5799e-06 -5.3884e-08 v ǁVelocityǁ 0.00099771 37.928 7.8829 8.1067 v Pressure -2.4528e+05 1.623e+05 -40872 -29572 v TurbVisc 2.0095e-19 0.016839 0.00017385 2.9211e-05 v CourantNb 1.7768e-08 0.011669 0.00016844 4.9431e-06 v FourierNb 1.2425e-07 0.04602 0.00014646 3.3235e-07 v total_pressure -1.4395e+05 2.6363e+05 60453 71753 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0477 0.10227 0.0028685 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.3001e-07 0.051374 0.0003149 5.2754e-06 INSTANT 0.875941000E-01 TIME STEP NUMBER 56139 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283227360E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.817903864E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13398E-02 0.20852E+01 Friction velocity uk : 0.13398E-02 0.20852E+01 Dimensionless distance yplus : 0.12956E-02 0.20475E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -2.763095587e-03 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29472E+08 1 0.18086E-09 0.25603E+02 0.19532E+04 c Velocity[X] 0.13544E+02 c Velocity[Y] 0.12059E+02 c Velocity[Z] 0.13839E-05 c Pressure 0.21108E-03 459 0.95260E-04 0.19853E-02 0.24642E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -24.148 37.815 5.6134 8.0068 v Velocity[Y] -26.951 28.19 -0.14571 -0.005566 v Velocity[Z] -2.9517 3.0542 2.5792e-06 -5.3884e-08 v ǁVelocityǁ 0.00098913 37.943 7.8846 8.1068 v Pressure -2.4717e+05 1.6066e+05 -42671 -30498 v TurbVisc 2.0469e-19 0.016857 0.00017391 2.926e-05 v CourantNb 1.3251e-08 0.011668 0.00016844 4.9431e-06 v FourierNb 1.2425e-07 0.046014 0.00014646 3.3268e-07 v total_pressure -1.4584e+05 2.6198e+05 58654 70827 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0475 0.10229 0.0028689 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.3e-07 0.051368 0.00031491 5.2758e-06 INSTANT 0.875942000E-01 TIME STEP NUMBER 56140 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283224316E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.817870351E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.14403E-02 0.20850E+01 Friction velocity uk : 0.14403E-02 0.20850E+01 Dimensionless distance yplus : 0.13928E-02 0.20473E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -6.204879371e-03 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29472E+08 1 0.18086E-09 0.25602E+02 0.19531E+04 c Velocity[X] 0.13552E+02 c Velocity[Y] 0.12050E+02 c Velocity[Z] 0.13785E-05 c Pressure 0.20936E-03 172 0.81142E-04 0.19681E-02 0.27396E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -24.158 37.83 5.6134 8.0067 v Velocity[Y] -26.963 28.2 -0.14573 -0.0056011 v Velocity[Z] -2.9515 3.0543 2.5785e-06 -5.3884e-08 v ǁVelocityǁ 0.00098062 37.958 7.8862 8.1069 v Pressure -2.4904e+05 1.5903e+05 -44492 -31658 v TurbVisc 2.112e-19 0.016876 0.00017398 2.9307e-05 v CourantNb 1.264e-08 0.011668 0.00016845 4.9432e-06 v FourierNb 1.2425e-07 0.046007 0.00014647 3.3301e-07 v total_pressure -1.4771e+05 2.6035e+05 56833 69667 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0473 0.10231 0.0028692 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2998e-07 0.051361 0.00031491 5.2762e-06 INSTANT 0.875943000E-01 TIME STEP NUMBER 56141 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283221240E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.817823446E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.32119E-02 0.20847E+01 Friction velocity uk : 0.32119E-02 0.20847E+01 Dimensionless distance yplus : 0.31059E-02 0.20470E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -9.864792420e-03 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29471E+08 1 0.18087E-09 0.25614E+02 0.19535E+04 c Velocity[X] 0.13560E+02 c Velocity[Y] 0.12055E+02 c Velocity[Z] 0.13792E-05 c Pressure 0.20551E-03 10 0.59319E-04 0.19309E-02 0.21376E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -24.168 37.845 5.6134 8.0067 v Velocity[Y] -26.974 28.211 -0.14575 -0.0056373 v Velocity[Z] -2.9513 3.0545 2.5778e-06 -5.3884e-08 v ǁVelocityǁ 0.00094852 37.973 7.8878 8.107 v Pressure -2.5082e+05 1.5749e+05 -46264 -32600 v TurbVisc 2.072e-19 0.016894 0.00017405 2.9356e-05 v CourantNb 9.3705e-09 0.011667 0.00016845 4.9432e-06 v FourierNb 1.2425e-07 0.046 0.00014647 3.3334e-07 v total_pressure -1.4949e+05 2.5882e+05 55061 68725 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.047 0.10233 0.0028694 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2997e-07 0.051355 0.00031492 5.2765e-06 INSTANT 0.875944000E-01 TIME STEP NUMBER 56142 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283217969E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.817765138E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.32863E-02 0.20845E+01 Friction velocity uk : 0.32863E-02 0.20845E+01 Dimensionless distance yplus : 0.31778E-02 0.20468E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.451518979e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29471E+08 1 0.18087E-09 0.25621E+02 0.19537E+04 c Velocity[X] 0.13569E+02 c Velocity[Y] 0.12052E+02 c Velocity[Z] 0.13684E-05 c Pressure 0.20394E-03 587 0.77192E-04 0.19151E-02 0.25848E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -24.179 37.859 5.6133 8.0066 v Velocity[Y] -26.986 28.221 -0.14577 -0.0056715 v Velocity[Z] -2.951 3.0547 2.5772e-06 -5.3885e-08 v ǁVelocityǁ 0.00095603 37.988 7.8894 8.1071 v Pressure -2.5271e+05 1.5584e+05 -48013 -33659 v TurbVisc 2.0291e-19 0.016913 0.00017411 2.9404e-05 v CourantNb 7.2304e-09 0.011667 0.00016845 4.9432e-06 v FourierNb 1.2425e-07 0.045993 0.00014648 3.3367e-07 v total_pressure -1.5138e+05 2.5717e+05 53312 67666 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0468 0.10234 0.0028696 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2996e-07 0.051348 0.00031493 5.2769e-06 INSTANT 0.875945000E-01 TIME STEP NUMBER 56143 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283214573E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.817694050E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13000E-02 0.20842E+01 Friction velocity uk : 0.13000E-02 0.20842E+01 Dimensionless distance yplus : 0.12571E-02 0.20465E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.762352708e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29471E+08 1 0.18087E-09 0.25631E+02 0.19540E+04 c Velocity[X] 0.13578E+02 c Velocity[Y] 0.12053E+02 c Velocity[Z] 0.13589E-05 c Pressure 0.20178E-03 93 0.82558E-04 0.18938E-02 0.26242E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -24.189 37.874 5.6133 8.0065 v Velocity[Y] -26.998 28.232 -0.14579 -0.0057083 v Velocity[Z] -2.9508 3.0548 2.5765e-06 -5.3885e-08 v ǁVelocityǁ 0.00094137 38.003 7.891 8.1072 v Pressure -2.5449e+05 1.543e+05 -49795 -34781 v TurbVisc 1.2943e-19 0.016931 0.00017418 2.9452e-05 v CourantNb 7.071e-09 0.011666 0.00016845 4.9433e-06 v FourierNb 1.2425e-07 0.045986 0.00014648 3.34e-07 v total_pressure -1.5317e+05 2.5562e+05 51530 66544 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0465 0.10236 0.0028699 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2994e-07 0.051341 0.00031493 5.2773e-06 INSTANT 0.875946000E-01 TIME STEP NUMBER 56144 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283211113E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.817618850E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.28487E-02 0.20840E+01 Friction velocity uk : 0.28487E-02 0.20840E+01 Dimensionless distance yplus : 0.27547E-02 0.20463E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -2.143779608e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29470E+08 1 0.18088E-09 0.25639E+02 0.19543E+04 c Velocity[X] 0.13586E+02 c Velocity[Y] 0.12053E+02 c Velocity[Z] 0.13527E-05 c Pressure 0.19974E-03 331 0.95819E-04 0.18736E-02 0.21995E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -24.199 37.888 5.6133 8.0064 v Velocity[Y] -27.01 28.242 -0.14581 -0.0057423 v Velocity[Z] -2.9506 3.055 2.5758e-06 -5.3885e-08 v ǁVelocityǁ 0.00092494 38.017 7.8926 8.1072 v Pressure -2.5628e+05 1.5276e+05 -51497 -35668 v TurbVisc 1.7926e-19 0.016949 0.00017424 2.9501e-05 v CourantNb 7.3481e-09 0.011666 0.00016846 4.9433e-06 v FourierNb 1.2425e-07 0.045979 0.00014648 3.3434e-07 v total_pressure -1.5496e+05 2.5408e+05 49828 65657 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0463 0.10237 0.0028701 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2992e-07 0.051334 0.00031494 5.2776e-06 INSTANT 0.875947000E-01 TIME STEP NUMBER 56145 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283207321E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.817534812E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.18704E-02 0.20837E+01 Friction velocity uk : 0.18704E-02 0.20837E+01 Dimensionless distance yplus : 0.18086E-02 0.20460E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -2.566074119e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29470E+08 1 0.18088E-09 0.25638E+02 0.19542E+04 c Velocity[X] 0.13594E+02 c Velocity[Y] 0.12044E+02 c Velocity[Z] 0.13441E-05 c Pressure 0.19760E-03 170 0.81459E-04 0.18526E-02 0.23303E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -24.209 37.902 5.6132 8.0064 v Velocity[Y] -27.022 28.252 -0.14583 -0.0057784 v Velocity[Z] -2.9503 3.0552 2.5751e-06 -5.3885e-08 v ǁVelocityǁ 0.00090569 38.032 7.8942 8.1073 v Pressure -2.5818e+05 1.5125e+05 -53199 -36732 v TurbVisc 1.8381e-19 0.016968 0.00017431 2.9549e-05 v CourantNb 3.2153e-09 0.011665 0.00016846 4.9433e-06 v FourierNb 1.2425e-07 0.045972 0.00014649 3.3467e-07 v total_pressure -1.5686e+05 2.5258e+05 48126 64593 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.046 0.10238 0.0028703 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2991e-07 0.051327 0.00031495 5.278e-06 INSTANT 0.875948000E-01 TIME STEP NUMBER 56146 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283203510E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.817438742E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.21725E-02 0.20834E+01 Friction velocity uk : 0.21725E-02 0.20834E+01 Dimensionless distance yplus : 0.21008E-02 0.20457E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -2.944901438e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29470E+08 1 0.18088E-09 0.25650E+02 0.19546E+04 c Velocity[X] 0.13602E+02 c Velocity[Y] 0.12048E+02 c Velocity[Z] 0.13438E-05 c Pressure 0.19316E-03 10 0.59134E-04 0.18100E-02 0.18655E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -24.219 37.917 5.6132 8.0063 v Velocity[Y] -27.034 28.262 -0.14585 -0.0058155 v Velocity[Z] -2.9501 3.0554 2.5745e-06 -5.3885e-08 v ǁVelocityǁ 0.00086564 38.046 7.8958 8.1074 v Pressure -2.5996e+05 1.4984e+05 -54861 -37621 v TurbVisc 1.9856e-19 0.016986 0.00017437 2.9598e-05 v CourantNb 6.3971e-09 0.011665 0.00016846 4.9434e-06 v FourierNb 1.2425e-07 0.045964 0.00014649 3.35e-07 v total_pressure -1.5864e+05 2.5117e+05 46464 63704 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0457 0.1024 0.0028704 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2989e-07 0.05132 0.00031495 5.2784e-06 INSTANT 0.875949000E-01 TIME STEP NUMBER 56147 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283199523E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.817331565E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.18928E-02 0.20831E+01 Friction velocity uk : 0.18928E-02 0.20831E+01 Dimensionless distance yplus : 0.18303E-02 0.20454E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -3.446479360e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29469E+08 1 0.18089E-09 0.25657E+02 0.19548E+04 c Velocity[X] 0.13612E+02 c Velocity[Y] 0.12045E+02 c Velocity[Z] 0.13352E-05 c Pressure 0.19121E-03 735 0.77441E-04 0.17908E-02 0.22853E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -24.229 37.931 5.6132 8.0062 v Velocity[Y] -27.045 28.272 -0.14586 -0.0058504 v Velocity[Z] -2.9498 3.0555 2.5738e-06 -5.3885e-08 v ǁVelocityǁ 0.00085974 38.061 7.8974 8.1074 v Pressure -2.6189e+05 1.4833e+05 -56497 -38622 v TurbVisc 1.9471e-19 0.017005 0.00017443 2.9646e-05 v CourantNb 1.0789e-08 0.011664 0.00016846 4.9434e-06 v FourierNb 1.2425e-07 0.045957 0.0001465 3.3533e-07 v total_pressure -1.6057e+05 2.4965e+05 44828 62703 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0454 0.10241 0.0028705 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2988e-07 0.051312 0.00031496 5.2787e-06 INSTANT 0.875950000E-01 TIME STEP NUMBER 56148 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283195408E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.817212581E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.37477E-02 0.20827E+01 Friction velocity uk : 0.37477E-02 0.20827E+01 Dimensionless distance yplus : 0.36240E-02 0.20450E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -3.818067778e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29469E+08 1 0.18089E-09 0.25666E+02 0.19551E+04 c Velocity[X] 0.13621E+02 c Velocity[Y] 0.12045E+02 c Velocity[Z] 0.13246E-05 c Pressure 0.18863E-03 203 0.83137E-04 0.17657E-02 0.23025E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -24.24 37.945 5.6131 8.0061 v Velocity[Y] -27.057 28.282 -0.14588 -0.0058884 v Velocity[Z] -2.9496 3.0557 2.5731e-06 -5.3885e-08 v ǁVelocityǁ 0.0008339 38.075 7.899 8.1075 v Pressure -2.6371e+05 1.4689e+05 -58153 -39672 v TurbVisc 2.2079e-19 0.017023 0.0001745 2.9695e-05 v CourantNb 1.6926e-08 0.011664 0.00016847 4.9434e-06 v FourierNb 1.2425e-07 0.045949 0.0001465 3.3566e-07 v total_pressure -1.6238e+05 2.4822e+05 43172 61653 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.045 0.10242 0.0028708 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2986e-07 0.051305 0.00031497 5.2791e-06 INSTANT 0.875951000E-01 TIME STEP NUMBER 56149 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283191242E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.817090380E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.76926E-02 0.20823E+01 Friction velocity uk : 0.76926E-02 0.20823E+01 Dimensionless distance yplus : 0.74387E-02 0.20447E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -4.206525033e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29469E+08 1 0.18089E-09 0.25674E+02 0.19554E+04 c Velocity[X] 0.13629E+02 c Velocity[Y] 0.12045E+02 c Velocity[Z] 0.13167E-05 c Pressure 0.18621E-03 231 0.96516E-04 0.17422E-02 0.19240E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -24.25 37.959 5.6131 8.006 v Velocity[Y] -27.069 28.292 -0.1459 -0.0059233 v Velocity[Z] -2.9494 3.0559 2.5725e-06 -5.3885e-08 v ǁVelocityǁ 0.0008067 38.089 7.9005 8.1076 v Pressure -2.6546e+05 1.4551e+05 -59723 -40486 v TurbVisc 1.4858e-19 0.017041 0.00017456 2.9744e-05 v CourantNb 2.2587e-08 0.011663 0.00016847 4.9434e-06 v FourierNb 1.2425e-07 0.045941 0.0001465 3.36e-07 v total_pressure -1.6414e+05 2.4683e+05 41602 60839 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0447 0.10243 0.0028709 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2984e-07 0.051297 0.00031497 5.2794e-06 INSTANT 0.875952000E-01 TIME STEP NUMBER 56150 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283186753E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.816960126E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10626E-01 0.20820E+01 Friction velocity uk : 0.10626E-01 0.20820E+01 Dimensionless distance yplus : 0.10275E-01 0.20443E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -4.643470954e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29468E+08 1 0.18089E-09 0.25673E+02 0.19553E+04 c Velocity[X] 0.13637E+02 c Velocity[Y] 0.12035E+02 c Velocity[Z] 0.13133E-05 c Pressure 0.18369E-03 387 0.82012E-04 0.17177E-02 0.19697E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -24.26 37.973 5.613 8.0059 v Velocity[Y] -27.08 28.302 -0.14592 -0.0059601 v Velocity[Z] -2.9491 3.056 2.5718e-06 -5.3885e-08 v ǁVelocityǁ 0.00077424 38.104 7.9021 8.1076 v Pressure -2.672e+05 1.4416e+05 -61293 -41449 v TurbVisc 2.2235e-19 0.01706 0.00017462 2.9792e-05 v CourantNb 1.7481e-08 0.011663 0.00016847 4.9435e-06 v FourierNb 1.2425e-07 0.045933 0.00014651 3.3633e-07 v total_pressure -1.6587e+05 2.4548e+05 40032 59876 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0443 0.10244 0.0028711 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2983e-07 0.051289 0.00031498 5.2798e-06 INSTANT 0.875953000E-01 TIME STEP NUMBER 56151 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283182278E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.816818427E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12153E-01 0.20816E+01 Friction velocity uk : 0.12153E-01 0.20816E+01 Dimensionless distance yplus : 0.11798E-01 0.20439E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -5.037591289e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29468E+08 1 0.18089E-09 0.25685E+02 0.19557E+04 c Velocity[X] 0.13645E+02 c Velocity[Y] 0.12039E+02 c Velocity[Z] 0.13274E-05 c Pressure 0.17867E-03 9 0.59582E-04 0.16699E-02 0.16648E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -24.269 37.987 5.6129 8.0058 v Velocity[Y] -27.092 28.312 -0.14593 -0.0059984 v Velocity[Z] -2.9489 3.0562 2.5711e-06 -5.3885e-08 v ǁVelocityǁ 0.00072547 38.118 7.9037 8.1077 v Pressure -2.689e+05 1.4286e+05 -62826 -42299 v TurbVisc 2.245e-19 0.017078 0.00017469 2.9841e-05 v CourantNb 1.3827e-08 0.011662 0.00016847 4.9435e-06 v FourierNb 1.2425e-07 0.045925 0.00014651 3.3666e-07 v total_pressure -1.6757e+05 2.4419e+05 38499 59026 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0439 0.10245 0.0028712 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2981e-07 0.05128 0.00031499 5.2801e-06 INSTANT 0.875954000E-01 TIME STEP NUMBER 56152 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283177617E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.816667177E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.67052E-02 0.20811E+01 Friction velocity uk : 0.67052E-02 0.20811E+01 Dimensionless distance yplus : 0.65093E-02 0.20435E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -5.553273990e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29467E+08 1 0.18089E-09 0.25691E+02 0.19559E+04 c Velocity[X] 0.13656E+02 c Velocity[Y] 0.12035E+02 c Velocity[Z] 0.13096E-05 c Pressure 0.17646E-03 467 0.77862E-04 0.16483E-02 0.19801E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -24.279 38.001 5.6129 8.0057 v Velocity[Y] -27.103 28.322 -0.14595 -0.0060342 v Velocity[Z] -2.9487 3.0564 2.5704e-06 -5.3885e-08 v ǁVelocityǁ 0.000705 38.132 7.9053 8.1077 v Pressure -2.7067e+05 1.4149e+05 -64320 -43212 v TurbVisc 2.0411e-19 0.017097 0.00017475 2.989e-05 v CourantNb 1.2909e-08 0.011662 0.00016847 4.9435e-06 v FourierNb 1.2425e-07 0.045917 0.00014652 3.37e-07 v total_pressure -1.6935e+05 2.4282e+05 37005 58113 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0435 0.10246 0.0028713 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2979e-07 0.051272 0.00031499 5.2805e-06 INSTANT 0.875955000E-01 TIME STEP NUMBER 56153 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283172847E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.816506557E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.72090E-02 0.20807E+01 Friction velocity uk : 0.72090E-02 0.20807E+01 Dimensionless distance yplus : 0.70402E-02 0.20430E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -5.863843988e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29467E+08 1 0.18089E-09 0.25700E+02 0.19562E+04 c Velocity[X] 0.13664E+02 c Velocity[Y] 0.12035E+02 c Velocity[Z] 0.12963E-05 c Pressure 0.17347E-03 50 0.83279E-04 0.16196E-02 0.19203E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -24.289 38.015 5.6128 8.0056 v Velocity[Y] -27.115 28.331 -0.14597 -0.006073 v Velocity[Z] -2.9484 3.0566 2.5698e-06 -5.3885e-08 v ǁVelocityǁ 0.00066806 38.146 7.9068 8.1078 v Pressure -2.7232e+05 1.4025e+05 -65815 -44128 v TurbVisc 2.3562e-19 0.017115 0.00017481 2.9939e-05 v CourantNb 8.27e-09 0.011661 0.00016848 4.9435e-06 v FourierNb 1.2425e-07 0.045908 0.00014652 3.3733e-07 v total_pressure -1.7099e+05 2.4158e+05 35510 57197 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.043 0.10246 0.0028714 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2977e-07 0.051263 0.000315 5.2809e-06 INSTANT 0.875956000E-01 TIME STEP NUMBER 56154 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283168064E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.816340974E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.28873E-02 0.20802E+01 Friction velocity uk : 0.28873E-02 0.20802E+01 Dimensionless distance yplus : 0.28197E-02 0.20426E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -6.288251261e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29467E+08 1 0.18088E-09 0.25708E+02 0.19565E+04 c Velocity[X] 0.13672E+02 c Velocity[Y] 0.12035E+02 c Velocity[Z] 0.12863E-05 c Pressure 0.17071E-03 303 0.96766E-04 0.15930E-02 0.17594E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -24.299 38.029 5.6127 8.0055 v Velocity[Y] -27.126 28.341 -0.14598 -0.0061091 v Velocity[Z] -2.9482 3.0567 2.5691e-06 -5.3885e-08 v ǁVelocityǁ 0.00062992 38.16 7.9084 8.1078 v Pressure -2.7396e+05 1.39e+05 -67261 -44939 v TurbVisc 2.2825e-19 0.017133 0.00017487 2.9988e-05 v CourantNb 8.234e-09 0.011661 0.00016848 4.9435e-06 v FourierNb 1.2425e-07 0.0459 0.00014653 3.3767e-07 v total_pressure -1.7264e+05 2.4032e+05 34064 56386 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0426 0.10247 0.0028715 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2975e-07 0.051254 0.00031501 5.2812e-06 INSTANT 0.875957000E-01 TIME STEP NUMBER 56155 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283162923E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.816168370E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.95820E-02 0.20797E+01 Friction velocity uk : 0.95820E-02 0.20797E+01 Dimensionless distance yplus : 0.92948E-02 0.20421E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -6.678193375e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29466E+08 1 0.18088E-09 0.25706E+02 0.19563E+04 c Velocity[X] 0.13680E+02 c Velocity[Y] 0.12025E+02 c Velocity[Z] 0.12808E-05 c Pressure 0.16794E-03 118 0.82010E-04 0.15664E-02 0.16694E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -24.309 38.043 5.6127 8.0054 v Velocity[Y] -27.138 28.35 -0.146 -0.006147 v Velocity[Z] -2.948 3.0569 2.5684e-06 -5.3885e-08 v ǁVelocityǁ 0.00059181 38.174 7.91 8.1079 v Pressure -2.7556e+05 1.3784e+05 -68668 -45801 v TurbVisc 2.3326e-19 0.017152 0.00017493 3.0036e-05 v CourantNb 1.1442e-08 0.01166 0.00016848 4.9436e-06 v FourierNb 1.2425e-07 0.045891 0.00014653 3.38e-07 v total_pressure -1.7423e+05 2.3917e+05 32657 55524 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0421 0.10248 0.0028717 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2974e-07 0.051245 0.00031501 5.2816e-06 INSTANT 0.875958000E-01 TIME STEP NUMBER 56156 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283157825E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.815987238E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.29959E-02 0.20792E+01 Friction velocity uk : 0.29959E-02 0.20792E+01 Dimensionless distance yplus : 0.29061E-02 0.20416E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -7.081255600e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29466E+08 1 0.18088E-09 0.25717E+02 0.19567E+04 c Velocity[X] 0.13688E+02 c Velocity[Y] 0.12028E+02 c Velocity[Z] 0.12894E-05 c Pressure 0.16238E-03 9 0.58287E-04 0.15137E-02 0.13423E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -24.319 38.056 5.6126 8.0053 v Velocity[Y] -27.149 28.359 -0.14601 -0.0061861 v Velocity[Z] -2.9477 3.0571 2.5678e-06 -5.3885e-08 v ǁVelocityǁ 0.00054296 38.188 7.9115 8.1079 v Pressure -2.7706e+05 1.3675e+05 -70034 -46526 v TurbVisc 2.3026e-19 0.01717 0.000175 3.0086e-05 v CourantNb 1.7507e-08 0.01166 0.00016848 4.9436e-06 v FourierNb 1.2425e-07 0.045882 0.00014654 3.3834e-07 v total_pressure -1.7573e+05 2.3808e+05 31291 54799 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0416 0.1025 0.0028718 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2972e-07 0.051236 0.00031502 5.2819e-06 INSTANT 0.875959000E-01 TIME STEP NUMBER 56157 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283152594E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.815796922E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10479E-01 0.20787E+01 Friction velocity uk : 0.10479E-01 0.20787E+01 Dimensionless distance yplus : 0.10165E-01 0.20411E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -7.565587365e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29465E+08 1 0.18088E-09 0.25722E+02 0.19569E+04 c Velocity[X] 0.13698E+02 c Velocity[Y] 0.12025E+02 c Velocity[Z] 0.12755E-05 c Pressure 0.15994E-03 159 0.77579E-04 0.14902E-02 0.17008E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -24.328 38.07 5.6125 8.0052 v Velocity[Y] -27.161 28.369 -0.14603 -0.006223 v Velocity[Z] -2.9475 3.0572 2.5671e-06 -5.3885e-08 v ǁVelocityǁ 0.00051529 38.202 7.9131 8.108 v Pressure -2.7868e+05 1.3556e+05 -71370 -47358 v TurbVisc 2.1123e-19 0.017189 0.00017506 3.0135e-05 v CourantNb 2.3644e-08 0.01166 0.00016848 4.9436e-06 v FourierNb 1.2425e-07 0.045873 0.00014654 3.3868e-07 v total_pressure -1.7735e+05 2.3689e+05 29955 53967 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0411 0.1025 0.0028719 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.297e-07 0.051226 0.00031503 5.2823e-06 INSTANT 0.875960000E-01 TIME STEP NUMBER 56158 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283147217E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.815598105E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13883E-01 0.20781E+01 Friction velocity uk : 0.13883E-01 0.20781E+01 Dimensionless distance yplus : 0.13467E-01 0.20405E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -7.850914459e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29465E+08 1 0.18087E-09 0.25730E+02 0.19571E+04 c Velocity[X] 0.13707E+02 c Velocity[Y] 0.12024E+02 c Velocity[Z] 0.12622E-05 c Pressure 0.15667E-03 400 0.83170E-04 0.14589E-02 0.17507E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -24.338 38.084 5.6124 8.0051 v Velocity[Y] -27.172 28.378 -0.14604 -0.0062628 v Velocity[Z] -2.9472 3.0574 2.5664e-06 -5.3885e-08 v ǁVelocityǁ 0.00048027 38.216 7.9146 8.108 v Pressure -2.8017e+05 1.3446e+05 -72720 -48238 v TurbVisc 2.334e-19 0.017207 0.00017512 3.0184e-05 v CourantNb 3.1014e-08 0.011659 0.00016849 4.9436e-06 v FourierNb 1.2425e-07 0.045864 0.00014655 3.3901e-07 v total_pressure -1.7885e+05 2.3579e+05 28605 53087 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0405 0.10251 0.002872 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2968e-07 0.051217 0.00031503 5.2826e-06 INSTANT 0.875961000E-01 TIME STEP NUMBER 56159 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283141852E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.815394605E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.86001E-02 0.20775E+01 Friction velocity uk : 0.86001E-02 0.20775E+01 Dimensionless distance yplus : 0.83555E-02 0.20399E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -8.235391703e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29464E+08 1 0.18087E-09 0.25737E+02 0.19574E+04 c Velocity[X] 0.13714E+02 c Velocity[Y] 0.12024E+02 c Velocity[Z] 0.12544E-05 c Pressure 0.15375E-03 204 0.96974E-04 0.14311E-02 0.13677E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -24.348 38.097 5.6123 8.005 v Velocity[Y] -27.183 28.387 -0.14605 -0.0062996 v Velocity[Z] -2.947 3.0576 2.5658e-06 -5.3885e-08 v ǁVelocityǁ 0.00044896 38.229 7.9162 8.108 v Pressure -2.8156e+05 1.3344e+05 -73953 -48817 v TurbVisc 2.3065e-19 0.017225 0.00017518 3.0233e-05 v CourantNb 3.9002e-08 0.011659 0.00016849 4.9436e-06 v FourierNb 1.2425e-07 0.045854 0.00014655 3.3935e-07 v total_pressure -1.8024e+05 2.3476e+05 27372 52508 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0399 0.10252 0.002872 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2966e-07 0.051207 0.00031504 5.283e-06 INSTANT 0.875962000E-01 TIME STEP NUMBER 56160 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283136184E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.815186781E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.49968E-02 0.20769E+01 Friction velocity uk : 0.49968E-02 0.20769E+01 Dimensionless distance yplus : 0.48920E-02 0.20394E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -8.614364461e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29464E+08 1 0.18087E-09 0.25734E+02 0.19572E+04 c Velocity[X] 0.13722E+02 c Velocity[Y] 0.12013E+02 c Velocity[Z] 0.12475E-05 c Pressure 0.15075E-03 94 0.82068E-04 0.14024E-02 0.15648E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -24.357 38.111 5.6122 8.0049 v Velocity[Y] -27.194 28.396 -0.14606 -0.0063384 v Velocity[Z] -2.9468 3.0578 2.5651e-06 -5.3885e-08 v ǁVelocityǁ 0.00042463 38.243 7.9177 8.1081 v Pressure -2.8302e+05 1.324e+05 -75214 -49669 v TurbVisc 2.3624e-19 0.017244 0.00017524 3.0282e-05 v CourantNb 4.6525e-08 0.011658 0.00016849 4.9436e-06 v FourierNb 1.2425e-07 0.045844 0.00014656 3.3968e-07 v total_pressure -1.817e+05 2.3372e+05 26111 51656 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0394 0.10252 0.002872 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2964e-07 0.051197 0.00031505 5.2833e-06 INSTANT 0.875963000E-01 TIME STEP NUMBER 56161 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283130544E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.814968573E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.93938E-02 0.20763E+01 Friction velocity uk : 0.93938E-02 0.20763E+01 Dimensionless distance yplus : 0.91968E-02 0.20387E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -8.969039206e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29463E+08 1 0.18086E-09 0.25744E+02 0.19575E+04 c Velocity[X] 0.13729E+02 c Velocity[Y] 0.12016E+02 c Velocity[Z] 0.12486E-05 c Pressure 0.14472E-03 9 0.57525E-04 0.13457E-02 0.11003E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -24.367 38.124 5.6121 8.0048 v Velocity[Y] -27.206 28.405 -0.14608 -0.0063785 v Velocity[Z] -2.9465 3.0579 2.5644e-06 -5.3885e-08 v ǁVelocityǁ 0.00037597 38.257 7.9193 8.1081 v Pressure -2.8432e+05 1.3147e+05 -76401 -50288 v TurbVisc 2.3277e-19 0.017262 0.0001753 3.0331e-05 v CourantNb 5.4454e-08 0.011658 0.00016849 4.9436e-06 v FourierNb 1.2425e-07 0.045835 0.00014656 3.4002e-07 v total_pressure -1.83e+05 2.328e+05 24924 51037 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0387 0.10253 0.0028721 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2962e-07 0.051187 0.00031505 5.2836e-06 INSTANT 0.875964000E-01 TIME STEP NUMBER 56162 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283124806E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.814743128E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.16244E-01 0.20757E+01 Friction velocity uk : 0.16244E-01 0.20757E+01 Dimensionless distance yplus : 0.15757E-01 0.20381E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -9.409451780e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29463E+08 1 0.18086E-09 0.25749E+02 0.19577E+04 c Velocity[X] 0.13738E+02 c Velocity[Y] 0.12012E+02 c Velocity[Z] 0.12404E-05 c Pressure 0.14223E-03 165 0.77888E-04 0.13218E-02 0.14514E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -24.376 38.138 5.612 8.0046 v Velocity[Y] -27.217 28.414 -0.14609 -0.0064164 v Velocity[Z] -2.9463 3.0581 2.5638e-06 -5.3885e-08 v ǁVelocityǁ 0.00030471 38.27 7.9208 8.1081 v Pressure -2.8576e+05 1.3045e+05 -77556 -51017 v TurbVisc 2.0905e-19 0.01728 0.00017536 3.0381e-05 v CourantNb 6.1926e-08 0.011657 0.00016849 4.9436e-06 v FourierNb 1.2425e-07 0.045825 0.00014657 3.4036e-07 v total_pressure -1.8444e+05 2.3177e+05 23769 50308 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0381 0.10254 0.0028721 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.296e-07 0.051176 0.00031506 5.284e-06 INSTANT 0.875965000E-01 TIME STEP NUMBER 56163 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283118904E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.814510113E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.18422E-01 0.20750E+01 Friction velocity uk : 0.18422E-01 0.20750E+01 Dimensionless distance yplus : 0.17869E-01 0.20375E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -9.643795713e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29462E+08 1 0.18085E-09 0.25756E+02 0.19579E+04 c Velocity[X] 0.13746E+02 c Velocity[Y] 0.12010E+02 c Velocity[Z] 0.12365E-05 c Pressure 0.13883E-03 49 0.83264E-04 0.12895E-02 0.14107E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -24.386 38.151 5.6119 8.0045 v Velocity[Y] -27.228 28.422 -0.1461 -0.0064569 v Velocity[Z] -2.9461 3.0583 2.5631e-06 -5.3885e-08 v ǁVelocityǁ 0.00024777 38.284 7.9223 8.1082 v Pressure -2.87e+05 1.2955e+05 -78699 -51721 v TurbVisc 2.3373e-19 0.017299 0.00017542 3.043e-05 v CourantNb 7.1046e-08 0.011657 0.00016849 4.9436e-06 v FourierNb 1.2425e-07 0.045815 0.00014658 3.407e-07 v total_pressure -1.8568e+05 2.3088e+05 22626 49604 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0375 0.10254 0.0028721 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2958e-07 0.051166 0.00031507 5.2843e-06 INSTANT 0.875966000E-01 TIME STEP NUMBER 56164 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283113075E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.814272742E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.20913E-01 0.20744E+01 Friction velocity uk : 0.20913E-01 0.20744E+01 Dimensionless distance yplus : 0.20286E-01 0.20368E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -9.990434221e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29462E+08 1 0.18085E-09 0.25762E+02 0.19581E+04 c Velocity[X] 0.13752E+02 c Velocity[Y] 0.12010E+02 c Velocity[Z] 0.12250E-05 c Pressure 0.13581E-03 235 0.97214E-04 0.12609E-02 0.13320E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -24.395 38.164 5.6118 8.0044 v Velocity[Y] -27.239 28.431 -0.14611 -0.0064949 v Velocity[Z] -2.9458 3.0584 2.5624e-06 -5.3886e-08 v ǁVelocityǁ 0.00023964 38.297 7.9239 8.1082 v Pressure -2.8829e+05 1.2862e+05 -79790 -52346 v TurbVisc 2.3306e-19 0.017317 0.00017547 3.048e-05 v CourantNb 7.8639e-08 0.011656 0.00016849 4.9436e-06 v FourierNb 1.2425e-07 0.045805 0.00014658 3.4104e-07 v total_pressure -1.8696e+05 2.2995e+05 21535 48979 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0368 0.10254 0.0028721 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2956e-07 0.051155 0.00031507 5.2847e-06 INSTANT 0.875967000E-01 TIME STEP NUMBER 56165 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283106901E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.814030234E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12420E-01 0.20737E+01 Friction velocity uk : 0.12420E-01 0.20737E+01 Dimensionless distance yplus : 0.12194E-01 0.20362E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.030660486e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29461E+08 1 0.18084E-09 0.25758E+02 0.19579E+04 c Velocity[X] 0.13759E+02 c Velocity[Y] 0.11999E+02 c Velocity[Z] 0.12153E-05 c Pressure 0.13288E-03 88 0.82309E-04 0.12331E-02 0.11754E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -24.405 38.178 5.6117 8.0043 v Velocity[Y] -27.25 28.44 -0.14612 -0.0065347 v Velocity[Z] -2.9456 3.0586 2.5617e-06 -5.3886e-08 v ǁVelocityǁ 0.0002349 38.311 7.9254 8.1082 v Pressure -2.8947e+05 1.278e+05 -80834 -52992 v TurbVisc 2.3206e-19 0.017335 0.00017553 3.0529e-05 v CourantNb 7.8161e-08 0.011656 0.00016849 4.9436e-06 v FourierNb 1.2425e-07 0.045794 0.00014659 3.4137e-07 v total_pressure -1.8814e+05 2.2912e+05 20491 48333 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0362 0.10254 0.002872 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2954e-07 0.051145 0.00031508 5.285e-06 INSTANT 0.875968000E-01 TIME STEP NUMBER 56166 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283100814E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.813780732E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.43888E-02 0.20730E+01 Friction velocity uk : 0.43888E-02 0.20730E+01 Dimensionless distance yplus : 0.43089E-02 0.20355E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.059272020e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29461E+08 1 0.18084E-09 0.25766E+02 0.19582E+04 c Velocity[X] 0.13765E+02 c Velocity[Y] 0.12001E+02 c Velocity[Z] 0.12141E-05 c Pressure 0.12641E-03 9 0.57060E-04 0.11724E-02 0.92389E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -24.414 38.191 5.6115 8.0041 v Velocity[Y] -27.261 28.448 -0.14613 -0.0065758 v Velocity[Z] -2.9453 3.0588 2.5611e-06 -5.3886e-08 v ǁVelocityǁ 0.0002801 38.324 7.9269 8.1083 v Pressure -2.9058e+05 1.2704e+05 -81833 -53527 v TurbVisc 2.3387e-19 0.017354 0.00017559 3.0579e-05 v CourantNb 7.9419e-08 0.011655 0.0001685 4.9436e-06 v FourierNb 1.2425e-07 0.045784 0.00014659 3.4171e-07 v total_pressure -1.8925e+05 2.2836e+05 19492 47798 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0355 0.10253 0.0028719 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2952e-07 0.051134 0.00031509 5.2854e-06 INSTANT 0.875969000E-01 TIME STEP NUMBER 56167 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283094644E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.813524091E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.72313E-02 0.20723E+01 Friction velocity uk : 0.72313E-02 0.20723E+01 Dimensionless distance yplus : 0.63845E-02 0.20348E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.095297682e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29460E+08 1 0.18083E-09 0.25770E+02 0.19583E+04 c Velocity[X] 0.13773E+02 c Velocity[Y] 0.11997E+02 c Velocity[Z] 0.12058E-05 c Pressure 0.12408E-03 263 0.78371E-04 0.11503E-02 0.12332E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -24.423 38.204 5.6114 8.004 v Velocity[Y] -27.272 28.457 -0.14614 -0.0066147 v Velocity[Z] -2.9451 3.0589 2.5604e-06 -5.3886e-08 v ǁVelocityǁ 0.00035463 38.338 7.9285 8.1083 v Pressure -2.9179e+05 1.2618e+05 -82795 -54146 v TurbVisc 2.0761e-19 0.017372 0.00017565 3.0628e-05 v CourantNb 8.641e-08 0.011655 0.0001685 4.9436e-06 v FourierNb 1.2425e-07 0.045774 0.0001466 3.4205e-07 v total_pressure -1.9046e+05 2.2751e+05 18530 47179 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0348 0.10254 0.0028719 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.295e-07 0.051122 0.00031509 5.2857e-06 INSTANT 0.875970000E-01 TIME STEP NUMBER 56168 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283088311E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.813260500E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.24968E-01 0.20716E+01 Friction velocity uk : 0.24968E-01 0.20716E+01 Dimensionless distance yplus : 0.24258E-01 0.20341E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.112496061e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29460E+08 1 0.18083E-09 0.25775E+02 0.19584E+04 c Velocity[X] 0.13780E+02 c Velocity[Y] 0.11995E+02 c Velocity[Z] 0.11972E-05 c Pressure 0.12074E-03 78 0.83753E-04 0.11188E-02 0.11737E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -24.433 38.217 5.6113 8.0039 v Velocity[Y] -27.282 28.465 -0.14615 -0.0066562 v Velocity[Z] -2.9449 3.0591 2.5597e-06 -5.3886e-08 v ǁVelocityǁ 0.00044928 38.351 7.93 8.1083 v Pressure -2.928e+05 1.2548e+05 -83728 -54710 v TurbVisc 2.2663e-19 0.01739 0.00017571 3.0678e-05 v CourantNb 9.254e-08 0.011654 0.0001685 4.9437e-06 v FourierNb 1.2425e-07 0.045763 0.0001466 3.4239e-07 v total_pressure -1.9148e+05 2.268e+05 17597 46615 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0341 0.10255 0.0028718 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2948e-07 0.051112 0.0003151 5.286e-06 INSTANT 0.875971000E-01 TIME STEP NUMBER 56169 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283082078E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.812992584E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.24673E-01 0.20708E+01 Friction velocity uk : 0.24673E-01 0.20708E+01 Dimensionless distance yplus : 0.23972E-01 0.20334E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.139202723e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29459E+08 1 0.18082E-09 0.25780E+02 0.19586E+04 c Velocity[X] 0.13785E+02 c Velocity[Y] 0.11994E+02 c Velocity[Z] 0.11894E-05 c Pressure 0.11790E-03 399 0.97707E-04 0.10919E-02 0.11528E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -24.442 38.23 5.6112 8.0038 v Velocity[Y] -27.293 28.473 -0.14616 -0.006695 v Velocity[Z] -2.9446 3.0593 2.5591e-06 -5.3886e-08 v ǁVelocityǁ 0.00045892 38.364 7.9315 8.1083 v Pressure -2.9385e+05 1.2473e+05 -84619 -55212 v TurbVisc 2.2472e-19 0.017409 0.00017576 3.0728e-05 v CourantNb 9.9382e-08 0.011654 0.0001685 4.9437e-06 v FourierNb 1.2425e-07 0.045753 0.00014661 3.4273e-07 v total_pressure -1.9252e+05 2.2605e+05 16706 46113 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0334 0.10256 0.0028717 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2946e-07 0.0511 0.00031511 5.2864e-06 INSTANT 0.875972000E-01 TIME STEP NUMBER 56170 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283075534E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.812719654E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.14041E-01 0.20701E+01 Friction velocity uk : 0.14041E-01 0.20701E+01 Dimensionless distance yplus : 0.13828E-01 0.20327E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.160324811e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29458E+08 1 0.18081E-09 0.25774E+02 0.19583E+04 c Velocity[X] 0.13791E+02 c Velocity[Y] 0.11983E+02 c Velocity[Z] 0.11847E-05 c Pressure 0.11520E-03 343 0.82992E-04 0.10664E-02 0.99460E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -24.451 38.243 5.611 8.0036 v Velocity[Y] -27.304 28.482 -0.14617 -0.0067358 v Velocity[Z] -2.9444 3.0594 2.5584e-06 -5.3886e-08 v ǁVelocityǁ 0.00036453 38.378 7.933 8.1083 v Pressure -2.9482e+05 1.2408e+05 -85459 -55761 v TurbVisc 1.5804e-19 0.017427 0.00017582 3.0777e-05 v CourantNb 9.455e-08 0.011653 0.0001685 4.9437e-06 v FourierNb 1.2425e-07 0.045742 0.00014662 3.4307e-07 v total_pressure -1.9349e+05 2.2541e+05 15866 45564 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0327 0.10257 0.0028715 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2943e-07 0.051089 0.00031512 5.2867e-06 INSTANT 0.875973000E-01 TIME STEP NUMBER 56171 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283069071E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.812440611E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.58018E-02 0.20694E+01 Friction velocity uk : 0.58018E-02 0.20694E+01 Dimensionless distance yplus : 0.57138E-02 0.20320E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.179481001e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29458E+08 1 0.18081E-09 0.25781E+02 0.19585E+04 c Velocity[X] 0.13796E+02 c Velocity[Y] 0.11985E+02 c Velocity[Z] 0.11814E-05 c Pressure 0.10841E-03 9 0.57175E-04 0.10030E-02 0.77729E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -24.46 38.256 5.6109 8.0035 v Velocity[Y] -27.315 28.49 -0.14618 -0.0067781 v Velocity[Z] -2.9441 3.0596 2.5577e-06 -5.3886e-08 v ǁVelocityǁ 0.00029485 38.391 7.9345 8.1084 v Pressure -2.9573e+05 1.2347e+05 -86263 -56212 v TurbVisc 2.1284e-19 0.017445 0.00017588 3.0827e-05 v CourantNb 8.6601e-08 0.011653 0.0001685 4.9437e-06 v FourierNb 1.2425e-07 0.045731 0.00014662 3.4341e-07 v total_pressure -1.9441e+05 2.2479e+05 15062 45113 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.032 0.10257 0.0028713 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2941e-07 0.051078 0.00031512 5.2871e-06 INSTANT 0.875974000E-01 TIME STEP NUMBER 56172 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283062546E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.812154861E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.17068E-01 0.20687E+01 Friction velocity uk : 0.17068E-01 0.20687E+01 Dimensionless distance yplus : 0.16809E-01 0.20312E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.200389613e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29457E+08 1 0.18080E-09 0.25783E+02 0.19586E+04 c Velocity[X] 0.13802E+02 c Velocity[Y] 0.11980E+02 c Velocity[Z] 0.11719E-05 c Pressure 0.10660E-03 179 0.79131E-04 0.98582E-03 0.10027E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -24.469 38.269 5.6108 8.0033 v Velocity[Y] -27.325 28.498 -0.14619 -0.006818 v Velocity[Z] -2.9439 3.0598 2.5571e-06 -5.3886e-08 v ǁVelocityǁ 0.0002863 38.404 7.936 8.1084 v Pressure -2.9665e+05 1.2283e+05 -87005 -56673 v TurbVisc 2.1485e-19 0.017464 0.00017593 3.0877e-05 v CourantNb 8.5978e-08 0.011652 0.0001685 4.9436e-06 v FourierNb 1.2425e-07 0.045721 0.00014663 3.4376e-07 v total_pressure -1.9533e+05 2.2415e+05 14320 44652 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0312 0.10257 0.0028711 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2939e-07 0.051066 0.00031513 5.2874e-06 INSTANT 0.875975000E-01 TIME STEP NUMBER 56173 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283055876E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.811864304E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.20818E-01 0.20679E+01 Friction velocity uk : 0.20818E-01 0.20679E+01 Dimensionless distance yplus : 0.20184E-01 0.20305E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.211621616e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29457E+08 1 0.18079E-09 0.25787E+02 0.19587E+04 c Velocity[X] 0.13808E+02 c Velocity[Y] 0.11979E+02 c Velocity[Z] 0.11671E-05 c Pressure 0.10357E-03 54 0.84611E-04 0.95733E-03 0.10306E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -24.479 38.282 5.6107 8.0032 v Velocity[Y] -27.336 28.506 -0.1462 -0.0068605 v Velocity[Z] -2.9437 3.0599 2.5564e-06 -5.3886e-08 v ǁVelocityǁ 0.00028891 38.417 7.9375 8.1084 v Pressure -2.9746e+05 1.2229e+05 -87736 -57147 v TurbVisc 2.1799e-19 0.017482 0.00017599 3.0927e-05 v CourantNb 8.5825e-08 0.011652 0.0001685 4.9436e-06 v FourierNb 1.2425e-07 0.04571 0.00014664 3.441e-07 v total_pressure -1.9614e+05 2.2362e+05 13589 44178 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0305 0.10258 0.0028709 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2937e-07 0.051055 0.00031514 5.2877e-06 INSTANT 0.875976000E-01 TIME STEP NUMBER 56174 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283049325E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.811568451E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.17443E-01 0.20672E+01 Friction velocity uk : 0.17443E-01 0.20672E+01 Dimensionless distance yplus : 0.16912E-01 0.20298E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.222938646e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29456E+08 1 0.18079E-09 0.25789E+02 0.19587E+04 c Velocity[X] 0.13812E+02 c Velocity[Y] 0.11978E+02 c Velocity[Z] 0.11606E-05 c Pressure 0.10124E-03 230 0.98816E-04 0.93535E-03 0.99526E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -24.488 38.295 5.6105 8.0031 v Velocity[Y] -27.346 28.514 -0.1462 -0.0069004 v Velocity[Z] -2.9434 3.0601 2.5557e-06 -5.3886e-08 v ǁVelocityǁ 0.00034041 38.43 7.939 8.1084 v Pressure -2.9827e+05 1.2173e+05 -88408 -57513 v TurbVisc 2.1538e-19 0.0175 0.00017605 3.0977e-05 v CourantNb 8.5693e-08 0.011651 0.0001685 4.9436e-06 v FourierNb 1.2425e-07 0.045699 0.00014664 3.4444e-07 v total_pressure -1.9695e+05 2.2306e+05 12917 43812 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0298 0.10258 0.0028707 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2935e-07 0.051044 0.00031514 5.2881e-06 INSTANT 0.875977000E-01 TIME STEP NUMBER 56175 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283042487E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.811269054E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.17022E-01 0.20665E+01 Friction velocity uk : 0.17022E-01 0.20665E+01 Dimensionless distance yplus : 0.16503E-01 0.20291E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.231228406e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29456E+08 1 0.18078E-09 0.25781E+02 0.19584E+04 c Velocity[X] 0.13816E+02 c Velocity[Y] 0.11965E+02 c Velocity[Z] 0.11504E-05 c Pressure 0.99146E-04 524 0.83881E-04 0.91555E-03 0.79444E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -24.497 38.308 5.6104 8.0029 v Velocity[Y] -27.357 28.522 -0.14621 -0.0069421 v Velocity[Z] -2.9432 3.0603 2.5551e-06 -5.3886e-08 v ǁVelocityǁ 0.00034656 38.443 7.9405 8.1084 v Pressure -2.9898e+05 1.2128e+05 -89031 -57930 v TurbVisc 2.1462e-19 0.017519 0.0001761 3.1027e-05 v CourantNb 8.5653e-08 0.011651 0.0001685 4.9436e-06 v FourierNb 1.2425e-07 0.045688 0.00014665 3.4478e-07 v total_pressure -1.9765e+05 2.2261e+05 12294 43395 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0291 0.10257 0.0028704 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2932e-07 0.051032 0.00031515 5.2884e-06 INSTANT 0.875978000E-01 TIME STEP NUMBER 56176 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283035753E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.810964619E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.66749E-02 0.20657E+01 Friction velocity uk : 0.66749E-02 0.20657E+01 Dimensionless distance yplus : 0.66266E-02 0.20284E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.236249880e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29455E+08 1 0.18077E-09 0.25787E+02 0.19586E+04 c Velocity[X] 0.13820E+02 c Velocity[Y] 0.11967E+02 c Velocity[Z] 0.11472E-05 c Pressure 0.92180E-04 17 0.58258E-04 0.85081E-03 0.62757E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -24.506 38.321 5.6103 8.0028 v Velocity[Y] -27.367 28.529 -0.14622 -0.0069857 v Velocity[Z] -2.9429 3.0605 2.5544e-06 -5.3886e-08 v ǁVelocityǁ 0.00034778 38.456 7.942 8.1084 v Pressure -2.9967e+05 1.2085e+05 -89618 -58276 v TurbVisc 2.1285e-19 0.017537 0.00017616 3.1077e-05 v CourantNb 8.5646e-08 0.01165 0.0001685 4.9436e-06 v FourierNb 1.2425e-07 0.045678 0.00014665 3.4513e-07 v total_pressure -1.9835e+05 2.2218e+05 11707 43049 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0284 0.10256 0.00287 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.293e-07 0.051021 0.00031516 5.2888e-06 INSTANT 0.875979000E-01 TIME STEP NUMBER 56177 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283028974E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.810654108E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.39819E-02 0.20650E+01 Friction velocity uk : 0.39819E-02 0.20650E+01 Dimensionless distance yplus : 0.38335E-02 0.20277E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.238720221e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29454E+08 1 0.18077E-09 0.25787E+02 0.19585E+04 c Velocity[X] 0.13825E+02 c Velocity[Y] 0.11962E+02 c Velocity[Z] 0.11437E-05 c Pressure 0.91316E-04 688 0.80538E-04 0.84243E-03 0.86728E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -24.515 38.333 5.6102 8.0027 v Velocity[Y] -27.378 28.537 -0.14623 -0.0070262 v Velocity[Z] -2.9427 3.0606 2.5537e-06 -5.3886e-08 v ǁVelocityǁ 0.00038095 38.469 7.9436 8.1084 v Pressure -3.0034e+05 1.2041e+05 -90148 -58597 v TurbVisc 7.8072e-20 0.017555 0.00017621 3.1128e-05 v CourantNb 8.5165e-08 0.01165 0.00016851 4.9436e-06 v FourierNb 1.2425e-07 0.045667 0.00014666 3.4547e-07 v total_pressure -1.9901e+05 2.2173e+05 11177 42728 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0277 0.10257 0.0028697 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2928e-07 0.05101 0.00031517 5.2891e-06 INSTANT 0.875980000E-01 TIME STEP NUMBER 56178 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283022068E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.810339300E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12774E-01 0.20643E+01 Friction velocity uk : 0.12774E-01 0.20643E+01 Dimensionless distance yplus : 0.12615E-01 0.20270E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.238872994e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29454E+08 1 0.18076E-09 0.25789E+02 0.19586E+04 c Velocity[X] 0.13829E+02 c Velocity[Y] 0.11961E+02 c Velocity[Z] 0.11359E-05 c Pressure 0.89034E-04 372 0.86331E-04 0.82098E-03 0.98738E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -24.524 38.346 5.61 8.0025 v Velocity[Y] -27.388 28.545 -0.14624 -0.0070705 v Velocity[Z] -2.9425 3.0608 2.5531e-06 -5.3886e-08 v ǁVelocityǁ 0.00046091 38.482 7.9451 8.1085 v Pressure -3.0096e+05 1.2003e+05 -90669 -59002 v TurbVisc 1.9575e-19 0.017573 0.00017627 3.1178e-05 v CourantNb 8.5529e-08 0.01165 0.00016851 4.9436e-06 v FourierNb 1.2425e-07 0.045656 0.00014667 3.4581e-07 v total_pressure -1.9963e+05 2.2135e+05 10656 42323 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.027 0.10257 0.0028694 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2926e-07 0.050998 0.00031517 5.2894e-06 INSTANT 0.875981000E-01 TIME STEP NUMBER 56179 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283015266E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.810020944E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.14438E-01 0.20636E+01 Friction velocity uk : 0.14438E-01 0.20636E+01 Dimensionless distance yplus : 0.13918E-01 0.20263E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.232828565e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29453E+08 1 0.18075E-09 0.25781E+02 0.19582E+04 c Velocity[X] 0.13831E+02 c Velocity[Y] 0.11950E+02 c Velocity[Z] 0.11286E-05 c Pressure 0.87679E-04 62 0.75340E-04 0.80811E-03 0.52542E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -24.533 38.359 5.6099 8.0024 v Velocity[Y] -27.398 28.552 -0.14625 -0.0071126 v Velocity[Z] -2.9422 3.061 2.5524e-06 -5.3886e-08 v ǁVelocityǁ 0.0005701 38.495 7.9466 8.1085 v Pressure -3.0143e+05 1.1975e+05 -91084 -59151 v TurbVisc 2.0099e-19 0.017592 0.00017632 3.1228e-05 v CourantNb 9.3357e-08 0.011649 0.00016851 4.9436e-06 v FourierNb 1.2425e-07 0.045646 0.00014667 3.4616e-07 v total_pressure -2.0011e+05 2.2107e+05 10241 42174 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0263 0.10258 0.0028691 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2923e-07 0.050987 0.00031518 5.2898e-06 INSTANT 0.875982000E-01 TIME STEP NUMBER 56180 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283008346E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.809700061E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.98580E-02 0.20629E+01 Friction velocity uk : 0.98580E-02 0.20629E+01 Dimensionless distance yplus : 0.95415E-02 0.20256E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.225205628e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29453E+08 1 0.18074E-09 0.25784E+02 0.19583E+04 c Velocity[X] 0.13833E+02 c Velocity[Y] 0.11952E+02 c Velocity[Z] 0.11270E-05 c Pressure 0.81797E-04 7 0.54587E-04 0.75353E-03 0.42071E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -24.542 38.371 5.6098 8.0022 v Velocity[Y] -27.408 28.56 -0.14626 -0.0071543 v Velocity[Z] -2.942 3.0611 2.5517e-06 -5.3886e-08 v ǁVelocityǁ 0.0007067 38.507 7.9481 8.1085 v Pressure -3.0191e+05 1.1948e+05 -91469 -59364 v TurbVisc 2.0119e-19 0.01761 0.00017638 3.1279e-05 v CourantNb 1.0419e-07 0.011649 0.00016851 4.9436e-06 v FourierNb 1.2425e-07 0.045635 0.00014668 3.465e-07 v total_pressure -2.0059e+05 2.208e+05 9855.9 41961 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0256 0.10258 0.0028687 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2921e-07 0.050976 0.00031519 5.2901e-06 INSTANT 0.875983000E-01 TIME STEP NUMBER 56181 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283001334E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.809372969E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.20634E-02 0.20622E+01 Friction velocity uk : 0.20634E-02 0.20622E+01 Dimensionless distance yplus : 0.19972E-02 0.20249E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.213050117e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29452E+08 1 0.18074E-09 0.25780E+02 0.19581E+04 c Velocity[X] 0.13837E+02 c Velocity[Y] 0.11943E+02 c Velocity[Z] 0.11210E-05 c Pressure 0.81538E-04 84 0.97347E-04 0.75079E-03 0.67358E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -24.551 38.384 5.6097 8.0021 v Velocity[Y] -27.418 28.567 -0.14627 -0.007197 v Velocity[Z] -2.9417 3.0613 2.5511e-06 -5.3886e-08 v ǁVelocityǁ 0.0005963 38.52 7.9496 8.1085 v Pressure -3.0246e+05 1.1913e+05 -91898 -59792 v TurbVisc 1.9883e-19 0.017628 0.00017643 3.1329e-05 v CourantNb 1.1394e-07 0.011648 0.00016851 4.9436e-06 v FourierNb 1.2425e-07 0.045624 0.00014669 3.4685e-07 v total_pressure -2.0113e+05 2.2046e+05 9427.1 41533 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0249 0.10257 0.0028683 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2919e-07 0.050964 0.00031519 5.2905e-06 INSTANT 0.875984000E-01 TIME STEP NUMBER 56182 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282994323E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.809039956E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.50164E-02 0.20615E+01 Friction velocity uk : 0.50164E-02 0.20615E+01 Dimensionless distance yplus : 0.48361E-02 0.20242E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.198086549e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29451E+08 1 0.18073E-09 0.25777E+02 0.19580E+04 c Velocity[X] 0.13839E+02 c Velocity[Y] 0.11938E+02 c Velocity[Z] 0.11075E-05 c Pressure 0.79173E-04 326 0.81239E-04 0.72867E-03 0.27619E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -24.559 38.396 5.6095 8.0019 v Velocity[Y] -27.429 28.575 -0.14628 -0.0072402 v Velocity[Z] -2.9415 3.0615 2.5504e-06 -5.3886e-08 v ǁVelocityǁ 0.00048501 38.533 7.9511 8.1085 v Pressure -3.028e+05 1.1899e+05 -92189 -59936 v TurbVisc 1.4316e-19 0.017647 0.00017648 3.1379e-05 v CourantNb 1.1016e-07 0.011648 0.00016851 4.9436e-06 v FourierNb 1.2425e-07 0.045614 0.00014669 3.4719e-07 v total_pressure -2.0148e+05 2.2031e+05 9136.5 41389 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0242 0.10257 0.0028679 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2917e-07 0.050954 0.0003152 5.2908e-06 INSTANT 0.875985000E-01 TIME STEP NUMBER 56183 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282987369E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.808708932E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.32365E-02 0.20609E+01 Friction velocity uk : 0.32365E-02 0.20609E+01 Dimensionless distance yplus : 0.31200E-02 0.20236E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.184680306e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29451E+08 1 0.18072E-09 0.25779E+02 0.19580E+04 c Velocity[X] 0.13840E+02 c Velocity[Y] 0.11939E+02 c Velocity[Z] 0.11061E-05 c Pressure 0.76437E-04 7 0.51110E-04 0.70316E-03 0.38600E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -24.568 38.408 5.6094 8.0018 v Velocity[Y] -27.439 28.583 -0.14629 -0.007285 v Velocity[Z] -2.9412 3.0616 2.5497e-06 -5.3886e-08 v ǁVelocityǁ 0.00040035 38.545 7.9526 8.1085 v Pressure -3.0314e+05 1.1885e+05 -92432 -60092 v TurbVisc 2.0903e-19 0.017665 0.00017654 3.143e-05 v CourantNb 1.0576e-07 0.011647 0.00016851 4.9436e-06 v FourierNb 1.2425e-07 0.045603 0.0001467 3.4754e-07 v total_pressure -2.0181e+05 2.2017e+05 8892.9 41233 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0236 0.10258 0.0028678 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2914e-07 0.050943 0.00031521 5.2911e-06 INSTANT 0.875986000E-01 TIME STEP NUMBER 56184 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282980425E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.808373780E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.30055E-02 0.20602E+01 Friction velocity uk : 0.30055E-02 0.20602E+01 Dimensionless distance yplus : 0.28973E-02 0.20229E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.155360239e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29450E+08 1 0.18072E-09 0.25773E+02 0.19578E+04 c Velocity[X] 0.13842E+02 c Velocity[Y] 0.11931E+02 c Velocity[Z] 0.11008E-05 c Pressure 0.77235E-04 30 0.98094E-04 0.71017E-03 0.33459E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -24.577 38.421 5.6093 8.0017 v Velocity[Y] -27.449 28.591 -0.1463 -0.0073291 v Velocity[Z] -2.941 3.0618 2.5491e-06 -5.3886e-08 v ǁVelocityǁ 0.00029218 38.558 7.954 8.1085 v Pressure -3.0347e+05 1.187e+05 -92681 -60265 v TurbVisc 2.0071e-19 0.017683 0.00017659 3.1481e-05 v CourantNb 1.0129e-07 0.011646 0.00016851 4.9436e-06 v FourierNb 1.2425e-07 0.045593 0.0001467 3.4788e-07 v total_pressure -2.0215e+05 2.2002e+05 8643.5 41060 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0229 0.10258 0.0028677 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2912e-07 0.050931 0.00031522 5.2915e-06 INSTANT 0.875987000E-01 TIME STEP NUMBER 56185 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282973385E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.808032960E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.43310E-02 0.20595E+01 Friction velocity uk : 0.43310E-02 0.20595E+01 Dimensionless distance yplus : 0.41750E-02 0.20223E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.138870752e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29449E+08 1 0.18071E-09 0.25769E+02 0.19576E+04 c Velocity[X] 0.13843E+02 c Velocity[Y] 0.11926E+02 c Velocity[Z] 0.10911E-05 c Pressure 0.75739E-04 13 0.83673E-04 0.69609E-03 0.24080E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -24.586 38.433 5.6092 8.0015 v Velocity[Y] -27.459 28.599 -0.14632 -0.0073727 v Velocity[Z] -2.9408 3.062 2.5484e-06 -5.3886e-08 v ǁVelocityǁ 0.0002245 38.57 7.9555 8.1085 v Pressure -3.0372e+05 1.1861e+05 -92853 -60376 v TurbVisc 1.8779e-19 0.017701 0.00017664 3.1531e-05 v CourantNb 9.7488e-08 0.011646 0.00016851 4.9436e-06 v FourierNb 1.2425e-07 0.045582 0.00014671 3.4823e-07 v total_pressure -2.0239e+05 2.1994e+05 8472.4 40949 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0223 0.10259 0.0028676 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.291e-07 0.050921 0.00031522 5.2918e-06 INSTANT 0.875988000E-01 TIME STEP NUMBER 56186 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282966350E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.807692053E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.61928E-02 0.20589E+01 Friction velocity uk : 0.61928E-02 0.20589E+01 Dimensionless distance yplus : 0.59699E-02 0.20217E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.111921045e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29449E+08 1 0.18070E-09 0.25771E+02 0.19576E+04 c Velocity[X] 0.13843E+02 c Velocity[Y] 0.11928E+02 c Velocity[Z] 0.10976E-05 c Pressure 0.73844E-04 13 0.54762E-04 0.67835E-03 0.30687E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -24.594 38.445 5.6091 8.0014 v Velocity[Y] -27.469 28.607 -0.14633 -0.0074156 v Velocity[Z] -2.9405 3.0621 2.5477e-06 -5.3887e-08 v ǁVelocityǁ 0.00019978 38.582 7.957 8.1085 v Pressure -3.0389e+05 1.1859e+05 -92940 -60412 v TurbVisc 1.8393e-19 0.01772 0.0001767 3.1582e-05 v CourantNb 9.3385e-08 0.011645 0.00016852 4.9436e-06 v FourierNb 1.2425e-07 0.045572 0.00014672 3.4858e-07 v total_pressure -2.0257e+05 2.1991e+05 8385 40913 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0217 0.1026 0.0028676 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2907e-07 0.05091 0.00031523 5.2922e-06 INSTANT 0.875989000E-01 TIME STEP NUMBER 56187 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282959302E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.807348486E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.34326E-02 0.20582E+01 Friction velocity uk : 0.34326E-02 0.20582E+01 Dimensionless distance yplus : 0.33035E-02 0.20210E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.086722056e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29448E+08 1 0.18069E-09 0.25767E+02 0.19574E+04 c Velocity[X] 0.13845E+02 c Velocity[Y] 0.11922E+02 c Velocity[Z] 0.10870E-05 c Pressure 0.75870E-04 29 0.77243E-04 0.69663E-03 0.71305E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -24.603 38.457 5.609 8.0012 v Velocity[Y] -27.478 28.615 -0.14634 -0.007461 v Velocity[Z] -2.9403 3.0623 2.5471e-06 -5.3887e-08 v ǁVelocityǁ 0.00016331 38.595 7.9585 8.1085 v Pressure -3.041e+05 1.1856e+05 -93118 -60654 v TurbVisc 3.8252e-20 0.017738 0.00017675 3.1633e-05 v CourantNb 8.9828e-08 0.011645 0.00016852 4.9436e-06 v FourierNb 1.2425e-07 0.045562 0.00014672 3.4892e-07 v total_pressure -2.0277e+05 2.1989e+05 8206.8 40671 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.021 0.10262 0.0028676 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2905e-07 0.050899 0.00031524 5.2925e-06 INSTANT 0.875990000E-01 TIME STEP NUMBER 56188 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282952327E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.806999166E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11076E-02 0.20576E+01 Friction velocity uk : 0.11076E-02 0.20576E+01 Dimensionless distance yplus : 0.10715E-02 0.20204E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.041225592e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29448E+08 1 0.18069E-09 0.25765E+02 0.19573E+04 c Velocity[X] 0.13844E+02 c Velocity[Y] 0.11921E+02 c Velocity[Z] 0.10778E-05 c Pressure 0.76335E-04 41 0.81793E-04 0.70058E-03 0.67179E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -24.611 38.469 5.6089 8.0011 v Velocity[Y] -27.488 28.623 -0.14636 -0.0075043 v Velocity[Z] -2.94 3.0625 2.5464e-06 -5.3887e-08 v ǁVelocityǁ 0.00016277 38.607 7.96 8.1085 v Pressure -3.042e+05 1.1861e+05 -93120 -60635 v TurbVisc 2.5517e-19 0.017756 0.0001768 3.1684e-05 v CourantNb 8.5712e-08 0.011644 0.00016852 4.9436e-06 v FourierNb 1.2425e-07 0.045551 0.00014673 3.4927e-07 v total_pressure -2.0288e+05 2.1994e+05 8204.9 40690 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0204 0.10263 0.0028676 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2903e-07 0.050888 0.00031525 5.2928e-06 INSTANT 0.875991000E-01 TIME STEP NUMBER 56189 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282945190E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.806656019E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.72188E-02 0.20570E+01 Friction velocity uk : 0.72188E-02 0.20570E+01 Dimensionless distance yplus : 0.69835E-02 0.20198E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.015597010e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29447E+08 1 0.18068E-09 0.25763E+02 0.19572E+04 c Velocity[X] 0.13845E+02 c Velocity[Y] 0.11917E+02 c Velocity[Z] 0.10730E-05 c Pressure 0.77793E-04 68 0.95018E-04 0.71363E-03 0.77372E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -24.62 38.481 5.6088 8.0009 v Velocity[Y] -27.498 28.63 -0.14637 -0.0075505 v Velocity[Z] -2.9398 3.0626 2.5457e-06 -5.3887e-08 v ǁVelocityǁ 0.00019157 38.619 7.9615 8.1086 v Pressure -3.0424e+05 1.1874e+05 -93102 -60662 v TurbVisc 2.1825e-19 0.017774 0.00017686 3.1735e-05 v CourantNb 8.2056e-08 0.011644 0.00016852 4.9436e-06 v FourierNb 1.2425e-07 0.045541 0.00014673 3.4962e-07 v total_pressure -2.0291e+05 2.2007e+05 8222.5 40663 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0198 0.10264 0.0028678 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.29e-07 0.050878 0.00031525 5.2932e-06 INSTANT 0.875992000E-01 TIME STEP NUMBER 56190 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282938294E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.806308184E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.91095E-02 0.20564E+01 Friction velocity uk : 0.91095E-02 0.20564E+01 Dimensionless distance yplus : 0.87669E-02 0.20192E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -9.807798250e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29446E+08 1 0.18068E-09 0.25749E+02 0.19566E+04 c Velocity[X] 0.13843E+02 c Velocity[Y] 0.11906E+02 c Velocity[Z] 0.10674E-05 c Pressure 0.79634E-04 88 0.80384E-04 0.73018E-03 0.46393E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -24.629 38.494 5.6087 8.0008 v Velocity[Y] -27.508 28.638 -0.14639 -0.0075953 v Velocity[Z] -2.9395 3.0628 2.5451e-06 -5.3887e-08 v ǁVelocityǁ 0.00023209 38.632 7.963 8.1086 v Pressure -3.0426e+05 1.1887e+05 -93049 -60623 v TurbVisc 1.9639e-19 0.017793 0.00017691 3.1786e-05 v CourantNb 7.856e-08 0.011643 0.00016852 4.9436e-06 v FourierNb 1.2425e-07 0.045531 0.00014674 3.4997e-07 v total_pressure -2.0294e+05 2.2019e+05 8276.3 40702 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0192 0.10266 0.0028679 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2898e-07 0.050867 0.00031526 5.2935e-06 INSTANT 0.875993000E-01 TIME STEP NUMBER 56191 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282931261E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.805957982E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.14764E-01 0.20559E+01 Friction velocity uk : 0.14764E-01 0.20559E+01 Dimensionless distance yplus : 0.14208E-01 0.20187E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -9.447391114e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29446E+08 1 0.18067E-09 0.25750E+02 0.19566E+04 c Velocity[X] 0.13843E+02 c Velocity[Y] 0.11907E+02 c Velocity[Z] 0.10698E-05 c Pressure 0.76098E-04 7 0.55870E-04 0.69743E-03 0.30492E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -24.637 38.505 5.6086 8.0006 v Velocity[Y] -27.517 28.646 -0.1464 -0.0076395 v Velocity[Z] -2.9393 3.063 2.5444e-06 -5.3887e-08 v ǁVelocityǁ 0.00030666 38.644 7.9645 8.1086 v Pressure -3.0428e+05 1.1902e+05 -93000 -60642 v TurbVisc 1.8624e-19 0.017811 0.00017696 3.1837e-05 v CourantNb 7.5192e-08 0.011643 0.00016852 4.9436e-06 v FourierNb 1.2425e-07 0.045521 0.00014675 3.5032e-07 v total_pressure -2.0295e+05 2.2035e+05 8324.6 40683 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0187 0.10267 0.0028681 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2896e-07 0.050857 0.00031527 5.2939e-06 INSTANT 0.875994000E-01 TIME STEP NUMBER 56192 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282924202E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.805606912E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11319E-01 0.20553E+01 Friction velocity uk : 0.11319E-01 0.20553E+01 Dimensionless distance yplus : 0.11129E-01 0.20181E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -9.048250236e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29445E+08 1 0.18066E-09 0.25744E+02 0.19563E+04 c Velocity[X] 0.13842E+02 c Velocity[Y] 0.11901E+02 c Velocity[Z] 0.10601E-05 c Pressure 0.79558E-04 52 0.76426E-04 0.72881E-03 0.61804E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -24.645 38.517 5.6085 8.0005 v Velocity[Y] -27.527 28.654 -0.14642 -0.007686 v Velocity[Z] -2.939 3.0631 2.5437e-06 -5.3887e-08 v ǁVelocityǁ 0.00040167 38.656 7.966 8.1086 v Pressure -3.0414e+05 1.1927e+05 -92784 -60585 v TurbVisc 2.11e-19 0.017829 0.00017701 3.1888e-05 v CourantNb 7.163e-08 0.011642 0.00016852 4.9436e-06 v FourierNb 1.2425e-07 0.045511 0.00014675 3.5067e-07 v total_pressure -2.0282e+05 2.2059e+05 8540.6 40740 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0181 0.10267 0.0028681 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2893e-07 0.050847 0.00031528 5.2942e-06 INSTANT 0.875995000E-01 TIME STEP NUMBER 56193 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282917318E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.805259303E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12674E-01 0.20547E+01 Friction velocity uk : 0.12674E-01 0.20547E+01 Dimensionless distance yplus : 0.12389E-01 0.20175E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -8.696090942e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29445E+08 1 0.18066E-09 0.25740E+02 0.19562E+04 c Velocity[X] 0.13840E+02 c Velocity[Y] 0.11900E+02 c Velocity[Z] 0.10513E-05 c Pressure 0.81582E-04 59 0.81768E-04 0.74701E-03 0.69798E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -24.654 38.529 5.6084 8.0004 v Velocity[Y] -27.537 28.661 -0.14643 -0.0077305 v Velocity[Z] -2.9388 3.0633 2.5431e-06 -5.3887e-08 v ǁVelocityǁ 0.00051118 38.668 7.9675 8.1086 v Pressure -3.0405e+05 1.1952e+05 -92627 -60481 v TurbVisc 1.6397e-19 0.017847 0.00017706 3.1939e-05 v CourantNb 6.8893e-08 0.011642 0.00016853 4.9436e-06 v FourierNb 1.2425e-07 0.045501 0.00014676 3.5102e-07 v total_pressure -2.0273e+05 2.2085e+05 8698.5 40844 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0175 0.10269 0.0028683 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2891e-07 0.050836 0.00031528 5.2946e-06 INSTANT 0.875996000E-01 TIME STEP NUMBER 56194 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282910265E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.804904663E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.77605E-02 0.20542E+01 Friction velocity uk : 0.77605E-02 0.20542E+01 Dimensionless distance yplus : 0.76452E-02 0.20170E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -8.329155696e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29444E+08 1 0.18065E-09 0.25736E+02 0.19560E+04 c Velocity[X] 0.13839E+02 c Velocity[Y] 0.11896E+02 c Velocity[Z] 0.10473E-05 c Pressure 0.84381E-04 76 0.94729E-04 0.77228E-03 0.78594E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -24.662 38.541 5.6083 8.0002 v Velocity[Y] -27.546 28.669 -0.14645 -0.0077778 v Velocity[Z] -2.9386 3.0635 2.5424e-06 -5.3887e-08 v ǁVelocityǁ 0.00062792 38.68 7.969 8.1086 v Pressure -3.0387e+05 1.1988e+05 -92393 -60406 v TurbVisc 1.6378e-19 0.017865 0.00017712 3.199e-05 v CourantNb 6.5948e-08 0.011641 0.00016853 4.9435e-06 v FourierNb 1.2425e-07 0.045491 0.00014677 3.5137e-07 v total_pressure -2.0254e+05 2.212e+05 8932.5 40919 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.017 0.10271 0.0028685 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2888e-07 0.050826 0.00031529 5.2949e-06 INSTANT 0.875997000E-01 TIME STEP NUMBER 56195 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282903469E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.804552990E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.48351E-02 0.20536E+01 Friction velocity uk : 0.48351E-02 0.20536E+01 Dimensionless distance yplus : 0.47633E-02 0.20165E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -7.932706879e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29443E+08 1 0.18065E-09 0.25721E+02 0.19554E+04 c Velocity[X] 0.13836E+02 c Velocity[Y] 0.11885E+02 c Velocity[Z] 0.10444E-05 c Pressure 0.87481E-04 489 0.80595E-04 0.80029E-03 0.53428E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -24.67 38.553 5.6082 8.0001 v Velocity[Y] -27.556 28.676 -0.14647 -0.0078241 v Velocity[Z] -2.9383 3.0636 2.5417e-06 -5.3887e-08 v ǁVelocityǁ 0.00074779 38.692 7.9705 8.1086 v Pressure -3.0368e+05 1.2021e+05 -92111 -60244 v TurbVisc 1.6178e-19 0.017884 0.00017717 3.2042e-05 v CourantNb 6.3121e-08 0.011641 0.00016853 4.9435e-06 v FourierNb 1.2425e-07 0.045481 0.00014677 3.5172e-07 v total_pressure -2.0235e+05 2.2154e+05 9214 41081 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0165 0.10274 0.0028686 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2886e-07 0.050816 0.0003153 5.2953e-06 INSTANT 0.875998000E-01 TIME STEP NUMBER 56196 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282896547E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.804201100E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12719E-01 0.20531E+01 Friction velocity uk : 0.12719E-01 0.20531E+01 Dimensionless distance yplus : 0.12531E-01 0.20159E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -7.561369402e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29443E+08 1 0.18064E-09 0.25720E+02 0.19553E+04 c Velocity[X] 0.13835E+02 c Velocity[Y] 0.11885E+02 c Velocity[Z] 0.10463E-05 c Pressure 0.85674E-04 7 0.55881E-04 0.78340E-03 0.38036E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -24.679 38.565 5.6081 7.9999 v Velocity[Y] -27.565 28.684 -0.14649 -0.007869 v Velocity[Z] -2.9381 3.0638 2.5411e-06 -5.3887e-08 v ǁVelocityǁ 0.00088288 38.704 7.972 8.1086 v Pressure -3.0344e+05 1.2059e+05 -91818 -60128 v TurbVisc 1.5718e-19 0.017902 0.00017722 3.2093e-05 v CourantNb 6.0439e-08 0.01164 0.00016853 4.9435e-06 v FourierNb 1.2425e-07 0.045471 0.00014678 3.5207e-07 v total_pressure -2.0212e+05 2.2191e+05 9507.5 41197 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0159 0.10276 0.0028688 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2884e-07 0.050806 0.00031531 5.2956e-06 INSTANT 0.875999000E-01 TIME STEP NUMBER 56197 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282889653E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.803849651E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15366E-01 0.20526E+01 Friction velocity uk : 0.15366E-01 0.20526E+01 Dimensionless distance yplus : 0.15286E-01 0.20154E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -7.120500313e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29442E+08 1 0.18063E-09 0.25712E+02 0.19550E+04 c Velocity[X] 0.13832E+02 c Velocity[Y] 0.11880E+02 c Velocity[Z] 0.10409E-05 c Pressure 0.90091E-04 69 0.77023E-04 0.82342E-03 0.72222E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -24.687 38.576 5.608 7.9998 v Velocity[Y] -27.575 28.691 -0.14651 -0.0079168 v Velocity[Z] -2.9378 3.064 2.5404e-06 -5.3887e-08 v ǁVelocityǁ 0.0009945 38.716 7.9735 8.1086 v Pressure -3.0309e+05 1.2109e+05 -91410 -59931 v TurbVisc 1.5558e-19 0.01792 0.00017727 3.2145e-05 v CourantNb 5.8383e-08 0.01164 0.00016853 4.9435e-06 v FourierNb 1.2425e-07 0.045462 0.00014678 3.5242e-07 v total_pressure -2.0176e+05 2.2242e+05 9914.5 41394 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0154 0.10278 0.0028689 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2881e-07 0.050796 0.00031531 5.296e-06 INSTANT 0.876000000E-01 TIME STEP NUMBER 56198 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282882923E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.803501032E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10064E-01 0.20520E+01 Friction velocity uk : 0.10064E-01 0.20520E+01 Dimensionless distance yplus : 0.10012E-01 0.20149E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -6.890398877e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29442E+08 1 0.18063E-09 0.25707E+02 0.19547E+04 c Velocity[X] 0.13828E+02 c Velocity[Y] 0.11879E+02 c Velocity[Z] 0.10353E-05 c Pressure 0.93147E-04 66 0.82793E-04 0.85096E-03 0.79925E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -24.695 38.588 5.6079 7.9997 v Velocity[Y] -27.584 28.699 -0.14653 -0.0079624 v Velocity[Z] -2.9376 3.0641 2.5398e-06 -5.3887e-08 v ǁVelocityǁ 0.0011183 38.728 7.975 8.1087 v Pressure -3.0278e+05 1.2156e+05 -91008 -59692 v TurbVisc 1.547e-19 0.017938 0.00017732 3.2196e-05 v CourantNb 5.5411e-08 0.011639 0.00016853 4.9435e-06 v FourierNb 1.2425e-07 0.045451 0.00014679 3.5278e-07 v total_pressure -2.0145e+05 2.2288e+05 10317 41633 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0149 0.1028 0.0028691 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2879e-07 0.050785 0.00031532 5.2963e-06 INSTANT 0.876001000E-01 TIME STEP NUMBER 56199 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282876054E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.803150136E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.42338E-02 0.20515E+01 Friction velocity uk : 0.42338E-02 0.20515E+01 Dimensionless distance yplus : 0.42118E-02 0.20144E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -6.514441160e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29441E+08 1 0.18062E-09 0.25702E+02 0.19545E+04 c Velocity[X] 0.13826E+02 c Velocity[Y] 0.11875E+02 c Velocity[Z] 0.10284E-05 c Pressure 0.96814E-04 422 0.96111E-04 0.88406E-03 0.86147E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -24.703 38.6 5.6079 7.9995 v Velocity[Y] -27.593 28.706 -0.14655 -0.0080111 v Velocity[Z] -2.9373 3.0643 2.5391e-06 -5.3887e-08 v ǁVelocityǁ 0.0012423 38.74 7.9765 8.1087 v Pressure -3.0238e+05 1.2214e+05 -90551 -59503 v TurbVisc 1.5276e-19 0.017956 0.00017737 3.2248e-05 v CourantNb 5.3159e-08 0.011639 0.00016854 4.9435e-06 v FourierNb 1.2425e-07 0.045442 0.00014679 3.5313e-07 v total_pressure -2.0106e+05 2.2346e+05 10774 41822 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0144 0.10282 0.0028693 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2877e-07 0.050775 0.00031533 5.2967e-06 INSTANT 0.876002000E-01 TIME STEP NUMBER 56200 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282869454E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.802800877E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.26943E-02 0.20510E+01 Friction velocity uk : 0.26943E-02 0.20510E+01 Dimensionless distance yplus : 0.26803E-02 0.20139E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -6.189265065e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29440E+08 1 0.18062E-09 0.25685E+02 0.19538E+04 c Velocity[X] 0.13822E+02 c Velocity[Y] 0.11863E+02 c Velocity[Z] 0.10246E-05 c Pressure 0.10067E-03 82 0.81788E-04 0.91889E-03 0.68757E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -24.711 38.611 5.6078 7.9994 v Velocity[Y] -27.603 28.714 -0.14657 -0.008058 v Velocity[Z] -2.9371 3.0644 2.5384e-06 -5.3887e-08 v ǁVelocityǁ 0.0013658 38.751 7.978 8.1087 v Pressure -3.0195e+05 1.2271e+05 -90048 -59197 v TurbVisc 1.3469e-19 0.017975 0.00017742 3.23e-05 v CourantNb 5.0996e-08 0.011638 0.00016854 4.9435e-06 v FourierNb 1.2425e-07 0.045432 0.0001468 3.5348e-07 v total_pressure -2.0062e+05 2.2403e+05 11277 42128 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0139 0.10284 0.0028695 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2874e-07 0.050765 0.00031534 5.297e-06 INSTANT 0.876003000E-01 TIME STEP NUMBER 56201 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282862780E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.802453004E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12448E-01 0.20505E+01 Friction velocity uk : 0.12448E-01 0.20505E+01 Dimensionless distance yplus : 0.12384E-01 0.20134E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -5.893520299e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29440E+08 1 0.18062E-09 0.25683E+02 0.19537E+04 c Velocity[X] 0.13819E+02 c Velocity[Y] 0.11864E+02 c Velocity[Z] 0.10254E-05 c Pressure 0.10005E-03 9 0.57176E-04 0.91283E-03 0.46354E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -24.719 38.623 5.6077 7.9992 v Velocity[Y] -27.612 28.721 -0.14659 -0.0081045 v Velocity[Z] -2.9368 3.0646 2.5378e-06 -5.3887e-08 v ǁVelocityǁ 0.0014915 38.763 7.9795 8.1087 v Pressure -3.0154e+05 1.2328e+05 -89526 -58993 v TurbVisc 1.4959e-19 0.017993 0.00017747 3.2351e-05 v CourantNb 4.8926e-08 0.011637 0.00016854 4.9435e-06 v FourierNb 1.2425e-07 0.045422 0.00014681 3.5384e-07 v total_pressure -2.0022e+05 2.2461e+05 11799 42332 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0134 0.10287 0.0028697 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2872e-07 0.050755 0.00031535 5.2974e-06 INSTANT 0.876004000E-01 TIME STEP NUMBER 56202 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282856136E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.802107621E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.16370E-01 0.20500E+01 Friction velocity uk : 0.16370E-01 0.20500E+01 Dimensionless distance yplus : 0.16286E-01 0.20129E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -5.552472508e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29439E+08 1 0.18061E-09 0.25674E+02 0.19533E+04 c Velocity[X] 0.13815E+02 c Velocity[Y] 0.11859E+02 c Velocity[Z] 0.10195E-05 c Pressure 0.10490E-03 265 0.78131E-04 0.95657E-03 0.86707E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -24.727 38.634 5.6076 7.9991 v Velocity[Y] -27.621 28.728 -0.14661 -0.0081534 v Velocity[Z] -2.9366 3.0648 2.5371e-06 -5.3887e-08 v ǁVelocityǁ 0.0016116 38.775 7.981 8.1087 v Pressure -3.0094e+05 1.2402e+05 -88918 -58642 v TurbVisc 1.5184e-19 0.018011 0.00017752 3.2403e-05 v CourantNb 4.7662e-08 0.011637 0.00016854 4.9435e-06 v FourierNb 1.2425e-07 0.045413 0.00014681 3.5419e-07 v total_pressure -1.9961e+05 2.2534e+05 12407 42683 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0129 0.10289 0.0028699 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.287e-07 0.050746 0.00031535 5.2977e-06 INSTANT 0.876005000E-01 TIME STEP NUMBER 56203 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282849654E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.801765215E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.17907E-01 0.20495E+01 Friction velocity uk : 0.17907E-01 0.20495E+01 Dimensionless distance yplus : 0.17303E-01 0.20124E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -5.414544878e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29439E+08 1 0.18061E-09 0.25668E+02 0.19531E+04 c Velocity[X] 0.13811E+02 c Velocity[Y] 0.11857E+02 c Velocity[Z] 0.10165E-05 c Pressure 0.10846E-03 65 0.83987E-04 0.98865E-03 0.87829E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -24.735 38.646 5.6076 7.999 v Velocity[Y] -27.63 28.736 -0.14663 -0.0082001 v Velocity[Z] -2.9363 3.0649 2.5364e-06 -5.3887e-08 v ǁVelocityǁ 0.0017338 38.787 7.9825 8.1088 v Pressure -3.0045e+05 1.2469e+05 -88301 -58329 v TurbVisc 1.4253e-19 0.018029 0.00017757 3.2455e-05 v CourantNb 4.4954e-08 0.011636 0.00016854 4.9435e-06 v FourierNb 1.2425e-07 0.045403 0.00014682 3.5454e-07 v total_pressure -1.9913e+05 2.2602e+05 13024 42996 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0124 0.10291 0.0028701 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2869e-07 0.050736 0.00031536 5.2981e-06 INSTANT 0.876006000E-01 TIME STEP NUMBER 56204 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282843055E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.801423513E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.17416E-01 0.20490E+01 Friction velocity uk : 0.17416E-01 0.20490E+01 Dimensionless distance yplus : 0.16828E-01 0.20119E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -5.164186502e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29438E+08 1 0.18061E-09 0.25662E+02 0.19528E+04 c Velocity[X] 0.13807E+02 c Velocity[Y] 0.11855E+02 c Velocity[Z] 0.10114E-05 c Pressure 0.11249E-03 289 0.97519E-04 0.10249E-02 0.99085E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -24.743 38.657 5.6075 7.9988 v Velocity[Y] -27.639 28.743 -0.14665 -0.00825 v Velocity[Z] -2.9361 3.0651 2.5358e-06 -5.3887e-08 v ǁVelocityǁ 0.0018443 38.798 7.984 8.1088 v Pressure -2.9983e+05 1.2551e+05 -87616 -57983 v TurbVisc 1.4208e-19 0.018047 0.00017762 3.2507e-05 v CourantNb 4.3199e-08 0.011636 0.00016855 4.9435e-06 v FourierNb 1.2425e-07 0.045393 0.00014682 3.549e-07 v total_pressure -1.985e+05 2.2683e+05 13709 43342 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0119 0.10293 0.0028703 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2876e-07 0.050726 0.00031537 5.2984e-06 INSTANT 0.876007000E-01 TIME STEP NUMBER 56205 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282836765E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.801084910E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.16087E-01 0.20485E+01 Friction velocity uk : 0.16087E-01 0.20485E+01 Dimensionless distance yplus : 0.15487E-01 0.20114E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -4.975037094e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29438E+08 1 0.18060E-09 0.25644E+02 0.19521E+04 c Velocity[X] 0.13802E+02 c Velocity[Y] 0.11842E+02 c Velocity[Z] 0.10069E-05 c Pressure 0.11666E-03 96 0.83001E-04 0.10624E-02 0.85294E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -24.751 38.669 5.6074 7.9987 v Velocity[Y] -27.648 28.75 -0.14668 -0.0082981 v Velocity[Z] -2.9358 3.0653 2.5351e-06 -5.3887e-08 v ǁVelocityǁ 0.0018357 38.81 7.9855 8.1088 v Pressure -2.9919e+05 1.263e+05 -86899 -57550 v TurbVisc 1.4285e-19 0.018066 0.00017767 3.2559e-05 v CourantNb 4.1486e-08 0.011635 0.00016855 4.9435e-06 v FourierNb 1.2425e-07 0.045383 0.00014683 3.5526e-07 v total_pressure -1.9786e+05 2.2763e+05 14426 43775 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0114 0.10295 0.0028705 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2884e-07 0.050716 0.00031538 5.2988e-06 INSTANT 0.876008000E-01 TIME STEP NUMBER 56206 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282830411E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.800748575E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.14085E-01 0.20480E+01 Friction velocity uk : 0.14085E-01 0.20480E+01 Dimensionless distance yplus : 0.13560E-01 0.20109E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -4.825812652e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29437E+08 1 0.18060E-09 0.25641E+02 0.19519E+04 c Velocity[X] 0.13798E+02 c Velocity[Y] 0.11843E+02 c Velocity[Z] 0.10188E-05 c Pressure 0.11676E-03 16 0.58353E-04 0.10629E-02 0.58418E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -24.758 38.68 5.6074 7.9986 v Velocity[Y] -27.657 28.757 -0.1467 -0.0083457 v Velocity[Z] -2.9356 3.0654 2.5344e-06 -5.3887e-08 v ǁVelocityǁ 0.0018221 38.822 7.987 8.1088 v Pressure -2.9859e+05 1.2709e+05 -86170 -57254 v TurbVisc 1.3901e-19 0.018084 0.00017772 3.2611e-05 v CourantNb 3.9799e-08 0.011635 0.00016855 4.9435e-06 v FourierNb 1.2425e-07 0.045373 0.00014683 3.5561e-07 v total_pressure -1.9727e+05 2.2841e+05 15155 44071 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0109 0.10297 0.0028707 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2891e-07 0.050706 0.00031539 5.2991e-06 INSTANT 0.876009000E-01 TIME STEP NUMBER 56207 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282824116E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.800416000E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11759E-01 0.20475E+01 Friction velocity uk : 0.11759E-01 0.20475E+01 Dimensionless distance yplus : 0.11321E-01 0.20105E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -4.647674771e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29436E+08 1 0.18060E-09 0.25631E+02 0.19515E+04 c Velocity[X] 0.13793E+02 c Velocity[Y] 0.11838E+02 c Velocity[Z] 0.10039E-05 c Pressure 0.12168E-03 166 0.79394E-04 0.11071E-02 0.10402E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -24.766 38.692 5.6073 7.9985 v Velocity[Y] -27.666 28.764 -0.14672 -0.0083958 v Velocity[Z] -2.9353 3.0656 2.5338e-06 -5.3887e-08 v ǁVelocityǁ 0.0018265 38.833 7.9885 8.1089 v Pressure -2.9778e+05 1.2804e+05 -85355 -56774 v TurbVisc 1.6502e-19 0.018102 0.00017777 3.2663e-05 v CourantNb 3.8765e-08 0.011634 0.00016855 4.9435e-06 v FourierNb 1.2425e-07 0.045364 0.00014684 3.5597e-07 v total_pressure -1.9646e+05 2.2937e+05 15970 44551 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0105 0.10299 0.0028709 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2899e-07 0.050696 0.00031539 5.2995e-06 INSTANT 0.876010000E-01 TIME STEP NUMBER 56208 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282817985E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.800088521E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.90417E-02 0.20470E+01 Friction velocity uk : 0.90417E-02 0.20470E+01 Dimensionless distance yplus : 0.87046E-02 0.20100E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -4.625999869e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29436E+08 1 0.18060E-09 0.25625E+02 0.19512E+04 c Velocity[X] 0.13788E+02 c Velocity[Y] 0.11837E+02 c Velocity[Z] 0.10015E-05 c Pressure 0.12538E-03 387 0.85609E-04 0.11403E-02 0.11395E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -24.774 38.703 5.6072 7.9983 v Velocity[Y] -27.675 28.771 -0.14674 -0.0084434 v Velocity[Z] -2.9351 3.0658 2.5331e-06 -5.3888e-08 v ǁVelocityǁ 0.0018335 38.845 7.99 8.1089 v Pressure -2.9704e+05 1.2899e+05 -84496 -56245 v TurbVisc 1.1347e-19 0.01812 0.00017782 3.2716e-05 v CourantNb 3.6429e-08 0.011633 0.00016856 4.9435e-06 v FourierNb 1.2425e-07 0.045354 0.00014685 3.5633e-07 v total_pressure -1.9572e+05 2.3031e+05 16829 45080 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.01 0.10301 0.0028711 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2907e-07 0.050686 0.0003154 5.2999e-06 INSTANT 0.876011000E-01 TIME STEP NUMBER 56209 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282811786E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.799761965E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.53471E-02 0.20465E+01 Friction velocity uk : 0.53471E-02 0.20465E+01 Dimensionless distance yplus : 0.51478E-02 0.20095E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -4.548467408e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29435E+08 1 0.18059E-09 0.25618E+02 0.19509E+04 c Velocity[X] 0.13784E+02 c Velocity[Y] 0.11834E+02 c Velocity[Z] 0.99607E-06 c Pressure 0.12954E-03 138 0.99522E-04 0.11776E-02 0.10302E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -24.781 38.714 5.6072 7.9982 v Velocity[Y] -27.684 28.779 -0.14677 -0.0084946 v Velocity[Z] -2.9348 3.0659 2.5325e-06 -5.3888e-08 v ǁVelocityǁ 0.0018473 38.856 7.9915 8.1089 v Pressure -2.963e+05 1.2993e+05 -83653 -55926 v TurbVisc 1.2367e-19 0.018138 0.00017787 3.2768e-05 v CourantNb 3.4912e-08 0.011633 0.00016856 4.9435e-06 v FourierNb 1.2425e-07 0.045344 0.00014685 3.5668e-07 v total_pressure -1.9497e+05 2.3126e+05 17672 45399 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0095 0.10303 0.0028712 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2914e-07 0.050676 0.00031541 5.3002e-06 INSTANT 0.876012000E-01 TIME STEP NUMBER 56210 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282805883E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.799438151E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.54458E-02 0.20460E+01 Friction velocity uk : 0.54458E-02 0.20460E+01 Dimensionless distance yplus : 0.52428E-02 0.20090E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -4.524841488e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29435E+08 1 0.18059E-09 0.25599E+02 0.19501E+04 c Velocity[X] 0.13777E+02 c Velocity[Y] 0.11822E+02 c Velocity[Z] 0.99295E-06 c Pressure 0.13366E-03 335 0.84683E-04 0.12145E-02 0.10627E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -24.789 38.726 5.6071 7.9981 v Velocity[Y] -27.693 28.786 -0.14679 -0.0085443 v Velocity[Z] -2.9346 3.0661 2.5318e-06 -5.3888e-08 v ǁVelocityǁ 0.0018676 38.868 7.993 8.1089 v Pressure -2.9547e+05 1.3094e+05 -82723 -55356 v TurbVisc 1.2901e-19 0.018156 0.00017792 3.282e-05 v CourantNb 3.3346e-08 0.011632 0.00016856 4.9436e-06 v FourierNb 1.2425e-07 0.045334 0.00014686 3.5704e-07 v total_pressure -1.9415e+05 2.3227e+05 18602 45969 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.009 0.10305 0.0028714 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2922e-07 0.050666 0.00031542 5.3006e-06 INSTANT 0.876013000E-01 TIME STEP NUMBER 56211 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282799919E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.799120945E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.90906E-02 0.20456E+01 Friction velocity uk : 0.90906E-02 0.20456E+01 Dimensionless distance yplus : 0.87517E-02 0.20086E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -4.529543593e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29434E+08 1 0.18059E-09 0.25596E+02 0.19500E+04 c Velocity[X] 0.13774E+02 c Velocity[Y] 0.11822E+02 c Velocity[Z] 0.99164E-06 c Pressure 0.13407E-03 9 0.58547E-04 0.12177E-02 0.83988E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -24.796 38.737 5.607 7.998 v Velocity[Y] -27.702 28.793 -0.14682 -0.0085928 v Velocity[Z] -2.9343 3.0662 2.5311e-06 -5.3888e-08 v ǁVelocityǁ 0.0018943 38.879 7.9945 8.109 v Pressure -2.9463e+05 1.3196e+05 -81769 -54885 v TurbVisc 1.3094e-19 0.018175 0.00017797 3.2873e-05 v CourantNb 3.2595e-08 0.011632 0.00016856 4.9436e-06 v FourierNb 1.2425e-07 0.045324 0.00014686 3.574e-07 v total_pressure -1.9331e+05 2.3329e+05 19556 46440 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0086 0.10307 0.0028716 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.293e-07 0.050656 0.00031543 5.301e-06 INSTANT 0.876014000E-01 TIME STEP NUMBER 56212 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282794082E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.798808522E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11289E-01 0.20451E+01 Friction velocity uk : 0.11289E-01 0.20451E+01 Dimensionless distance yplus : 0.10868E-01 0.20081E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -4.534552302e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29434E+08 1 0.18059E-09 0.25586E+02 0.19495E+04 c Velocity[X] 0.13767E+02 c Velocity[Y] 0.11818E+02 c Velocity[Z] 0.98666E-06 c Pressure 0.13884E-03 312 0.80856E-04 0.12605E-02 0.12003E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -24.804 38.748 5.607 7.9978 v Velocity[Y] -27.71 28.8 -0.14684 -0.0086441 v Velocity[Z] -2.9341 3.0664 2.5305e-06 -5.3888e-08 v ǁVelocityǁ 0.0019254 38.891 7.996 8.109 v Pressure -2.9366e+05 1.3314e+05 -80779 -54320 v TurbVisc 1.3911e-19 0.018193 0.00017802 3.2925e-05 v CourantNb 3.2529e-08 0.011631 0.00016856 4.9436e-06 v FourierNb 1.2425e-07 0.045315 0.00014687 3.5776e-07 v total_pressure -1.9233e+05 2.3446e+05 20546 47005 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0081 0.10308 0.0028717 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2938e-07 0.050646 0.00031543 5.3013e-06 INSTANT 0.876015000E-01 TIME STEP NUMBER 56213 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282788388E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.798501149E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13837E-01 0.20446E+01 Friction velocity uk : 0.13837E-01 0.20446E+01 Dimensionless distance yplus : 0.13322E-01 0.20076E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -4.609305739e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29433E+08 1 0.18059E-09 0.25579E+02 0.19492E+04 c Velocity[X] 0.13762E+02 c Velocity[Y] 0.11817E+02 c Velocity[Z] 0.98100E-06 c Pressure 0.14248E-03 97 0.86764E-04 0.12929E-02 0.12681E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -24.811 38.76 5.6069 7.9977 v Velocity[Y] -27.719 28.807 -0.14686 -0.0086929 v Velocity[Z] -2.9338 3.0666 2.5298e-06 -5.3888e-08 v ǁVelocityǁ 0.0019633 38.903 7.9975 8.1091 v Pressure -2.9274e+05 1.3423e+05 -79735 -53718 v TurbVisc 1.2617e-19 0.018211 0.00017807 3.2978e-05 v CourantNb 3.2286e-08 0.011631 0.00016857 4.9436e-06 v FourierNb 1.2425e-07 0.045305 0.00014688 3.5812e-07 v total_pressure -1.9142e+05 2.3555e+05 21590 47607 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0076 0.1031 0.0028718 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2946e-07 0.050636 0.00031544 5.3017e-06 INSTANT 0.876016000E-01 TIME STEP NUMBER 56214 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282782660E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.798196656E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15728E-01 0.20441E+01 Friction velocity uk : 0.15728E-01 0.20441E+01 Dimensionless distance yplus : 0.15142E-01 0.20071E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -4.699581688e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29433E+08 1 0.18059E-09 0.25562E+02 0.19486E+04 c Velocity[X] 0.13756E+02 c Velocity[Y] 0.11806E+02 c Velocity[Z] 0.97692E-06 c Pressure 0.14643E-03 178 0.75548E-04 0.13282E-02 0.96236E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -24.818 38.771 5.6068 7.9976 v Velocity[Y] -27.728 28.814 -0.14688 -0.0087438 v Velocity[Z] -2.9336 3.0667 2.5292e-06 -5.3888e-08 v ǁVelocityǁ 0.0019568 38.914 7.999 8.1091 v Pressure -2.918e+05 1.354e+05 -78681 -53228 v TurbVisc 1.2591e-19 0.018229 0.00017812 3.303e-05 v CourantNb 3.2346e-08 0.01163 0.00016857 4.9436e-06 v FourierNb 1.2425e-07 0.045295 0.00014688 3.5848e-07 v total_pressure -1.9048e+05 2.3673e+05 22644 48097 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0071 0.10312 0.0028719 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2954e-07 0.050626 0.00031545 5.3021e-06 INSTANT 0.876017000E-01 TIME STEP NUMBER 56215 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282777133E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.797897093E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.17304E-01 0.20436E+01 Friction velocity uk : 0.17304E-01 0.20436E+01 Dimensionless distance yplus : 0.16644E-01 0.20066E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -4.810652802e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29432E+08 1 0.18059E-09 0.25558E+02 0.19484E+04 c Velocity[X] 0.13753E+02 c Velocity[Y] 0.11805E+02 c Velocity[Z] 0.97829E-06 c Pressure 0.14755E-03 9 0.53513E-04 0.13378E-02 0.86420E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -24.826 38.782 5.6068 7.9975 v Velocity[Y] -27.737 28.821 -0.14691 -0.0087958 v Velocity[Z] -2.9333 3.0669 2.5285e-06 -5.3888e-08 v ǁVelocityǁ 0.0019187 38.926 8.0005 8.1091 v Pressure -2.9086e+05 1.3655e+05 -77592 -52724 v TurbVisc 1.3249e-19 0.018247 0.00017817 3.3083e-05 v CourantNb 3.1076e-08 0.011629 0.00016857 4.9436e-06 v FourierNb 1.2425e-07 0.045285 0.00014689 3.5884e-07 v total_pressure -1.8954e+05 2.3788e+05 23733 48601 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0066 0.10313 0.002872 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2962e-07 0.050615 0.00031546 5.3024e-06 INSTANT 0.876018000E-01 TIME STEP NUMBER 56216 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282771841E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.797604376E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13653E-01 0.20431E+01 Friction velocity uk : 0.13653E-01 0.20431E+01 Dimensionless distance yplus : 0.13133E-01 0.20061E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -4.928753351e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29432E+08 1 0.18059E-09 0.25545E+02 0.19478E+04 c Velocity[X] 0.13746E+02 c Velocity[Y] 0.11799E+02 c Velocity[Z] 0.97551E-06 c Pressure 0.15178E-03 154 0.96743E-04 0.13755E-02 0.13608E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -24.833 38.794 5.6067 7.9974 v Velocity[Y] -27.745 28.828 -0.14693 -0.008847 v Velocity[Z] -2.9331 3.0671 2.5278e-06 -5.3888e-08 v ǁVelocityǁ 0.0018866 38.937 8.002 8.1092 v Pressure -2.897e+05 1.3787e+05 -76443 -51949 v TurbVisc 1.3808e-19 0.018265 0.00017822 3.3136e-05 v CourantNb 2.9552e-08 0.011629 0.00016857 4.9436e-06 v FourierNb 1.2425e-07 0.045275 0.00014689 3.592e-07 v total_pressure -1.8838e+05 2.392e+05 24882 49376 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0061 0.10315 0.0028721 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.297e-07 0.050605 0.00031547 5.3028e-06 INSTANT 0.876019000E-01 TIME STEP NUMBER 56217 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282766525E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.797319190E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.92952E-02 0.20426E+01 Friction velocity uk : 0.92952E-02 0.20426E+01 Dimensionless distance yplus : 0.89410E-02 0.20056E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -5.093336573e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29431E+08 1 0.18059E-09 0.25535E+02 0.19474E+04 c Velocity[X] 0.13741E+02 c Velocity[Y] 0.11795E+02 c Velocity[Z] 0.97047E-06 c Pressure 0.15464E-03 65 0.81052E-04 0.14008E-02 0.11151E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -24.84 38.805 5.6067 7.9973 v Velocity[Y] -27.754 28.835 -0.14695 -0.008898 v Velocity[Z] -2.9328 3.0672 2.5272e-06 -5.3888e-08 v ǁVelocityǁ 0.0018614 38.948 8.0034 8.1092 v Pressure -2.8866e+05 1.3914e+05 -75248 -51299 v TurbVisc 9.5085e-20 0.018283 0.00017827 3.3189e-05 v CourantNb 2.7639e-08 0.011628 0.00016857 4.9436e-06 v FourierNb 1.2425e-07 0.045265 0.0001469 3.5956e-07 v total_pressure -1.8733e+05 2.4047e+05 26077 50026 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0056 0.10316 0.0028721 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2978e-07 0.050595 0.00031547 5.3032e-06 INSTANT 0.876020000E-01 TIME STEP NUMBER 56218 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282761312E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.797038765E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.91439E-03 0.20421E+01 Friction velocity uk : 0.91439E-03 0.20421E+01 Dimensionless distance yplus : 0.87955E-03 0.20051E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -5.292569642e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29431E+08 1 0.18059E-09 0.25531E+02 0.19472E+04 c Velocity[X] 0.13736E+02 c Velocity[Y] 0.11795E+02 c Velocity[Z] 0.97354E-06 c Pressure 0.15721E-03 9 0.52818E-04 0.14235E-02 0.10876E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -24.848 38.816 5.6066 7.9972 v Velocity[Y] -27.762 28.842 -0.14697 -0.0089486 v Velocity[Z] -2.9326 3.0674 2.5265e-06 -5.3888e-08 v ǁVelocityǁ 0.0018411 38.96 8.0049 8.1093 v Pressure -2.8759e+05 1.4042e+05 -74030 -50692 v TurbVisc 6.8512e-20 0.018302 0.00017832 3.3242e-05 v CourantNb 2.5717e-08 0.011628 0.00016858 4.9436e-06 v FourierNb 1.2425e-07 0.045254 0.00014691 3.5992e-07 v total_pressure -1.8627e+05 2.4174e+05 27295 50633 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0051 0.10318 0.0028721 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2987e-07 0.050585 0.00031548 5.3035e-06 INSTANT 0.876021000E-01 TIME STEP NUMBER 56219 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282756204E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.796762086E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10104E-01 0.20416E+01 Friction velocity uk : 0.10104E-01 0.20416E+01 Dimensionless distance yplus : 0.97187E-02 0.20046E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -5.347162888e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29431E+08 1 0.18059E-09 0.25518E+02 0.19467E+04 c Velocity[X] 0.13730E+02 c Velocity[Y] 0.11788E+02 c Velocity[Z] 0.97056E-06 c Pressure 0.16134E-03 222 0.98425E-04 0.14602E-02 0.13180E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -24.855 38.827 5.6065 7.9971 v Velocity[Y] -27.771 28.849 -0.147 -0.0089998 v Velocity[Z] -2.9323 3.0676 2.5259e-06 -5.3888e-08 v ǁVelocityǁ 0.0018293 38.971 8.0064 8.1093 v Pressure -2.8636e+05 1.4179e+05 -72813 -49963 v TurbVisc 1.0091e-19 0.01832 0.00017837 3.3295e-05 v CourantNb 2.5639e-08 0.011627 0.00016858 4.9436e-06 v FourierNb 1.2425e-07 0.045244 0.00014691 3.6028e-07 v total_pressure -1.8503e+05 2.4311e+05 28512 51362 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0046 0.1032 0.0028724 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.2995e-07 0.050574 0.00031549 5.3039e-06 INSTANT 0.876022000E-01 TIME STEP NUMBER 56220 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282751226E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.796492416E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.95359E-02 0.20410E+01 Friction velocity uk : 0.95359E-02 0.20410E+01 Dimensionless distance yplus : 0.91775E-02 0.20041E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -5.576329758e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29430E+08 1 0.18059E-09 0.25509E+02 0.19463E+04 c Velocity[X] 0.13725E+02 c Velocity[Y] 0.11784E+02 c Velocity[Z] 0.96279E-06 c Pressure 0.16402E-03 39 0.82965E-04 0.14838E-02 0.10636E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -24.862 38.839 5.6065 7.997 v Velocity[Y] -27.779 28.857 -0.14702 -0.0090519 v Velocity[Z] -2.9321 3.0677 2.5252e-06 -5.3888e-08 v ǁVelocityǁ 0.0018231 38.983 8.0079 8.1094 v Pressure -2.8526e+05 1.4315e+05 -71546 -49361 v TurbVisc 9.7987e-20 0.018338 0.00017842 3.3348e-05 v CourantNb 2.5726e-08 0.011626 0.00016858 4.9436e-06 v FourierNb 1.2425e-07 0.045234 0.00014692 3.6065e-07 v total_pressure -1.8394e+05 2.4447e+05 29779 51964 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0041 0.10321 0.0028726 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.3003e-07 0.050564 0.0003155 5.3043e-06 INSTANT 0.876023000E-01 TIME STEP NUMBER 56221 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282746381E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.796230901E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.52446E-02 0.20405E+01 Friction velocity uk : 0.52446E-02 0.20405E+01 Dimensionless distance yplus : 0.50474E-02 0.20036E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -5.786534004e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29430E+08 1 0.18059E-09 0.25506E+02 0.19461E+04 c Velocity[X] 0.13721E+02 c Velocity[Y] 0.11785E+02 c Velocity[Z] 0.96660E-06 c Pressure 0.16634E-03 9 0.54322E-04 0.15041E-02 0.11682E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -24.869 38.85 5.6064 7.9969 v Velocity[Y] -27.788 28.864 -0.14704 -0.0091057 v Velocity[Z] -2.9318 3.0679 2.5245e-06 -5.3888e-08 v ǁVelocityǁ 0.0018231 38.994 8.0094 8.1094 v Pressure -2.8411e+05 1.4455e+05 -70222 -48717 v TurbVisc 1.0949e-19 0.018356 0.00017847 3.3401e-05 v CourantNb 2.5725e-08 0.011626 0.00016858 4.9436e-06 v FourierNb 1.2425e-07 0.045224 0.00014692 3.6101e-07 v total_pressure -1.8278e+05 2.4588e+05 31103 52608 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0036 0.10323 0.0028727 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.3012e-07 0.050553 0.00031551 5.3047e-06 INSTANT 0.876024000E-01 TIME STEP NUMBER 56222 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282741753E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.795975058E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.57463E-02 0.20400E+01 Friction velocity uk : 0.57463E-02 0.20400E+01 Dimensionless distance yplus : 0.55303E-02 0.20031E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -5.940549620e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29429E+08 1 0.18060E-09 0.25496E+02 0.19457E+04 c Velocity[X] 0.13714E+02 c Velocity[Y] 0.11782E+02 c Velocity[Z] 0.96466E-06 c Pressure 0.17028E-03 31 0.76443E-04 0.15391E-02 0.19826E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -24.876 38.861 5.6063 7.9968 v Velocity[Y] -27.796 28.871 -0.14706 -0.0091566 v Velocity[Z] -2.9316 3.068 2.5239e-06 -5.3888e-08 v ǁVelocityǁ 0.0018256 39.006 8.0108 8.1095 v Pressure -2.8271e+05 1.4605e+05 -68869 -47717 v TurbVisc 1.2322e-19 0.018374 0.00017852 3.3454e-05 v CourantNb 2.5632e-08 0.011625 0.00016858 4.9437e-06 v FourierNb 1.2425e-07 0.045213 0.00014693 3.6137e-07 v total_pressure -1.8138e+05 2.4738e+05 32456 53608 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0031 0.10324 0.0028729 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.302e-07 0.050543 0.00031551 5.305e-06 INSTANT 0.876025000E-01 TIME STEP NUMBER 56223 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282737045E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.795725841E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.89740E-02 0.20395E+01 Friction velocity uk : 0.89740E-02 0.20395E+01 Dimensionless distance yplus : 0.89564E-02 0.20026E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -6.088318927e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29429E+08 1 0.18060E-09 0.25491E+02 0.19454E+04 c Velocity[X] 0.13710E+02 c Velocity[Y] 0.11781E+02 c Velocity[Z] 0.96123E-06 c Pressure 0.17330E-03 1196 0.80613E-04 0.15657E-02 0.13243E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -24.883 38.873 5.6062 7.9967 v Velocity[Y] -27.805 28.878 -0.14708 -0.0092109 v Velocity[Z] -2.9313 3.0682 2.5232e-06 -5.3888e-08 v ǁVelocityǁ 0.0018343 39.018 8.0123 8.1096 v Pressure -2.8153e+05 1.4749e+05 -67514 -47155 v TurbVisc 1.1263e-19 0.018392 0.00017857 3.3507e-05 v CourantNb 2.5769e-08 0.011625 0.00016859 4.9437e-06 v FourierNb 1.2425e-07 0.045203 0.00014694 3.6174e-07 v total_pressure -1.8021e+05 2.4882e+05 33811 54170 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0026 0.10326 0.002873 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.3029e-07 0.050532 0.00031552 5.3054e-06 INSTANT 0.876026000E-01 TIME STEP NUMBER 56224 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282732652E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.795482718E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.33480E-02 0.20389E+01 Friction velocity uk : 0.33480E-02 0.20389E+01 Dimensionless distance yplus : 0.33414E-02 0.20020E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -6.328901077e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29429E+08 1 0.18060E-09 0.25485E+02 0.19452E+04 c Velocity[X] 0.13706E+02 c Velocity[Y] 0.11779E+02 c Velocity[Z] 0.95865E-06 c Pressure 0.17653E-03 33 0.94690E-04 0.15942E-02 0.18113E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -24.89 38.884 5.6062 7.9966 v Velocity[Y] -27.813 28.885 -0.1471 -0.009262 v Velocity[Z] -2.9311 3.0684 2.5226e-06 -5.3888e-08 v ǁVelocityǁ 0.0018358 39.029 8.0138 8.1096 v Pressure -2.8022e+05 1.4895e+05 -66118 -46307 v TurbVisc 1.2544e-19 0.01841 0.00017862 3.3561e-05 v CourantNb 2.5719e-08 0.011624 0.00016859 4.9437e-06 v FourierNb 1.2425e-07 0.045192 0.00014694 3.621e-07 v total_pressure -1.7889e+05 2.5028e+05 35207 55018 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.002 0.10327 0.0028731 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.3037e-07 0.050521 0.00031553 5.3058e-06 INSTANT 0.876027000E-01 TIME STEP NUMBER 56225 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282728260E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.795246261E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.37359E-02 0.20384E+01 Friction velocity uk : 0.37359E-02 0.20384E+01 Dimensionless distance yplus : 0.37286E-02 0.20015E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -6.513570730e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29428E+08 1 0.18060E-09 0.25469E+02 0.19445E+04 c Velocity[X] 0.13701E+02 c Velocity[Y] 0.11769E+02 c Velocity[Z] 0.95388E-06 c Pressure 0.17965E-03 176 0.79931E-04 0.16216E-02 0.13984E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -24.897 38.895 5.6061 7.9965 v Velocity[Y] -27.821 28.892 -0.14712 -0.0093155 v Velocity[Z] -2.9308 3.0685 2.5219e-06 -5.3888e-08 v ǁVelocityǁ 0.0018164 39.041 8.0153 8.1097 v Pressure -2.7891e+05 1.5048e+05 -64703 -45626 v TurbVisc 1.2212e-19 0.018428 0.00017867 3.3614e-05 v CourantNb 2.57e-08 0.011623 0.00016859 4.9437e-06 v FourierNb 1.2425e-07 0.045182 0.00014695 3.6247e-07 v total_pressure -1.7758e+05 2.5181e+05 36622 55699 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0015 0.10329 0.0028732 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.3046e-07 0.05051 0.00031554 5.3062e-06 INSTANT 0.876028000E-01 TIME STEP NUMBER 56226 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282724068E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.795020121E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.89542E-02 0.20378E+01 Friction velocity uk : 0.89542E-02 0.20378E+01 Dimensionless distance yplus : 0.89367E-02 0.20010E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -6.680630742e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29428E+08 1 0.18061E-09 0.25468E+02 0.19444E+04 c Velocity[X] 0.13698E+02 c Velocity[Y] 0.11769E+02 c Velocity[Z] 0.96429E-06 c Pressure 0.18019E-03 9 0.55870E-04 0.16258E-02 0.12599E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -24.904 38.907 5.606 7.9964 v Velocity[Y] -27.83 28.899 -0.14714 -0.0093702 v Velocity[Z] -2.9306 3.0687 2.5212e-06 -5.3888e-08 v ǁVelocityǁ 0.0018105 39.052 8.0167 8.1098 v Pressure -2.7762e+05 1.5196e+05 -63265 -44940 v TurbVisc 1.2378e-19 0.018446 0.00017872 3.3668e-05 v CourantNb 2.5695e-08 0.011623 0.00016859 4.9437e-06 v FourierNb 1.2425e-07 0.045171 0.00014696 3.6283e-07 v total_pressure -1.763e+05 2.5329e+05 38060 56385 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.001 0.10331 0.0028733 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.3055e-07 0.0505 0.00031555 5.3065e-06 INSTANT 0.876029000E-01 TIME STEP NUMBER 56227 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282720161E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.794801394E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11481E-01 0.20373E+01 Friction velocity uk : 0.11481E-01 0.20373E+01 Dimensionless distance yplus : 0.11049E-01 0.20004E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -6.858256117e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29428E+08 1 0.18061E-09 0.25459E+02 0.19440E+04 c Velocity[X] 0.13692E+02 c Velocity[Y] 0.11767E+02 c Velocity[Z] 0.95782E-06 c Pressure 0.18358E-03 32 0.75869E-04 0.16557E-02 0.22395E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -24.911 38.918 5.606 7.9963 v Velocity[Y] -27.838 28.907 -0.14716 -0.0094224 v Velocity[Z] -2.9303 3.0688 2.5206e-06 -5.3888e-08 v ǁVelocityǁ 0.0017982 39.064 8.0182 8.1098 v Pressure -2.7608e+05 1.5364e+05 -61750 -43847 v TurbVisc 1.3081e-19 0.018465 0.00017877 3.3721e-05 v CourantNb 2.5658e-08 0.011622 0.00016859 4.9437e-06 v FourierNb 1.2425e-07 0.045161 0.00014696 3.632e-07 v total_pressure -1.7476e+05 2.5496e+05 39575 57478 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0004 0.10332 0.0028734 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.3063e-07 0.050489 0.00031556 5.3069e-06 INSTANT 0.876030000E-01 TIME STEP NUMBER 56228 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282716134E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.794591175E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.58299E-02 0.20367E+01 Friction velocity uk : 0.58299E-02 0.20367E+01 Dimensionless distance yplus : 0.56108E-02 0.19999E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -6.915919314e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29427E+08 1 0.18061E-09 0.25456E+02 0.19438E+04 c Velocity[X] 0.13689E+02 c Velocity[Y] 0.11767E+02 c Velocity[Z] 0.95354E-06 c Pressure 0.18621E-03 65 0.80498E-04 0.16787E-02 0.15043E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -24.918 38.93 5.6059 7.9963 v Velocity[Y] -27.846 28.914 -0.14717 -0.0094776 v Velocity[Z] -2.9301 3.069 2.5199e-06 -5.3888e-08 v ǁVelocityǁ 0.0017951 39.076 8.0197 8.1099 v Pressure -2.7474e+05 1.5521e+05 -60261 -43191 v TurbVisc 1.194e-19 0.018483 0.00017882 3.3775e-05 v CourantNb 2.577e-08 0.011622 0.00016859 4.9438e-06 v FourierNb 1.2425e-07 0.04515 0.00014697 3.6356e-07 v total_pressure -1.7342e+05 2.5653e+05 41064 58134 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 1.9999 0.10334 0.0028734 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.3072e-07 0.050478 0.00031557 5.3073e-06 INSTANT 0.876031000E-01 TIME STEP NUMBER 56229 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282712431E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.794384896E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.55653E-02 0.20362E+01 Friction velocity uk : 0.55653E-02 0.20362E+01 Dimensionless distance yplus : 0.54654E-02 0.19993E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -7.084579798e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29427E+08 1 0.18062E-09 0.25451E+02 0.19436E+04 c Velocity[X] 0.13686E+02 c Velocity[Y] 0.11766E+02 c Velocity[Z] 0.95334E-06 c Pressure 0.18897E-03 37 0.94274E-04 0.17028E-02 0.20469E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -24.925 38.941 5.6058 7.9962 v Velocity[Y] -27.854 28.921 -0.14719 -0.0095301 v Velocity[Z] -2.9298 3.0692 2.5193e-06 -5.3889e-08 v ǁVelocityǁ 0.0017956 39.087 8.0212 8.11 v Pressure -2.7329e+05 1.568e+05 -58716 -42253 v TurbVisc 1.2443e-19 0.018501 0.00017887 3.3829e-05 v CourantNb 2.5721e-08 0.011621 0.0001686 4.9438e-06 v FourierNb 1.2425e-07 0.045139 0.00014698 3.6393e-07 v total_pressure -1.7196e+05 2.5812e+05 42609 59072 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 1.9993 0.10335 0.0028735 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.3081e-07 0.050467 0.00031557 5.3077e-06 INSTANT 0.876032000E-01 TIME STEP NUMBER 56230 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282708733E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.794186093E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.45932E-02 0.20356E+01 Friction velocity uk : 0.45932E-02 0.20356E+01 Dimensionless distance yplus : 0.44505E-02 0.19988E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -7.222579229e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29427E+08 1 0.18062E-09 0.25437E+02 0.19430E+04 c Velocity[X] 0.13682E+02 c Velocity[Y] 0.11756E+02 c Velocity[Z] 0.94767E-06 c Pressure 0.19166E-03 201 0.79651E-04 0.17263E-02 0.15715E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -24.932 38.953 5.6058 7.9961 v Velocity[Y] -27.863 28.928 -0.14721 -0.0095848 v Velocity[Z] -2.9296 3.0693 2.5186e-06 -5.3889e-08 v ǁVelocityǁ 0.0017976 39.099 8.0226 8.1101 v Pressure -2.7184e+05 1.5844e+05 -57179 -41509 v TurbVisc 1.2572e-19 0.018519 0.00017892 3.3883e-05 v CourantNb 2.678e-08 0.011621 0.0001686 4.9438e-06 v FourierNb 1.2425e-07 0.045128 0.00014698 3.643e-07 v total_pressure -1.7051e+05 2.5976e+05 44146 59816 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 1.9988 0.10337 0.0028736 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.309e-07 0.050456 0.00031558 5.3081e-06 INSTANT 0.876033000E-01 TIME STEP NUMBER 56231 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282705251E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.793997431E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.38309E-02 0.20351E+01 Friction velocity uk : 0.38309E-02 0.20351E+01 Dimensionless distance yplus : 0.37118E-02 0.19982E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -7.295463133e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29426E+08 1 0.18063E-09 0.25437E+02 0.19430E+04 c Velocity[X] 0.13680E+02 c Velocity[Y] 0.11757E+02 c Velocity[Z] 0.96090E-06 c Pressure 0.19189E-03 9 0.55976E-04 0.17276E-02 0.14479E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -24.939 38.964 5.6057 7.996 v Velocity[Y] -27.871 28.936 -0.14723 -0.0096407 v Velocity[Z] -2.9293 3.0695 2.5179e-06 -5.3889e-08 v ǁVelocityǁ 0.0018059 39.111 8.0241 8.1102 v Pressure -2.7044e+05 1.6003e+05 -55617 -40755 v TurbVisc 1.2677e-19 0.018537 0.00017897 3.3936e-05 v CourantNb 2.6904e-08 0.01162 0.0001686 4.9438e-06 v FourierNb 1.2425e-07 0.045118 0.00014699 3.6467e-07 v total_pressure -1.6912e+05 2.6135e+05 45708 60570 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 1.9982 0.10339 0.0028737 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.3099e-07 0.050445 0.00031559 5.3085e-06 INSTANT 0.876034000E-01 TIME STEP NUMBER 56232 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282702074E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.793818428E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.56416E-02 0.20345E+01 Friction velocity uk : 0.56416E-02 0.20345E+01 Dimensionless distance yplus : 0.54663E-02 0.19977E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -7.358170456e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29426E+08 1 0.18063E-09 0.25427E+02 0.19425E+04 c Velocity[X] 0.13675E+02 c Velocity[Y] 0.11752E+02 c Velocity[Z] 0.96308E-06 c Pressure 0.19476E-03 25 0.99902E-04 0.17527E-02 0.21089E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -24.945 38.976 5.6056 7.996 v Velocity[Y] -27.879 28.943 -0.14724 -0.0096957 v Velocity[Z] -2.9291 3.0697 2.5173e-06 -5.3889e-08 v ǁVelocityǁ 0.0018203 39.122 8.0256 8.1102 v Pressure -2.6881e+05 1.6177e+05 -54010 -39713 v TurbVisc 1.3e-19 0.018555 0.00017902 3.399e-05 v CourantNb 2.8392e-08 0.011619 0.0001686 4.9438e-06 v FourierNb 1.2425e-07 0.045107 0.000147 3.6504e-07 v total_pressure -1.6748e+05 2.631e+05 47315 61612 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 1.9977 0.10341 0.0028739 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.3109e-07 0.050434 0.0003156 5.3089e-06 INSTANT 0.876035000E-01 TIME STEP NUMBER 56233 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282698888E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.793649197E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.76582E-02 0.20339E+01 Friction velocity uk : 0.76582E-02 0.20339E+01 Dimensionless distance yplus : 0.74202E-02 0.19971E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -7.362831865e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29426E+08 1 0.18064E-09 0.25422E+02 0.19423E+04 c Velocity[X] 0.13673E+02 c Velocity[Y] 0.11749E+02 c Velocity[Z] 0.95432E-06 c Pressure 0.19642E-03 73 0.84115E-04 0.17668E-02 0.18699E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -24.952 38.987 5.6055 7.9959 v Velocity[Y] -27.887 28.95 -0.14726 -0.0097505 v Velocity[Z] -2.9288 3.0698 2.5166e-06 -5.3889e-08 v ǁVelocityǁ 0.0018373 39.134 8.027 8.1103 v Pressure -2.673e+05 1.6349e+05 -52372 -38770 v TurbVisc 1.4098e-19 0.018573 0.00017907 3.4045e-05 v CourantNb 3.0454e-08 0.011619 0.0001686 4.9439e-06 v FourierNb 1.2425e-07 0.045096 0.000147 3.6541e-07 v total_pressure -1.6597e+05 2.6481e+05 48953 62555 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 1.9971 0.10343 0.0028741 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.3118e-07 0.050422 0.00031561 5.3093e-06 INSTANT 0.876036000E-01 TIME STEP NUMBER 56234 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282695856E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.793487462E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11388E-01 0.20334E+01 Friction velocity uk : 0.11388E-01 0.20334E+01 Dimensionless distance yplus : 0.10960E-01 0.19966E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -7.393745794e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29426E+08 1 0.18064E-09 0.25424E+02 0.19423E+04 c Velocity[X] 0.13672E+02 c Velocity[Y] 0.11752E+02 c Velocity[Z] 0.98212E-06 c Pressure 0.19778E-03 15 0.56349E-04 0.17783E-02 0.16747E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -24.959 38.999 5.6055 7.9958 v Velocity[Y] -27.895 28.958 -0.14727 -0.0098049 v Velocity[Z] -2.9286 3.07 2.516e-06 -5.3889e-08 v ǁVelocityǁ 0.0018818 39.146 8.0285 8.1104 v Pressure -2.6582e+05 1.6514e+05 -50715 -37954 v TurbVisc 1.0921e-19 0.018591 0.00017912 3.4099e-05 v CourantNb 3.3145e-08 0.011618 0.0001686 4.9439e-06 v FourierNb 1.2425e-07 0.045085 0.00014701 3.6578e-07 v total_pressure -1.645e+05 2.6647e+05 50610 63371 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 1.9966 0.10345 0.0028742 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.3127e-07 0.050411 0.00031562 5.3097e-06 INSTANT 0.876037000E-01 TIME STEP NUMBER 56235 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282692965E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.793331018E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12800E-01 0.20328E+01 Friction velocity uk : 0.12800E-01 0.20328E+01 Dimensionless distance yplus : 0.12319E-01 0.19960E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -7.266043540e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29425E+08 1 0.18065E-09 0.25419E+02 0.19420E+04 c Velocity[X] 0.13669E+02 c Velocity[Y] 0.11750E+02 c Velocity[Z] 0.96266E-06 c Pressure 0.20046E-03 153 0.76641E-04 0.18016E-02 0.21363E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -24.966 39.011 5.6054 7.9958 v Velocity[Y] -27.904 28.965 -0.14729 -0.0098614 v Velocity[Z] -2.9283 3.0701 2.5153e-06 -5.3889e-08 v ǁVelocityǁ 0.0019191 39.158 8.03 8.1105 v Pressure -2.6415e+05 1.6692e+05 -49089 -37010 v TurbVisc 2.9484e-20 0.018609 0.00017917 3.4153e-05 v CourantNb 3.5546e-08 0.011618 0.00016861 4.9439e-06 v FourierNb 1.2425e-07 0.045074 0.00014702 3.6615e-07 v total_pressure -1.6282e+05 2.6825e+05 52236 64315 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 1.996 0.10347 0.0028744 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.3136e-07 0.0504 0.00031562 5.3101e-06 INSTANT 0.876038000E-01 TIME STEP NUMBER 56236 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282690246E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.793185173E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15084E-01 0.20322E+01 Friction velocity uk : 0.15084E-01 0.20322E+01 Dimensionless distance yplus : 0.14517E-01 0.19955E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -7.241845472e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29425E+08 1 0.18065E-09 0.25418E+02 0.19420E+04 c Velocity[X] 0.13668E+02 c Velocity[Y] 0.11751E+02 c Velocity[Z] 0.95289E-06 c Pressure 0.20226E-03 196 0.81725E-04 0.18170E-02 0.22214E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -24.973 39.023 5.6053 7.9957 v Velocity[Y] -27.912 28.972 -0.14731 -0.0099159 v Velocity[Z] -2.928 3.0703 2.5147e-06 -5.3889e-08 v ǁVelocityǁ 0.0019757 39.17 8.0314 8.1106 v Pressure -2.6259e+05 1.6866e+05 -47374 -36018 v TurbVisc 9.6627e-20 0.018627 0.00017922 3.4207e-05 v CourantNb 3.7707e-08 0.011617 0.00016861 4.9439e-06 v FourierNb 1.2425e-07 0.045063 0.00014702 3.6652e-07 v total_pressure -1.6127e+05 2.6999e+05 53951 65307 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 1.9955 0.10349 0.0028745 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.3146e-07 0.050389 0.00031563 5.3105e-06 INSTANT 0.876039000E-01 TIME STEP NUMBER 56237 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282687597E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.793047061E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.16691E-01 0.20317E+01 Friction velocity uk : 0.16691E-01 0.20317E+01 Dimensionless distance yplus : 0.16063E-01 0.19949E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -7.205614665e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29425E+08 1 0.18066E-09 0.25418E+02 0.19419E+04 c Velocity[X] 0.13667E+02 c Velocity[Y] 0.11751E+02 c Velocity[Z] 0.94880E-06 c Pressure 0.20427E-03 184 0.94834E-04 0.18342E-02 0.19348E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -24.979 39.034 5.6053 7.9957 v Velocity[Y] -27.92 28.98 -0.14732 -0.0099736 v Velocity[Z] -2.9278 3.0705 2.514e-06 -5.3889e-08 v ǁVelocityǁ 0.0020431 39.182 8.0329 8.1107 v Pressure -2.611e+05 1.7038e+05 -45713 -35236 v TurbVisc 1.0391e-19 0.018645 0.00017927 3.4262e-05 v CourantNb 4.0225e-08 0.011616 0.00016861 4.944e-06 v FourierNb 1.2425e-07 0.045052 0.00014703 3.6689e-07 v total_pressure -1.5978e+05 2.7171e+05 55612 66089 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 1.9949 0.10351 0.0028747 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.3155e-07 0.050378 0.00031564 5.3109e-06 INSTANT 0.876040000E-01 TIME STEP NUMBER 56238 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282685307E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.792917626E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.18329E-01 0.20311E+01 Friction velocity uk : 0.18329E-01 0.20311E+01 Dimensionless distance yplus : 0.17640E-01 0.19944E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -7.084685450e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29425E+08 1 0.18066E-09 0.25407E+02 0.19414E+04 c Velocity[X] 0.13665E+02 c Velocity[Y] 0.11741E+02 c Velocity[Z] 0.94629E-06 c Pressure 0.20611E-03 153 0.80652E-04 0.18499E-02 0.22704E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -24.986 39.046 5.6052 7.9956 v Velocity[Y] -27.928 28.987 -0.14734 -0.01003 v Velocity[Z] -2.9275 3.0706 2.5134e-06 -5.3889e-08 v ǁVelocityǁ 0.0021199 39.194 8.0344 8.1108 v Pressure -2.5956e+05 1.7216e+05 -43985 -34193 v TurbVisc 9.1974e-20 0.018663 0.00017932 3.4316e-05 v CourantNb 4.252e-08 0.011616 0.00016861 4.944e-06 v FourierNb 1.2425e-07 0.045041 0.00014704 3.6726e-07 v total_pressure -1.5824e+05 2.7348e+05 57340 67132 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 1.9944 0.10352 0.0028748 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.3165e-07 0.050367 0.00031565 5.3113e-06 INSTANT 0.876041000E-01 TIME STEP NUMBER 56239 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282683049E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.792800959E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19858E-01 0.20306E+01 Friction velocity uk : 0.19858E-01 0.20306E+01 Dimensionless distance yplus : 0.19111E-01 0.19939E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -6.934804947e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29425E+08 1 0.18067E-09 0.25411E+02 0.19415E+04 c Velocity[X] 0.13666E+02 c Velocity[Y] 0.11745E+02 c Velocity[Z] 0.98199E-06 c Pressure 0.20565E-03 15 0.58060E-04 0.18450E-02 0.17694E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -24.993 39.058 5.6052 7.9956 v Velocity[Y] -27.936 28.995 -0.14735 -0.010085 v Velocity[Z] -2.9273 3.0708 2.5127e-06 -5.3889e-08 v ǁVelocityǁ 0.0022087 39.206 8.0359 8.1109 v Pressure -2.581e+05 1.7386e+05 -42277 -33373 v TurbVisc 1.2312e-19 0.018681 0.00017938 3.4371e-05 v CourantNb 4.4748e-08 0.011615 0.00016861 4.944e-06 v FourierNb 1.2425e-07 0.045031 0.00014704 3.6764e-07 v total_pressure -1.5677e+05 2.7518e+05 59048 67952 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 1.9939 0.10354 0.002875 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.3174e-07 0.050356 0.00031566 5.3117e-06 INSTANT 0.876042000E-01 TIME STEP NUMBER 56240 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282680994E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.792693963E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.14810E-01 0.20301E+01 Friction velocity uk : 0.14810E-01 0.20301E+01 Dimensionless distance yplus : 0.14824E-01 0.19933E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -6.710197517e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29424E+08 1 0.18067E-09 0.25408E+02 0.19413E+04 c Velocity[X] 0.13664E+02 c Velocity[Y] 0.11744E+02 c Velocity[Z] 0.96388E-06 c Pressure 0.20769E-03 356 0.76433E-04 0.18625E-02 0.24557E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -25 39.07 5.6051 7.9955 v Velocity[Y] -27.944 29.002 -0.14736 -0.010143 v Velocity[Z] -2.927 3.0709 2.512e-06 -5.3889e-08 v ǁVelocityǁ 0.0023008 39.218 8.0373 8.1111 v Pressure -2.5645e+05 1.7573e+05 -40545 -32334 v TurbVisc 1.3806e-20 0.018699 0.00017943 3.4426e-05 v CourantNb 4.6898e-08 0.011615 0.00016862 4.9441e-06 v FourierNb 1.2425e-07 0.04502 0.00014705 3.6801e-07 v total_pressure -1.5513e+05 2.7705e+05 60780 68991 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 1.9933 0.10356 0.0028751 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.3184e-07 0.050345 0.00031567 5.3121e-06 INSTANT 0.876043000E-01 TIME STEP NUMBER 56241 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282679081E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.792597833E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12935E-01 0.20295E+01 Friction velocity uk : 0.12935E-01 0.20295E+01 Dimensionless distance yplus : 0.12947E-01 0.19928E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -6.497196550e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29424E+08 1 0.18068E-09 0.25410E+02 0.19414E+04 c Velocity[X] 0.13665E+02 c Velocity[Y] 0.11745E+02 c Velocity[Z] 0.94944E-06 c Pressure 0.20902E-03 73 0.82144E-04 0.18736E-02 0.23948E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.006 39.082 5.605 7.9955 v Velocity[Y] -27.952 29.01 -0.14738 -0.010199 v Velocity[Z] -2.9268 3.0711 2.5114e-06 -5.3889e-08 v ǁVelocityǁ 0.0024021 39.23 8.0388 8.1112 v Pressure -2.5491e+05 1.7751e+05 -38765 -31328 v TurbVisc 9.8841e-20 0.018718 0.00017948 3.448e-05 v CourantNb 4.8792e-08 0.011614 0.00016862 4.9441e-06 v FourierNb 1.2425e-07 0.045009 0.00014706 3.6838e-07 v total_pressure -1.5358e+05 2.7884e+05 62560 69997 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 1.9928 0.10357 0.0028753 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.3194e-07 0.050334 0.00031567 5.3125e-06 INSTANT 0.876044000E-01 TIME STEP NUMBER 56242 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282677210E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.792506263E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.88359E-02 0.20290E+01 Friction velocity uk : 0.88359E-02 0.20290E+01 Dimensionless distance yplus : 0.88442E-02 0.19923E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -6.287647774e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29424E+08 1 0.18069E-09 0.25413E+02 0.19414E+04 c Velocity[X] 0.13666E+02 c Velocity[Y] 0.11746E+02 c Velocity[Z] 0.94809E-06 c Pressure 0.21046E-03 306 0.94918E-04 0.18857E-02 0.23056E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.013 39.094 5.605 7.9955 v Velocity[Y] -27.96 29.017 -0.14739 -0.010258 v Velocity[Z] -2.9265 3.0713 2.5107e-06 -5.3889e-08 v ǁVelocityǁ 0.0023637 39.242 8.0403 8.1113 v Pressure -2.533e+05 1.7935e+05 -36996 -30393 v TurbVisc 9.5296e-20 0.018736 0.00017953 3.4535e-05 v CourantNb 5.0954e-08 0.011614 0.00016862 4.9441e-06 v FourierNb 1.2425e-07 0.044998 0.00014706 3.6876e-07 v total_pressure -1.5198e+05 2.8067e+05 64329 70932 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 1.9923 0.10359 0.0028754 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.3204e-07 0.050323 0.00031568 5.3129e-06 INSTANT 0.876045000E-01 TIME STEP NUMBER 56243 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282675765E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.792422988E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.50219E-02 0.20285E+01 Friction velocity uk : 0.50219E-02 0.20285E+01 Dimensionless distance yplus : 0.50266E-02 0.19918E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -6.042581176e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29424E+08 1 0.18070E-09 0.25404E+02 0.19410E+04 c Velocity[X] 0.13667E+02 c Velocity[Y] 0.11737E+02 c Velocity[Z] 0.94806E-06 c Pressure 0.21185E-03 99 0.80856E-04 0.18973E-02 0.23356E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.02 39.106 5.6049 7.9954 v Velocity[Y] -27.968 29.025 -0.14741 -0.010315 v Velocity[Z] -2.9263 3.0714 2.5101e-06 -5.3889e-08 v ǁVelocityǁ 0.0022876 39.255 8.0418 8.1114 v Pressure -2.5174e+05 1.8114e+05 -35228 -29386 v TurbVisc 1.0145e-19 0.018754 0.00017958 3.459e-05 v CourantNb 5.2838e-08 0.011613 0.00016862 4.9442e-06 v FourierNb 1.2425e-07 0.044988 0.00014707 3.6913e-07 v total_pressure -1.5042e+05 2.8246e+05 66097 71939 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 1.9918 0.10361 0.0028755 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.3214e-07 0.050312 0.00031569 5.3133e-06 INSTANT 0.876046000E-01 TIME STEP NUMBER 56244 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282674316E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.792350586E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11097E-01 0.20280E+01 Friction velocity uk : 0.11097E-01 0.20280E+01 Dimensionless distance yplus : 0.11107E-01 0.19913E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -5.726873085e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29424E+08 1 0.18070E-09 0.25411E+02 0.19412E+04 c Velocity[X] 0.13670E+02 c Velocity[Y] 0.11741E+02 c Velocity[Z] 0.95173E-06 c Pressure 0.21085E-03 10 0.58549E-04 0.18875E-02 0.19692E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.027 39.118 5.6049 7.9954 v Velocity[Y] -27.976 29.033 -0.14742 -0.010372 v Velocity[Z] -2.926 3.0716 2.5094e-06 -5.3889e-08 v ǁVelocityǁ 0.0022122 39.267 8.0432 8.1115 v Pressure -2.5024e+05 1.8288e+05 -33458 -28519 v TurbVisc 1.0428e-19 0.018772 0.00017963 3.4645e-05 v CourantNb 5.4604e-08 0.011612 0.00016862 4.9442e-06 v FourierNb 1.2425e-07 0.044977 0.00014708 3.6951e-07 v total_pressure -1.4891e+05 2.842e+05 67867 72806 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 1.9913 0.10362 0.0028757 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.3224e-07 0.050301 0.0003157 5.3137e-06 INSTANT 0.876047000E-01 TIME STEP NUMBER 56245 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282673086E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.792290176E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.71351E-02 0.20275E+01 Friction velocity uk : 0.71351E-02 0.20275E+01 Dimensionless distance yplus : 0.71417E-02 0.19908E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -5.338292602e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29424E+08 1 0.18071E-09 0.25412E+02 0.19411E+04 c Velocity[X] 0.13670E+02 c Velocity[Y] 0.11741E+02 c Velocity[Z] 0.95395E-06 c Pressure 0.21231E-03 191 0.76853E-04 0.18998E-02 0.26553E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.033 39.13 5.6049 7.9954 v Velocity[Y] -27.984 29.04 -0.14744 -0.010431 v Velocity[Z] -2.9257 3.0717 2.5088e-06 -5.3889e-08 v ǁVelocityǁ 0.0021536 39.279 8.0447 8.1117 v Pressure -2.4855e+05 1.8479e+05 -31670 -27456 v TurbVisc 1.1835e-19 0.01879 0.00017969 3.47e-05 v CourantNb 5.624e-08 0.011612 0.00016863 4.9443e-06 v FourierNb 1.2425e-07 0.044966 0.00014708 3.6989e-07 v total_pressure -1.4723e+05 2.8611e+05 69655 73869 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 1.9908 0.10364 0.0028758 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.3234e-07 0.05029 0.00031571 5.3141e-06 INSTANT 0.876048000E-01 TIME STEP NUMBER 56246 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282671996E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.792242401E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.70038E-02 0.20270E+01 Friction velocity uk : 0.70038E-02 0.20270E+01 Dimensionless distance yplus : 0.70103E-02 0.19904E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -4.992780413e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29424E+08 1 0.18072E-09 0.25416E+02 0.19413E+04 c Velocity[X] 0.13673E+02 c Velocity[Y] 0.11743E+02 c Velocity[Z] 0.95441E-06 c Pressure 0.21312E-03 70 0.82816E-04 0.19061E-02 0.26717E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.04 39.142 5.6048 7.9953 v Velocity[Y] -27.992 29.048 -0.14745 -0.010488 v Velocity[Z] -2.9255 3.0719 2.5081e-06 -5.3889e-08 v ǁVelocityǁ 0.002098 39.291 8.0462 8.1118 v Pressure -2.4696e+05 1.8662e+05 -29831 -26378 v TurbVisc 1.0919e-19 0.018808 0.00017974 3.4755e-05 v CourantNb 5.7626e-08 0.011611 0.00016863 4.9443e-06 v FourierNb 1.2425e-07 0.044956 0.00014709 3.7026e-07 v total_pressure -1.4564e+05 2.8794e+05 71494 74947 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 1.9904 0.10365 0.002876 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.3244e-07 0.05028 0.00031572 5.3146e-06 INSTANT 0.876049000E-01 TIME STEP NUMBER 56247 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282670982E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.792198959E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.58109E-02 0.20266E+01 Friction velocity uk : 0.58109E-02 0.20266E+01 Dimensionless distance yplus : 0.58163E-02 0.19899E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -4.642670169e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29424E+08 1 0.18072E-09 0.25422E+02 0.19414E+04 c Velocity[X] 0.13676E+02 c Velocity[Y] 0.11745E+02 c Velocity[Z] 0.95184E-06 c Pressure 0.21403E-03 191 0.95874E-04 0.19134E-02 0.23272E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.047 39.154 5.6048 7.9953 v Velocity[Y] -28 29.056 -0.14747 -0.010548 v Velocity[Z] -2.9252 3.072 2.5075e-06 -5.3889e-08 v ǁVelocityǁ 0.0020477 39.304 8.0477 8.1119 v Pressure -2.4536e+05 1.8845e+05 -28048 -25523 v TurbVisc 1.0728e-19 0.018826 0.00017979 3.4811e-05 v CourantNb 5.9125e-08 0.011611 0.00016863 4.9443e-06 v FourierNb 1.2425e-07 0.044945 0.00014709 3.7064e-07 v total_pressure -1.4403e+05 2.8977e+05 73277 75802 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 1.9899 0.10367 0.0028761 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.3254e-07 0.05027 0.00031572 5.315e-06 INSTANT 0.876050000E-01 TIME STEP NUMBER 56248 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282670333E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.792163950E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.48491E-02 0.20262E+01 Friction velocity uk : 0.48491E-02 0.20262E+01 Dimensionless distance yplus : 0.48536E-02 0.19895E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -4.233325043e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29424E+08 1 0.18073E-09 0.25416E+02 0.19411E+04 c Velocity[X] 0.13679E+02 c Velocity[Y] 0.11737E+02 c Velocity[Z] 0.95303E-06 c Pressure 0.21481E-03 123 0.81619E-04 0.19196E-02 0.26730E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.054 39.167 5.6048 7.9953 v Velocity[Y] -28.008 29.064 -0.14749 -0.010607 v Velocity[Z] -2.925 3.0722 2.5068e-06 -5.3889e-08 v ǁVelocityǁ 0.0020048 39.316 8.0492 8.1121 v Pressure -2.4375e+05 1.9028e+05 -26219 -24418 v TurbVisc 1.0312e-19 0.018844 0.00017984 3.4866e-05 v CourantNb 6.0358e-08 0.01161 0.00016863 4.9444e-06 v FourierNb 1.2425e-07 0.044935 0.0001471 3.7102e-07 v total_pressure -1.4243e+05 2.9161e+05 75106 76907 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 1.9895 0.10369 0.0028762 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.3264e-07 0.050259 0.00031573 5.3154e-06 INSTANT 0.876051000E-01 TIME STEP NUMBER 56249 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282669725E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.792141697E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.46836E-02 0.20257E+01 Friction velocity uk : 0.46836E-02 0.20257E+01 Dimensionless distance yplus : 0.46880E-02 0.19891E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -3.789015037e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29424E+08 1 0.18074E-09 0.25426E+02 0.19414E+04 c Velocity[X] 0.13684E+02 c Velocity[Y] 0.11742E+02 c Velocity[Z] 0.95586E-06 c Pressure 0.21326E-03 10 0.59202E-04 0.19049E-02 0.20912E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.06 39.179 5.6047 7.9953 v Velocity[Y] -28.016 29.072 -0.1475 -0.010665 v Velocity[Z] -2.9247 3.0724 2.5061e-06 -5.3889e-08 v ǁVelocityǁ 0.0019613 39.329 8.0507 8.1122 v Pressure -2.4223e+05 1.9204e+05 -24420 -23542 v TurbVisc 1.0438e-19 0.018862 0.0001799 3.4921e-05 v CourantNb 6.1422e-08 0.011609 0.00016863 4.9444e-06 v FourierNb 1.2425e-07 0.044925 0.00014711 3.714e-07 v total_pressure -1.409e+05 2.9336e+05 76905 77783 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 1.9891 0.1037 0.0028764 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.3275e-07 0.050249 0.00031574 5.3158e-06 INSTANT 0.876052000E-01 TIME STEP NUMBER 56250 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282669336E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.792130406E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.66700E-02 0.20253E+01 Friction velocity uk : 0.66700E-02 0.20253E+01 Dimensionless distance yplus : 0.64177E-02 0.19887E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -3.220527305e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29424E+08 1 0.18074E-09 0.25430E+02 0.19415E+04 c Velocity[X] 0.13687E+02 c Velocity[Y] 0.11743E+02 c Velocity[Z] 0.95825E-06 c Pressure 0.21416E-03 188 0.77615E-04 0.19121E-02 0.28091E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.067 39.191 5.6047 7.9953 v Velocity[Y] -28.024 29.08 -0.14752 -0.010726 v Velocity[Z] -2.9245 3.0725 2.5055e-06 -5.389e-08 v ǁVelocityǁ 0.0019421 39.341 8.0522 8.1124 v Pressure -2.4053e+05 1.9397e+05 -22607 -22472 v TurbVisc 1.0835e-19 0.01888 0.00017995 3.4977e-05 v CourantNb 6.2321e-08 0.011609 0.00016864 4.9445e-06 v FourierNb 1.2425e-07 0.044915 0.00014711 3.7178e-07 v total_pressure -1.3921e+05 2.9529e+05 78718 78853 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 1.9887 0.10372 0.0028766 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.3285e-07 0.050239 0.00031575 5.3163e-06 INSTANT 0.876053000E-01 TIME STEP NUMBER 56251 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282669084E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.792131866E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.30436E-02 0.20249E+01 Friction velocity uk : 0.30436E-02 0.20249E+01 Dimensionless distance yplus : 0.29285E-02 0.19883E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -2.854195395e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29424E+08 1 0.18075E-09 0.25438E+02 0.19417E+04 c Velocity[X] 0.13692E+02 c Velocity[Y] 0.11745E+02 c Velocity[Z] 0.95912E-06 c Pressure 0.21441E-03 40 0.83756E-04 0.19135E-02 0.28313E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.074 39.203 5.6047 7.9953 v Velocity[Y] -28.032 29.088 -0.14754 -0.010784 v Velocity[Z] -2.9242 3.0727 2.5048e-06 -5.389e-08 v ǁVelocityǁ 0.0019243 39.354 8.0537 8.1125 v Pressure -2.3893e+05 1.958e+05 -20747 -21383 v TurbVisc 1.0341e-19 0.018898 0.00018 3.5032e-05 v CourantNb 6.2927e-08 0.011608 0.00016864 4.9445e-06 v FourierNb 1.2425e-07 0.044905 0.00014712 3.7216e-07 v total_pressure -1.3761e+05 2.9713e+05 80578 79942 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 1.9883 0.10373 0.0028767 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.3295e-07 0.050229 0.00031576 5.3167e-06 INSTANT 0.876054000E-01 TIME STEP NUMBER 56252 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282668908E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.792137490E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.54298E-02 0.20246E+01 Friction velocity uk : 0.54298E-02 0.20246E+01 Dimensionless distance yplus : 0.52244E-02 0.19879E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -2.355136568e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29424E+08 1 0.18076E-09 0.25446E+02 0.19420E+04 c Velocity[X] 0.13698E+02 c Velocity[Y] 0.11749E+02 c Velocity[Z] 0.95639E-06 c Pressure 0.21476E-03 231 0.96773E-04 0.19157E-02 0.24734E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.081 39.216 5.6047 7.9953 v Velocity[Y] -28.04 29.096 -0.14755 -0.010845 v Velocity[Z] -2.9239 3.0728 2.5042e-06 -5.389e-08 v ǁVelocityǁ 0.0019106 39.366 8.0552 8.1127 v Pressure -2.3732e+05 1.9765e+05 -18946 -20513 v TurbVisc 1.0043e-19 0.018916 0.00018006 3.5088e-05 v CourantNb 6.3051e-08 0.011607 0.00016864 4.9446e-06 v FourierNb 1.2425e-07 0.044895 0.00014712 3.7254e-07 v total_pressure -1.36e+05 2.9897e+05 82379 80812 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 1.9879 0.10375 0.0028769 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.3306e-07 0.050219 0.00031576 5.3171e-06 INSTANT 0.876055000E-01 TIME STEP NUMBER 56253 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282669106E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.792151776E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.38860E-02 0.20242E+01 Friction velocity uk : 0.38860E-02 0.20242E+01 Dimensionless distance yplus : 0.38897E-02 0.19876E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.839913819e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29424E+08 1 0.18077E-09 0.25444E+02 0.19418E+04 c Velocity[X] 0.13703E+02 c Velocity[Y] 0.11741E+02 c Velocity[Z] 0.96051E-06 c Pressure 0.21499E-03 119 0.82595E-04 0.19169E-02 0.27895E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.087 39.228 5.6047 7.9953 v Velocity[Y] -28.048 29.104 -0.14757 -0.010905 v Velocity[Z] -2.9237 3.073 2.5035e-06 -5.389e-08 v ǁVelocityǁ 0.0019098 39.379 8.0567 8.1128 v Pressure -2.3572e+05 1.9948e+05 -17110 -19410 v TurbVisc 9.5025e-20 0.018934 0.00018011 3.5144e-05 v CourantNb 6.2853e-08 0.011607 0.00016864 4.9446e-06 v FourierNb 1.2425e-07 0.044885 0.00014713 3.7292e-07 v total_pressure -1.3439e+05 3.0081e+05 84215 81915 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 1.9876 0.10376 0.0028771 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.3317e-07 0.05021 0.00031577 5.3176e-06 INSTANT 0.876056000E-01 TIME STEP NUMBER 56254 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282669339E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.792178770E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.56980E-02 0.20239E+01 Friction velocity uk : 0.56980E-02 0.20239E+01 Dimensionless distance yplus : 0.54825E-02 0.19873E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.310040190e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29424E+08 1 0.18078E-09 0.25457E+02 0.19423E+04 c Velocity[X] 0.13710E+02 c Velocity[Y] 0.11747E+02 c Velocity[Z] 0.96383E-06 c Pressure 0.21281E-03 10 0.59821E-04 0.18966E-02 0.21874E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.094 39.241 5.6047 7.9953 v Velocity[Y] -28.056 29.112 -0.14759 -0.010965 v Velocity[Z] -2.9234 3.0731 2.5029e-06 -5.389e-08 v ǁVelocityǁ 0.0019105 39.391 8.0582 8.113 v Pressure -2.3421e+05 2.0123e+05 -15306 -18532 v TurbVisc 9.814e-20 0.018952 0.00018016 3.52e-05 v CourantNb 6.2136e-08 0.011606 0.00016865 4.9447e-06 v FourierNb 1.2425e-07 0.044875 0.00014713 3.733e-07 v total_pressure -1.3288e+05 3.0256e+05 86019 82793 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 1.9873 0.10377 0.0028773 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.3327e-07 0.0502 0.00031578 5.318e-06 INSTANT 0.876057000E-01 TIME STEP NUMBER 56255 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282669789E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.792217145E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.61193E-02 0.20235E+01 Friction velocity uk : 0.61193E-02 0.20235E+01 Dimensionless distance yplus : 0.58879E-02 0.19869E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -6.736653563e-03 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29424E+08 1 0.18078E-09 0.25464E+02 0.19424E+04 c Velocity[X] 0.13715E+02 c Velocity[Y] 0.11748E+02 c Velocity[Z] 0.96487E-06 c Pressure 0.21316E-03 436 0.78483E-04 0.18989E-02 0.29252E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.101 39.253 5.6047 7.9953 v Velocity[Y] -28.064 29.12 -0.14761 -0.011027 v Velocity[Z] -2.9232 3.0733 2.5022e-06 -5.389e-08 v ǁVelocityǁ 0.0019296 39.404 8.0597 8.1132 v Pressure -2.3255e+05 2.0316e+05 -13493 -17462 v TurbVisc 1.0157e-19 0.01897 0.00018022 3.5256e-05 v CourantNb 6.1122e-08 0.011606 0.00016865 4.9448e-06 v FourierNb 1.2425e-07 0.044866 0.00014714 3.7368e-07 v total_pressure -1.3122e+05 3.0448e+05 87832 83863 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 1.9869 0.10379 0.0028775 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.3338e-07 0.05019 0.00031579 5.3184e-06 INSTANT 0.876058000E-01 TIME STEP NUMBER 56256 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282670382E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.792268401E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.50016E-02 0.20233E+01 Friction velocity uk : 0.50016E-02 0.20233E+01 Dimensionless distance yplus : 0.50063E-02 0.19867E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -2.113613908e-03 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29424E+08 1 0.18079E-09 0.25475E+02 0.19428E+04 c Velocity[X] 0.13723E+02 c Velocity[Y] 0.11752E+02 c Velocity[Z] 0.96384E-06 c Pressure 0.21284E-03 35 0.84612E-04 0.18952E-02 0.29516E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.108 39.266 5.6047 7.9953 v Velocity[Y] -28.072 29.128 -0.14763 -0.011086 v Velocity[Z] -2.9229 3.0735 2.5016e-06 -5.389e-08 v ǁVelocityǁ 0.0019539 39.417 8.0612 8.1133 v Pressure -2.3099e+05 2.0498e+05 -11638 -16368 v TurbVisc 7.5074e-20 0.018988 0.00018027 3.5312e-05 v CourantNb 6.051e-08 0.011605 0.00016865 4.9448e-06 v FourierNb 1.2425e-07 0.044856 0.00014715 3.7406e-07 v total_pressure -1.2967e+05 3.063e+05 89687 84957 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 1.9867 0.10381 0.0028777 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.3349e-07 0.050181 0.0003158 5.3189e-06 INSTANT 0.876059000E-01 TIME STEP NUMBER 56257 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282671049E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.792323882E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.75342E-02 0.20230E+01 Friction velocity uk : 0.75342E-02 0.20230E+01 Dimensionless distance yplus : 0.72492E-02 0.19864E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 3.275404225e-03 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29424E+08 1 0.18080E-09 0.25487E+02 0.19432E+04 c Velocity[X] 0.13731E+02 c Velocity[Y] 0.11756E+02 c Velocity[Z] 0.96748E-06 c Pressure 0.21263E-03 154 0.97789E-04 0.18925E-02 0.25418E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.114 39.278 5.6047 7.9953 v Velocity[Y] -28.081 29.137 -0.14765 -0.011149 v Velocity[Z] -2.9226 3.0736 2.5009e-06 -5.389e-08 v ǁVelocityǁ 0.0019853 39.429 8.0627 8.1135 v Pressure -2.2943e+05 2.0681e+05 -9852.3 -15511 v TurbVisc 8.2551e-20 0.019006 0.00018033 3.5368e-05 v CourantNb 6.0204e-08 0.011604 0.00016865 4.9449e-06 v FourierNb 1.2425e-07 0.044847 0.00014715 3.7445e-07 v total_pressure -1.281e+05 3.0813e+05 91473 85814 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 1.9864 0.10382 0.002878 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.336e-07 0.050172 0.0003158 5.3193e-06 INSTANT 0.876060000E-01 TIME STEP NUMBER 56258 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282672090E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.792388116E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.72748E-02 0.20227E+01 Friction velocity uk : 0.72748E-02 0.20227E+01 Dimensionless distance yplus : 0.69997E-02 0.19861E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 9.003320274e-03 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29424E+08 1 0.18081E-09 0.25487E+02 0.19431E+04 c Velocity[X] 0.13738E+02 c Velocity[Y] 0.11749E+02 c Velocity[Z] 0.96565E-06 c Pressure 0.21230E-03 131 0.83360E-04 0.18887E-02 0.28512E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.121 39.291 5.6047 7.9953 v Velocity[Y] -28.089 29.145 -0.14767 -0.011211 v Velocity[Z] -2.9224 3.0738 2.5003e-06 -5.389e-08 v ǁVelocityǁ 0.0020257 39.442 8.0642 8.1137 v Pressure -2.2787e+05 2.0862e+05 -8027.9 -14419 v TurbVisc 8.4279e-20 0.019024 0.00018038 3.5424e-05 v CourantNb 5.931e-08 0.011604 0.00016866 4.9449e-06 v FourierNb 1.2425e-07 0.044838 0.00014716 3.7483e-07 v total_pressure -1.2655e+05 3.0995e+05 93297 86906 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 1.9861 0.10384 0.0028782 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.3371e-07 0.050163 0.00031581 5.3198e-06 INSTANT 0.876061000E-01 TIME STEP NUMBER 56259 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282673158E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.792465449E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.65468E-02 0.20225E+01 Friction velocity uk : 0.65468E-02 0.20225E+01 Dimensionless distance yplus : 0.62992E-02 0.19859E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.430097283e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29424E+08 1 0.18082E-09 0.25504E+02 0.19437E+04 c Velocity[X] 0.13748E+02 c Velocity[Y] 0.11756E+02 c Velocity[Z] 0.97112E-06 c Pressure 0.20949E-03 10 0.60252E-04 0.18629E-02 0.22232E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.128 39.303 5.6047 7.9954 v Velocity[Y] -28.097 29.153 -0.14769 -0.011272 v Velocity[Z] -2.9221 3.0739 2.4996e-06 -5.389e-08 v ǁVelocityǁ 0.0020705 39.455 8.0657 8.1139 v Pressure -2.2641e+05 2.104e+05 -6249.2 -13554 v TurbVisc 8.4949e-20 0.019041 0.00018044 3.548e-05 v CourantNb 5.9856e-08 0.011603 0.00016866 4.945e-06 v FourierNb 1.2425e-07 0.044828 0.00014716 3.7522e-07 v total_pressure -1.2509e+05 3.1173e+05 95076 87771 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 1.9859 0.10385 0.0028785 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.3382e-07 0.050155 0.00031582 5.3202e-06 INSTANT 0.876062000E-01 TIME STEP NUMBER 56260 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282674443E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.792553397E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.50894E-02 0.20223E+01 Friction velocity uk : 0.50894E-02 0.20223E+01 Dimensionless distance yplus : 0.48969E-02 0.19857E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 2.084475301e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29424E+08 1 0.18083E-09 0.25514E+02 0.19440E+04 c Velocity[X] 0.13755E+02 c Velocity[Y] 0.11758E+02 c Velocity[Z] 0.97686E-06 c Pressure 0.20931E-03 538 0.79169E-04 0.18604E-02 0.29769E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.135 39.316 5.6048 7.9954 v Velocity[Y] -28.105 29.162 -0.14772 -0.011335 v Velocity[Z] -2.9219 3.0741 2.499e-06 -5.389e-08 v ǁVelocityǁ 0.0021331 39.468 8.0672 8.114 v Pressure -2.2479e+05 2.1239e+05 -4462.8 -12501 v TurbVisc 8.9201e-20 0.019059 0.00018049 3.5536e-05 v CourantNb 5.8484e-08 0.011602 0.00016866 4.9451e-06 v FourierNb 1.2425e-07 0.044819 0.00014717 3.756e-07 v total_pressure -1.2346e+05 3.1372e+05 96862 88824 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 1.9857 0.10387 0.0028788 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.3393e-07 0.050146 0.00031583 5.3207e-06 INSTANT 0.876063000E-01 TIME STEP NUMBER 56261 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282675866E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.792654638E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.54517E-02 0.20221E+01 Friction velocity uk : 0.54517E-02 0.20221E+01 Dimensionless distance yplus : 0.52455E-02 0.19855E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 2.556594001e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29424E+08 1 0.18084E-09 0.25528E+02 0.19444E+04 c Velocity[X] 0.13766E+02 c Velocity[Y] 0.11762E+02 c Velocity[Z] 0.97575E-06 c Pressure 0.20844E-03 35 0.85350E-04 0.18519E-02 0.29782E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.141 39.329 5.6048 7.9954 v Velocity[Y] -28.113 29.17 -0.14774 -0.011396 v Velocity[Z] -2.9216 3.0743 2.4983e-06 -5.389e-08 v ǁVelocityǁ 0.0022008 39.481 8.0688 8.1142 v Pressure -2.2325e+05 2.1423e+05 -2645.6 -11426 v TurbVisc 8.3261e-20 0.019077 0.00018055 3.5593e-05 v CourantNb 5.7972e-08 0.011602 0.00016867 4.9451e-06 v FourierNb 1.2425e-07 0.04481 0.00014717 3.7599e-07 v total_pressure -1.2193e+05 3.1556e+05 98679 89899 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 1.9855 0.10388 0.0028791 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.3404e-07 0.050137 0.00031584 5.3211e-06 INSTANT 0.876064000E-01 TIME STEP NUMBER 56262 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282677370E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.792760062E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.51936E-02 0.20219E+01 Friction velocity uk : 0.51936E-02 0.20219E+01 Dimensionless distance yplus : 0.49971E-02 0.19853E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 3.082756037e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29425E+08 1 0.18084E-09 0.25543E+02 0.19449E+04 c Velocity[X] 0.13775E+02 c Velocity[Y] 0.11768E+02 c Velocity[Z] 0.97537E-06 c Pressure 0.20768E-03 229 0.98629E-04 0.18443E-02 0.25593E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.148 39.341 5.6048 7.9954 v Velocity[Y] -28.121 29.179 -0.14776 -0.01146 v Velocity[Z] -2.9213 3.0744 2.4977e-06 -5.389e-08 v ǁVelocityǁ 0.0020274 39.494 8.0703 8.1144 v Pressure -2.2172e+05 2.161e+05 -894.76 -10595 v TurbVisc 8.3623e-20 0.019095 0.0001806 3.5649e-05 v CourantNb 5.7465e-08 0.011601 0.00016867 4.9452e-06 v FourierNb 1.2425e-07 0.044802 0.00014718 3.7637e-07 v total_pressure -1.204e+05 3.1743e+05 1.0043e+05 90730 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 1.9853 0.1039 0.0028793 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.3416e-07 0.050129 0.00031584 5.3216e-06 INSTANT 0.876065000E-01 TIME STEP NUMBER 56263 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282679237E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.792874786E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10932E-02 0.20217E+01 Friction velocity uk : 0.10932E-02 0.20217E+01 Dimensionless distance yplus : 0.10518E-02 0.19852E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 3.605955335e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29425E+08 1 0.18086E-09 0.25546E+02 0.19450E+04 c Velocity[X] 0.13785E+02 c Velocity[Y] 0.11761E+02 c Velocity[Z] 0.97764E-06 c Pressure 0.20683E-03 376 0.83931E-04 0.18359E-02 0.28029E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.155 39.354 5.6049 7.9955 v Velocity[Y] -28.129 29.188 -0.14779 -0.011523 v Velocity[Z] -2.9211 3.0746 2.497e-06 -5.389e-08 v ǁVelocityǁ 0.0020198 39.507 8.0718 8.1146 v Pressure -2.2023e+05 2.1797e+05 873.93 -9544.6 v TurbVisc 8.0432e-20 0.019113 0.00018066 3.5706e-05 v CourantNb 5.6563e-08 0.0116 0.00016867 4.9453e-06 v FourierNb 1.2425e-07 0.044793 0.00014718 3.7676e-07 v total_pressure -1.189e+05 3.193e+05 1.022e+05 91780 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 1.9852 0.10391 0.0028796 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.3427e-07 0.050121 0.00031585 5.322e-06 INSTANT 0.876066000E-01 TIME STEP NUMBER 56264 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282681121E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.793001898E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.69282E-02 0.20216E+01 Friction velocity uk : 0.69282E-02 0.20216E+01 Dimensionless distance yplus : 0.66661E-02 0.19850E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 4.120493554e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29425E+08 1 0.18086E-09 0.25566E+02 0.19456E+04 c Velocity[X] 0.13798E+02 c Velocity[Y] 0.11769E+02 c Velocity[Z] 0.98313E-06 c Pressure 0.20336E-03 10 0.60453E-04 0.18043E-02 0.22701E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.162 39.367 5.6049 7.9955 v Velocity[Y] -28.137 29.196 -0.14781 -0.011585 v Velocity[Z] -2.9208 3.0747 2.4964e-06 -5.389e-08 v ǁVelocityǁ 0.002268 39.52 8.0734 8.1148 v Pressure -2.1878e+05 2.1973e+05 2617.7 -8669.1 v TurbVisc 8.3182e-20 0.019131 0.00018072 3.5762e-05 v CourantNb 5.5648e-08 0.0116 0.00016868 4.9453e-06 v FourierNb 1.2425e-07 0.044784 0.00014718 3.7715e-07 v total_pressure -1.1746e+05 3.2106e+05 1.0394e+05 92656 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 1.985 0.10393 0.0028799 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.3438e-07 0.050112 0.00031586 5.3225e-06 INSTANT 0.876067000E-01 TIME STEP NUMBER 56265 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282683237E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.793140721E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10374E-01 0.20214E+01 Friction velocity uk : 0.10374E-01 0.20214E+01 Dimensionless distance yplus : 0.99812E-02 0.19849E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 4.686125565e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29425E+08 1 0.18087E-09 0.25579E+02 0.19460E+04 c Velocity[X] 0.13807E+02 c Velocity[Y] 0.11772E+02 c Velocity[Z] 0.98654E-06 c Pressure 0.20271E-03 468 0.79786E-04 0.17978E-02 0.29019E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.169 39.38 5.605 7.9956 v Velocity[Y] -28.145 29.205 -0.14784 -0.01165 v Velocity[Z] -2.9206 3.0749 2.4957e-06 -5.389e-08 v ǁVelocityǁ 0.0023861 39.533 8.0749 8.115 v Pressure -2.1721e+05 2.2168e+05 4341.8 -7669.1 v TurbVisc 8.4756e-20 0.019149 0.00018077 3.5819e-05 v CourantNb 5.409e-08 0.011599 0.00016868 4.9454e-06 v FourierNb 1.2425e-07 0.044775 0.00014719 3.7753e-07 v total_pressure -1.1588e+05 3.23e+05 1.0567e+05 93656 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 1.9849 0.10394 0.0028802 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.345e-07 0.050104 0.00031587 5.3229e-06 INSTANT 0.876068000E-01 TIME STEP NUMBER 56266 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282685474E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.793291620E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12784E-01 0.20213E+01 Friction velocity uk : 0.12784E-01 0.20213E+01 Dimensionless distance yplus : 0.12300E-01 0.19848E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 5.105775173e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29425E+08 1 0.18088E-09 0.25596E+02 0.19466E+04 c Velocity[X] 0.13820E+02 c Velocity[Y] 0.11777E+02 c Velocity[Z] 0.98810E-06 c Pressure 0.20131E-03 62 0.85860E-04 0.17845E-02 0.29129E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.175 39.393 5.605 7.9956 v Velocity[Y] -28.153 29.214 -0.14786 -0.011712 v Velocity[Z] -2.9203 3.075 2.4951e-06 -5.389e-08 v ǁVelocityǁ 0.0024343 39.546 8.0764 8.1152 v Pressure -2.1573e+05 2.2346e+05 6097.9 -6631.4 v TurbVisc 7.8647e-20 0.019167 0.00018083 3.5876e-05 v CourantNb 5.2017e-08 0.011598 0.00016868 4.9455e-06 v FourierNb 1.2425e-07 0.044767 0.00014719 3.7792e-07 v total_pressure -1.144e+05 3.2478e+05 1.0742e+05 94694 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 1.9848 0.10395 0.0028805 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.3461e-07 0.050096 0.00031588 5.3234e-06 INSTANT 0.876069000E-01 TIME STEP NUMBER 56267 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282687786E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.793447192E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.76225E-02 0.20212E+01 Friction velocity uk : 0.76225E-02 0.20212E+01 Dimensionless distance yplus : 0.73857E-02 0.19847E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 5.538595567e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29426E+08 1 0.18089E-09 0.25614E+02 0.19472E+04 c Velocity[X] 0.13831E+02 c Velocity[Y] 0.11783E+02 c Velocity[Z] 0.99242E-06 c Pressure 0.20005E-03 152 0.99244E-04 0.17726E-02 0.25018E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.182 39.406 5.6051 7.9956 v Velocity[Y] -28.161 29.223 -0.14789 -0.011778 v Velocity[Z] -2.92 3.0752 2.4944e-06 -5.389e-08 v ǁVelocityǁ 0.0024598 39.559 8.078 8.1154 v Pressure -2.1426e+05 2.2525e+05 7779.8 -5835.1 v TurbVisc 8.0412e-20 0.019185 0.00018089 3.5933e-05 v CourantNb 5.0041e-08 0.011598 0.00016869 4.9456e-06 v FourierNb 1.2425e-07 0.044758 0.0001472 3.7831e-07 v total_pressure -1.1293e+05 3.2658e+05 1.091e+05 95490 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 1.9847 0.10396 0.0028808 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.3473e-07 0.050088 0.00031589 5.3239e-06 INSTANT 0.876070000E-01 TIME STEP NUMBER 56268 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282690459E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.793611846E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.23601E-02 0.20211E+01 Friction velocity uk : 0.23601E-02 0.20211E+01 Dimensionless distance yplus : 0.22868E-02 0.19846E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 5.970556039e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29426E+08 1 0.18090E-09 0.25620E+02 0.19474E+04 c Velocity[X] 0.13843E+02 c Velocity[Y] 0.11777E+02 c Velocity[Z] 0.99352E-06 c Pressure 0.19871E-03 491 0.84477E-04 0.17598E-02 0.26953E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.189 39.419 5.6051 7.9957 v Velocity[Y] -28.17 29.232 -0.14792 -0.011842 v Velocity[Z] -2.9198 3.0754 2.4938e-06 -5.389e-08 v ǁVelocityǁ 0.0022059 39.572 8.0795 8.1156 v Pressure -2.1282e+05 2.2706e+05 9482.6 -4829.9 v TurbVisc 7.9772e-20 0.019203 0.00018095 3.599e-05 v CourantNb 4.781e-08 0.011597 0.00016869 4.9456e-06 v FourierNb 1.2425e-07 0.04475 0.0001472 3.787e-07 v total_pressure -1.115e+05 3.2839e+05 1.1081e+05 96495 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 1.9846 0.10397 0.0028811 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.3485e-07 0.050081 0.00031589 5.3243e-06 INSTANT 0.876071000E-01 TIME STEP NUMBER 56269 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282693135E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.793789183E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.45752E-02 0.20211E+01 Friction velocity uk : 0.45752E-02 0.20211E+01 Dimensionless distance yplus : 0.44331E-02 0.19845E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 6.346334720e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29426E+08 1 0.18091E-09 0.25643E+02 0.19481E+04 c Velocity[X] 0.13857E+02 c Velocity[Y] 0.11786E+02 c Velocity[Z] 0.10313E-05 c Pressure 0.19461E-03 15 0.60413E-04 0.17228E-02 0.21714E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.196 39.432 5.6052 7.9957 v Velocity[Y] -28.178 29.241 -0.14795 -0.011905 v Velocity[Z] -2.9195 3.0755 2.4931e-06 -5.389e-08 v ǁVelocityǁ 0.0022035 39.585 8.0811 8.1158 v Pressure -2.1144e+05 2.2876e+05 11148 -3994.6 v TurbVisc 7.8494e-20 0.019221 0.000181 3.6047e-05 v CourantNb 4.5434e-08 0.011596 0.00016869 4.9457e-06 v FourierNb 1.2425e-07 0.044742 0.00014721 3.7909e-07 v total_pressure -1.1012e+05 3.3009e+05 1.1247e+05 97330 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 1.9845 0.10398 0.0028814 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.3497e-07 0.050073 0.0003159 5.3248e-06 INSTANT 0.876072000E-01 TIME STEP NUMBER 56270 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282696038E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.793977233E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.99627E-02 0.20210E+01 Friction velocity uk : 0.99627E-02 0.20210E+01 Dimensionless distance yplus : 0.99432E-02 0.19844E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 6.790419732e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29426E+08 1 0.18092E-09 0.25659E+02 0.19487E+04 c Velocity[X] 0.13869E+02 c Velocity[Y] 0.11790E+02 c Velocity[Z] 0.10181E-05 c Pressure 0.19355E-03 140 0.80087E-04 0.17126E-02 0.27724E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.203 39.445 5.6053 7.9958 v Velocity[Y] -28.186 29.25 -0.14797 -0.011971 v Velocity[Z] -2.9196 3.0757 2.4925e-06 -5.389e-08 v ǁVelocityǁ 0.0024204 39.598 8.0826 8.1161 v Pressure -2.0992e+05 2.3069e+05 12789 -3037.4 v TurbVisc 5.8499e-20 0.019239 0.00018106 3.6104e-05 v CourantNb 4.3011e-08 0.011595 0.0001687 4.9458e-06 v FourierNb 1.2425e-07 0.044733 0.00014721 3.7948e-07 v total_pressure -1.086e+05 3.3202e+05 1.1411e+05 98288 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 1.9844 0.104 0.0028818 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.3509e-07 0.050065 0.00031591 5.3253e-06 INSTANT 0.876073000E-01 TIME STEP NUMBER 56271 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282699071E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.794177226E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10820E-01 0.20209E+01 Friction velocity uk : 0.10820E-01 0.20209E+01 Dimensionless distance yplus : 0.10413E-01 0.19844E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 7.084679690e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29427E+08 1 0.18093E-09 0.25679E+02 0.19493E+04 c Velocity[X] 0.13883E+02 c Velocity[Y] 0.11795E+02 c Velocity[Z] 0.10082E-05 c Pressure 0.19162E-03 32 0.86111E-04 0.16948E-02 0.27680E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.209 39.458 5.6053 7.9959 v Velocity[Y] -28.194 29.259 -0.148 -0.012035 v Velocity[Z] -2.92 3.0758 2.4918e-06 -5.3891e-08 v ǁVelocityǁ 0.0025336 39.612 8.0842 8.1163 v Pressure -2.0853e+05 2.3246e+05 14461 -2055.1 v TurbVisc 5.9616e-20 0.019257 0.00018112 3.6161e-05 v CourantNb 4.011e-08 0.011595 0.0001687 4.9459e-06 v FourierNb 1.2425e-07 0.044725 0.00014722 3.7987e-07 v total_pressure -1.072e+05 3.3379e+05 1.1579e+05 99270 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 1.9844 0.10401 0.0028822 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.352e-07 0.050058 0.00031592 5.3258e-06 INSTANT 0.876074000E-01 TIME STEP NUMBER 56272 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282702150E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.794382714E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11555E-01 0.20209E+01 Friction velocity uk : 0.11555E-01 0.20209E+01 Dimensionless distance yplus : 0.11120E-01 0.19843E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 7.367726252e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29427E+08 1 0.18094E-09 0.25699E+02 0.19500E+04 c Velocity[X] 0.13896E+02 c Velocity[Y] 0.11803E+02 c Velocity[Z] 0.10104E-05 c Pressure 0.18993E-03 152 0.99581E-04 0.16790E-02 0.23647E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.216 39.471 5.6054 7.9959 v Velocity[Y] -28.202 29.268 -0.14803 -0.012102 v Velocity[Z] -2.9205 3.076 2.4912e-06 -5.3891e-08 v ǁVelocityǁ 0.0028052 39.625 8.0857 8.1165 v Pressure -2.0713e+05 2.3422e+05 16050 -1308.6 v TurbVisc 6.8164e-20 0.019275 0.00018118 3.6218e-05 v CourantNb 3.7657e-08 0.011594 0.00016871 4.946e-06 v FourierNb 1.2425e-07 0.044717 0.00014722 3.8026e-07 v total_pressure -1.058e+05 3.3554e+05 1.1738e+05 1.0002e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 1.9843 0.10403 0.0028826 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.3533e-07 0.05005 0.00031593 5.3262e-06 INSTANT 0.876075000E-01 TIME STEP NUMBER 56273 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282705594E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.794596232E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.20184E-02 0.20209E+01 Friction velocity uk : 0.20184E-02 0.20209E+01 Dimensionless distance yplus : 0.19822E-02 0.19843E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 7.641077127e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29427E+08 1 0.18095E-09 0.25707E+02 0.19502E+04 c Velocity[X] 0.13910E+02 c Velocity[Y] 0.11797E+02 c Velocity[Z] 0.10116E-05 c Pressure 0.18816E-03 130 0.84526E-04 0.16626E-02 0.25724E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.223 39.484 5.6055 7.996 v Velocity[Y] -28.211 29.277 -0.14806 -0.012168 v Velocity[Z] -2.9209 3.0761 2.4906e-06 -5.3891e-08 v ǁVelocityǁ 0.0028771 39.638 8.0873 8.1167 v Pressure -2.0575e+05 2.3597e+05 17661 -339.99 v TurbVisc 7.2668e-20 0.019292 0.00018124 3.6276e-05 v CourantNb 3.4912e-08 0.011593 0.00016871 4.9461e-06 v FourierNb 1.2425e-07 0.044709 0.00014722 3.8065e-07 v total_pressure -1.0443e+05 3.373e+05 1.1899e+05 1.0099e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 1.9843 0.10405 0.002883 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.3545e-07 0.050043 0.00031593 5.3267e-06 INSTANT 0.876076000E-01 TIME STEP NUMBER 56274 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282709042E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.794822228E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.97959E-02 0.20208E+01 Friction velocity uk : 0.97959E-02 0.20208E+01 Dimensionless distance yplus : 0.94277E-02 0.19843E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 7.856501862e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29428E+08 1 0.18096E-09 0.25733E+02 0.19511E+04 c Velocity[X] 0.13926E+02 c Velocity[Y] 0.11807E+02 c Velocity[Z] 0.10321E-05 c Pressure 0.18346E-03 9 0.60259E-04 0.16204E-02 0.19135E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.23 39.497 5.6056 7.9961 v Velocity[Y] -28.219 29.287 -0.14809 -0.012233 v Velocity[Z] -2.9214 3.0763 2.4899e-06 -5.3891e-08 v ǁVelocityǁ 0.002958 39.652 8.0888 8.117 v Pressure -2.0448e+05 2.376e+05 19212 394.82 v TurbVisc 7.3967e-20 0.01931 0.0001813 3.6333e-05 v CourantNb 3.2074e-08 0.011593 0.00016871 4.9461e-06 v FourierNb 1.2425e-07 0.044701 0.00014723 3.8105e-07 v total_pressure -1.0316e+05 3.3893e+05 1.2054e+05 1.0172e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 1.9843 0.10407 0.0028835 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.3557e-07 0.050035 0.00031594 5.3272e-06 INSTANT 0.876077000E-01 TIME STEP NUMBER 56275 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282712671E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.795058331E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.41752E-02 0.20208E+01 Friction velocity uk : 0.41752E-02 0.20208E+01 Dimensionless distance yplus : 0.40391E-02 0.19843E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 8.106490897e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29428E+08 1 0.18097E-09 0.25751E+02 0.19517E+04 c Velocity[X] 0.13939E+02 c Velocity[Y] 0.11812E+02 c Velocity[Z] 0.10318E-05 c Pressure 0.18201E-03 159 0.80029E-04 0.16068E-02 0.26179E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.237 39.511 5.6056 7.9961 v Velocity[Y] -28.227 29.296 -0.14812 -0.0123 v Velocity[Z] -2.9218 3.0764 2.4893e-06 -5.3891e-08 v ǁVelocityǁ 0.0025114 39.665 8.0904 8.1172 v Pressure -2.0305e+05 2.3943e+05 20755 1315.4 v TurbVisc 7.8796e-20 0.019328 0.00018136 3.6391e-05 v CourantNb 2.9275e-08 0.011592 0.00016872 4.9462e-06 v FourierNb 1.2425e-07 0.044693 0.00014723 3.8144e-07 v total_pressure -1.0173e+05 3.4076e+05 1.2208e+05 1.0264e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 1.9843 0.10409 0.002884 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.3569e-07 0.050028 0.00031595 5.3277e-06 INSTANT 0.876078000E-01 TIME STEP NUMBER 56276 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282716458E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.795305511E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11588E-01 0.20208E+01 Friction velocity uk : 0.11588E-01 0.20208E+01 Dimensionless distance yplus : 0.11210E-01 0.19842E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 8.265331607e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29428E+08 1 0.18098E-09 0.25773E+02 0.19525E+04 c Velocity[X] 0.13955E+02 c Velocity[Y] 0.11818E+02 c Velocity[Z] 0.10278E-05 c Pressure 0.17964E-03 34 0.86111E-04 0.15851E-02 0.25572E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.244 39.524 5.6057 7.9962 v Velocity[Y] -28.236 29.305 -0.14815 -0.012365 v Velocity[Z] -2.9222 3.0766 2.4886e-06 -5.3891e-08 v ǁVelocityǁ 0.0021829 39.679 8.092 8.1174 v Pressure -2.0174e+05 2.4107e+05 22312 2224.1 v TurbVisc 7.5725e-20 0.019346 0.00018142 3.6448e-05 v CourantNb 2.6249e-08 0.011591 0.00016872 4.9463e-06 v FourierNb 1.2425e-07 0.044684 0.00014724 3.8183e-07 v total_pressure -1.0042e+05 3.4239e+05 1.2364e+05 1.0355e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 1.9842 0.10411 0.0028845 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.3581e-07 0.050021 0.00031596 5.3282e-06 INSTANT 0.876079000E-01 TIME STEP NUMBER 56277 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282720268E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.795559853E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.56600E-02 0.20208E+01 Friction velocity uk : 0.56600E-02 0.20208E+01 Dimensionless distance yplus : 0.54473E-02 0.19842E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 8.358246058e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29429E+08 1 0.18099E-09 0.25796E+02 0.19532E+04 c Velocity[X] 0.13970E+02 c Velocity[Y] 0.11826E+02 c Velocity[Z] 0.10336E-05 c Pressure 0.17756E-03 114 0.99504E-04 0.15661E-02 0.21988E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.251 39.537 5.6058 7.9963 v Velocity[Y] -28.244 29.315 -0.14818 -0.012434 v Velocity[Z] -2.9227 3.0768 2.488e-06 -5.3891e-08 v ǁVelocityǁ 0.0021535 39.692 8.0935 8.1177 v Pressure -2.0044e+05 2.4269e+05 23786 2911.1 v TurbVisc 7.6397e-20 0.019364 0.00018148 3.6506e-05 v CourantNb 2.6422e-08 0.011591 0.00016873 4.9464e-06 v FourierNb 1.2425e-07 0.044676 0.00014724 3.8223e-07 v total_pressure -99112 3.4401e+05 1.2511e+05 1.0424e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 1.9842 0.10413 0.0028851 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.3594e-07 0.050013 0.00031597 5.3286e-06 INSTANT 0.876080000E-01 TIME STEP NUMBER 56278 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282724436E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.795821096E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10327E-01 0.20208E+01 Friction velocity uk : 0.10327E-01 0.20208E+01 Dimensionless distance yplus : 0.99390E-02 0.19842E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 8.450108924e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29429E+08 1 0.18100E-09 0.25806E+02 0.19535E+04 c Velocity[X] 0.13985E+02 c Velocity[Y] 0.11821E+02 c Velocity[Z] 0.10368E-05 c Pressure 0.17542E-03 385 0.84533E-04 0.15465E-02 0.23133E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.258 39.551 5.6059 7.9964 v Velocity[Y] -28.252 29.324 -0.14821 -0.012501 v Velocity[Z] -2.9231 3.0769 2.4873e-06 -5.3891e-08 v ǁVelocityǁ 0.0024384 39.706 8.0951 8.1179 v Pressure -1.9918e+05 2.4429e+05 25271 3789.7 v TurbVisc 7.844e-20 0.019382 0.00018154 3.6564e-05 v CourantNb 2.5232e-08 0.01159 0.00016873 4.9465e-06 v FourierNb 1.2425e-07 0.044668 0.00014724 3.8262e-07 v total_pressure -97853 3.4561e+05 1.266e+05 1.0511e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 1.9842 0.10415 0.0028857 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.3606e-07 0.050006 0.00031597 5.3291e-06 INSTANT 0.876081000E-01 TIME STEP NUMBER 56279 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282728582E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.796094141E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15568E-01 0.20208E+01 Friction velocity uk : 0.15568E-01 0.20208E+01 Dimensionless distance yplus : 0.14983E-01 0.19842E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 8.497121252e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29430E+08 1 0.18101E-09 0.25834E+02 0.19545E+04 c Velocity[X] 0.14002E+02 c Velocity[Y] 0.11831E+02 c Velocity[Z] 0.10534E-05 c Pressure 0.17013E-03 9 0.59948E-04 0.14992E-02 0.17994E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.265 39.564 5.606 7.9965 v Velocity[Y] -28.261 29.334 -0.14824 -0.012567 v Velocity[Z] -2.9236 3.0771 2.4867e-06 -5.3891e-08 v ǁVelocityǁ 0.002876 39.72 8.0967 8.1182 v Pressure -1.9798e+05 2.4582e+05 26708 4498.3 v TurbVisc 7.9151e-20 0.0194 0.0001816 3.6622e-05 v CourantNb 2.5189e-08 0.011589 0.00016873 4.9466e-06 v FourierNb 1.2425e-07 0.04466 0.00014725 3.8302e-07 v total_pressure -96660 3.4715e+05 1.2803e+05 1.0582e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 1.9842 0.10416 0.0028863 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.3619e-07 0.049999 0.00031598 5.3296e-06 INSTANT 0.876082000E-01 TIME STEP NUMBER 56280 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282732921E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.796376867E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.80640E-02 0.20208E+01 Friction velocity uk : 0.80640E-02 0.20208E+01 Dimensionless distance yplus : 0.71197E-02 0.19842E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 8.533060082e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29430E+08 1 0.18102E-09 0.25853E+02 0.19551E+04 c Velocity[X] 0.14016E+02 c Velocity[Y] 0.11837E+02 c Velocity[Z] 0.10537E-05 c Pressure 0.16841E-03 463 0.80294E-04 0.14833E-02 0.23350E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.272 39.578 5.6061 7.9965 v Velocity[Y] -28.269 29.344 -0.14827 -0.012636 v Velocity[Z] -2.924 3.0772 2.486e-06 -5.3891e-08 v ǁVelocityǁ 0.0027399 39.733 8.0982 8.1184 v Pressure -1.9666e+05 2.4746e+05 28117 5313.1 v TurbVisc 8.1099e-20 0.019418 0.00018166 3.668e-05 v CourantNb 2.5128e-08 0.011588 0.00016874 4.9467e-06 v FourierNb 1.2425e-07 0.044652 0.00014725 3.8342e-07 v total_pressure -95338 3.4879e+05 1.2944e+05 1.0664e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 1.9842 0.10418 0.0028868 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.3631e-07 0.049991 0.00031599 5.3301e-06 INSTANT 0.876083000E-01 TIME STEP NUMBER 56281 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282737396E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.796669663E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.89785E-02 0.20208E+01 Friction velocity uk : 0.89785E-02 0.20208E+01 Dimensionless distance yplus : 0.89320E-02 0.19842E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 8.568621870e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29430E+08 1 0.18103E-09 0.25878E+02 0.19560E+04 c Velocity[X] 0.14034E+02 c Velocity[Y] 0.11844E+02 c Velocity[Z] 0.10491E-05 c Pressure 0.16569E-03 33 0.86483E-04 0.14586E-02 0.23393E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.278 39.591 5.6061 7.9966 v Velocity[Y] -28.278 29.354 -0.1483 -0.012702 v Velocity[Z] -2.9244 3.0774 2.4854e-06 -5.3891e-08 v ǁVelocityǁ 0.0024774 39.747 8.0998 8.1186 v Pressure -1.9549e+05 2.4896e+05 29534 6151.2 v TurbVisc 8.0737e-20 0.019435 0.00018172 3.6738e-05 v CourantNb 2.5219e-08 0.011588 0.00016874 4.9468e-06 v FourierNb 1.2425e-07 0.044644 0.00014726 3.8381e-07 v total_pressure -94165 3.5029e+05 1.3086e+05 1.0748e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 1.9842 0.1042 0.0028873 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.3644e-07 0.049984 0.000316 5.3306e-06 INSTANT 0.876084000E-01 TIME STEP NUMBER 56282 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282741889E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.796968803E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.52244E-02 0.20208E+01 Friction velocity uk : 0.52244E-02 0.20208E+01 Dimensionless distance yplus : 0.51973E-02 0.19842E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 8.481553684e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29431E+08 1 0.18104E-09 0.25892E+02 0.19564E+04 c Velocity[X] 0.14049E+02 c Velocity[Y] 0.11843E+02 c Velocity[Z] 0.10538E-05 c Pressure 0.16329E-03 1194 0.75109E-04 0.14368E-02 0.17259E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.285 39.605 5.6062 7.9967 v Velocity[Y] -28.286 29.363 -0.14833 -0.012771 v Velocity[Z] -2.9249 3.0775 2.4848e-06 -5.3891e-08 v ǁVelocityǁ 0.002212 39.761 8.1014 8.1189 v Pressure -1.9431e+05 2.5042e+05 30877 6788.4 v TurbVisc 7.7897e-20 0.019453 0.00018178 3.6796e-05 v CourantNb 2.5135e-08 0.011587 0.00016875 4.9469e-06 v FourierNb 1.2425e-07 0.044635 0.00014726 3.8421e-07 v total_pressure -92987 3.5174e+05 1.322e+05 1.0811e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 1.9842 0.10424 0.0028879 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.3657e-07 0.049976 0.00031601 5.3311e-06 INSTANT 0.876085000E-01 TIME STEP NUMBER 56283 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282746604E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.797275419E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.86514E-02 0.20208E+01 Friction velocity uk : 0.86514E-02 0.20208E+01 Dimensionless distance yplus : 0.83288E-02 0.19842E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 8.410218620e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29431E+08 1 0.18106E-09 0.25919E+02 0.19573E+04 c Velocity[X] 0.14065E+02 c Velocity[Y] 0.11854E+02 c Velocity[Z] 0.10645E-05 c Pressure 0.15811E-03 9 0.53585E-04 0.13906E-02 0.14289E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.292 39.619 5.6063 7.9968 v Velocity[Y] -28.295 29.373 -0.14836 -0.012841 v Velocity[Z] -2.9253 3.0777 2.4841e-06 -5.3891e-08 v ǁVelocityǁ 0.0020167 39.775 8.1029 8.1192 v Pressure -1.9323e+05 2.5177e+05 32183 7373.3 v TurbVisc 8.0008e-20 0.019471 0.00018184 3.6854e-05 v CourantNb 2.5082e-08 0.011586 0.00016875 4.947e-06 v FourierNb 1.2426e-07 0.044627 0.00014727 3.8461e-07 v total_pressure -91903 3.531e+05 1.3351e+05 1.087e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 1.9842 0.10427 0.0028884 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.367e-07 0.049969 0.00031602 5.3316e-06 INSTANT 0.876086000E-01 TIME STEP NUMBER 56284 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282751587E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.797592348E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.83376E-02 0.20208E+01 Friction velocity uk : 0.83376E-02 0.20208E+01 Dimensionless distance yplus : 0.80268E-02 0.19842E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 8.317282526e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29432E+08 1 0.18107E-09 0.25937E+02 0.19579E+04 c Velocity[X] 0.14083E+02 c Velocity[Y] 0.11854E+02 c Velocity[Z] 0.10687E-05 c Pressure 0.15591E-03 152 0.95820E-04 0.13706E-02 0.21926E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.299 39.633 5.6064 7.9969 v Velocity[Y] -28.303 29.383 -0.14839 -0.01291 v Velocity[Z] -2.9258 3.0778 2.4835e-06 -5.3891e-08 v ǁVelocityǁ 0.002137 39.789 8.1045 8.1194 v Pressure -1.9201e+05 2.5333e+05 33489 8257 v TurbVisc 8.4608e-20 0.019489 0.00018191 3.6912e-05 v CourantNb 2.4913e-08 0.011586 0.00016875 4.9471e-06 v FourierNb 1.2426e-07 0.044619 0.00014727 3.8501e-07 v total_pressure -90689 3.5466e+05 1.3481e+05 1.0958e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 1.9842 0.1043 0.0028889 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.3682e-07 0.049961 0.00031602 5.3321e-06 INSTANT 0.876087000E-01 TIME STEP NUMBER 56285 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282756543E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.797920798E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.94609E-02 0.20208E+01 Friction velocity uk : 0.94609E-02 0.20208E+01 Dimensionless distance yplus : 0.91001E-02 0.19842E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 8.210230642e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29432E+08 1 0.18108E-09 0.25959E+02 0.19586E+04 c Velocity[X] 0.14100E+02 c Velocity[Y] 0.11860E+02 c Velocity[Z] 0.10696E-05 c Pressure 0.15235E-03 65 0.80264E-04 0.13387E-02 0.16870E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.306 39.646 5.6065 7.997 v Velocity[Y] -28.312 29.393 -0.14842 -0.012979 v Velocity[Z] -2.9262 3.078 2.4828e-06 -5.3891e-08 v ǁVelocityǁ 0.0020937 39.803 8.1061 8.1197 v Pressure -1.9092e+05 2.5468e+05 34781 8961.9 v TurbVisc 6.0121e-20 0.019507 0.00018197 3.6971e-05 v CourantNb 2.5086e-08 0.011585 0.00016876 4.9472e-06 v FourierNb 1.2426e-07 0.04461 0.00014727 3.8541e-07 v total_pressure -89598 3.56e+05 1.3611e+05 1.1029e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 1.9842 0.10433 0.0028893 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.3695e-07 0.049954 0.00031603 5.3326e-06 INSTANT 0.876088000E-01 TIME STEP NUMBER 56286 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282761609E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.798255986E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.35869E-02 0.20208E+01 Friction velocity uk : 0.35869E-02 0.20208E+01 Dimensionless distance yplus : 0.34502E-02 0.19842E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 8.010929412e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29433E+08 1 0.18109E-09 0.25987E+02 0.19596E+04 c Velocity[X] 0.14117E+02 c Velocity[Y] 0.11871E+02 c Velocity[Z] 0.10801E-05 c Pressure 0.14844E-03 9 0.52489E-04 0.13037E-02 0.15145E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.314 39.66 5.6066 7.9971 v Velocity[Y] -28.321 29.403 -0.14845 -0.013047 v Velocity[Z] -2.9266 3.0781 2.4822e-06 -5.3891e-08 v ǁVelocityǁ 0.0022512 39.817 8.1077 8.1199 v Pressure -1.899e+05 2.5597e+05 36025 9572.4 v TurbVisc 5.1732e-20 0.019525 0.00018203 3.7029e-05 v CourantNb 2.5422e-08 0.011584 0.00016876 4.9473e-06 v FourierNb 1.2426e-07 0.044602 0.00014728 3.8581e-07 v total_pressure -88573 3.5729e+05 1.3735e+05 1.109e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 1.9842 0.10435 0.0028897 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.3708e-07 0.049946 0.00031604 5.3331e-06 INSTANT 0.876089000E-01 TIME STEP NUMBER 56287 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282766780E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.798596490E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11619E-01 0.20207E+01 Friction velocity uk : 0.11619E-01 0.20207E+01 Dimensionless distance yplus : 0.11176E-01 0.19842E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 7.993202360e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29433E+08 1 0.18110E-09 0.26006E+02 0.19602E+04 c Velocity[X] 0.14134E+02 c Velocity[Y] 0.11872E+02 c Velocity[Z] 0.10843E-05 c Pressure 0.14629E-03 138 0.97384E-04 0.12842E-02 0.16814E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.321 39.674 5.6067 7.9972 v Velocity[Y] -28.329 29.414 -0.14847 -0.013116 v Velocity[Z] -2.9271 3.0783 2.4815e-06 -5.3891e-08 v ǁVelocityǁ 0.0026535 39.831 8.1092 8.1202 v Pressure -1.8884e+05 2.5738e+05 37191 10254 v TurbVisc 7.1534e-20 0.019542 0.00018209 3.7088e-05 v CourantNb 2.8431e-08 0.011584 0.00016877 4.9474e-06 v FourierNb 1.2426e-07 0.044594 0.00014728 3.8621e-07 v total_pressure -87512 3.587e+05 1.3852e+05 1.1158e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 1.9842 0.10438 0.0028905 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.3721e-07 0.049938 0.00031605 5.3336e-06 INSTANT 0.876090000E-01 TIME STEP NUMBER 56288 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282772079E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.798946127E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.60492E-02 0.20207E+01 Friction velocity uk : 0.60492E-02 0.20207E+01 Dimensionless distance yplus : 0.59593E-02 0.19843E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 7.756708701e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29434E+08 1 0.18112E-09 0.26029E+02 0.19610E+04 c Velocity[X] 0.14150E+02 c Velocity[Y] 0.11879E+02 c Velocity[Z] 0.10854E-05 c Pressure 0.14254E-03 36 0.81903E-04 0.12507E-02 0.13562E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.328 39.688 5.6067 7.9973 v Velocity[Y] -28.338 29.424 -0.1485 -0.013186 v Velocity[Z] -2.9275 3.0785 2.4809e-06 -5.3891e-08 v ǁVelocityǁ 0.0025421 39.845 8.1108 8.1205 v Pressure -1.8785e+05 2.5858e+05 38359 10818 v TurbVisc 6.6583e-20 0.01956 0.00018216 3.7146e-05 v CourantNb 3.0781e-08 0.011583 0.00016877 4.9475e-06 v FourierNb 1.2426e-07 0.044585 0.00014729 3.8661e-07 v total_pressure -86520 3.599e+05 1.3968e+05 1.1214e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 1.9843 0.1044 0.0028911 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.3735e-07 0.049931 0.00031606 5.3341e-06 INSTANT 0.876091000E-01 TIME STEP NUMBER 56289 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282777495E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.799305343E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11093E-01 0.20207E+01 Friction velocity uk : 0.11093E-01 0.20207E+01 Dimensionless distance yplus : 0.10928E-01 0.19848E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 7.560000723e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29434E+08 1 0.18113E-09 0.26057E+02 0.19620E+04 c Velocity[X] 0.14166E+02 c Velocity[Y] 0.11891E+02 c Velocity[Z] 0.10932E-05 c Pressure 0.13837E-03 9 0.53011E-04 0.12135E-02 0.13132E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.335 39.702 5.6068 7.9974 v Velocity[Y] -28.347 29.434 -0.14853 -0.013258 v Velocity[Z] -2.928 3.0786 2.4803e-06 -5.3891e-08 v ǁVelocityǁ 0.0023926 39.86 8.1124 8.1207 v Pressure -1.8687e+05 2.5976e+05 39502 11349 v TurbVisc 7.135e-20 0.019578 0.00018222 3.7205e-05 v CourantNb 3.1679e-08 0.011582 0.00016877 4.9476e-06 v FourierNb 1.2426e-07 0.044576 0.00014729 3.8701e-07 v total_pressure -85543 3.6108e+05 1.4083e+05 1.1267e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 1.9848 0.10443 0.0028917 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.3748e-07 0.049923 0.00031607 5.3346e-06 INSTANT 0.876092000E-01 TIME STEP NUMBER 56290 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282783109E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.799671142E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.14695E-01 0.20207E+01 Friction velocity uk : 0.14695E-01 0.20207E+01 Dimensionless distance yplus : 0.14213E-01 0.19853E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 7.423177187e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29435E+08 1 0.18114E-09 0.26076E+02 0.19626E+04 c Velocity[X] 0.14185E+02 c Velocity[Y] 0.11891E+02 c Velocity[Z] 0.11053E-05 c Pressure 0.13626E-03 24 0.99714E-04 0.11944E-02 0.17829E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.342 39.717 5.6069 7.9975 v Velocity[Y] -28.355 29.445 -0.14856 -0.013329 v Velocity[Z] -2.9284 3.0788 2.4796e-06 -5.3891e-08 v ǁVelocityǁ 0.0021774 39.874 8.114 8.121 v Pressure -1.8589e+05 2.6109e+05 40596 12089 v TurbVisc 8.7449e-20 0.019596 0.00018229 3.7264e-05 v CourantNb 3.1846e-08 0.011581 0.00016878 4.9477e-06 v FourierNb 1.2426e-07 0.044568 0.0001473 3.8741e-07 v total_pressure -84567 3.6241e+05 1.4192e+05 1.1341e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 1.9853 0.10446 0.0028923 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.3761e-07 0.049915 0.00031607 5.3351e-06 INSTANT 0.876093000E-01 TIME STEP NUMBER 56291 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282788730E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.800044502E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11376E-01 0.20206E+01 Friction velocity uk : 0.11376E-01 0.20206E+01 Dimensionless distance yplus : 0.11010E-01 0.19857E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 7.162084414e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29435E+08 1 0.18115E-09 0.26099E+02 0.19633E+04 c Velocity[X] 0.14202E+02 c Velocity[Y] 0.11897E+02 c Velocity[Z] 0.11066E-05 c Pressure 0.13242E-03 65 0.84692E-04 0.11603E-02 0.13210E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.349 39.731 5.607 7.9977 v Velocity[Y] -28.364 29.455 -0.14859 -0.013399 v Velocity[Z] -2.9288 3.079 2.479e-06 -5.3892e-08 v ǁVelocityǁ 0.0019445 39.888 8.1155 8.1213 v Pressure -1.8499e+05 2.622e+05 41654 12657 v TurbVisc 9.527e-20 0.019614 0.00018235 3.7323e-05 v CourantNb 3.2445e-08 0.011581 0.00016878 4.9478e-06 v FourierNb 1.2426e-07 0.044559 0.0001473 3.8781e-07 v total_pressure -83667 3.6353e+05 1.4298e+05 1.1398e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 1.9857 0.10449 0.0028928 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.3775e-07 0.049907 0.00031608 5.3356e-06 INSTANT 0.876094000E-01 TIME STEP NUMBER 56292 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282794461E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.800425657E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.25219E-02 0.20206E+01 Friction velocity uk : 0.25219E-02 0.20206E+01 Dimensionless distance yplus : 0.24409E-02 0.19862E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 6.975902508e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29436E+08 1 0.18117E-09 0.26129E+02 0.19643E+04 c Velocity[X] 0.14220E+02 c Velocity[Y] 0.11909E+02 c Velocity[Z] 0.11080E-05 c Pressure 0.12809E-03 9 0.55756E-04 0.11218E-02 0.11871E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.356 39.745 5.6071 7.9978 v Velocity[Y] -28.373 29.466 -0.14861 -0.013469 v Velocity[Z] -2.9293 3.0792 2.4783e-06 -5.3892e-08 v ǁVelocityǁ 0.0019777 39.903 8.1171 8.1216 v Pressure -1.8417e+05 2.6327e+05 42685 13129 v TurbVisc 8.2309e-20 0.019631 0.00018241 3.7382e-05 v CourantNb 3.3637e-08 0.01158 0.00016879 4.9479e-06 v FourierNb 1.2426e-07 0.04455 0.0001473 3.8822e-07 v total_pressure -82847 3.646e+05 1.4401e+05 1.1445e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 1.9862 0.10451 0.0028933 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.3788e-07 0.049899 0.00031609 5.3361e-06 INSTANT 0.876095000E-01 TIME STEP NUMBER 56293 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282800255E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.800813156E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.74472E-02 0.20205E+01 Friction velocity uk : 0.74472E-02 0.20205E+01 Dimensionless distance yplus : 0.72081E-02 0.19867E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 6.877915902e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29436E+08 1 0.18118E-09 0.26152E+02 0.19651E+04 c Velocity[X] 0.14236E+02 c Velocity[Y] 0.11915E+02 c Velocity[Z] 0.11133E-05 c Pressure 0.12614E-03 152 0.77823E-04 0.11042E-02 0.15667E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.364 39.759 5.6072 7.9979 v Velocity[Y] -28.382 29.476 -0.14864 -0.013542 v Velocity[Z] -2.9297 3.0794 2.4777e-06 -5.3892e-08 v ǁVelocityǁ 0.0018486 39.917 8.1187 8.1218 v Pressure -1.8329e+05 2.6445e+05 43648 13667 v TurbVisc 9.1437e-20 0.019649 0.00018248 3.7441e-05 v CourantNb 3.2985e-08 0.011579 0.00016879 4.948e-06 v FourierNb 1.2426e-07 0.044542 0.00014731 3.8862e-07 v total_pressure -81961 3.6577e+05 1.4497e+05 1.1499e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 1.9867 0.10454 0.0028938 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.3801e-07 0.049891 0.0003161 5.3366e-06 INSTANT 0.876096000E-01 TIME STEP NUMBER 56294 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282806231E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.801208317E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.54712E-02 0.20210E+01 Friction velocity uk : 0.54712E-02 0.20210E+01 Dimensionless distance yplus : 0.54243E-02 0.19872E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 6.624434009e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29437E+08 1 0.18120E-09 0.26178E+02 0.19660E+04 c Velocity[X] 0.14254E+02 c Velocity[Y] 0.11924E+02 c Velocity[Z] 0.11150E-05 c Pressure 0.12293E-03 70 0.82783E-04 0.10755E-02 0.15572E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.371 39.774 5.6072 7.998 v Velocity[Y] -28.391 29.487 -0.14867 -0.013612 v Velocity[Z] -2.9301 3.0795 2.4771e-06 -5.3892e-08 v ǁVelocityǁ 0.0017208 39.932 8.1203 8.1221 v Pressure -1.8252e+05 2.6544e+05 44604 14182 v TurbVisc 8.5556e-20 0.019667 0.00018254 3.75e-05 v CourantNb 3.209e-08 0.011579 0.00016879 4.9481e-06 v FourierNb 1.2426e-07 0.044533 0.00014731 3.8903e-07 v total_pressure -81196 3.6676e+05 1.4593e+05 1.1551e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 1.9872 0.10457 0.0028944 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.3815e-07 0.049883 0.00031611 5.3371e-06 INSTANT 0.876097000E-01 TIME STEP NUMBER 56295 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282812127E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.801610273E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.97645E-02 0.20215E+01 Friction velocity uk : 0.97645E-02 0.20215E+01 Dimensionless distance yplus : 0.96808E-02 0.19877E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 6.431972486e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29438E+08 1 0.18121E-09 0.26204E+02 0.19669E+04 c Velocity[X] 0.14271E+02 c Velocity[Y] 0.11934E+02 c Velocity[Z] 0.11207E-05 c Pressure 0.12024E-03 295 0.96207E-04 0.10515E-02 0.15326E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.378 39.788 5.6073 7.9981 v Velocity[Y] -28.4 29.498 -0.14869 -0.013686 v Velocity[Z] -2.9306 3.0797 2.4764e-06 -5.3892e-08 v ǁVelocityǁ 0.0015988 39.946 8.1219 8.1224 v Pressure -1.8171e+05 2.6647e+05 45515 14637 v TurbVisc 9.0382e-20 0.019685 0.00018261 3.7559e-05 v CourantNb 3.1016e-08 0.011578 0.0001688 4.9482e-06 v FourierNb 1.2426e-07 0.044524 0.00014732 3.8943e-07 v total_pressure -80389 3.678e+05 1.4684e+05 1.1596e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 1.9877 0.1046 0.002895 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.3829e-07 0.049875 0.00031612 5.3377e-06 INSTANT 0.876098000E-01 TIME STEP NUMBER 56296 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282818379E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.802019025E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.20117E-01 0.20220E+01 Friction velocity uk : 0.20117E-01 0.20220E+01 Dimensionless distance yplus : 0.19801E-01 0.19882E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 6.242539259e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29438E+08 1 0.18122E-09 0.26219E+02 0.19673E+04 c Velocity[X] 0.14288E+02 c Velocity[Y] 0.11931E+02 c Velocity[Z] 0.11274E-05 c Pressure 0.11772E-03 89 0.81549E-04 0.10290E-02 0.12831E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.385 39.803 5.6074 7.9982 v Velocity[Y] -28.408 29.508 -0.14872 -0.013758 v Velocity[Z] -2.931 3.0799 2.4758e-06 -5.3892e-08 v ǁVelocityǁ 0.0014827 39.961 8.1234 8.1227 v Pressure -1.8103e+05 2.6742e+05 46376 15114 v TurbVisc 8.6414e-20 0.019702 0.00018268 3.7619e-05 v CourantNb 3.0034e-08 0.011577 0.0001688 4.9483e-06 v FourierNb 1.2426e-07 0.044515 0.00014732 3.8984e-07 v total_pressure -79701 3.6875e+05 1.477e+05 1.1644e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 1.9882 0.10463 0.0028955 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.3842e-07 0.049866 0.00031613 5.3382e-06 INSTANT 0.876099000E-01 TIME STEP NUMBER 56297 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282824547E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.802434365E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.20702E-01 0.20224E+01 Friction velocity uk : 0.20702E-01 0.20224E+01 Dimensionless distance yplus : 0.20072E-01 0.19886E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 6.088275206e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29439E+08 1 0.18124E-09 0.26249E+02 0.19683E+04 c Velocity[X] 0.14305E+02 c Velocity[Y] 0.11944E+02 c Velocity[Z] 0.11438E-05 c Pressure 0.11078E-03 18 0.57154E-04 0.96787E-03 0.89849E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.393 39.817 5.6075 7.9984 v Velocity[Y] -28.417 29.519 -0.14874 -0.013829 v Velocity[Z] -2.9315 3.0801 2.4752e-06 -5.3892e-08 v ǁVelocityǁ 0.0013804 39.976 8.125 8.123 v Pressure -1.804e+05 2.6829e+05 47182 15453 v TurbVisc 9.4772e-20 0.01972 0.00018274 3.7678e-05 v CourantNb 2.9091e-08 0.011577 0.00016881 4.9484e-06 v FourierNb 1.2426e-07 0.044506 0.00014733 3.9024e-07 v total_pressure -79078 3.6961e+05 1.4851e+05 1.1678e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 1.9886 0.10465 0.002896 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.3856e-07 0.049858 0.00031613 5.3387e-06 INSTANT 0.876100000E-01 TIME STEP NUMBER 56298 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282830792E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.802857340E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.21327E-01 0.20229E+01 Friction velocity uk : 0.21327E-01 0.20229E+01 Dimensionless distance yplus : 0.20678E-01 0.19891E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 5.945230712e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29439E+08 1 0.18125E-09 0.26272E+02 0.19691E+04 c Velocity[X] 0.14322E+02 c Velocity[Y] 0.11950E+02 c Velocity[Z] 0.11426E-05 c Pressure 0.10911E-03 154 0.77663E-04 0.95279E-03 0.14154E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.4 39.832 5.6076 7.9985 v Velocity[Y] -28.426 29.53 -0.14877 -0.013903 v Velocity[Z] -2.9319 3.0803 2.4745e-06 -5.3892e-08 v ǁVelocityǁ 0.0012752 39.99 8.1266 8.1233 v Pressure -1.7969e+05 2.6927e+05 47979 15922 v TurbVisc 1.2061e-19 0.019738 0.00018281 3.7737e-05 v CourantNb 2.8555e-08 0.011576 0.00016881 4.9485e-06 v FourierNb 1.2426e-07 0.044497 0.00014733 3.9065e-07 v total_pressure -78369 3.7059e+05 1.493e+05 1.1725e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 1.9891 0.10468 0.0028965 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.387e-07 0.04985 0.00031614 5.3392e-06 INSTANT 0.876101000E-01 TIME STEP NUMBER 56299 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282837198E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.803287755E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.22101E-01 0.20234E+01 Friction velocity uk : 0.22101E-01 0.20234E+01 Dimensionless distance yplus : 0.21473E-01 0.19895E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 5.833023427e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29440E+08 1 0.18127E-09 0.26298E+02 0.19700E+04 c Velocity[X] 0.14339E+02 c Velocity[Y] 0.11959E+02 c Velocity[Z] 0.11453E-05 c Pressure 0.10612E-03 56 0.83207E-04 0.92621E-03 0.13724E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.407 39.846 5.6076 7.9986 v Velocity[Y] -28.436 29.541 -0.14879 -0.013975 v Velocity[Z] -2.9323 3.0805 2.4739e-06 -5.3892e-08 v ǁVelocityǁ 0.0011867 40.005 8.1282 8.1235 v Pressure -1.7911e+05 2.7007e+05 48732 16334 v TurbVisc 6.5815e-20 0.019756 0.00018287 3.7797e-05 v CourantNb 2.7305e-08 0.011575 0.00016881 4.9487e-06 v FourierNb 1.2426e-07 0.044487 0.00014734 3.9106e-07 v total_pressure -77789 3.714e+05 1.5006e+05 1.1766e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 1.9895 0.1047 0.0028969 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.3884e-07 0.049841 0.00031615 5.3397e-06 INSTANT 0.876102000E-01 TIME STEP NUMBER 56300 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282843499E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.803721225E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.21412E-01 0.20238E+01 Friction velocity uk : 0.21412E-01 0.20238E+01 Dimensionless distance yplus : 0.20803E-01 0.19900E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 5.711592365e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29440E+08 1 0.18128E-09 0.26324E+02 0.19708E+04 c Velocity[X] 0.14355E+02 c Velocity[Y] 0.11969E+02 c Velocity[Z] 0.11498E-05 c Pressure 0.10378E-03 293 0.96560E-04 0.90537E-03 0.13549E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.415 39.861 5.6077 7.9987 v Velocity[Y] -28.445 29.552 -0.14882 -0.01405 v Velocity[Z] -2.9328 3.0807 2.4732e-06 -5.3892e-08 v ǁVelocityǁ 0.0011127 40.02 8.1298 8.1238 v Pressure -1.7853e+05 2.7089e+05 49434 16650 v TurbVisc 7.836e-20 0.019773 0.00018294 3.7857e-05 v CourantNb 2.6572e-08 0.011574 0.00016882 4.9488e-06 v FourierNb 1.2426e-07 0.044478 0.00014734 3.9147e-07 v total_pressure -77204 3.7222e+05 1.5076e+05 1.1798e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 1.99 0.10473 0.0028974 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.3898e-07 0.049833 0.00031616 5.3402e-06 INSTANT 0.876103000E-01 TIME STEP NUMBER 56301 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282850122E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.804160443E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.21533E-01 0.20243E+01 Friction velocity uk : 0.21533E-01 0.20243E+01 Dimensionless distance yplus : 0.20920E-01 0.19905E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 5.610814878e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29441E+08 1 0.18130E-09 0.26338E+02 0.19712E+04 c Velocity[X] 0.14372E+02 c Velocity[Y] 0.11966E+02 c Velocity[Z] 0.11528E-05 c Pressure 0.10169E-03 98 0.82151E-04 0.88668E-03 0.11267E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.422 39.876 5.6078 7.9989 v Velocity[Y] -28.454 29.563 -0.14884 -0.014123 v Velocity[Z] -2.9332 3.0809 2.4726e-06 -5.3892e-08 v ǁVelocityǁ 0.0010544 40.035 8.1313 8.1241 v Pressure -1.7805e+05 2.7167e+05 50100 17051 v TurbVisc 8.9527e-20 0.019791 0.00018301 3.7917e-05 v CourantNb 2.5774e-08 0.011574 0.00016882 4.9489e-06 v FourierNb 1.2426e-07 0.044469 0.00014735 3.9187e-07 v total_pressure -76724 3.7299e+05 1.5143e+05 1.1838e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 1.9905 0.10475 0.0028978 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.3912e-07 0.049824 0.00031617 5.3408e-06 INSTANT 0.876104000E-01 TIME STEP NUMBER 56302 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282856667E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.804605703E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.22393E-01 0.20248E+01 Friction velocity uk : 0.22393E-01 0.20248E+01 Dimensionless distance yplus : 0.21756E-01 0.19909E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 5.545202764e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29442E+08 1 0.18132E-09 0.26368E+02 0.19723E+04 c Velocity[X] 0.14389E+02 c Velocity[Y] 0.11979E+02 c Velocity[Z] 0.11716E-05 c Pressure 0.94473E-04 12 0.57676E-04 0.82338E-03 0.68742E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.43 39.891 5.6079 7.999 v Velocity[Y] -28.463 29.575 -0.14886 -0.014196 v Velocity[Z] -2.9336 3.0811 2.472e-06 -5.3892e-08 v ǁVelocityǁ 0.0010209 40.05 8.1329 8.1244 v Pressure -1.7766e+05 2.7231e+05 50691 17268 v TurbVisc 9.3724e-20 0.019809 0.00018308 3.7976e-05 v CourantNb 2.5013e-08 0.011573 0.00016882 4.949e-06 v FourierNb 1.2426e-07 0.04446 0.00014735 3.9228e-07 v total_pressure -76339 3.7364e+05 1.5202e+05 1.1859e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 1.9909 0.10477 0.0028982 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.3926e-07 0.049815 0.00031618 5.3413e-06 INSTANT 0.876105000E-01 TIME STEP NUMBER 56303 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282863249E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.805057468E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.23749E-01 0.20253E+01 Friction velocity uk : 0.23749E-01 0.20253E+01 Dimensionless distance yplus : 0.23074E-01 0.19914E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 5.517673219e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29442E+08 1 0.18133E-09 0.26391E+02 0.19730E+04 c Velocity[X] 0.14404E+02 c Velocity[Y] 0.11986E+02 c Velocity[Z] 0.11674E-05 c Pressure 0.93518E-04 153 0.78314E-04 0.81466E-03 0.11908E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.437 39.906 5.6079 7.9991 v Velocity[Y] -28.472 29.586 -0.14889 -0.014271 v Velocity[Z] -2.9341 3.0812 2.4713e-06 -5.3892e-08 v ǁVelocityǁ 0.00099768 40.065 8.1345 8.1247 v Pressure -1.7719e+05 2.7309e+05 51284 17597 v TurbVisc 1.0377e-19 0.019827 0.00018314 3.8036e-05 v CourantNb 2.4369e-08 0.011572 0.00016883 4.9491e-06 v FourierNb 1.2426e-07 0.04445 0.00014736 3.9269e-07 v total_pressure -75862 3.7442e+05 1.5261e+05 1.1892e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 1.9914 0.10479 0.0028985 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.394e-07 0.049807 0.00031619 5.3418e-06 INSTANT 0.876106000E-01 TIME STEP NUMBER 56304 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282869994E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.805516619E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.22882E-01 0.20257E+01 Friction velocity uk : 0.22882E-01 0.20257E+01 Dimensionless distance yplus : 0.22608E-01 0.19918E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 5.496545895e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29443E+08 1 0.18135E-09 0.26416E+02 0.19738E+04 c Velocity[X] 0.14421E+02 c Velocity[Y] 0.11995E+02 c Velocity[Z] 0.11688E-05 c Pressure 0.91133E-04 64 0.84020E-04 0.79349E-03 0.12002E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.445 39.921 5.608 7.9993 v Velocity[Y] -28.481 29.597 -0.14891 -0.014345 v Velocity[Z] -2.9345 3.0814 2.4707e-06 -5.3892e-08 v ǁVelocityǁ 0.00099791 40.08 8.1361 8.125 v Pressure -1.7685e+05 2.7368e+05 51815 17881 v TurbVisc 8.2275e-20 0.019844 0.00018321 3.8096e-05 v CourantNb 2.3633e-08 0.011572 0.00016883 4.9492e-06 v FourierNb 1.2426e-07 0.044441 0.00014736 3.9311e-07 v total_pressure -75525 3.7501e+05 1.5314e+05 1.1921e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 1.9918 0.10481 0.0028989 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.3954e-07 0.049798 0.00031619 5.3423e-06 INSTANT 0.876107000E-01 TIME STEP NUMBER 56305 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282876602E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.805977758E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.16426E-01 0.20261E+01 Friction velocity uk : 0.16426E-01 0.20261E+01 Dimensionless distance yplus : 0.16229E-01 0.19923E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 5.502663946e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29444E+08 1 0.18136E-09 0.26442E+02 0.19747E+04 c Velocity[X] 0.14436E+02 c Velocity[Y] 0.12006E+02 c Velocity[Z] 0.11748E-05 c Pressure 0.89552E-04 235 0.97549E-04 0.77934E-03 0.12610E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.452 39.936 5.6081 7.9994 v Velocity[Y] -28.491 29.608 -0.14893 -0.014421 v Velocity[Z] -2.935 3.0816 2.4701e-06 -5.3892e-08 v ǁVelocityǁ 0.0010172 40.096 8.1377 8.1253 v Pressure -1.7647e+05 2.7431e+05 52311 18094 v TurbVisc 9.1232e-20 0.019862 0.00018328 3.8156e-05 v CourantNb 2.2997e-08 0.011571 0.00016884 4.9493e-06 v FourierNb 1.2426e-07 0.044431 0.00014737 3.9352e-07 v total_pressure -75147 3.7564e+05 1.5364e+05 1.1942e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 1.9923 0.10483 0.0028993 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.3968e-07 0.049789 0.0003162 5.3428e-06 INSTANT 0.876108000E-01 TIME STEP NUMBER 56306 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282883515E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.806444026E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.84371E-02 0.20266E+01 Friction velocity uk : 0.84371E-02 0.20266E+01 Dimensionless distance yplus : 0.83361E-02 0.19927E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 5.527633071e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29444E+08 1 0.18138E-09 0.26455E+02 0.19751E+04 c Velocity[X] 0.14452E+02 c Velocity[Y] 0.12003E+02 c Velocity[Z] 0.11804E-05 c Pressure 0.88368E-04 368 0.83075E-04 0.76866E-03 0.87327E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.46 39.951 5.6082 7.9995 v Velocity[Y] -28.5 29.62 -0.14895 -0.014496 v Velocity[Z] -2.9354 3.0818 2.4694e-06 -5.3892e-08 v ǁVelocityǁ 0.0010574 40.111 8.1393 8.1256 v Pressure -1.7624e+05 2.7482e+05 52746 18331 v TurbVisc 9.6091e-20 0.01988 0.00018335 3.8217e-05 v CourantNb 2.2322e-08 0.01157 0.00016884 4.9494e-06 v FourierNb 1.2426e-07 0.044422 0.00014737 3.9393e-07 v total_pressure -74910 3.7615e+05 1.5407e+05 1.1966e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 1.9927 0.10485 0.0028996 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.3983e-07 0.049781 0.00031621 5.3434e-06 INSTANT 0.876109000E-01 TIME STEP NUMBER 56307 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282890318E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.806914269E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.67915E-02 0.20270E+01 Friction velocity uk : 0.67915E-02 0.20270E+01 Dimensionless distance yplus : 0.67103E-02 0.19932E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 5.582322967e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29445E+08 1 0.18140E-09 0.26484E+02 0.19760E+04 c Velocity[X] 0.14469E+02 c Velocity[Y] 0.12015E+02 c Velocity[Z] 0.11960E-05 c Pressure 0.81164E-04 7 0.57911E-04 0.70564E-03 0.57741E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.468 39.966 5.6082 7.9997 v Velocity[Y] -28.509 29.631 -0.14898 -0.01457 v Velocity[Z] -2.9358 3.082 2.4688e-06 -5.3892e-08 v ǁVelocityǁ 0.0011051 40.126 8.1409 8.1259 v Pressure -1.7604e+05 2.7531e+05 53117 18468 v TurbVisc 9.9876e-20 0.019897 0.00018342 3.8277e-05 v CourantNb 2.1657e-08 0.01157 0.00016884 4.9496e-06 v FourierNb 1.2426e-07 0.044412 0.00014738 3.9434e-07 v total_pressure -74714 3.7664e+05 1.5444e+05 1.1979e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 1.9932 0.10487 0.0029 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.3997e-07 0.049772 0.00031622 5.3439e-06 INSTANT 0.876110000E-01 TIME STEP NUMBER 56308 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282897142E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.807390531E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.99255E-02 0.20275E+01 Friction velocity uk : 0.99255E-02 0.20275E+01 Dimensionless distance yplus : 0.98068E-02 0.19936E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 5.686204401e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29445E+08 1 0.18142E-09 0.26506E+02 0.19767E+04 c Velocity[X] 0.14482E+02 c Velocity[Y] 0.12023E+02 c Velocity[Z] 0.11980E-05 c Pressure 0.81517E-04 667 0.79361E-04 0.70837E-03 0.10919E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.476 39.981 5.6083 7.9998 v Velocity[Y] -28.519 29.643 -0.149 -0.014648 v Velocity[Z] -2.9363 3.0822 2.4682e-06 -5.3892e-08 v ǁVelocityǁ 0.0011916 40.141 8.1425 8.1262 v Pressure -1.7577e+05 2.7586e+05 53522 18675 v TurbVisc 9.8361e-20 0.019915 0.00018349 3.8337e-05 v CourantNb 2.1056e-08 0.011569 0.00016885 4.9497e-06 v FourierNb 1.2426e-07 0.044403 0.00014738 3.9475e-07 v total_pressure -74450 3.7718e+05 1.5485e+05 1.2e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 1.9936 0.10489 0.0029003 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.4012e-07 0.049763 0.00031623 5.3444e-06 INSTANT 0.876111000E-01 TIME STEP NUMBER 56309 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282904129E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.807873451E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.17313E-01 0.20279E+01 Friction velocity uk : 0.17313E-01 0.20279E+01 Dimensionless distance yplus : 0.17106E-01 0.19940E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 5.749259880e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29446E+08 1 0.18144E-09 0.26530E+02 0.19776E+04 c Velocity[X] 0.14499E+02 c Velocity[Y] 0.12031E+02 c Velocity[Z] 0.12002E-05 c Pressure 0.80256E-04 72 0.85153E-04 0.69706E-03 0.11040E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.483 39.996 5.6084 7.9999 v Velocity[Y] -28.528 29.654 -0.14902 -0.014722 v Velocity[Z] -2.9367 3.0824 2.4675e-06 -5.3892e-08 v ǁVelocityǁ 0.0012802 40.157 8.1441 8.1265 v Pressure -1.7566e+05 2.7625e+05 53813 18832 v TurbVisc 1.0706e-19 0.019933 0.00018356 3.8398e-05 v CourantNb 2.0088e-08 0.011568 0.00016885 4.9498e-06 v FourierNb 1.2426e-07 0.044393 0.00014739 3.9517e-07 v total_pressure -74339 3.7758e+05 1.5514e+05 1.2016e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 1.994 0.10491 0.0029008 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.4026e-07 0.049754 0.00031624 5.3449e-06 INSTANT 0.876112000E-01 TIME STEP NUMBER 56310 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282910963E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.808354872E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.21803E-01 0.20284E+01 Friction velocity uk : 0.21803E-01 0.20284E+01 Dimensionless distance yplus : 0.21556E-01 0.19945E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 5.884827092e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29447E+08 1 0.18145E-09 0.26555E+02 0.19784E+04 c Velocity[X] 0.14512E+02 c Velocity[Y] 0.12043E+02 c Velocity[Z] 0.12036E-05 c Pressure 0.79977E-04 122 0.98439E-04 0.69430E-03 0.11960E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.491 40.011 5.6085 8.0001 v Velocity[Y] -28.538 29.666 -0.14904 -0.0148 v Velocity[Z] -2.9371 3.0826 2.4669e-06 -5.3892e-08 v ǁVelocityǁ 0.0013807 40.172 8.1457 8.1268 v Pressure -1.7552e+05 2.7663e+05 54077 18889 v TurbVisc 1.0876e-19 0.019951 0.00018363 3.8458e-05 v CourantNb 1.9803e-08 0.011567 0.00016885 4.9499e-06 v FourierNb 1.2426e-07 0.044384 0.00014739 3.9558e-07 v total_pressure -74195 3.7796e+05 1.554e+05 1.2021e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 1.9945 0.10494 0.0029011 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.4041e-07 0.049745 0.00031625 5.3455e-06 INSTANT 0.876113000E-01 TIME STEP NUMBER 56311 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282918070E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.808841630E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.18366E-01 0.20289E+01 Friction velocity uk : 0.18366E-01 0.20289E+01 Dimensionless distance yplus : 0.18158E-01 0.19949E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 6.023087752e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29447E+08 1 0.18148E-09 0.26566E+02 0.19787E+04 c Velocity[X] 0.14527E+02 c Velocity[Y] 0.12039E+02 c Velocity[Z] 0.12098E-05 c Pressure 0.80148E-04 133 0.83693E-04 0.69543E-03 0.78961E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.499 40.027 5.6085 8.0002 v Velocity[Y] -28.547 29.677 -0.14907 -0.014876 v Velocity[Z] -2.9376 3.0828 2.4663e-06 -5.3893e-08 v ǁVelocityǁ 0.0014894 40.188 8.1473 8.1271 v Pressure -1.7548e+05 2.7699e+05 54307 19049 v TurbVisc 1.0614e-19 0.019968 0.0001837 3.8519e-05 v CourantNb 1.908e-08 0.011567 0.00016886 4.95e-06 v FourierNb 1.2426e-07 0.044374 0.0001474 3.96e-07 v total_pressure -74158 3.7831e+05 1.5563e+05 1.2037e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 1.9949 0.10496 0.0029015 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.4055e-07 0.049736 0.00031626 5.346e-06 INSTANT 0.876114000E-01 TIME STEP NUMBER 56312 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282925048E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.809331370E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13959E-01 0.20293E+01 Friction velocity uk : 0.13959E-01 0.20293E+01 Dimensionless distance yplus : 0.13801E-01 0.19954E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 6.181221892e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29448E+08 1 0.18149E-09 0.26594E+02 0.19796E+04 c Velocity[X] 0.14542E+02 c Velocity[Y] 0.12053E+02 c Velocity[Z] 0.12232E-05 c Pressure 0.73664E-04 15 0.58635E-04 0.63886E-03 0.47207E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.507 40.042 5.6086 8.0003 v Velocity[Y] -28.557 29.689 -0.14909 -0.014952 v Velocity[Z] -2.938 3.0829 2.4656e-06 -5.3893e-08 v ǁVelocityǁ 0.0015921 40.203 8.1489 8.1274 v Pressure -1.7552e+05 2.7722e+05 54413 19030 v TurbVisc 1.0866e-19 0.019986 0.00018377 3.858e-05 v CourantNb 1.8321e-08 0.011566 0.00016886 4.9501e-06 v FourierNb 1.2426e-07 0.044365 0.0001474 3.9641e-07 v total_pressure -74194 3.7855e+05 1.5574e+05 1.2036e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 1.9954 0.10498 0.0029019 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.407e-07 0.049727 0.00031627 5.3465e-06 INSTANT 0.876115000E-01 TIME STEP NUMBER 56313 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282931993E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.809824467E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.68079E-02 0.20298E+01 Friction velocity uk : 0.68079E-02 0.20298E+01 Dimensionless distance yplus : 0.67308E-02 0.19958E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 6.452976904e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29449E+08 1 0.18151E-09 0.26615E+02 0.19803E+04 c Velocity[X] 0.14555E+02 c Velocity[Y] 0.12060E+02 c Velocity[Z] 0.12263E-05 c Pressure 0.75742E-04 66 0.79585E-04 0.65655E-03 0.93650E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.515 40.057 5.6087 8.0005 v Velocity[Y] -28.566 29.701 -0.14911 -0.015031 v Velocity[Z] -2.9384 3.0831 2.465e-06 -5.3893e-08 v ǁVelocityǁ 0.0017276 40.219 8.1505 8.1277 v Pressure -1.7552e+05 2.7753e+05 54637 19077 v TurbVisc 1.208e-19 0.020004 0.00018384 3.864e-05 v CourantNb 1.6113e-08 0.011565 0.00016887 4.9502e-06 v FourierNb 1.2426e-07 0.044355 0.00014741 3.9683e-07 v total_pressure -74192 3.7885e+05 1.5596e+05 1.204e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 1.9958 0.10499 0.0029022 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.4085e-07 0.049719 0.00031627 5.3471e-06 INSTANT 0.876116000E-01 TIME STEP NUMBER 56314 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282939136E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.810325845E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.39034E-02 0.20302E+01 Friction velocity uk : 0.39034E-02 0.20302E+01 Dimensionless distance yplus : 0.38591E-02 0.19963E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 6.475321714e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29449E+08 1 0.18153E-09 0.26638E+02 0.19810E+04 c Velocity[X] 0.14570E+02 c Velocity[Y] 0.12069E+02 c Velocity[Z] 0.12288E-05 c Pressure 0.76026E-04 56 0.85242E-04 0.65868E-03 0.10273E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.523 40.073 5.6088 8.0006 v Velocity[Y] -28.576 29.713 -0.14914 -0.015107 v Velocity[Z] -2.9389 3.0833 2.4644e-06 -5.3893e-08 v ǁVelocityǁ 0.0018567 40.234 8.1521 8.128 v Pressure -1.7562e+05 2.7771e+05 54683 19118 v TurbVisc 7.7768e-20 0.020021 0.00018391 3.8701e-05 v CourantNb 1.6398e-08 0.011565 0.00016887 4.9504e-06 v FourierNb 1.2426e-07 0.044345 0.00014741 3.9724e-07 v total_pressure -74290 3.7903e+05 1.5601e+05 1.2044e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 1.9963 0.10502 0.0029026 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.4086e-07 0.04971 0.00031628 5.3476e-06 INSTANT 0.876117000E-01 TIME STEP NUMBER 56315 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282946070E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.810820093E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10509E-01 0.20307E+01 Friction velocity uk : 0.10509E-01 0.20307E+01 Dimensionless distance yplus : 0.10390E-01 0.19968E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 6.740851127e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29450E+08 1 0.18155E-09 0.26661E+02 0.19818E+04 c Velocity[X] 0.14582E+02 c Velocity[Y] 0.12079E+02 c Velocity[Z] 0.12318E-05 c Pressure 0.77377E-04 39 0.98841E-04 0.67005E-03 0.11784E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.531 40.088 5.6089 8.0008 v Velocity[Y] -28.586 29.724 -0.14916 -0.015186 v Velocity[Z] -2.9393 3.0835 2.4637e-06 -5.3893e-08 v ǁVelocityǁ 0.0019894 40.25 8.1537 8.1283 v Pressure -1.757e+05 2.7789e+05 54722 19069 v TurbVisc 9.2273e-20 0.020039 0.00018398 3.8762e-05 v CourantNb 1.6086e-08 0.011564 0.00016887 4.9505e-06 v FourierNb 1.2426e-07 0.044336 0.00014742 3.9766e-07 v total_pressure -74375 3.7921e+05 1.5605e+05 1.2039e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 1.9968 0.10504 0.0029029 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.4085e-07 0.049701 0.00031629 5.3481e-06 INSTANT 0.876118000E-01 TIME STEP NUMBER 56316 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282953273E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.811320510E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.36820E-02 0.20312E+01 Friction velocity uk : 0.36820E-02 0.20312E+01 Dimensionless distance yplus : 0.35772E-02 0.19972E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 6.966626676e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29451E+08 1 0.18158E-09 0.26671E+02 0.19820E+04 c Velocity[X] 0.14595E+02 c Velocity[Y] 0.12076E+02 c Velocity[Z] 0.12376E-05 c Pressure 0.79179E-04 79 0.83756E-04 0.68532E-03 0.69797E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.539 40.104 5.609 8.0009 v Velocity[Y] -28.596 29.736 -0.14918 -0.015264 v Velocity[Z] -2.9397 3.0837 2.4631e-06 -5.3893e-08 v ǁVelocityǁ 0.0021269 40.266 8.1553 8.1286 v Pressure -1.7589e+05 2.7799e+05 54713 19062 v TurbVisc 9.9582e-20 0.020056 0.00018405 3.8823e-05 v CourantNb 1.5079e-08 0.011563 0.00016888 4.9506e-06 v FourierNb 1.2426e-07 0.044326 0.00014742 3.9808e-07 v total_pressure -74567 3.7932e+05 1.5604e+05 1.2039e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 1.9972 0.10506 0.0029033 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.4084e-07 0.049692 0.0003163 5.3487e-06 INSTANT 0.876119000E-01 TIME STEP NUMBER 56317 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282960316E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.811822107E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11033E-01 0.20317E+01 Friction velocity uk : 0.11033E-01 0.20317E+01 Dimensionless distance yplus : 0.10719E-01 0.19977E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 7.184449832e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29451E+08 1 0.18160E-09 0.26697E+02 0.19829E+04 c Velocity[X] 0.14609E+02 c Velocity[Y] 0.12089E+02 c Velocity[Z] 0.12468E-05 c Pressure 0.74266E-04 6 0.58522E-04 0.64247E-03 0.46978E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.547 40.119 5.609 8.001 v Velocity[Y] -28.605 29.748 -0.14921 -0.015342 v Velocity[Z] -2.9402 3.0839 2.4625e-06 -5.3893e-08 v ǁVelocityǁ 0.0022705 40.281 8.1569 8.129 v Pressure -1.7609e+05 2.7807e+05 54680 19021 v TurbVisc 1.0407e-19 0.020074 0.00018412 3.8884e-05 v CourantNb 1.4167e-08 0.011562 0.00016888 4.9507e-06 v FourierNb 1.2426e-07 0.044317 0.00014743 3.985e-07 v total_pressure -74764 3.794e+05 1.5601e+05 1.2035e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 1.9977 0.10508 0.0029037 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.4084e-07 0.049683 0.00031631 5.3492e-06 INSTANT 0.876120000E-01 TIME STEP NUMBER 56318 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282967332E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.812325621E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12069E-01 0.20321E+01 Friction velocity uk : 0.12069E-01 0.20321E+01 Dimensionless distance yplus : 0.11886E-01 0.19982E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 7.345761647e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29452E+08 1 0.18162E-09 0.26717E+02 0.19835E+04 c Velocity[X] 0.14620E+02 c Velocity[Y] 0.12097E+02 c Velocity[Z] 0.12499E-05 c Pressure 0.78007E-04 51 0.79366E-04 0.67450E-03 0.10158E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.555 40.135 5.6091 8.0012 v Velocity[Y] -28.615 29.76 -0.14923 -0.015422 v Velocity[Z] -2.9406 3.0841 2.4618e-06 -5.3893e-08 v ǁVelocityǁ 0.0024124 40.297 8.1585 8.1293 v Pressure -1.7641e+05 2.7807e+05 54523 18799 v TurbVisc 9.9538e-20 0.020092 0.00018419 3.8945e-05 v CourantNb 1.3698e-08 0.011562 0.00016889 4.9508e-06 v FourierNb 1.2426e-07 0.044307 0.00014744 3.9891e-07 v total_pressure -75086 3.7939e+05 1.5585e+05 1.2012e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 1.9982 0.1051 0.0029041 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.4083e-07 0.049675 0.00031632 5.3497e-06 INSTANT 0.876121000E-01 TIME STEP NUMBER 56319 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282974478E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.812827832E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.59338E-02 0.20326E+01 Friction velocity uk : 0.59338E-02 0.20326E+01 Dimensionless distance yplus : 0.58438E-02 0.19987E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 7.715262996e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29453E+08 1 0.18164E-09 0.26739E+02 0.19842E+04 c Velocity[X] 0.14633E+02 c Velocity[Y] 0.12105E+02 c Velocity[Z] 0.12548E-05 c Pressure 0.79858E-04 65 0.85129E-04 0.69015E-03 0.10100E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.563 40.15 5.6092 8.0013 v Velocity[Y] -28.625 29.772 -0.14926 -0.0155 v Velocity[Z] -2.941 3.0843 2.4612e-06 -5.3893e-08 v ǁVelocityǁ 0.0025599 40.313 8.1601 8.1296 v Pressure -1.7671e+05 2.7804e+05 54398 18735 v TurbVisc 1.1205e-19 0.020109 0.00018426 3.9007e-05 v CourantNb 1.2692e-08 0.011561 0.00016889 4.9509e-06 v FourierNb 1.2426e-07 0.044298 0.00014744 3.9933e-07 v total_pressure -75389 3.7937e+05 1.5572e+05 1.2006e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 1.9987 0.10512 0.0029044 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.4082e-07 0.049666 0.00031633 5.3503e-06 INSTANT 0.876122000E-01 TIME STEP NUMBER 56320 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282981420E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.813336246E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.56153E-02 0.20331E+01 Friction velocity uk : 0.56153E-02 0.20331E+01 Dimensionless distance yplus : 0.55301E-02 0.19992E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 7.876989119e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29453E+08 1 0.18166E-09 0.26760E+02 0.19849E+04 c Velocity[X] 0.14644E+02 c Velocity[Y] 0.12116E+02 c Velocity[Z] 0.12596E-05 c Pressure 0.82698E-04 101 0.98592E-04 0.71433E-03 0.12431E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.572 40.166 5.6093 8.0015 v Velocity[Y] -28.635 29.784 -0.14928 -0.015581 v Velocity[Z] -2.9415 3.0844 2.4606e-06 -5.3893e-08 v ǁVelocityǁ 0.0024613 40.329 8.1618 8.1299 v Pressure -1.7702e+05 2.7798e+05 54205 18541 v TurbVisc 1.1078e-19 0.020127 0.00018434 3.9068e-05 v CourantNb 1.1959e-08 0.01156 0.00016889 4.9511e-06 v FourierNb 1.2426e-07 0.044288 0.00014745 3.9975e-07 v total_pressure -75692 3.7931e+05 1.5553e+05 1.1987e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 1.9992 0.10515 0.0029048 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.4087e-07 0.049657 0.00031634 5.3508e-06 INSTANT 0.876123000E-01 TIME STEP NUMBER 56321 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282988592E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.813843320E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.50091E-02 0.20336E+01 Friction velocity uk : 0.50091E-02 0.20336E+01 Dimensionless distance yplus : 0.48224E-02 0.19997E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 8.112982731e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29454E+08 1 0.18169E-09 0.26768E+02 0.19851E+04 c Velocity[X] 0.14656E+02 c Velocity[Y] 0.12112E+02 c Velocity[Z] 0.12639E-05 c Pressure 0.85861E-04 95 0.83604E-04 0.74129E-03 0.72742E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.58 40.182 5.6094 8.0016 v Velocity[Y] -28.645 29.796 -0.14931 -0.01566 v Velocity[Z] -2.9419 3.0846 2.4599e-06 -5.3893e-08 v ǁVelocityǁ 0.0025579 40.344 8.1634 8.1302 v Pressure -1.7741e+05 2.779e+05 53983 18461 v TurbVisc 1.1632e-19 0.020145 0.00018441 3.913e-05 v CourantNb 1.1203e-08 0.01156 0.0001689 4.9512e-06 v FourierNb 1.2426e-07 0.044279 0.00014745 4.0017e-07 v total_pressure -76089 3.7923e+05 1.5531e+05 1.1979e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 1.9997 0.10517 0.0029052 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.4103e-07 0.049649 0.00031635 5.3514e-06 INSTANT 0.876124000E-01 TIME STEP NUMBER 56322 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282995624E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.814349971E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.71560E-02 0.20342E+01 Friction velocity uk : 0.71560E-02 0.20342E+01 Dimensionless distance yplus : 0.69172E-02 0.20002E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 8.335225163e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29455E+08 1 0.18171E-09 0.26793E+02 0.19859E+04 c Velocity[X] 0.14668E+02 c Velocity[Y] 0.12124E+02 c Velocity[Z] 0.12730E-05 c Pressure 0.82855E-04 7 0.58538E-04 0.71497E-03 0.52764E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.588 40.197 5.6095 8.0017 v Velocity[Y] -28.655 29.808 -0.14933 -0.015739 v Velocity[Z] -2.9423 3.0848 2.4593e-06 -5.3893e-08 v ǁVelocityǁ 0.0026422 40.36 8.165 8.1305 v Pressure -1.7783e+05 2.7777e+05 53742 18326 v TurbVisc 1.0937e-19 0.020162 0.00018448 3.9191e-05 v CourantNb 1.0518e-08 0.011559 0.0001689 4.9513e-06 v FourierNb 1.2426e-07 0.044269 0.00014746 4.0059e-07 v total_pressure -76510 3.7909e+05 1.5507e+05 1.1965e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0002 0.10519 0.0029056 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.4119e-07 0.04964 0.00031636 5.3519e-06 INSTANT 0.876125000E-01 TIME STEP NUMBER 56323 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283002587E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.814855967E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.52767E-02 0.20347E+01 Friction velocity uk : 0.52767E-02 0.20347E+01 Dimensionless distance yplus : 0.51006E-02 0.20007E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 8.548257759e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29455E+08 1 0.18173E-09 0.26811E+02 0.19864E+04 c Velocity[X] 0.14677E+02 c Velocity[Y] 0.12133E+02 c Velocity[Z] 0.12787E-05 c Pressure 0.87593E-04 44 0.79614E-04 0.75548E-03 0.13343E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.597 40.213 5.6096 8.0019 v Velocity[Y] -28.665 29.82 -0.14936 -0.015821 v Velocity[Z] -2.9428 3.085 2.4587e-06 -5.3893e-08 v ǁVelocityǁ 0.0024918 40.376 8.1666 8.1308 v Pressure -1.7839e+05 2.7746e+05 53301 17855 v TurbVisc 1.0948e-19 0.02018 0.00018455 3.9252e-05 v CourantNb 1.0524e-08 0.011558 0.00016891 4.9514e-06 v FourierNb 1.2426e-07 0.04426 0.00014746 4.0101e-07 v total_pressure -77065 3.7879e+05 1.5463e+05 1.1918e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0007 0.10522 0.002906 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.4135e-07 0.049631 0.00031637 5.3524e-06 INSTANT 0.876126000E-01 TIME STEP NUMBER 56324 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283009653E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.815357884E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.14050E-01 0.20352E+01 Friction velocity uk : 0.14050E-01 0.20352E+01 Dimensionless distance yplus : 0.13581E-01 0.20012E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 8.804960755e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29456E+08 1 0.18176E-09 0.26831E+02 0.19871E+04 c Velocity[X] 0.14690E+02 c Velocity[Y] 0.12141E+02 c Velocity[Z] 0.12812E-05 c Pressure 0.90699E-04 79 0.85106E-04 0.78186E-03 0.10495E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.605 40.229 5.6097 8.002 v Velocity[Y] -28.675 29.832 -0.14939 -0.0159 v Velocity[Z] -2.9432 3.0852 2.4581e-06 -5.3893e-08 v ǁVelocityǁ 0.0025641 40.392 8.1683 8.1311 v Pressure -1.7891e+05 2.7724e+05 52977 17725 v TurbVisc 1.1588e-19 0.020197 0.00018463 3.9314e-05 v CourantNb 8.9355e-09 0.011557 0.00016891 4.9515e-06 v FourierNb 1.2426e-07 0.044251 0.00014747 4.0144e-07 v total_pressure -77587 3.7857e+05 1.543e+05 1.1905e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0012 0.10525 0.0029065 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.4151e-07 0.049623 0.00031638 5.353e-06 INSTANT 0.876127000E-01 TIME STEP NUMBER 56325 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283016505E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.815867786E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19338E-01 0.20357E+01 Friction velocity uk : 0.19338E-01 0.20357E+01 Dimensionless distance yplus : 0.18693E-01 0.20017E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 8.998153219e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29457E+08 1 0.18178E-09 0.26851E+02 0.19877E+04 c Velocity[X] 0.14699E+02 c Velocity[Y] 0.12152E+02 c Velocity[Z] 0.12821E-05 c Pressure 0.94492E-04 103 0.99110E-04 0.81415E-03 0.13832E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.614 40.245 5.6098 8.0022 v Velocity[Y] -28.685 29.844 -0.14941 -0.015983 v Velocity[Z] -2.9436 3.0854 2.4574e-06 -5.3893e-08 v ǁVelocityǁ 0.0027335 40.408 8.1699 8.1314 v Pressure -1.7944e+05 2.7695e+05 52549 17382 v TurbVisc 1.1513e-19 0.020215 0.0001847 3.9376e-05 v CourantNb 8.2594e-09 0.011557 0.00016892 4.9516e-06 v FourierNb 1.2426e-07 0.044241 0.00014747 4.0186e-07 v total_pressure -78111 3.7827e+05 1.5387e+05 1.1871e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0017 0.10527 0.002907 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.4167e-07 0.049615 0.00031639 5.3535e-06 INSTANT 0.876128000E-01 TIME STEP NUMBER 56326 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283023561E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.816373812E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.14426E-01 0.20363E+01 Friction velocity uk : 0.14426E-01 0.20363E+01 Dimensionless distance yplus : 0.14163E-01 0.20023E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 9.203897335e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29457E+08 1 0.18181E-09 0.26857E+02 0.19878E+04 c Velocity[X] 0.14709E+02 c Velocity[Y] 0.12148E+02 c Velocity[Z] 0.12867E-05 c Pressure 0.98507E-04 678 0.84247E-04 0.84831E-03 0.84959E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.622 40.26 5.6099 8.0023 v Velocity[Y] -28.695 29.856 -0.14944 -0.016064 v Velocity[Z] -2.9441 3.0856 2.4568e-06 -5.3893e-08 v ǁVelocityǁ 0.0027155 40.424 8.1715 8.1317 v Pressure -1.8008e+05 2.766e+05 52087 17136 v TurbVisc 1.1826e-19 0.020233 0.00018477 3.9438e-05 v CourantNb 7.4777e-09 0.011556 0.00016892 4.9518e-06 v FourierNb 1.2426e-07 0.044232 0.00014748 4.0228e-07 v total_pressure -78753 3.7793e+05 1.5341e+05 1.1846e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0023 0.10529 0.0029074 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.4183e-07 0.049606 0.0003164 5.354e-06 INSTANT 0.876129000E-01 TIME STEP NUMBER 56327 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283030445E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.816877714E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.28155E-02 0.20368E+01 Friction velocity uk : 0.28155E-02 0.20368E+01 Dimensionless distance yplus : 0.27642E-02 0.20028E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 9.389886798e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29458E+08 1 0.18183E-09 0.26880E+02 0.19885E+04 c Velocity[X] 0.14721E+02 c Velocity[Y] 0.12159E+02 c Velocity[Z] 0.12983E-05 c Pressure 0.97063E-04 7 0.59270E-04 0.83545E-03 0.58021E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.631 40.276 5.61 8.0024 v Velocity[Y] -28.705 29.868 -0.14947 -0.016144 v Velocity[Z] -2.9445 3.0857 2.4562e-06 -5.3893e-08 v ǁVelocityǁ 0.0027007 40.44 8.1732 8.132 v Pressure -1.8066e+05 2.7631e+05 51639 16960 v TurbVisc 1.153e-19 0.02025 0.00018485 3.95e-05 v CourantNb 6.7595e-09 0.011555 0.00016892 4.9519e-06 v FourierNb 1.2426e-07 0.044223 0.00014748 4.0271e-07 v total_pressure -79336 3.7763e+05 1.5296e+05 1.1829e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0028 0.10531 0.0029079 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.4199e-07 0.049598 0.0003164 5.3546e-06 INSTANT 0.876130000E-01 TIME STEP NUMBER 56328 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283037266E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.817380470E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.79052E-02 0.20374E+01 Friction velocity uk : 0.79052E-02 0.20374E+01 Dimensionless distance yplus : 0.77612E-02 0.20033E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 9.562181496e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29459E+08 1 0.18185E-09 0.26896E+02 0.19890E+04 c Velocity[X] 0.14727E+02 c Velocity[Y] 0.12169E+02 c Velocity[Z] 0.13064E-05 c Pressure 0.10225E-03 60 0.80382E-04 0.87966E-03 0.16130E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.639 40.292 5.6101 8.0026 v Velocity[Y] -28.715 29.88 -0.1495 -0.016227 v Velocity[Z] -2.9449 3.0859 2.4555e-06 -5.3893e-08 v ǁVelocityǁ 0.0026976 40.456 8.1748 8.1323 v Pressure -1.8144e+05 2.7574e+05 50979 16323 v TurbVisc 1.1517e-19 0.020268 0.00018492 3.9561e-05 v CourantNb 6.3087e-09 0.011554 0.00016893 4.952e-06 v FourierNb 1.2426e-07 0.044213 0.00014749 4.0313e-07 v total_pressure -80110 3.7706e+05 1.523e+05 1.1765e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0033 0.10534 0.0029084 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.4216e-07 0.049589 0.00031641 5.3551e-06 INSTANT 0.876131000E-01 TIME STEP NUMBER 56329 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283044158E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.817876899E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19188E-01 0.20380E+01 Friction velocity uk : 0.19188E-01 0.20380E+01 Dimensionless distance yplus : 0.18466E-01 0.20039E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 9.745713748e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29459E+08 1 0.18188E-09 0.26914E+02 0.19896E+04 c Velocity[X] 0.14739E+02 c Velocity[Y] 0.12175E+02 c Velocity[Z] 0.13021E-05 c Pressure 0.10601E-03 339 0.86224E-04 0.91153E-03 0.11374E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.648 40.308 5.6102 8.0027 v Velocity[Y] -28.725 29.893 -0.14953 -0.016308 v Velocity[Z] -2.9454 3.0861 2.4549e-06 -5.3893e-08 v ǁVelocityǁ 0.0026415 40.472 8.1764 8.1326 v Pressure -1.8216e+05 2.7531e+05 50426 16088 v TurbVisc 1.1714e-19 0.020285 0.00018499 3.9624e-05 v CourantNb 6.7808e-09 0.011554 0.00016893 4.9521e-06 v FourierNb 1.2426e-07 0.044204 0.00014749 4.0355e-07 v total_pressure -80834 3.7663e+05 1.5175e+05 1.1741e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0039 0.10537 0.0029088 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.4232e-07 0.049582 0.00031642 5.3557e-06 INSTANT 0.876132000E-01 TIME STEP NUMBER 56330 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283050827E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.818379191E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.16281E-01 0.20385E+01 Friction velocity uk : 0.16281E-01 0.20385E+01 Dimensionless distance yplus : 0.15669E-01 0.20045E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 9.890670471e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29460E+08 1 0.18191E-09 0.26922E+02 0.19898E+04 c Velocity[X] 0.14745E+02 c Velocity[Y] 0.12177E+02 c Velocity[Z] 0.13017E-05 c Pressure 0.11028E-03 56 0.75111E-04 0.94777E-03 0.12080E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.656 40.323 5.6103 8.0028 v Velocity[Y] -28.736 29.905 -0.14956 -0.016391 v Velocity[Z] -2.9458 3.0863 2.4543e-06 -5.3893e-08 v ǁVelocityǁ 0.0027073 40.488 8.1781 8.1329 v Pressure -1.8296e+05 2.7473e+05 49759 15579 v TurbVisc 1.1848e-19 0.020303 0.00018507 3.9686e-05 v CourantNb 5.251e-09 0.011553 0.00016894 4.9522e-06 v FourierNb 1.2426e-07 0.044195 0.0001475 4.0398e-07 v total_pressure -81634 3.7606e+05 1.5108e+05 1.169e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0045 0.10539 0.0029092 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.4248e-07 0.049573 0.00031643 5.3562e-06 INSTANT 0.876133000E-01 TIME STEP NUMBER 56331 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283057567E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.818877061E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12728E-01 0.20391E+01 Friction velocity uk : 0.12728E-01 0.20391E+01 Dimensionless distance yplus : 0.12249E-01 0.20050E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.003666870e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29460E+08 1 0.18193E-09 0.26942E+02 0.19904E+04 c Velocity[X] 0.14754E+02 c Velocity[Y] 0.12188E+02 c Velocity[Z] 0.13274E-05 c Pressure 0.11061E-03 15 0.54166E-04 0.95010E-03 0.77492E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.665 40.339 5.6104 8.003 v Velocity[Y] -28.746 29.917 -0.14959 -0.016475 v Velocity[Z] -2.9462 3.0865 2.4537e-06 -5.3894e-08 v ǁVelocityǁ 0.0027226 40.503 8.1797 8.1332 v Pressure -1.837e+05 2.7424e+05 49099 15251 v TurbVisc 1.1965e-19 0.02032 0.00018514 3.9748e-05 v CourantNb 3.8408e-09 0.011552 0.00016894 4.9524e-06 v FourierNb 1.2426e-07 0.044186 0.0001475 4.044e-07 v total_pressure -82376 3.7556e+05 1.5042e+05 1.1658e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.005 0.10541 0.0029096 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.4265e-07 0.049565 0.00031644 5.3568e-06 INSTANT 0.876134000E-01 TIME STEP NUMBER 56332 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283064296E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.819372414E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.81905E-02 0.20397E+01 Friction velocity uk : 0.81905E-02 0.20397E+01 Dimensionless distance yplus : 0.78825E-02 0.20056E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.016796194e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29461E+08 1 0.18196E-09 0.26953E+02 0.19907E+04 c Velocity[X] 0.14763E+02 c Velocity[Y] 0.12190E+02 c Velocity[Z] 0.13210E-05 c Pressure 0.11562E-03 44 0.97078E-04 0.99264E-03 0.10189E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.674 40.355 5.6106 8.0031 v Velocity[Y] -28.756 29.929 -0.14963 -0.016559 v Velocity[Z] -2.9467 3.0867 2.453e-06 -5.3894e-08 v ǁVelocityǁ 0.0027465 40.519 8.1814 8.1335 v Pressure -1.8456e+05 2.7356e+05 48374 14770 v TurbVisc 8.9832e-20 0.020338 0.00018521 3.981e-05 v CourantNb 2.2899e-09 0.011551 0.00016895 4.9525e-06 v FourierNb 1.2426e-07 0.044177 0.00014751 4.0483e-07 v total_pressure -83237 3.7489e+05 1.497e+05 1.1609e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0056 0.10543 0.00291 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.4281e-07 0.049557 0.00031645 5.3573e-06 INSTANT 0.876135000E-01 TIME STEP NUMBER 56333 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283070900E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.819862989E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.92040E-02 0.20403E+01 Friction velocity uk : 0.92040E-02 0.20403E+01 Dimensionless distance yplus : 0.89002E-02 0.20062E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.025808810e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29462E+08 1 0.18199E-09 0.26967E+02 0.19911E+04 c Velocity[X] 0.14771E+02 c Velocity[Y] 0.12196E+02 c Velocity[Z] 0.13125E-05 c Pressure 0.11865E-03 47 0.81146E-04 0.10181E-02 0.10008E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.682 40.371 5.6107 8.0032 v Velocity[Y] -28.766 29.942 -0.14966 -0.016642 v Velocity[Z] -2.9471 3.0869 2.4524e-06 -5.3894e-08 v ǁVelocityǁ 0.0027773 40.535 8.183 8.1338 v Pressure -1.8549e+05 2.7289e+05 47582 14281 v TurbVisc 1.3035e-19 0.020355 0.00018529 3.9873e-05 v CourantNb 8.8268e-10 0.011551 0.00016895 4.9526e-06 v FourierNb 1.2426e-07 0.044168 0.00014751 4.0526e-07 v total_pressure -84166 3.7422e+05 1.4891e+05 1.1561e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0062 0.10545 0.0029103 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.4298e-07 0.049549 0.00031646 5.3578e-06 INSTANT 0.876136000E-01 TIME STEP NUMBER 56334 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283077444E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.820350637E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.40592E-02 0.20409E+01 Friction velocity uk : 0.40592E-02 0.20409E+01 Dimensionless distance yplus : 0.39741E-02 0.20068E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.034536485e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29462E+08 1 0.18201E-09 0.26986E+02 0.19917E+04 c Velocity[X] 0.14780E+02 c Velocity[Y] 0.12206E+02 c Velocity[Z] 0.13254E-05 c Pressure 0.12139E-03 16 0.53865E-04 0.10411E-02 0.92353E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.691 40.386 5.6108 8.0034 v Velocity[Y] -28.777 29.954 -0.14969 -0.016725 v Velocity[Z] -2.9475 3.0871 2.4518e-06 -5.3894e-08 v ǁVelocityǁ 0.0028137 40.551 8.1847 8.1341 v Pressure -1.8642e+05 2.7223e+05 46765 13860 v TurbVisc 1.3021e-19 0.020373 0.00018536 3.9935e-05 v CourantNb 2.336e-09 0.01155 0.00016896 4.9527e-06 v FourierNb 1.2426e-07 0.044159 0.00014752 4.0568e-07 v total_pressure -85096 3.7356e+05 1.4809e+05 1.1518e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0068 0.10547 0.0029107 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.4314e-07 0.049541 0.00031647 5.3584e-06 INSTANT 0.876137000E-01 TIME STEP NUMBER 56335 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283083895E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.820837123E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.63331E-02 0.20415E+01 Friction velocity uk : 0.63331E-02 0.20415E+01 Dimensionless distance yplus : 0.60949E-02 0.20074E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.037968285e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29463E+08 1 0.18204E-09 0.26996E+02 0.19920E+04 c Velocity[X] 0.14786E+02 c Velocity[Y] 0.12210E+02 c Velocity[Z] 0.13331E-05 c Pressure 0.12652E-03 108 0.98807E-04 0.10846E-02 0.15002E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.7 40.402 5.6109 8.0035 v Velocity[Y] -28.787 29.966 -0.14972 -0.016809 v Velocity[Z] -2.948 3.0872 2.4511e-06 -5.3894e-08 v ǁVelocityǁ 0.0025399 40.567 8.1863 8.1344 v Pressure -1.8745e+05 2.7137e+05 45894 13140 v TurbVisc 8.7526e-20 0.02039 0.00018544 3.9997e-05 v CourantNb 1.192e-09 0.011549 0.00016896 4.9528e-06 v FourierNb 1.2426e-07 0.044149 0.00014752 4.0611e-07 v total_pressure -86124 3.7269e+05 1.4722e+05 1.1446e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0074 0.10549 0.0029113 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.4331e-07 0.049533 0.00031648 5.3589e-06 INSTANT 0.876138000E-01 TIME STEP NUMBER 56336 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283090274E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.821320464E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.45971E-02 0.20421E+01 Friction velocity uk : 0.45971E-02 0.20421E+01 Dimensionless distance yplus : 0.44242E-02 0.20080E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.044382492e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29463E+08 1 0.18207E-09 0.27009E+02 0.19923E+04 c Velocity[X] 0.14793E+02 c Velocity[Y] 0.12216E+02 c Velocity[Z] 0.13249E-05 c Pressure 0.12971E-03 347 0.83618E-04 0.11114E-02 0.10643E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.709 40.418 5.611 8.0036 v Velocity[Y] -28.797 29.979 -0.14976 -0.016894 v Velocity[Z] -2.9484 3.0874 2.4505e-06 -5.3894e-08 v ǁVelocityǁ 0.0024369 40.583 8.188 8.1347 v Pressure -1.8842e+05 2.7063e+05 44994 12623 v TurbVisc 1.2029e-19 0.020408 0.00018551 4.006e-05 v CourantNb 1.5931e-09 0.011548 0.00016897 4.9529e-06 v FourierNb 1.2426e-07 0.04414 0.00014753 4.0654e-07 v total_pressure -87091 3.7195e+05 1.4632e+05 1.1395e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.008 0.10552 0.0029118 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.4347e-07 0.049525 0.00031649 5.3595e-06 INSTANT 0.876139000E-01 TIME STEP NUMBER 56337 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283096638E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.821800541E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.90758E-02 0.20427E+01 Friction velocity uk : 0.90758E-02 0.20427E+01 Dimensionless distance yplus : 0.87344E-02 0.20086E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.044273293e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29464E+08 1 0.18210E-09 0.27028E+02 0.19929E+04 c Velocity[X] 0.14799E+02 c Velocity[Y] 0.12228E+02 c Velocity[Z] 0.13305E-05 c Pressure 0.13251E-03 9 0.54601E-04 0.11347E-02 0.11301E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.717 40.434 5.6111 8.0037 v Velocity[Y] -28.808 29.991 -0.14979 -0.01698 v Velocity[Z] -2.9488 3.0876 2.4499e-06 -5.3894e-08 v ǁVelocityǁ 0.0025788 40.599 8.1896 8.135 v Pressure -1.8941e+05 2.6983e+05 44036 12103 v TurbVisc 6.963e-20 0.020425 0.00018559 4.0123e-05 v CourantNb 2.9036e-09 0.011548 0.00016897 4.953e-06 v FourierNb 1.2426e-07 0.044131 0.00014753 4.0697e-07 v total_pressure -88089 3.7115e+05 1.4536e+05 1.1343e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0086 0.10556 0.0029124 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.4364e-07 0.049517 0.0003165 5.36e-06 INSTANT 0.876140000E-01 TIME STEP NUMBER 56338 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283102957E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.822277140E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11895E-01 0.20433E+01 Friction velocity uk : 0.11895E-01 0.20433E+01 Dimensionless distance yplus : 0.11616E-01 0.20092E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.055022707e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29465E+08 1 0.18212E-09 0.27040E+02 0.19932E+04 c Velocity[X] 0.14808E+02 c Velocity[Y] 0.12232E+02 c Velocity[Z] 0.13303E-05 c Pressure 0.13763E-03 155 0.76426E-04 0.11780E-02 0.15586E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.726 40.45 5.6112 8.0039 v Velocity[Y] -28.818 30.003 -0.14983 -0.017064 v Velocity[Z] -2.9493 3.0878 2.4493e-06 -5.3894e-08 v ǁVelocityǁ 0.0022 40.615 8.1913 8.1353 v Pressure -1.9055e+05 2.6888e+05 43078 11489 v TurbVisc 1.1083e-19 0.020443 0.00018566 4.0186e-05 v CourantNb 4.5693e-09 0.011547 0.00016898 4.9532e-06 v FourierNb 1.2426e-07 0.044122 0.00014754 4.074e-07 v total_pressure -89224 3.702e+05 1.444e+05 1.1281e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0092 0.1056 0.0029129 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.4381e-07 0.049509 0.00031651 5.3606e-06 INSTANT 0.876141000E-01 TIME STEP NUMBER 56339 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283109088E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.822750568E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.28534E-02 0.20439E+01 Friction velocity uk : 0.28534E-02 0.20439E+01 Dimensionless distance yplus : 0.27866E-02 0.20098E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.049758312e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29465E+08 1 0.18215E-09 0.27056E+02 0.19937E+04 c Velocity[X] 0.14814E+02 c Velocity[Y] 0.12242E+02 c Velocity[Z] 0.13309E-05 c Pressure 0.14145E-03 80 0.80803E-04 0.12101E-02 0.16461E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.735 40.465 5.6113 8.004 v Velocity[Y] -28.829 30.016 -0.14986 -0.017151 v Velocity[Z] -2.9497 3.088 2.4486e-06 -5.3894e-08 v ǁVelocityǁ 0.0015703 40.631 8.1929 8.1356 v Pressure -1.9164e+05 2.68e+05 42039 10840 v TurbVisc 1.2041e-19 0.02046 0.00018574 4.0248e-05 v CourantNb 5.1158e-09 0.011546 0.00016898 4.9533e-06 v FourierNb 1.2426e-07 0.044113 0.00014754 4.0783e-07 v total_pressure -90310 3.6932e+05 1.4336e+05 1.1217e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0098 0.10564 0.0029134 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.4398e-07 0.049501 0.00031652 5.3611e-06 INSTANT 0.876142000E-01 TIME STEP NUMBER 56340 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283115311E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.823218540E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.71493E-02 0.20445E+01 Friction velocity uk : 0.71493E-02 0.20445E+01 Dimensionless distance yplus : 0.68804E-02 0.20104E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.046664755e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29466E+08 1 0.18218E-09 0.27070E+02 0.19941E+04 c Velocity[X] 0.14821E+02 c Velocity[Y] 0.12249E+02 c Velocity[Z] 0.13345E-05 c Pressure 0.14572E-03 315 0.94323E-04 0.12460E-02 0.16811E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.744 40.481 5.6115 8.0041 v Velocity[Y] -28.839 30.028 -0.1499 -0.017235 v Velocity[Z] -2.9501 3.0882 2.448e-06 -5.3894e-08 v ǁVelocityǁ 0.001224 40.647 8.1946 8.1359 v Pressure -1.9284e+05 2.6699e+05 40966 10207 v TurbVisc 1.2531e-19 0.020478 0.00018581 4.0311e-05 v CourantNb 4.0841e-09 0.011545 0.00016899 4.9534e-06 v FourierNb 1.2426e-07 0.044104 0.00014755 4.0826e-07 v total_pressure -91513 3.6832e+05 1.4229e+05 1.1153e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0104 0.10569 0.002914 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.4415e-07 0.049492 0.00031653 5.3616e-06 INSTANT 0.876143000E-01 TIME STEP NUMBER 56341 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283121192E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.823683038E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.78037E-02 0.20451E+01 Friction velocity uk : 0.78037E-02 0.20451E+01 Dimensionless distance yplus : 0.75049E-02 0.20109E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.044212263e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29466E+08 1 0.18221E-09 0.27073E+02 0.19941E+04 c Velocity[X] 0.14826E+02 c Velocity[Y] 0.12247E+02 c Velocity[Z] 0.13364E-05 c Pressure 0.14999E-03 83 0.79762E-04 0.12818E-02 0.15811E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.753 40.497 5.6116 8.0042 v Velocity[Y] -28.85 30.04 -0.14993 -0.017322 v Velocity[Z] -2.9506 3.0883 2.4474e-06 -5.3894e-08 v ǁVelocityǁ 0.0013967 40.663 8.1962 8.1362 v Pressure -1.9399e+05 2.6599e+05 39865 9507.6 v TurbVisc 1.3505e-19 0.020495 0.00018589 4.0374e-05 v CourantNb 3.284e-09 0.011545 0.00016899 4.9535e-06 v FourierNb 1.2426e-07 0.044094 0.00014755 4.0869e-07 v total_pressure -92665 3.6732e+05 1.4119e+05 1.1083e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0109 0.10573 0.0029145 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.4431e-07 0.049484 0.00031654 5.3622e-06 INSTANT 0.876144000E-01 TIME STEP NUMBER 56342 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283127148E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.824143342E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.79270E-02 0.20457E+01 Friction velocity uk : 0.79270E-02 0.20457E+01 Dimensionless distance yplus : 0.76235E-02 0.20115E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.036121405e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29467E+08 1 0.18224E-09 0.27090E+02 0.19947E+04 c Velocity[X] 0.14831E+02 c Velocity[Y] 0.12259E+02 c Velocity[Z] 0.13441E-05 c Pressure 0.15087E-03 9 0.55831E-04 0.12886E-02 0.13358E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.762 40.512 5.6117 8.0043 v Velocity[Y] -28.861 30.053 -0.14997 -0.017409 v Velocity[Z] -2.951 3.0885 2.4468e-06 -5.3894e-08 v ǁVelocityǁ 0.0019479 40.679 8.1979 8.1364 v Pressure -1.9515e+05 2.6502e+05 38729 8890.4 v TurbVisc 1.371e-19 0.020513 0.00018596 4.0437e-05 v CourantNb 2.4656e-09 0.011544 0.000169 4.9536e-06 v FourierNb 1.2426e-07 0.044085 0.00014756 4.0912e-07 v total_pressure -93821 3.6635e+05 1.4005e+05 1.1022e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0115 0.10577 0.0029152 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.4448e-07 0.049476 0.00031655 5.3627e-06 INSTANT 0.876145000E-01 TIME STEP NUMBER 56343 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283133012E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.824598137E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.59075E-02 0.20463E+01 Friction velocity uk : 0.59075E-02 0.20463E+01 Dimensionless distance yplus : 0.56854E-02 0.20121E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.022766564e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29467E+08 1 0.18227E-09 0.27102E+02 0.19950E+04 c Velocity[X] 0.14839E+02 c Velocity[Y] 0.12263E+02 c Velocity[Z] 0.13432E-05 c Pressure 0.15562E-03 154 0.75541E-04 0.13286E-02 0.18254E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.771 40.528 5.6118 8.0044 v Velocity[Y] -28.871 30.065 -0.15 -0.017495 v Velocity[Z] -2.9514 3.0887 2.4462e-06 -5.3894e-08 v ǁVelocityǁ 0.0016477 40.695 8.1995 8.1367 v Pressure -1.9647e+05 2.638e+05 37558 8142 v TurbVisc 1.2867e-19 0.02053 0.00018604 4.0501e-05 v CourantNb 3.1602e-09 0.011543 0.000169 4.9537e-06 v FourierNb 1.2426e-07 0.044075 0.00014756 4.0955e-07 v total_pressure -95145 3.6513e+05 1.3888e+05 1.0947e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0121 0.10582 0.0029159 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.4465e-07 0.049468 0.00031656 5.3633e-06 INSTANT 0.876146000E-01 TIME STEP NUMBER 56344 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283138695E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.825048080E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.54574E-02 0.20469E+01 Friction velocity uk : 0.54574E-02 0.20469E+01 Dimensionless distance yplus : 0.53174E-02 0.20127E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.016306316e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29468E+08 1 0.18230E-09 0.27116E+02 0.19954E+04 c Velocity[X] 0.14844E+02 c Velocity[Y] 0.12273E+02 c Velocity[Z] 0.13418E-05 c Pressure 0.15935E-03 61 0.80594E-04 0.13597E-02 0.19063E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.779 40.544 5.6119 8.0045 v Velocity[Y] -28.882 30.078 -0.15004 -0.017583 v Velocity[Z] -2.9518 3.0889 2.4455e-06 -5.3894e-08 v ǁVelocityǁ 0.0017374 40.71 8.2012 8.137 v Pressure -1.9773e+05 2.6272e+05 36319 7365.3 v TurbVisc 1.4299e-19 0.020548 0.00018611 4.0564e-05 v CourantNb 2.806e-09 0.011542 0.00016901 4.9538e-06 v FourierNb 1.2426e-07 0.044066 0.00014757 4.0999e-07 v total_pressure -96402 3.6404e+05 1.3764e+05 1.0869e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0127 0.10586 0.0029166 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.4482e-07 0.049459 0.00031657 5.3638e-06 INSTANT 0.876147000E-01 TIME STEP NUMBER 56345 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283144453E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.825494487E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12070E-01 0.20475E+01 Friction velocity uk : 0.12070E-01 0.20475E+01 Dimensionless distance yplus : 0.11761E-01 0.20133E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.002730530e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29469E+08 1 0.18233E-09 0.27129E+02 0.19958E+04 c Velocity[X] 0.14850E+02 c Velocity[Y] 0.12279E+02 c Velocity[Z] 0.13442E-05 c Pressure 0.16339E-03 323 0.93853E-04 0.13934E-02 0.18845E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.788 40.559 5.612 8.0047 v Velocity[Y] -28.892 30.09 -0.15008 -0.017669 v Velocity[Z] -2.9523 3.0891 2.4449e-06 -5.3894e-08 v ǁVelocityǁ 0.0021701 40.726 8.2029 8.1373 v Pressure -1.991e+05 2.6151e+05 35055 6626.4 v TurbVisc 1.4292e-19 0.020565 0.00018619 4.0627e-05 v CourantNb 1.934e-09 0.011542 0.00016901 4.9539e-06 v FourierNb 1.2426e-07 0.044057 0.00014757 4.1042e-07 v total_pressure -97774 3.6283e+05 1.3638e+05 1.0795e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0133 0.1059 0.0029174 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.4499e-07 0.049451 0.00031658 5.3644e-06 INSTANT 0.876148000E-01 TIME STEP NUMBER 56346 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283149846E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.825937273E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12479E-01 0.20481E+01 Friction velocity uk : 0.12479E-01 0.20481E+01 Dimensionless distance yplus : 0.12004E-01 0.20138E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 9.886865967e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29469E+08 1 0.18235E-09 0.27131E+02 0.19957E+04 c Velocity[X] 0.14855E+02 c Velocity[Y] 0.12277E+02 c Velocity[Z] 0.13503E-05 c Pressure 0.16741E-03 521 0.79645E-04 0.14270E-02 0.17652E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.797 40.575 5.6121 8.0048 v Velocity[Y] -28.903 30.102 -0.15011 -0.017757 v Velocity[Z] -2.9527 3.0893 2.4443e-06 -5.3894e-08 v ǁVelocityǁ 0.0025729 40.742 8.2045 8.1376 v Pressure -2.004e+05 2.6032e+05 33774 5844.4 v TurbVisc 1.4942e-19 0.020583 0.00018627 4.069e-05 v CourantNb 2.5566e-09 0.011541 0.00016901 4.954e-06 v FourierNb 1.2426e-07 0.044047 0.00014758 4.1085e-07 v total_pressure -99071 3.6165e+05 1.351e+05 1.0717e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0138 0.10594 0.0029181 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.4517e-07 0.049442 0.00031659 5.3649e-06 INSTANT 0.876149000E-01 TIME STEP NUMBER 56347 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283155318E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.826374382E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10172E-01 0.20486E+01 Friction velocity uk : 0.10172E-01 0.20486E+01 Dimensionless distance yplus : 0.97853E-02 0.20144E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 9.705844910e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29470E+08 1 0.18238E-09 0.27147E+02 0.19962E+04 c Velocity[X] 0.14858E+02 c Velocity[Y] 0.12289E+02 c Velocity[Z] 0.13610E-05 c Pressure 0.16835E-03 9 0.57124E-04 0.14342E-02 0.16415E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.806 40.591 5.6122 8.0049 v Velocity[Y] -28.914 30.115 -0.15015 -0.017847 v Velocity[Z] -2.9531 3.0895 2.4437e-06 -5.3894e-08 v ǁVelocityǁ 0.0020671 40.758 8.2062 8.1379 v Pressure -2.0173e+05 2.5911e+05 32440 5083.8 v TurbVisc 1.4906e-19 0.0206 0.00018634 4.0754e-05 v CourantNb 3.3765e-09 0.01154 0.00016902 4.9542e-06 v FourierNb 1.2426e-07 0.044037 0.00014758 4.1129e-07 v total_pressure -1.004e+05 3.6044e+05 1.3376e+05 1.0641e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0144 0.10598 0.0029187 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.4534e-07 0.049433 0.0003166 5.3654e-06 INSTANT 0.876150000E-01 TIME STEP NUMBER 56348 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283160639E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.826804004E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.68331E-02 0.20491E+01 Friction velocity uk : 0.68331E-02 0.20491E+01 Dimensionless distance yplus : 0.65734E-02 0.20149E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 9.448163829e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29470E+08 1 0.18241E-09 0.27158E+02 0.19965E+04 c Velocity[X] 0.14867E+02 c Velocity[Y] 0.12292E+02 c Velocity[Z] 0.13540E-05 c Pressure 0.17275E-03 173 0.75750E-04 0.14710E-02 0.20444E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.815 40.606 5.6123 8.005 v Velocity[Y] -28.925 30.127 -0.15019 -0.017934 v Velocity[Z] -2.9536 3.0896 2.443e-06 -5.3894e-08 v ǁVelocityǁ 0.0018058 40.774 8.2078 8.1381 v Pressure -2.0322e+05 2.577e+05 31094 4240.3 v TurbVisc 1.4129e-19 0.020618 0.00018642 4.0817e-05 v CourantNb 4.1665e-09 0.011539 0.00016902 4.9543e-06 v FourierNb 1.2426e-07 0.044027 0.00014759 4.1172e-07 v total_pressure -1.0189e+05 3.5903e+05 1.3242e+05 1.0557e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0149 0.10602 0.0029192 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.4551e-07 0.049424 0.00031661 5.366e-06 INSTANT 0.876151000E-01 TIME STEP NUMBER 56349 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283165802E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.827227826E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10685E-02 0.20497E+01 Friction velocity uk : 0.10685E-02 0.20497E+01 Dimensionless distance yplus : 0.10279E-02 0.20154E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 9.273778800e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29471E+08 1 0.18245E-09 0.27172E+02 0.19969E+04 c Velocity[X] 0.14870E+02 c Velocity[Y] 0.12301E+02 c Velocity[Z] 0.13505E-05 c Pressure 0.17621E-03 69 0.80853E-04 0.14997E-02 0.21090E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.824 40.622 5.6124 8.0051 v Velocity[Y] -28.935 30.14 -0.15022 -0.018024 v Velocity[Z] -2.954 3.0898 2.4424e-06 -5.3894e-08 v ǁVelocityǁ 0.0018895 40.789 8.2095 8.1384 v Pressure -2.0462e+05 2.5643e+05 29674 3363.9 v TurbVisc 1.547e-19 0.020635 0.00018649 4.0881e-05 v CourantNb 4.9297e-09 0.011539 0.00016903 4.9544e-06 v FourierNb 1.2426e-07 0.044017 0.00014759 4.1216e-07 v total_pressure -1.033e+05 3.5775e+05 1.31e+05 1.0469e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0154 0.10605 0.0029198 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.4568e-07 0.049416 0.00031662 5.3665e-06 INSTANT 0.876152000E-01 TIME STEP NUMBER 56350 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283171014E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.827647764E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.37055E-02 0.20502E+01 Friction velocity uk : 0.37055E-02 0.20502E+01 Dimensionless distance yplus : 0.35647E-02 0.20160E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 9.031220540e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29471E+08 1 0.18248E-09 0.27184E+02 0.19972E+04 c Velocity[X] 0.14876E+02 c Velocity[Y] 0.12307E+02 c Velocity[Z] 0.13517E-05 c Pressure 0.17992E-03 309 0.94067E-04 0.15304E-02 0.20691E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.833 40.638 5.6125 8.0052 v Velocity[Y] -28.946 30.152 -0.15026 -0.018112 v Velocity[Z] -2.9544 3.09 2.4418e-06 -5.3894e-08 v ǁVelocityǁ 0.0019423 40.805 8.2111 8.1387 v Pressure -2.0614e+05 2.5505e+05 28237 2528.8 v TurbVisc 1.5603e-19 0.020652 0.00018657 4.0945e-05 v CourantNb 5.9619e-09 0.011538 0.00016903 4.9545e-06 v FourierNb 1.2426e-07 0.044007 0.0001476 4.1259e-07 v total_pressure -1.0482e+05 3.5638e+05 1.2956e+05 1.0385e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.016 0.10608 0.0029203 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.4586e-07 0.049406 0.00031663 5.3671e-06 INSTANT 0.876153000E-01 TIME STEP NUMBER 56351 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283175844E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.828063108E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.21648E-02 0.20507E+01 Friction velocity uk : 0.21648E-02 0.20507E+01 Dimensionless distance yplus : 0.20825E-02 0.20165E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 8.774770885e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29471E+08 1 0.18250E-09 0.27185E+02 0.19972E+04 c Velocity[X] 0.14880E+02 c Velocity[Y] 0.12304E+02 c Velocity[Z] 0.13533E-05 c Pressure 0.18359E-03 400 0.79749E-04 0.15609E-02 0.19834E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.842 40.653 5.6126 8.0053 v Velocity[Y] -28.957 30.164 -0.1503 -0.018201 v Velocity[Z] -2.9549 3.0902 2.4412e-06 -5.3895e-08 v ǁVelocityǁ 0.0019461 40.821 8.2128 8.1389 v Pressure -2.0759e+05 2.5373e+05 26785 1644.3 v TurbVisc 1.3708e-19 0.02067 0.00018665 4.1008e-05 v CourantNb 6.3265e-09 0.011537 0.00016904 4.9546e-06 v FourierNb 1.2426e-07 0.043997 0.0001476 4.1303e-07 v total_pressure -1.0627e+05 3.5506e+05 1.2811e+05 1.0297e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0165 0.10612 0.002921 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.4603e-07 0.049397 0.00031664 5.3676e-06 INSTANT 0.876154000E-01 TIME STEP NUMBER 56352 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283180737E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.828471749E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.68434E-02 0.20512E+01 Friction velocity uk : 0.68434E-02 0.20512E+01 Dimensionless distance yplus : 0.65833E-02 0.20169E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 8.473702988e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29472E+08 1 0.18254E-09 0.27200E+02 0.19976E+04 c Velocity[X] 0.14883E+02 c Velocity[Y] 0.12317E+02 c Velocity[Z] 0.13668E-05 c Pressure 0.18439E-03 9 0.57890E-04 0.15668E-02 0.18067E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.851 40.669 5.6127 8.0054 v Velocity[Y] -28.968 30.177 -0.15033 -0.018293 v Velocity[Z] -2.9553 3.0904 2.4406e-06 -5.3895e-08 v ǁVelocityǁ 0.0020167 40.837 8.2144 8.1392 v Pressure -2.0906e+05 2.5246e+05 25288 805.6 v TurbVisc 1.0989e-19 0.020687 0.00018672 4.1072e-05 v CourantNb 7.1668e-09 0.011536 0.00016904 4.9547e-06 v FourierNb 1.2426e-07 0.043987 0.00014761 4.1347e-07 v total_pressure -1.0773e+05 3.5378e+05 1.2661e+05 1.0213e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0169 0.10616 0.0029217 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.462e-07 0.049388 0.00031665 5.3681e-06 INSTANT 0.876155000E-01 TIME STEP NUMBER 56353 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283185463E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.828872169E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.92615E-02 0.20517E+01 Friction velocity uk : 0.92615E-02 0.20517E+01 Dimensionless distance yplus : 0.89095E-02 0.20174E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 8.092905203e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29472E+08 1 0.18257E-09 0.27211E+02 0.19979E+04 c Velocity[X] 0.14892E+02 c Velocity[Y] 0.12319E+02 c Velocity[Z] 0.13616E-05 c Pressure 0.18836E-03 151 0.75754E-04 0.15998E-02 0.22743E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.86 40.684 5.6127 8.0055 v Velocity[Y] -28.979 30.189 -0.15037 -0.018382 v Velocity[Z] -2.9557 3.0906 2.4399e-06 -5.3895e-08 v ǁVelocityǁ 0.0021423 40.853 8.2161 8.1395 v Pressure -2.107e+05 2.5095e+05 23776 -149.53 v TurbVisc 1.4972e-19 0.020705 0.0001868 4.1136e-05 v CourantNb 7.6049e-09 0.011535 0.00016905 4.9548e-06 v FourierNb 1.2426e-07 0.043976 0.00014762 4.139e-07 v total_pressure -1.0938e+05 3.5228e+05 1.251e+05 1.0118e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0174 0.1062 0.0029223 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.4638e-07 0.049378 0.00031666 5.3687e-06 INSTANT 0.876156000E-01 TIME STEP NUMBER 56354 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283190028E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.829265494E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11437E-01 0.20522E+01 Friction velocity uk : 0.11437E-01 0.20522E+01 Dimensionless distance yplus : 0.11003E-01 0.20179E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 7.817968462e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29473E+08 1 0.18260E-09 0.27223E+02 0.19983E+04 c Velocity[X] 0.14895E+02 c Velocity[Y] 0.12328E+02 c Velocity[Z] 0.13556E-05 c Pressure 0.19145E-03 63 0.80824E-04 0.16252E-02 0.22856E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.87 40.7 5.6128 8.0055 v Velocity[Y] -28.99 30.201 -0.15041 -0.018473 v Velocity[Z] -2.9561 3.0907 2.4393e-06 -5.3895e-08 v ǁVelocityǁ 0.0023022 40.868 8.2177 8.1397 v Pressure -2.1224e+05 2.4954e+05 22195 -1116.5 v TurbVisc 8.0781e-20 0.020722 0.00018687 4.12e-05 v CourantNb 8.7887e-09 0.011535 0.00016905 4.9549e-06 v FourierNb 1.2426e-07 0.043966 0.00014762 4.1434e-07 v total_pressure -1.1092e+05 3.5087e+05 1.2352e+05 1.0021e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0179 0.10623 0.0029229 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.4655e-07 0.049368 0.00031667 5.3692e-06 INSTANT 0.876157000E-01 TIME STEP NUMBER 56355 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283194621E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.829654685E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13053E-01 0.20526E+01 Friction velocity uk : 0.13053E-01 0.20526E+01 Dimensionless distance yplus : 0.12557E-01 0.20183E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 7.465230786e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29473E+08 1 0.18263E-09 0.27234E+02 0.19986E+04 c Velocity[X] 0.14901E+02 c Velocity[Y] 0.12334E+02 c Velocity[Z] 0.13557E-05 c Pressure 0.19476E-03 306 0.94100E-04 0.16524E-02 0.22158E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.879 40.715 5.6129 8.0056 v Velocity[Y] -29.001 30.214 -0.15044 -0.018563 v Velocity[Z] -2.9566 3.0909 2.4387e-06 -5.3895e-08 v ǁVelocityǁ 0.0023506 40.884 8.2194 8.14 v Pressure -2.139e+05 2.481e+05 20606 -2032 v TurbVisc 6.7463e-20 0.020739 0.00018695 4.1264e-05 v CourantNb 9.9619e-09 0.011534 0.00016906 4.955e-06 v FourierNb 1.2426e-07 0.043955 0.00014763 4.1478e-07 v total_pressure -1.1257e+05 3.4942e+05 1.2193e+05 99293 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0183 0.10626 0.0029234 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.4673e-07 0.049359 0.00031668 5.3697e-06 INSTANT 0.876158000E-01 TIME STEP NUMBER 56356 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283198819E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.830038541E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.91653E-02 0.20531E+01 Friction velocity uk : 0.91653E-02 0.20531E+01 Dimensionless distance yplus : 0.88976E-02 0.20188E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 7.101175572e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29474E+08 1 0.18266E-09 0.27235E+02 0.19985E+04 c Velocity[X] 0.14904E+02 c Velocity[Y] 0.12331E+02 c Velocity[Z] 0.13570E-05 c Pressure 0.19799E-03 110 0.79744E-04 0.16790E-02 0.22073E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.895 40.731 5.613 8.0057 v Velocity[Y] -29.012 30.226 -0.15048 -0.018654 v Velocity[Z] -2.957 3.0911 2.4381e-06 -5.3895e-08 v ǁVelocityǁ 0.0022444 40.9 8.221 8.1402 v Pressure -2.155e+05 2.4663e+05 18994 -3028.5 v TurbVisc 5.0872e-20 0.020757 0.00018702 4.1328e-05 v CourantNb 1.0795e-08 0.011533 0.00016906 4.9551e-06 v FourierNb 1.2426e-07 0.043944 0.00014763 4.1522e-07 v total_pressure -1.1418e+05 3.4795e+05 1.2032e+05 98297 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0188 0.10629 0.0029239 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.469e-07 0.049348 0.00031669 5.3703e-06 INSTANT 0.876159000E-01 TIME STEP NUMBER 56357 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283203053E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.830414233E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.56472E-02 0.20535E+01 Friction velocity uk : 0.56472E-02 0.20535E+01 Dimensionless distance yplus : 0.54822E-02 0.20192E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 6.705695587e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29474E+08 1 0.18269E-09 0.27250E+02 0.19990E+04 c Velocity[X] 0.14908E+02 c Velocity[Y] 0.12342E+02 c Velocity[Z] 0.13787E-05 c Pressure 0.19855E-03 9 0.58108E-04 0.16829E-02 0.18869E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.913 40.746 5.613 8.0058 v Velocity[Y] -29.022 30.238 -0.15051 -0.018747 v Velocity[Z] -2.9574 3.0913 2.4375e-06 -5.3895e-08 v ǁVelocityǁ 0.002157 40.915 8.2226 8.1405 v Pressure -2.1707e+05 2.4519e+05 17363 -3911.4 v TurbVisc 4.7276e-20 0.020774 0.0001871 4.1392e-05 v CourantNb 1.1635e-08 0.011533 0.00016906 4.9552e-06 v FourierNb 1.2426e-07 0.043933 0.00014764 4.1566e-07 v total_pressure -1.1575e+05 3.4652e+05 1.1869e+05 97414 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0192 0.10632 0.0029244 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.4708e-07 0.049338 0.0003167 5.3708e-06 INSTANT 0.876160000E-01 TIME STEP NUMBER 56358 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283207123E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.830781141E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.55680E-02 0.20539E+01 Friction velocity uk : 0.55680E-02 0.20539E+01 Dimensionless distance yplus : 0.54054E-02 0.20196E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 6.200696715e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29474E+08 1 0.18272E-09 0.27260E+02 0.19992E+04 c Velocity[X] 0.14916E+02 c Velocity[Y] 0.12344E+02 c Velocity[Z] 0.13689E-05 c Pressure 0.20202E-03 175 0.75475E-04 0.17114E-02 0.24432E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.93 40.762 5.6131 8.0059 v Velocity[Y] -29.033 30.25 -0.15055 -0.018837 v Velocity[Z] -2.9579 3.0915 2.4368e-06 -5.3895e-08 v ǁVelocityǁ 0.0020693 40.931 8.2243 8.1408 v Pressure -2.1884e+05 2.4356e+05 15704 -4956.3 v TurbVisc 6.4326e-20 0.020791 0.00018718 4.1457e-05 v CourantNb 1.2006e-08 0.011532 0.00016907 4.9552e-06 v FourierNb 1.2426e-07 0.043922 0.00014764 4.161e-07 v total_pressure -1.1752e+05 3.4489e+05 1.1703e+05 96369 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0196 0.10635 0.0029249 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.4725e-07 0.049328 0.00031671 5.3713e-06 INSTANT 0.876161000E-01 TIME STEP NUMBER 56359 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283211032E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.831139577E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.93942E-02 0.20543E+01 Friction velocity uk : 0.93942E-02 0.20543E+01 Dimensionless distance yplus : 0.90576E-02 0.20200E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 5.856833358e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29475E+08 1 0.18275E-09 0.27273E+02 0.19996E+04 c Velocity[X] 0.14920E+02 c Velocity[Y] 0.12353E+02 c Velocity[Z] 0.13596E-05 c Pressure 0.20467E-03 63 0.80641E-04 0.17329E-02 0.24434E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.948 40.777 5.6131 8.0059 v Velocity[Y] -29.044 30.262 -0.15058 -0.018931 v Velocity[Z] -2.9583 3.0917 2.4362e-06 -5.3895e-08 v ǁVelocityǁ 0.0020023 40.947 8.2259 8.141 v Pressure -2.2052e+05 2.4201e+05 13983 -6011.4 v TurbVisc 3.719e-20 0.020809 0.00018725 4.1521e-05 v CourantNb 1.3251e-08 0.011531 0.00016907 4.9553e-06 v FourierNb 1.2426e-07 0.043911 0.00014765 4.1654e-07 v total_pressure -1.192e+05 3.4334e+05 1.1531e+05 95314 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.02 0.10638 0.0029254 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.4743e-07 0.049317 0.00031672 5.3719e-06 INSTANT 0.876162000E-01 TIME STEP NUMBER 56360 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283214945E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.831493098E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.72002E-02 0.20547E+01 Friction velocity uk : 0.72002E-02 0.20547E+01 Dimensionless distance yplus : 0.69422E-02 0.20203E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 5.415569843e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29475E+08 1 0.18278E-09 0.27284E+02 0.19999E+04 c Velocity[X] 0.14925E+02 c Velocity[Y] 0.12358E+02 c Velocity[Z] 0.13558E-05 c Pressure 0.20751E-03 213 0.93807E-04 0.17560E-02 0.23116E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.965 40.793 5.6132 8.006 v Velocity[Y] -29.055 30.274 -0.15061 -0.019022 v Velocity[Z] -2.9587 3.0918 2.4356e-06 -5.3895e-08 v ǁVelocityǁ 0.0019503 40.962 8.2276 8.1412 v Pressure -2.2229e+05 2.4044e+05 12266 -6986.4 v TurbVisc 3.1522e-20 0.020826 0.00018733 4.1586e-05 v CourantNb 1.437e-08 0.01153 0.00016908 4.9554e-06 v FourierNb 1.2426e-07 0.0439 0.00014766 4.1698e-07 v total_pressure -1.2097e+05 3.4177e+05 1.1359e+05 94339 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0203 0.10641 0.0029258 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.4761e-07 0.049307 0.00031673 5.3724e-06 INSTANT 0.876163000E-01 TIME STEP NUMBER 56361 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283218449E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.831840644E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.46294E-02 0.20550E+01 Friction velocity uk : 0.46294E-02 0.20550E+01 Dimensionless distance yplus : 0.44635E-02 0.20207E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 4.969720441e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29476E+08 1 0.18281E-09 0.27284E+02 0.19998E+04 c Velocity[X] 0.14929E+02 c Velocity[Y] 0.12355E+02 c Velocity[Z] 0.13577E-05 c Pressure 0.21026E-03 126 0.79526E-04 0.17784E-02 0.24098E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -25.983 40.808 5.6132 8.0061 v Velocity[Y] -29.066 30.287 -0.15065 -0.019115 v Velocity[Z] -2.9591 3.092 2.435e-06 -5.3895e-08 v ǁVelocityǁ 0.0019137 40.978 8.2292 8.1415 v Pressure -2.2403e+05 2.3883e+05 10515 -8092.9 v TurbVisc 2.7952e-20 0.020843 0.0001874 4.165e-05 v CourantNb 1.5351e-08 0.01153 0.00016908 4.9555e-06 v FourierNb 1.2426e-07 0.043888 0.00014766 4.1742e-07 v total_pressure -1.227e+05 3.4016e+05 1.1184e+05 93232 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0207 0.10644 0.0029262 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.4779e-07 0.049296 0.00031675 5.3729e-06 INSTANT 0.876164000E-01 TIME STEP NUMBER 56362 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283221975E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.832178743E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.51867E-02 0.20554E+01 Friction velocity uk : 0.51867E-02 0.20554E+01 Dimensionless distance yplus : 0.50009E-02 0.20210E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 4.506886425e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29476E+08 1 0.18284E-09 0.27299E+02 0.20003E+04 c Velocity[X] 0.14934E+02 c Velocity[Y] 0.12366E+02 c Velocity[Z] 0.13938E-05 c Pressure 0.21049E-03 13 0.58369E-04 0.17794E-02 0.19726E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -26 40.824 5.6133 8.0061 v Velocity[Y] -29.077 30.299 -0.15068 -0.019209 v Velocity[Z] -2.9596 3.0922 2.4344e-06 -5.3895e-08 v ǁVelocityǁ 0.0018908 40.994 8.2308 8.1417 v Pressure -2.2572e+05 2.3729e+05 8763.3 -9028.1 v TurbVisc 2.7295e-20 0.020861 0.00018748 4.1715e-05 v CourantNb 1.6397e-08 0.011529 0.00016909 4.9556e-06 v FourierNb 1.2426e-07 0.043876 0.00014767 4.1786e-07 v total_pressure -1.2439e+05 3.3861e+05 1.1009e+05 92297 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.021 0.10647 0.0029266 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.4796e-07 0.049285 0.00031676 5.3735e-06 INSTANT 0.876165000E-01 TIME STEP NUMBER 56363 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283225327E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.832507645E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.42921E-02 0.20557E+01 Friction velocity uk : 0.42921E-02 0.20557E+01 Dimensionless distance yplus : 0.41383E-02 0.20213E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 3.938891505e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29476E+08 1 0.18287E-09 0.27310E+02 0.20005E+04 c Velocity[X] 0.14942E+02 c Velocity[Y] 0.12368E+02 c Velocity[Z] 0.13667E-05 c Pressure 0.21344E-03 149 0.75359E-04 0.18035E-02 0.25472E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -26.017 40.839 5.6133 8.0062 v Velocity[Y] -29.088 30.311 -0.15072 -0.019301 v Velocity[Z] -2.96 3.0924 2.4338e-06 -5.3895e-08 v ǁVelocityǁ 0.001888 41.009 8.2325 8.142 v Pressure -2.276e+05 2.3553e+05 6987.3 -10141 v TurbVisc 4.0134e-20 0.020878 0.00018756 4.1779e-05 v CourantNb 1.7746e-08 0.011528 0.00016909 4.9557e-06 v FourierNb 1.2426e-07 0.043865 0.00014768 4.183e-07 v total_pressure -1.2627e+05 3.3686e+05 1.0831e+05 91184 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0213 0.10649 0.002927 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.4814e-07 0.049274 0.00031677 5.374e-06 INSTANT 0.876166000E-01 TIME STEP NUMBER 56364 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283228515E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.832826816E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.47446E-02 0.20560E+01 Friction velocity uk : 0.47446E-02 0.20560E+01 Dimensionless distance yplus : 0.45746E-02 0.20217E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 3.548802335e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29477E+08 1 0.18290E-09 0.27322E+02 0.20009E+04 c Velocity[X] 0.14946E+02 c Velocity[Y] 0.12376E+02 c Velocity[Z] 0.13543E-05 c Pressure 0.21559E-03 69 0.80531E-04 0.18207E-02 0.25350E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -26.035 40.855 5.6134 8.0063 v Velocity[Y] -29.099 30.323 -0.15075 -0.019396 v Velocity[Z] -2.9604 3.0926 2.4331e-06 -5.3895e-08 v ǁVelocityǁ 0.0018906 41.025 8.2341 8.1422 v Pressure -2.2939e+05 2.3387e+05 5148.9 -11265 v TurbVisc 2.7666e-20 0.020895 0.00018763 4.1844e-05 v CourantNb 1.8185e-08 0.011527 0.00016909 4.9558e-06 v FourierNb 1.2426e-07 0.043853 0.00014768 4.1875e-07 v total_pressure -1.2806e+05 3.3519e+05 1.0647e+05 90060 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0217 0.10651 0.0029273 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.4832e-07 0.049262 0.00031678 5.3745e-06 INSTANT 0.876167000E-01 TIME STEP NUMBER 56365 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283231693E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.833141460E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.21007E-02 0.20563E+01 Friction velocity uk : 0.21007E-02 0.20563E+01 Dimensionless distance yplus : 0.20254E-02 0.20220E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 3.068314696e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29477E+08 1 0.18293E-09 0.27333E+02 0.20012E+04 c Velocity[X] 0.14952E+02 c Velocity[Y] 0.12381E+02 c Velocity[Z] 0.13519E-05 c Pressure 0.21792E-03 222 0.93659E-04 0.18394E-02 0.23819E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -26.052 40.87 5.6134 8.0063 v Velocity[Y] -29.11 30.335 -0.15078 -0.019489 v Velocity[Z] -2.9609 3.0928 2.4325e-06 -5.3895e-08 v ǁVelocityǁ 0.0019071 41.04 8.2357 8.1424 v Pressure -2.3127e+05 2.3219e+05 3320.6 -12301 v TurbVisc 2.9092e-20 0.020913 0.00018771 4.1909e-05 v CourantNb 2.1941e-08 0.011527 0.0001691 4.9559e-06 v FourierNb 1.2426e-07 0.043841 0.00014769 4.1919e-07 v total_pressure -1.2994e+05 3.3352e+05 1.0465e+05 89024 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.022 0.10654 0.0029276 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.485e-07 0.049251 0.00031679 5.375e-06 INSTANT 0.876168000E-01 TIME STEP NUMBER 56366 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283234450E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.833448749E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.43354E-02 0.20566E+01 Friction velocity uk : 0.43354E-02 0.20566E+01 Dimensionless distance yplus : 0.41801E-02 0.20222E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 2.610721096e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29477E+08 1 0.18295E-09 0.27334E+02 0.20011E+04 c Velocity[X] 0.14957E+02 c Velocity[Y] 0.12377E+02 c Velocity[Z] 0.13510E-05 c Pressure 0.22016E-03 187 0.79376E-04 0.18574E-02 0.24859E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -26.069 40.885 5.6134 8.0064 v Velocity[Y] -29.121 30.346 -0.15081 -0.019584 v Velocity[Z] -2.9613 3.0929 2.4319e-06 -5.3895e-08 v ǁVelocityǁ 0.001938 41.056 8.2373 8.1427 v Pressure -2.331e+05 2.3048e+05 1465.1 -13471 v TurbVisc 3.202e-20 0.02093 0.00018778 4.1974e-05 v CourantNb 2.4466e-08 0.011526 0.0001691 4.9559e-06 v FourierNb 1.2426e-07 0.043828 0.0001477 4.1963e-07 v total_pressure -1.3178e+05 3.3181e+05 1.0279e+05 87854 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0222 0.10656 0.0029279 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.4868e-07 0.049239 0.0003168 5.3756e-06 INSTANT 0.876169000E-01 TIME STEP NUMBER 56367 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283237224E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.833745502E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.78287E-02 0.20569E+01 Friction velocity uk : 0.78287E-02 0.20569E+01 Dimensionless distance yplus : 0.75482E-02 0.20225E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 2.122678738e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29477E+08 1 0.18298E-09 0.27349E+02 0.20016E+04 c Velocity[X] 0.14961E+02 c Velocity[Y] 0.12388E+02 c Velocity[Z] 0.13574E-05 c Pressure 0.21997E-03 10 0.58573E-04 0.18548E-02 0.20486E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -26.086 40.901 5.6134 8.0064 v Velocity[Y] -29.132 30.358 -0.15084 -0.01968 v Velocity[Z] -2.9617 3.0931 2.4313e-06 -5.3895e-08 v ǁVelocityǁ 0.0015745 41.071 8.2389 8.1429 v Pressure -2.3489e+05 2.2884e+05 -389.07 -14468 v TurbVisc 3.6973e-20 0.020947 0.00018786 4.2039e-05 v CourantNb 2.7357e-08 0.011525 0.0001691 4.956e-06 v FourierNb 1.2426e-07 0.043816 0.0001477 4.2008e-07 v total_pressure -1.3357e+05 3.3016e+05 1.0094e+05 86857 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0225 0.10659 0.0029284 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.4886e-07 0.049227 0.00031681 5.3761e-06 INSTANT 0.876170000E-01 TIME STEP NUMBER 56368 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283239804E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.834032058E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10328E-01 0.20572E+01 Friction velocity uk : 0.10328E-01 0.20572E+01 Dimensionless distance yplus : 0.99578E-02 0.20228E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.588599466e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29478E+08 1 0.18301E-09 0.27360E+02 0.20019E+04 c Velocity[X] 0.14971E+02 c Velocity[Y] 0.12390E+02 c Velocity[Z] 0.13532E-05 c Pressure 0.22234E-03 166 0.75359E-04 0.18739E-02 0.25666E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -26.103 40.916 5.6134 8.0065 v Velocity[Y] -29.143 30.37 -0.15087 -0.019774 v Velocity[Z] -2.9621 3.0933 2.4307e-06 -5.3895e-08 v ǁVelocityǁ 0.0012152 41.087 8.2406 8.1431 v Pressure -2.3686e+05 2.2701e+05 -2256.2 -15621 v TurbVisc 4.6069e-20 0.020965 0.00018793 4.2104e-05 v CourantNb 2.8757e-08 0.011524 0.00016911 4.9561e-06 v FourierNb 1.2426e-07 0.043804 0.00014771 4.2052e-07 v total_pressure -1.3553e+05 3.2834e+05 99069 85704 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0228 0.10661 0.0029288 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.4904e-07 0.049215 0.00031682 5.3766e-06 INSTANT 0.876171000E-01 TIME STEP NUMBER 56369 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283242229E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.834307156E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12446E-01 0.20574E+01 Friction velocity uk : 0.12446E-01 0.20574E+01 Dimensionless distance yplus : 0.12000E-01 0.20230E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.150976419e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29478E+08 1 0.18304E-09 0.27373E+02 0.20023E+04 c Velocity[X] 0.14976E+02 c Velocity[Y] 0.12397E+02 c Velocity[Z] 0.13489E-05 c Pressure 0.22403E-03 70 0.80775E-04 0.18871E-02 0.25831E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -26.12 40.931 5.6135 8.0065 v Velocity[Y] -29.154 30.382 -0.15091 -0.01987 v Velocity[Z] -2.9626 3.0935 2.4301e-06 -5.3895e-08 v ǁVelocityǁ 0.00073387 41.102 8.2422 8.1433 v Pressure -2.3875e+05 2.2537e+05 -4188.6 -16807 v TurbVisc 4.9745e-20 0.020982 0.00018801 4.2169e-05 v CourantNb 2.9981e-08 0.011524 0.00016911 4.9562e-06 v FourierNb 1.2426e-07 0.043791 0.00014772 4.2097e-07 v total_pressure -1.3742e+05 3.2669e+05 97136 84518 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.023 0.10663 0.0029292 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.4922e-07 0.049203 0.00031683 5.3771e-06 INSTANT 0.876172000E-01 TIME STEP NUMBER 56370 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283244629E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.834578453E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12885E-01 0.20576E+01 Friction velocity uk : 0.12885E-01 0.20576E+01 Dimensionless distance yplus : 0.12472E-01 0.20232E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 7.418414175e-03 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29478E+08 1 0.18307E-09 0.27385E+02 0.20026E+04 c Velocity[X] 0.14983E+02 c Velocity[Y] 0.12402E+02 c Velocity[Z] 0.13417E-05 c Pressure 0.22582E-03 219 0.93856E-04 0.19013E-02 0.23985E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -26.137 40.946 5.6135 8.0066 v Velocity[Y] -29.165 30.394 -0.15094 -0.019965 v Velocity[Z] -2.963 3.0937 2.4294e-06 -5.3895e-08 v ǁVelocityǁ 0.00064431 41.118 8.2438 8.1435 v Pressure -2.4072e+05 2.2365e+05 -6101.7 -17890 v TurbVisc 5.5916e-20 0.020999 0.00018808 4.2234e-05 v CourantNb 3.1089e-08 0.011523 0.00016911 4.9562e-06 v FourierNb 1.2426e-07 0.043779 0.00014772 4.2141e-07 v total_pressure -1.3939e+05 3.2497e+05 95223 83435 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0232 0.10666 0.0029295 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.494e-07 0.049191 0.00031684 5.3777e-06 INSTANT 0.876173000E-01 TIME STEP NUMBER 56371 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283246598E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.834841519E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12983E-01 0.20579E+01 Friction velocity uk : 0.12983E-01 0.20579E+01 Dimensionless distance yplus : 0.12566E-01 0.20235E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 3.166480282e-03 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29478E+08 1 0.18310E-09 0.27386E+02 0.20026E+04 c Velocity[X] 0.14988E+02 c Velocity[Y] 0.12398E+02 c Velocity[Z] 0.13412E-05 c Pressure 0.22752E-03 142 0.79791E-04 0.19146E-02 0.24995E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -26.154 40.962 5.6135 8.0066 v Velocity[Y] -29.176 30.405 -0.15097 -0.020061 v Velocity[Z] -2.9634 3.0938 2.4288e-06 -5.3896e-08 v ǁVelocityǁ 0.0008219 41.133 8.2454 8.1438 v Pressure -2.4264e+05 2.2196e+05 -8039 -19108 v TurbVisc 7.8811e-20 0.021016 0.00018816 4.2299e-05 v CourantNb 3.183e-08 0.011522 0.00016912 4.9563e-06 v FourierNb 1.2426e-07 0.043766 0.00014773 4.2186e-07 v total_pressure -1.4131e+05 3.2329e+05 93286 82217 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0235 0.10668 0.0029299 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.4959e-07 0.049179 0.00031685 5.3782e-06 INSTANT 0.876174000E-01 TIME STEP NUMBER 56372 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283248577E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.835093080E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13014E-01 0.20581E+01 Friction velocity uk : 0.13014E-01 0.20581E+01 Dimensionless distance yplus : 0.12596E-01 0.20237E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.017074575e-03 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29479E+08 1 0.18312E-09 0.27402E+02 0.20031E+04 c Velocity[X] 0.14993E+02 c Velocity[Y] 0.12408E+02 c Velocity[Z] 0.13478E-05 c Pressure 0.22684E-03 10 0.59130E-04 0.19079E-02 0.20563E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -26.171 40.977 5.6135 8.0066 v Velocity[Y] -29.187 30.417 -0.151 -0.020159 v Velocity[Z] -2.9638 3.094 2.4282e-06 -5.3896e-08 v ǁVelocityǁ 0.00096235 41.149 8.247 8.144 v Pressure -2.445e+05 2.2034e+05 -9967.7 -20146 v TurbVisc 7.8524e-20 0.021034 0.00018823 4.2364e-05 v CourantNb 3.2639e-08 0.011521 0.00016912 4.9564e-06 v FourierNb 1.2426e-07 0.043753 0.00014774 4.2231e-07 v total_pressure -1.4318e+05 3.2166e+05 91357 81179 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0237 0.1067 0.0029302 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.4977e-07 0.049166 0.00031686 5.3787e-06 INSTANT 0.876175000E-01 TIME STEP NUMBER 56373 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283250352E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.835333678E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12803E-01 0.20583E+01 Friction velocity uk : 0.12803E-01 0.20583E+01 Dimensionless distance yplus : 0.12392E-01 0.20239E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -5.570878774e-03 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29479E+08 1 0.18315E-09 0.27413E+02 0.20034E+04 c Velocity[X] 0.15004E+02 c Velocity[Y] 0.12410E+02 c Velocity[Z] 0.13407E-05 c Pressure 0.22867E-03 311 0.75844E-04 0.19223E-02 0.25505E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -26.188 40.992 5.6135 8.0067 v Velocity[Y] -29.198 30.429 -0.15103 -0.020254 v Velocity[Z] -2.9643 3.0942 2.4276e-06 -5.3896e-08 v ǁVelocityǁ 0.0014007 41.164 8.2486 8.1442 v Pressure -2.4655e+05 2.1854e+05 -11903 -21338 v TurbVisc 9.6812e-20 0.021051 0.00018831 4.243e-05 v CourantNb 3.3555e-08 0.011521 0.00016912 4.9565e-06 v FourierNb 1.2426e-07 0.043741 0.00014774 4.2275e-07 v total_pressure -1.4523e+05 3.1986e+05 89422 79987 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0239 0.10672 0.0029304 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.4995e-07 0.049154 0.00031687 5.3792e-06 INSTANT 0.876176000E-01 TIME STEP NUMBER 56374 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283251975E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.835561771E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12827E-01 0.20585E+01 Friction velocity uk : 0.12827E-01 0.20585E+01 Dimensionless distance yplus : 0.12415E-01 0.20241E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -9.353761433e-03 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29479E+08 1 0.18318E-09 0.27427E+02 0.20038E+04 c Velocity[X] 0.15009E+02 c Velocity[Y] 0.12418E+02 c Velocity[Z] 0.13327E-05 c Pressure 0.22981E-03 413 0.81343E-04 0.19309E-02 0.27174E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -26.205 41.007 5.6135 8.0067 v Velocity[Y] -29.209 30.44 -0.15106 -0.020353 v Velocity[Z] -2.9647 3.0944 2.427e-06 -5.3896e-08 v ǁVelocityǁ 0.0014844 41.179 8.2502 8.1444 v Pressure -2.4856e+05 2.1677e+05 -13929 -22653 v TurbVisc 1.18e-19 0.021068 0.00018838 4.2495e-05 v CourantNb 3.4415e-08 0.01152 0.00016913 4.9565e-06 v FourierNb 1.2426e-07 0.043728 0.00014775 4.232e-07 v total_pressure -1.4724e+05 3.1809e+05 87396 78672 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0241 0.10674 0.0029307 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.5013e-07 0.049141 0.00031688 5.3797e-06 INSTANT 0.876177000E-01 TIME STEP NUMBER 56375 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283253536E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.835785564E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12598E-01 0.20587E+01 Friction velocity uk : 0.12598E-01 0.20587E+01 Dimensionless distance yplus : 0.12194E-01 0.20243E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.223145194e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29479E+08 1 0.18321E-09 0.27439E+02 0.20042E+04 c Velocity[X] 0.15018E+02 c Velocity[Y] 0.12421E+02 c Velocity[Z] 0.13293E-05 c Pressure 0.23113E-03 447 0.94402E-04 0.19410E-02 0.21201E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -26.222 41.022 5.6135 8.0067 v Velocity[Y] -29.22 30.452 -0.15109 -0.020449 v Velocity[Z] -2.9651 3.0946 2.4264e-06 -5.3896e-08 v ǁVelocityǁ 0.0011924 41.194 8.2518 8.1446 v Pressure -2.505e+05 2.1507e+05 -15853 -23603 v TurbVisc 1.116e-19 0.021085 0.00018846 4.2561e-05 v CourantNb 3.7849e-08 0.011519 0.00016913 4.9566e-06 v FourierNb 1.2426e-07 0.043715 0.00014776 4.2365e-07 v total_pressure -1.4918e+05 3.1639e+05 85472 77722 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0243 0.10676 0.0029309 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.5032e-07 0.049129 0.00031689 5.3802e-06 INSTANT 0.876178000E-01 TIME STEP NUMBER 56376 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283254717E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.836002292E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12302E-01 0.20589E+01 Friction velocity uk : 0.12302E-01 0.20589E+01 Dimensionless distance yplus : 0.11907E-01 0.20245E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.560805862e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29479E+08 1 0.18323E-09 0.27441E+02 0.20041E+04 c Velocity[X] 0.15024E+02 c Velocity[Y] 0.12417E+02 c Velocity[Z] 0.13270E-05 c Pressure 0.23220E-03 130 0.80418E-04 0.19490E-02 0.25907E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -26.239 41.037 5.6135 8.0067 v Velocity[Y] -29.231 30.463 -0.15112 -0.020547 v Velocity[Z] -2.9656 3.0947 2.4257e-06 -5.3896e-08 v ǁVelocityǁ 0.0011633 41.21 8.2534 8.1448 v Pressure -2.5253e+05 2.1328e+05 -17866 -24927 v TurbVisc 1.3854e-19 0.021103 0.00018853 4.2626e-05 v CourantNb 4.1028e-08 0.011518 0.00016913 4.9567e-06 v FourierNb 1.2426e-07 0.043702 0.00014777 4.241e-07 v total_pressure -1.512e+05 3.1461e+05 83459 76398 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0245 0.10678 0.0029311 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.505e-07 0.049116 0.0003169 5.3808e-06 INSTANT 0.876179000E-01 TIME STEP NUMBER 56377 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283255871E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.836203914E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12073E-01 0.20591E+01 Friction velocity uk : 0.12073E-01 0.20591E+01 Dimensionless distance yplus : 0.11686E-01 0.20246E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.858022896e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29479E+08 1 0.18326E-09 0.27458E+02 0.20047E+04 c Velocity[X] 0.15031E+02 c Velocity[Y] 0.12427E+02 c Velocity[Z] 0.13331E-05 c Pressure 0.23099E-03 10 0.59770E-04 0.19378E-02 0.20162E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -26.255 41.052 5.6135 8.0067 v Velocity[Y] -29.242 30.475 -0.15114 -0.020646 v Velocity[Z] -2.966 3.0949 2.4251e-06 -5.3896e-08 v ǁVelocityǁ 0.00090105 41.225 8.255 8.145 v Pressure -2.5445e+05 2.116e+05 -19845 -25993 v TurbVisc 1.7195e-19 0.02112 0.00018861 4.2692e-05 v CourantNb 4.4447e-08 0.011518 0.00016914 4.9567e-06 v FourierNb 1.2426e-07 0.043688 0.00014777 4.2455e-07 v total_pressure -1.5313e+05 3.1292e+05 81480 75332 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0246 0.10679 0.0029313 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.5069e-07 0.049103 0.00031691 5.3813e-06 INSTANT 0.876180000E-01 TIME STEP NUMBER 56378 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283256817E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.836394736E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12142E-01 0.20592E+01 Friction velocity uk : 0.12142E-01 0.20592E+01 Dimensionless distance yplus : 0.11752E-01 0.20248E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -2.155250710e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29479E+08 1 0.18328E-09 0.27470E+02 0.20050E+04 c Velocity[X] 0.15042E+02 c Velocity[Y] 0.12428E+02 c Velocity[Z] 0.13257E-05 c Pressure 0.23226E-03 483 0.76585E-04 0.19475E-02 0.24946E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -26.272 41.067 5.6134 8.0068 v Velocity[Y] -29.254 30.486 -0.15117 -0.020744 v Velocity[Z] -2.9664 3.0951 2.4245e-06 -5.3896e-08 v ǁVelocityǁ 0.00082363 41.24 8.2567 8.1452 v Pressure -2.5656e+05 2.0973e+05 -21826 -27218 v TurbVisc 1.7709e-19 0.021137 0.00018868 4.2758e-05 v CourantNb 4.7725e-08 0.011517 0.00016914 4.9568e-06 v FourierNb 1.2426e-07 0.043675 0.00014778 4.25e-07 v total_pressure -1.5523e+05 3.1106e+05 79499 74107 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0248 0.10681 0.0029315 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.5087e-07 0.04909 0.00031692 5.3818e-06 INSTANT 0.876181000E-01 TIME STEP NUMBER 56379 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283257610E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.836572568E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12022E-01 0.20594E+01 Friction velocity uk : 0.12022E-01 0.20594E+01 Dimensionless distance yplus : 0.11636E-01 0.20250E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -2.442983669e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29480E+08 1 0.18331E-09 0.27485E+02 0.20055E+04 c Velocity[X] 0.15049E+02 c Velocity[Y] 0.12436E+02 c Velocity[Z] 0.13164E-05 c Pressure 0.23287E-03 66 0.82037E-04 0.19516E-02 0.25573E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -26.288 41.082 5.6134 8.0068 v Velocity[Y] -29.265 30.501 -0.1512 -0.020844 v Velocity[Z] -2.9668 3.0953 2.4239e-06 -5.3896e-08 v ǁVelocityǁ 0.0011279 41.255 8.2582 8.1453 v Pressure -2.5858e+05 2.0795e+05 -23875 -28517 v TurbVisc 1.0258e-19 0.021154 0.00018875 4.2823e-05 v CourantNb 5.0759e-08 0.011516 0.00016914 4.9569e-06 v FourierNb 1.2426e-07 0.043662 0.00014779 4.2544e-07 v total_pressure -1.5726e+05 3.0928e+05 77450 72808 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.025 0.10683 0.0029317 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.5106e-07 0.049077 0.00031693 5.3823e-06 INSTANT 0.876182000E-01 TIME STEP NUMBER 56380 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283258333E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.836746322E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12250E-01 0.20596E+01 Friction velocity uk : 0.12250E-01 0.20596E+01 Dimensionless distance yplus : 0.11892E-01 0.20252E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -2.572682096e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29480E+08 1 0.18334E-09 0.27498E+02 0.20059E+04 c Velocity[X] 0.15058E+02 c Velocity[Y] 0.12440E+02 c Velocity[Z] 0.13122E-05 c Pressure 0.23358E-03 197 0.95452E-04 0.19566E-02 0.21581E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -26.305 41.097 5.6134 8.0068 v Velocity[Y] -29.276 30.516 -0.15123 -0.020942 v Velocity[Z] -2.9673 3.0955 2.4233e-06 -5.3896e-08 v ǁVelocityǁ 0.0015454 41.27 8.2598 8.1455 v Pressure -2.6062e+05 2.0615e+05 -25858 -29554 v TurbVisc 1.415e-19 0.021172 0.00018883 4.2889e-05 v CourantNb 5.4983e-08 0.011516 0.00016915 4.9569e-06 v FourierNb 1.2426e-07 0.043649 0.0001478 4.259e-07 v total_pressure -1.593e+05 3.0747e+05 75467 71771 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0252 0.10684 0.0029318 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.5124e-07 0.049064 0.00031694 5.3828e-06 INSTANT 0.876183000E-01 TIME STEP NUMBER 56381 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283258682E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.836910972E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.89708E-02 0.20597E+01 Friction velocity uk : 0.89708E-02 0.20597E+01 Dimensionless distance yplus : 0.87087E-02 0.20253E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -2.746381487e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29480E+08 1 0.18336E-09 0.27500E+02 0.20059E+04 c Velocity[X] 0.15066E+02 c Velocity[Y] 0.12435E+02 c Velocity[Z] 0.13093E-05 c Pressure 0.23416E-03 124 0.81086E-04 0.19604E-02 0.24277E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -26.322 41.112 5.6134 8.0068 v Velocity[Y] -29.287 30.532 -0.15126 -0.021041 v Velocity[Z] -2.9677 3.0957 2.4227e-06 -5.3896e-08 v ǁVelocityǁ 0.0012182 41.285 8.2614 8.1457 v Pressure -2.6266e+05 2.0435e+05 -27887 -30862 v TurbVisc 1.5719e-19 0.021189 0.0001889 4.2955e-05 v CourantNb 5.8327e-08 0.011515 0.00016915 4.957e-06 v FourierNb 1.2426e-07 0.043635 0.0001478 4.2635e-07 v total_pressure -1.6134e+05 3.0568e+05 73438 70463 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0253 0.10686 0.002932 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.5143e-07 0.049051 0.00031695 5.3833e-06 INSTANT 0.876184000E-01 TIME STEP NUMBER 56382 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283258996E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.837062210E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.28011E-02 0.20599E+01 Friction velocity uk : 0.28011E-02 0.20599E+01 Dimensionless distance yplus : 0.27193E-02 0.20255E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -2.902098452e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29480E+08 1 0.18338E-09 0.27518E+02 0.20064E+04 c Velocity[X] 0.15073E+02 c Velocity[Y] 0.12445E+02 c Velocity[Z] 0.13135E-05 c Pressure 0.23233E-03 10 0.60292E-04 0.19442E-02 0.19408E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -26.338 41.126 5.6134 8.0068 v Velocity[Y] -29.298 30.547 -0.15129 -0.021143 v Velocity[Z] -2.9681 3.0958 2.4221e-06 -5.3896e-08 v ǁVelocityǁ 0.00098883 41.3 8.263 8.1459 v Pressure -2.6462e+05 2.0263e+05 -29888 -31946 v TurbVisc 1.6226e-19 0.021206 0.00018898 4.3021e-05 v CourantNb 6.1893e-08 0.011514 0.00016915 4.957e-06 v FourierNb 1.2426e-07 0.043622 0.00014781 4.268e-07 v total_pressure -1.6329e+05 3.0396e+05 71437 69379 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0255 0.10688 0.0029321 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.5161e-07 0.049038 0.00031696 5.3838e-06 INSTANT 0.876185000E-01 TIME STEP NUMBER 56383 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283259094E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.837201663E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.28486E-02 0.20601E+01 Friction velocity uk : 0.28486E-02 0.20601E+01 Dimensionless distance yplus : 0.27654E-02 0.20256E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -3.075613562e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29480E+08 1 0.18341E-09 0.27531E+02 0.20068E+04 c Velocity[X] 0.15086E+02 c Velocity[Y] 0.12445E+02 c Velocity[Z] 0.13069E-05 c Pressure 0.23305E-03 170 0.77107E-04 0.19492E-02 0.23591E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -26.354 41.141 5.6134 8.0068 v Velocity[Y] -29.309 30.562 -0.15132 -0.021242 v Velocity[Z] -2.9685 3.096 2.4214e-06 -5.3896e-08 v ǁVelocityǁ 0.0010343 41.315 8.2646 8.1461 v Pressure -2.6675e+05 2.0075e+05 -31884 -33167 v TurbVisc 1.6446e-19 0.021223 0.00018905 4.3087e-05 v CourantNb 6.5082e-08 0.011513 0.00016916 4.9571e-06 v FourierNb 1.2426e-07 0.043608 0.00014782 4.2725e-07 v total_pressure -1.6542e+05 3.0207e+05 69441 68158 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0256 0.10689 0.0029322 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.518e-07 0.049025 0.00031697 5.3843e-06 INSTANT 0.876186000E-01 TIME STEP NUMBER 56384 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283259050E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.837327509E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.34628E-02 0.20602E+01 Friction velocity uk : 0.34628E-02 0.20602E+01 Dimensionless distance yplus : 0.33616E-02 0.20258E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -3.146680052e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29480E+08 1 0.18343E-09 0.27547E+02 0.20073E+04 c Velocity[X] 0.15095E+02 c Velocity[Y] 0.12452E+02 c Velocity[Z] 0.12986E-05 c Pressure 0.23309E-03 93 0.82542E-04 0.19486E-02 0.24375E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -26.371 41.156 5.6133 8.0068 v Velocity[Y] -29.32 30.577 -0.15135 -0.021344 v Velocity[Z] -2.969 3.0962 2.4208e-06 -5.3896e-08 v ǁVelocityǁ 0.00091179 41.33 8.2662 8.1462 v Pressure -2.688e+05 1.9893e+05 -33946 -34477 v TurbVisc 1.6982e-19 0.02124 0.00018912 4.3153e-05 v CourantNb 6.8379e-08 0.011513 0.00016916 4.9571e-06 v FourierNb 1.2426e-07 0.043595 0.00014783 4.277e-07 v total_pressure -1.6747e+05 3.0026e+05 67379 66848 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0258 0.10691 0.0029323 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.5199e-07 0.049011 0.00031699 5.3848e-06 INSTANT 0.876187000E-01 TIME STEP NUMBER 56385 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283258931E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.837449229E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.77704E-02 0.20604E+01 Friction velocity uk : 0.77704E-02 0.20604E+01 Dimensionless distance yplus : 0.75434E-02 0.20259E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -3.166537981e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29480E+08 1 0.18345E-09 0.27561E+02 0.20077E+04 c Velocity[X] 0.15105E+02 c Velocity[Y] 0.12456E+02 c Velocity[Z] 0.12933E-05 c Pressure 0.23325E-03 197 0.95875E-04 0.19489E-02 0.20503E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -26.387 41.17 5.6133 8.0068 v Velocity[Y] -29.331 30.592 -0.15138 -0.021443 v Velocity[Z] -2.9694 3.0964 2.4202e-06 -5.3896e-08 v ǁVelocityǁ 0.00094621 41.344 8.2678 8.1464 v Pressure -2.7085e+05 1.9712e+05 -35935 -35520 v TurbVisc 1.7376e-19 0.021258 0.0001892 4.3219e-05 v CourantNb 7.2827e-08 0.011512 0.00016916 4.9572e-06 v FourierNb 1.2426e-07 0.043581 0.00014783 4.2815e-07 v total_pressure -1.6953e+05 2.9844e+05 65390 65805 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0259 0.10692 0.0029325 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.5217e-07 0.048998 0.000317 5.3853e-06 INSTANT 0.876188000E-01 TIME STEP NUMBER 56386 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283258435E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.837561655E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.84062E-02 0.20605E+01 Friction velocity uk : 0.84062E-02 0.20605E+01 Dimensionless distance yplus : 0.80900E-02 0.20261E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -3.186564439e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29480E+08 1 0.18347E-09 0.27564E+02 0.20078E+04 c Velocity[X] 0.15114E+02 c Velocity[Y] 0.12451E+02 c Velocity[Z] 0.12890E-05 c Pressure 0.23326E-03 123 0.81549E-04 0.19480E-02 0.22928E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -26.403 41.185 5.6133 8.0067 v Velocity[Y] -29.342 30.608 -0.15141 -0.021545 v Velocity[Z] -2.9698 3.0966 2.4196e-06 -5.3896e-08 v ǁVelocityǁ 0.0011173 41.359 8.2694 8.1466 v Pressure -2.729e+05 1.9531e+05 -37963 -36828 v TurbVisc 1.7492e-19 0.021275 0.00018927 4.3286e-05 v CourantNb 7.6275e-08 0.011511 0.00016917 4.9572e-06 v FourierNb 1.2426e-07 0.043567 0.00014784 4.2861e-07 v total_pressure -1.7157e+05 2.9664e+05 63362 64497 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0261 0.10694 0.0029326 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.5236e-07 0.048984 0.00031701 5.3858e-06 INSTANT 0.876189000E-01 TIME STEP NUMBER 56387 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283257906E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.837660274E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.56244E-02 0.20607E+01 Friction velocity uk : 0.56244E-02 0.20607E+01 Dimensionless distance yplus : 0.54128E-02 0.20262E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -3.206182922e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29480E+08 1 0.18350E-09 0.27584E+02 0.20084E+04 c Velocity[X] 0.15122E+02 c Velocity[Y] 0.12461E+02 c Velocity[Z] 0.12933E-05 c Pressure 0.23082E-03 10 0.60452E-04 0.19267E-02 0.18248E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -26.42 41.199 5.6133 8.0067 v Velocity[Y] -29.353 30.623 -0.15145 -0.021648 v Velocity[Z] -2.9702 3.0967 2.419e-06 -5.3896e-08 v ǁVelocityǁ 0.0015153 41.374 8.271 8.1467 v Pressure -2.7486e+05 1.9358e+05 -39959 -37908 v TurbVisc 1.7073e-19 0.021292 0.00018934 4.3352e-05 v CourantNb 7.9958e-08 0.01151 0.00016917 4.9573e-06 v FourierNb 1.2426e-07 0.043554 0.00014785 4.2906e-07 v total_pressure -1.7353e+05 2.9491e+05 61366 63417 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0262 0.10696 0.0029327 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.5255e-07 0.048971 0.00031702 5.3863e-06 INSTANT 0.876190000E-01 TIME STEP NUMBER 56388 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283257162E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.837746836E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.62400E-02 0.20608E+01 Friction velocity uk : 0.62400E-02 0.20608E+01 Dimensionless distance yplus : 0.60053E-02 0.20264E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -3.219517406e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29480E+08 1 0.18352E-09 0.27598E+02 0.20088E+04 c Velocity[X] 0.15137E+02 c Velocity[Y] 0.12461E+02 c Velocity[Z] 0.12857E-05 c Pressure 0.23099E-03 447 0.77397E-04 0.19271E-02 0.22161E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -26.436 41.214 5.6132 8.0067 v Velocity[Y] -29.363 30.638 -0.15148 -0.021749 v Velocity[Z] -2.9707 3.0969 2.4184e-06 -5.3896e-08 v ǁVelocityǁ 0.0019061 41.388 8.2726 8.1469 v Pressure -2.7698e+05 1.917e+05 -41944 -39124 v TurbVisc 1.6516e-19 0.021309 0.00018941 4.3418e-05 v CourantNb 8.3345e-08 0.01151 0.00016917 4.9573e-06 v FourierNb 1.2426e-07 0.04354 0.00014786 4.2952e-07 v total_pressure -1.7566e+05 2.9303e+05 59381 62201 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0264 0.10698 0.0029328 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.5274e-07 0.048958 0.00031703 5.3868e-06 INSTANT 0.876191000E-01 TIME STEP NUMBER 56389 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283256274E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.837819602E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10660E-01 0.20610E+01 Friction velocity uk : 0.10660E-01 0.20610E+01 Dimensionless distance yplus : 0.10252E-01 0.20265E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -3.206475455e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29480E+08 1 0.18354E-09 0.27614E+02 0.20093E+04 c Velocity[X] 0.15146E+02 c Velocity[Y] 0.12468E+02 c Velocity[Z] 0.12784E-05 c Pressure 0.23046E-03 97 0.82965E-04 0.19218E-02 0.22873E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -26.452 41.228 5.6132 8.0067 v Velocity[Y] -29.374 30.653 -0.15151 -0.021853 v Velocity[Z] -2.9711 3.0971 2.4178e-06 -5.3896e-08 v ǁVelocityǁ 0.0015383 41.403 8.2742 8.147 v Pressure -2.7903e+05 1.899e+05 -43990 -40427 v TurbVisc 1.3862e-19 0.021326 0.00018949 4.3485e-05 v CourantNb 8.6776e-08 0.011509 0.00016918 4.9574e-06 v FourierNb 1.2426e-07 0.043526 0.00014786 4.2997e-07 v total_pressure -1.777e+05 2.9122e+05 57335 60898 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0265 0.10699 0.0029329 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.5293e-07 0.048944 0.00031704 5.3873e-06 INSTANT 0.876192000E-01 TIME STEP NUMBER 56390 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283255315E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.837888427E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.73203E-02 0.20611E+01 Friction velocity uk : 0.73203E-02 0.20611E+01 Dimensionless distance yplus : 0.70402E-02 0.20267E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -3.098513656e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29480E+08 1 0.18356E-09 0.27629E+02 0.20098E+04 c Velocity[X] 0.15158E+02 c Velocity[Y] 0.12472E+02 c Velocity[Z] 0.12725E-05 c Pressure 0.23007E-03 457 0.96360E-04 0.19176E-02 0.19118E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -26.468 41.242 5.6132 8.0067 v Velocity[Y] -29.385 30.667 -0.15154 -0.021954 v Velocity[Z] -2.9715 3.0973 2.4172e-06 -5.3897e-08 v ǁVelocityǁ 0.0013405 41.418 8.2758 8.1472 v Pressure -2.8106e+05 1.881e+05 -45956 -41454 v TurbVisc 1.5193e-19 0.021343 0.00018956 4.3551e-05 v CourantNb 9.1366e-08 0.011508 0.00016918 4.9574e-06 v FourierNb 1.2426e-07 0.043513 0.00014787 4.3043e-07 v total_pressure -1.7974e+05 2.8942e+05 55369 59871 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0267 0.10701 0.002933 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.5312e-07 0.04893 0.00031705 5.3878e-06 INSTANT 0.876193000E-01 TIME STEP NUMBER 56391 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283253980E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.837947754E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10010E-02 0.20612E+01 Friction velocity uk : 0.10010E-02 0.20612E+01 Dimensionless distance yplus : 0.96268E-03 0.20268E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -3.012534583e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29480E+08 1 0.18358E-09 0.27633E+02 0.20099E+04 c Velocity[X] 0.15168E+02 c Velocity[Y] 0.12465E+02 c Velocity[Z] 0.12705E-05 c Pressure 0.22952E-03 160 0.82038E-04 0.19121E-02 0.21405E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -26.484 41.256 5.6132 8.0066 v Velocity[Y] -29.396 30.682 -0.15158 -0.022057 v Velocity[Z] -2.9719 3.0974 2.4165e-06 -5.3897e-08 v ǁVelocityǁ 0.001381 41.432 8.2774 8.1473 v Pressure -2.8309e+05 1.8631e+05 -47959 -42750 v TurbVisc 1.6075e-19 0.021361 0.00018963 4.3618e-05 v CourantNb 9.5007e-08 0.011507 0.00016918 4.9575e-06 v FourierNb 1.2426e-07 0.043499 0.00014788 4.3088e-07 v total_pressure -1.8177e+05 2.8763e+05 53366 58575 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0268 0.10702 0.002933 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.5331e-07 0.048917 0.00031706 5.3883e-06 INSTANT 0.876194000E-01 TIME STEP NUMBER 56392 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283252615E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.837993370E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.55218E-02 0.20614E+01 Friction velocity uk : 0.55218E-02 0.20614E+01 Dimensionless distance yplus : 0.53111E-02 0.20269E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -2.938993530e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29479E+08 1 0.18360E-09 0.27654E+02 0.20105E+04 c Velocity[X] 0.15178E+02 c Velocity[Y] 0.12476E+02 c Velocity[Z] 0.12738E-05 c Pressure 0.22647E-03 10 0.60557E-04 0.18857E-02 0.16842E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -26.5 41.271 5.6131 8.0066 v Velocity[Y] -29.407 30.697 -0.15161 -0.022162 v Velocity[Z] -2.9723 3.0976 2.4159e-06 -5.3897e-08 v ǁVelocityǁ 0.0016407 41.446 8.279 8.1475 v Pressure -2.8502e+05 1.8461e+05 -49920 -43807 v TurbVisc 1.6708e-19 0.021378 0.0001897 4.3685e-05 v CourantNb 9.8913e-08 0.011507 0.00016919 4.9575e-06 v FourierNb 1.2426e-07 0.043485 0.00014789 4.3134e-07 v total_pressure -1.837e+05 2.8593e+05 51405 57518 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0269 0.10704 0.0029334 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.535e-07 0.048903 0.00031707 5.3888e-06 INSTANT 0.876195000E-01 TIME STEP NUMBER 56393 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283251045E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.838027072E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.81875E-02 0.20616E+01 Friction velocity uk : 0.81875E-02 0.20616E+01 Dimensionless distance yplus : 0.78751E-02 0.20271E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -2.829610151e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29479E+08 1 0.18362E-09 0.27668E+02 0.20110E+04 c Velocity[X] 0.15193E+02 c Velocity[Y] 0.12475E+02 c Velocity[Z] 0.12625E-05 c Pressure 0.22610E-03 443 0.77812E-04 0.18817E-02 0.20658E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -26.516 41.285 5.6131 8.0066 v Velocity[Y] -29.418 30.712 -0.15164 -0.022265 v Velocity[Z] -2.9728 3.0978 2.4153e-06 -5.3897e-08 v ǁVelocityǁ 0.0020636 41.461 8.2805 8.1476 v Pressure -2.8712e+05 1.8275e+05 -51869 -45010 v TurbVisc 1.6166e-19 0.021395 0.00018977 4.3751e-05 v CourantNb 1.0266e-07 0.011506 0.00016919 4.9575e-06 v FourierNb 1.2426e-07 0.043471 0.00014789 4.3179e-07 v total_pressure -1.8579e+05 2.8408e+05 49456 56315 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0271 0.10706 0.0029336 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.5369e-07 0.04889 0.00031708 5.3893e-06 INSTANT 0.876196000E-01 TIME STEP NUMBER 56394 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283249321E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.838047105E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.69162E-02 0.20617E+01 Friction velocity uk : 0.69162E-02 0.20617E+01 Dimensionless distance yplus : 0.66523E-02 0.20272E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -2.843799355e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29479E+08 1 0.18364E-09 0.27686E+02 0.20116E+04 c Velocity[X] 0.15204E+02 c Velocity[Y] 0.12482E+02 c Velocity[Z] 0.12549E-05 c Pressure 0.22503E-03 70 0.83398E-04 0.18718E-02 0.21118E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -26.532 41.299 5.6131 8.0065 v Velocity[Y] -29.429 30.727 -0.15168 -0.022371 v Velocity[Z] -2.9732 3.098 2.4147e-06 -5.3897e-08 v ǁVelocityǁ 0.0022094 41.475 8.2821 8.1478 v Pressure -2.8912e+05 1.8099e+05 -53870 -46282 v TurbVisc 1.6526e-19 0.021412 0.00018985 4.3818e-05 v CourantNb 1.0628e-07 0.011505 0.00016919 4.9576e-06 v FourierNb 1.2426e-07 0.043457 0.0001479 4.3225e-07 v total_pressure -1.8779e+05 2.8231e+05 47455 55043 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0272 0.10708 0.0029339 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.5388e-07 0.048876 0.00031709 5.3898e-06 INSTANT 0.876197000E-01 TIME STEP NUMBER 56395 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283247539E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.838063131E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.48463E-02 0.20618E+01 Friction velocity uk : 0.48463E-02 0.20618E+01 Dimensionless distance yplus : 0.46614E-02 0.20274E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -2.647082287e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29479E+08 1 0.18366E-09 0.27702E+02 0.20121E+04 c Velocity[X] 0.15216E+02 c Velocity[Y] 0.12486E+02 c Velocity[Z] 0.12500E-05 c Pressure 0.22410E-03 238 0.97093E-04 0.18632E-02 0.17993E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -26.548 41.313 5.613 8.0065 v Velocity[Y] -29.44 30.741 -0.15171 -0.022473 v Velocity[Z] -2.9736 3.0982 2.4141e-06 -5.3897e-08 v ǁVelocityǁ 0.0021718 41.489 8.2837 8.1479 v Pressure -2.9113e+05 1.7922e+05 -55791 -47307 v TurbVisc 1.6e-19 0.021429 0.00018992 4.3885e-05 v CourantNb 1.1109e-07 0.011504 0.0001692 4.9576e-06 v FourierNb 1.2426e-07 0.043443 0.00014791 4.3271e-07 v total_pressure -1.898e+05 2.8055e+05 45534 54018 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0274 0.1071 0.0029342 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.5407e-07 0.048862 0.00031711 5.3903e-06 INSTANT 0.876198000E-01 TIME STEP NUMBER 56396 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283245376E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.838069770E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.54229E-02 0.20620E+01 Friction velocity uk : 0.54229E-02 0.20620E+01 Dimensionless distance yplus : 0.52160E-02 0.20275E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -2.537770238e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29479E+08 1 0.18367E-09 0.27707E+02 0.20122E+04 c Velocity[X] 0.15228E+02 c Velocity[Y] 0.12479E+02 c Velocity[Z] 0.12432E-05 c Pressure 0.22305E-03 123 0.82499E-04 0.18535E-02 0.19045E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -26.563 41.327 5.613 8.0064 v Velocity[Y] -29.45 30.756 -0.15175 -0.022579 v Velocity[Z] -2.974 3.0983 2.4135e-06 -5.3897e-08 v ǁVelocityǁ 0.0022604 41.503 8.2853 8.148 v Pressure -2.931e+05 1.775e+05 -57733 -48527 v TurbVisc 1.5744e-19 0.021446 0.00018999 4.3952e-05 v CourantNb 1.1521e-07 0.011504 0.0001692 4.9577e-06 v FourierNb 1.2426e-07 0.043429 0.00014792 4.3316e-07 v total_pressure -1.9178e+05 2.7882e+05 43592 52798 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0275 0.10712 0.0029345 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.5426e-07 0.048849 0.00031712 5.3908e-06 INSTANT 0.876199000E-01 TIME STEP NUMBER 56397 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283243204E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.838063002E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.35160E-02 0.20621E+01 Friction velocity uk : 0.35160E-02 0.20621E+01 Dimensionless distance yplus : 0.33818E-02 0.20277E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -2.427952782e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29479E+08 1 0.18369E-09 0.27728E+02 0.20129E+04 c Velocity[X] 0.15238E+02 c Velocity[Y] 0.12489E+02 c Velocity[Z] 0.12477E-05 c Pressure 0.21934E-03 10 0.60822E-04 0.18218E-02 0.15652E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -26.579 41.34 5.613 8.0064 v Velocity[Y] -29.461 30.77 -0.15179 -0.022685 v Velocity[Z] -2.9745 3.0985 2.4129e-06 -5.3897e-08 v ǁVelocityǁ 0.0020284 41.517 8.2869 8.1482 v Pressure -2.95e+05 1.7585e+05 -59637 -49570 v TurbVisc 1.5558e-19 0.021463 0.00019006 4.4019e-05 v CourantNb 1.1897e-07 0.011503 0.0001692 4.9577e-06 v FourierNb 1.2426e-07 0.043415 0.00014793 4.3362e-07 v total_pressure -1.9367e+05 2.7718e+05 41688 51755 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0277 0.10714 0.0029348 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.5446e-07 0.048835 0.00031713 5.3913e-06 INSTANT 0.876200000E-01 TIME STEP NUMBER 56398 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283240827E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.838044726E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.38948E-02 0.20623E+01 Friction velocity uk : 0.38948E-02 0.20623E+01 Dimensionless distance yplus : 0.38666E-02 0.20278E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -2.307354570e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29479E+08 1 0.18371E-09 0.27743E+02 0.20134E+04 c Velocity[X] 0.15255E+02 c Velocity[Y] 0.12488E+02 c Velocity[Z] 0.12401E-05 c Pressure 0.21849E-03 206 0.78465E-04 0.18139E-02 0.19041E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -26.595 41.354 5.613 8.0063 v Velocity[Y] -29.472 30.785 -0.15182 -0.02279 v Velocity[Z] -2.9749 3.0987 2.4123e-06 -5.3897e-08 v ǁVelocityǁ 0.0018557 41.531 8.2885 8.1483 v Pressure -2.9704e+05 1.7406e+05 -61523 -50741 v TurbVisc 1.5083e-19 0.02148 0.00019013 4.4086e-05 v CourantNb 1.1708e-07 0.011502 0.0001692 4.9577e-06 v FourierNb 1.2426e-07 0.043402 0.00014793 4.3408e-07 v total_pressure -1.9571e+05 2.7538e+05 39802 50584 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0278 0.10716 0.0029352 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.5465e-07 0.048821 0.00031714 5.3918e-06 INSTANT 0.876201000E-01 TIME STEP NUMBER 56399 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283238296E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.838012705E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.40834E-02 0.20624E+01 Friction velocity uk : 0.40834E-02 0.20624E+01 Dimensionless distance yplus : 0.39709E-02 0.20279E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -2.379670888e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29478E+08 1 0.18372E-09 0.27762E+02 0.20139E+04 c Velocity[X] 0.15267E+02 c Velocity[Y] 0.12494E+02 c Velocity[Z] 0.12292E-05 c Pressure 0.21689E-03 69 0.83976E-04 0.17998E-02 0.18738E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -26.61 41.368 5.6129 8.0063 v Velocity[Y] -29.483 30.799 -0.15186 -0.022897 v Velocity[Z] -2.9753 3.0989 2.4117e-06 -5.3897e-08 v ǁVelocityǁ 0.0018268 41.545 8.2901 8.1484 v Pressure -2.9896e+05 1.7239e+05 -63440 -51922 v TurbVisc 1.3342e-19 0.021497 0.0001902 4.4153e-05 v CourantNb 1.1619e-07 0.011501 0.00016921 4.9578e-06 v FourierNb 1.2426e-07 0.043387 0.00014794 4.3454e-07 v total_pressure -1.9763e+05 2.7371e+05 37885 49403 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0279 0.10718 0.0029357 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.5484e-07 0.048807 0.00031715 5.3923e-06 INSTANT 0.876202000E-01 TIME STEP NUMBER 56400 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283235750E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.837976853E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.56652E-02 0.20626E+01 Friction velocity uk : 0.56652E-02 0.20626E+01 Dimensionless distance yplus : 0.55092E-02 0.20281E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -2.194720646e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29478E+08 1 0.18374E-09 0.27779E+02 0.20145E+04 c Velocity[X] 0.15280E+02 c Velocity[Y] 0.12499E+02 c Velocity[Z] 0.12227E-05 c Pressure 0.21545E-03 192 0.97458E-04 0.17869E-02 0.17104E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -26.626 41.381 5.6129 8.0062 v Velocity[Y] -29.493 30.814 -0.1519 -0.023002 v Velocity[Z] -2.9757 3.0991 2.4111e-06 -5.3897e-08 v ǁVelocityǁ 0.001957 41.559 8.2916 8.1485 v Pressure -3.0092e+05 1.7067e+05 -65306 -52977 v TurbVisc 1.5128e-19 0.021514 0.00019027 4.422e-05 v CourantNb 1.1474e-07 0.011501 0.00016921 4.9578e-06 v FourierNb 1.2426e-07 0.043373 0.00014795 4.35e-07 v total_pressure -1.996e+05 2.7199e+05 36019 48348 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0281 0.10721 0.0029361 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.5504e-07 0.048793 0.00031716 5.3928e-06 INSTANT 0.876203000E-01 TIME STEP NUMBER 56401 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283232765E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.837931275E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.30119E-02 0.20627E+01 Friction velocity uk : 0.30119E-02 0.20627E+01 Dimensionless distance yplus : 0.29289E-02 0.20282E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -2.116110881e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29478E+08 1 0.18375E-09 0.27784E+02 0.20146E+04 c Velocity[X] 0.15293E+02 c Velocity[Y] 0.12491E+02 c Velocity[Z] 0.12180E-05 c Pressure 0.21393E-03 386 0.82789E-04 0.17734E-02 0.17105E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -26.642 41.395 5.6129 8.0061 v Velocity[Y] -29.504 30.828 -0.15194 -0.023109 v Velocity[Z] -2.9761 3.0992 2.4104e-06 -5.3897e-08 v ǁVelocityǁ 0.0017522 41.573 8.2932 8.1487 v Pressure -3.028e+05 1.6905e+05 -67157 -54130 v TurbVisc 1.624e-19 0.021532 0.00019034 4.4287e-05 v CourantNb 1.1329e-07 0.0115 0.00016922 4.9578e-06 v FourierNb 1.2426e-07 0.043359 0.00014796 4.3546e-07 v total_pressure -2.0147e+05 2.7037e+05 34168 47195 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0282 0.10723 0.0029365 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.5523e-07 0.048779 0.00031717 5.3933e-06 INSTANT 0.876204000E-01 TIME STEP NUMBER 56402 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283229821E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.837873648E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.84988E-02 0.20628E+01 Friction velocity uk : 0.84988E-02 0.20628E+01 Dimensionless distance yplus : 0.81791E-02 0.20284E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -2.084251437e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29478E+08 1 0.18377E-09 0.27806E+02 0.20153E+04 c Velocity[X] 0.15303E+02 c Velocity[Y] 0.12502E+02 c Velocity[Z] 0.12214E-05 c Pressure 0.20959E-03 10 0.61079E-04 0.17366E-02 0.14521E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -26.657 41.408 5.6128 8.0061 v Velocity[Y] -29.515 30.842 -0.15198 -0.023218 v Velocity[Z] -2.9766 3.0994 2.4098e-06 -5.3897e-08 v ǁVelocityǁ 0.0014267 41.586 8.2948 8.1488 v Pressure -3.0463e+05 1.675e+05 -68987 -55153 v TurbVisc 1.4101e-19 0.021549 0.00019041 4.4355e-05 v CourantNb 1.1195e-07 0.011499 0.00016922 4.9579e-06 v FourierNb 1.2427e-07 0.043345 0.00014797 4.3592e-07 v total_pressure -2.033e+05 2.6883e+05 32338 46172 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0284 0.10726 0.002937 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.5543e-07 0.048765 0.00031718 5.3938e-06 INSTANT 0.876205000E-01 TIME STEP NUMBER 56403 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283226660E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.837804203E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.81295E-02 0.20630E+01 Friction velocity uk : 0.81295E-02 0.20630E+01 Dimensionless distance yplus : 0.78237E-02 0.20285E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -2.041748224e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29478E+08 1 0.18378E-09 0.27822E+02 0.20158E+04 c Velocity[X] 0.15321E+02 c Velocity[Y] 0.12500E+02 c Velocity[Z] 0.12144E-05 c Pressure 0.20833E-03 447 0.78930E-04 0.17253E-02 0.16940E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -26.672 41.422 5.6128 8.006 v Velocity[Y] -29.525 30.857 -0.15202 -0.023324 v Velocity[Z] -2.977 3.0996 2.4092e-06 -5.3897e-08 v ǁVelocityǁ 0.001282 41.6 8.2964 8.1489 v Pressure -3.0656e+05 1.6584e+05 -70772 -56238 v TurbVisc 1.3913e-19 0.021566 0.00019048 4.4422e-05 v CourantNb 1.1022e-07 0.011498 0.00016922 4.9579e-06 v FourierNb 1.2427e-07 0.043331 0.00014797 4.3638e-07 v total_pressure -2.0524e+05 2.6717e+05 30553 45087 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0285 0.10728 0.0029374 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.5562e-07 0.048752 0.0003172 5.3943e-06 INSTANT 0.876206000E-01 TIME STEP NUMBER 56404 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283223364E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.837722441E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10403E-01 0.20631E+01 Friction velocity uk : 0.10403E-01 0.20631E+01 Dimensionless distance yplus : 0.10012E-01 0.20286E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -2.164022649e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29477E+08 1 0.18380E-09 0.27841E+02 0.20165E+04 c Velocity[X] 0.15334E+02 c Velocity[Y] 0.12506E+02 c Velocity[Z] 0.12043E-05 c Pressure 0.20624E-03 113 0.84404E-04 0.17072E-02 0.17643E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -26.688 41.435 5.6128 8.0059 v Velocity[Y] -29.536 30.871 -0.15206 -0.023434 v Velocity[Z] -2.9774 3.0998 2.4086e-06 -5.3897e-08 v ǁVelocityǁ 0.0013621 41.613 8.298 8.149 v Pressure -3.084e+05 1.6428e+05 -72608 -57418 v TurbVisc 1.4561e-19 0.021583 0.00019055 4.449e-05 v CourantNb 1.0946e-07 0.011497 0.00016923 4.9579e-06 v FourierNb 1.2427e-07 0.043317 0.00014798 4.3684e-07 v total_pressure -2.0708e+05 2.656e+05 28717 43907 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0286 0.10731 0.0029379 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.5582e-07 0.048737 0.00031721 5.3948e-06 INSTANT 0.876207000E-01 TIME STEP NUMBER 56405 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283220031E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.837636296E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13021E-01 0.20633E+01 Friction velocity uk : 0.13021E-01 0.20633E+01 Dimensionless distance yplus : 0.12531E-01 0.20288E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -2.087994776e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29477E+08 1 0.18381E-09 0.27858E+02 0.20170E+04 c Velocity[X] 0.15348E+02 c Velocity[Y] 0.12510E+02 c Velocity[Z] 0.11960E-05 c Pressure 0.20439E-03 231 0.98233E-04 0.16910E-02 0.14953E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -26.703 41.448 5.6127 8.0059 v Velocity[Y] -29.546 30.885 -0.1521 -0.02354 v Velocity[Z] -2.9778 3.0999 2.408e-06 -5.3897e-08 v ǁVelocityǁ 0.0016438 41.627 8.2995 8.1491 v Pressure -3.1022e+05 1.6273e+05 -74351 -58347 v TurbVisc 1.3663e-19 0.0216 0.00019062 4.4557e-05 v CourantNb 1.081e-07 0.011497 0.00016923 4.9579e-06 v FourierNb 1.2427e-07 0.043302 0.00014799 4.373e-07 v total_pressure -2.089e+05 2.6406e+05 26974 42978 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0288 0.10733 0.0029384 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.5601e-07 0.048723 0.00031722 5.3952e-06 INSTANT 0.876208000E-01 TIME STEP NUMBER 56406 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283216327E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.837541906E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15296E-01 0.20634E+01 Friction velocity uk : 0.15296E-01 0.20634E+01 Dimensionless distance yplus : 0.14720E-01 0.20289E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -2.138846759e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29477E+08 1 0.18382E-09 0.27863E+02 0.20171E+04 c Velocity[X] 0.15361E+02 c Velocity[Y] 0.12502E+02 c Velocity[Z] 0.11920E-05 c Pressure 0.20242E-03 467 0.83207E-04 0.16739E-02 0.15943E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -26.719 41.462 5.6127 8.0058 v Velocity[Y] -29.557 30.899 -0.15214 -0.023649 v Velocity[Z] -2.9783 3.1001 2.4074e-06 -5.3897e-08 v ǁVelocityǁ 0.0015036 41.64 8.3011 8.1492 v Pressure -3.1202e+05 1.6121e+05 -76117 -59486 v TurbVisc 1.3918e-19 0.021617 0.00019068 4.4625e-05 v CourantNb 1.0672e-07 0.011496 0.00016923 4.958e-06 v FourierNb 1.2427e-07 0.043288 0.000148 4.3776e-07 v total_pressure -2.107e+05 2.6253e+05 25208 41839 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0289 0.10736 0.0029388 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.5621e-07 0.048709 0.00031723 5.3957e-06 INSTANT 0.876209000E-01 TIME STEP NUMBER 56407 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283212633E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.837434394E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.17355E-01 0.20635E+01 Friction velocity uk : 0.17355E-01 0.20635E+01 Dimensionless distance yplus : 0.16702E-01 0.20290E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -2.196016133e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29476E+08 1 0.18383E-09 0.27885E+02 0.20179E+04 c Velocity[X] 0.15373E+02 c Velocity[Y] 0.12513E+02 c Velocity[Z] 0.12099E-05 c Pressure 0.19748E-03 9 0.60540E-04 0.16323E-02 0.11905E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -26.734 41.475 5.6126 8.0057 v Velocity[Y] -29.567 30.913 -0.15218 -0.02376 v Velocity[Z] -2.9787 3.1003 2.4068e-06 -5.3897e-08 v ǁVelocityǁ 0.0010013 41.654 8.3027 8.1493 v Pressure -3.1369e+05 1.5983e+05 -77808 -60365 v TurbVisc 1.3984e-19 0.021634 0.00019075 4.4692e-05 v CourantNb 1.0532e-07 0.011495 0.00016924 4.958e-06 v FourierNb 1.2427e-07 0.043273 0.00014801 4.3822e-07 v total_pressure -2.1237e+05 2.6115e+05 23517 40960 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.029 0.10738 0.0029392 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.5641e-07 0.048695 0.00031724 5.3962e-06 INSTANT 0.876210000E-01 TIME STEP NUMBER 56408 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283208783E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.837317162E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19465E-01 0.20636E+01 Friction velocity uk : 0.19465E-01 0.20636E+01 Dimensionless distance yplus : 0.18733E-01 0.20291E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -2.328621313e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29476E+08 1 0.18385E-09 0.27902E+02 0.20184E+04 c Velocity[X] 0.15391E+02 c Velocity[Y] 0.12511E+02 c Velocity[Z] 0.11947E-05 c Pressure 0.19584E-03 270 0.78778E-04 0.16179E-02 0.15876E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -26.749 41.488 5.6126 8.0056 v Velocity[Y] -29.578 30.927 -0.15222 -0.023868 v Velocity[Z] -2.9791 3.1005 2.4062e-06 -5.3897e-08 v ǁVelocityǁ 0.00061078 41.667 8.3042 8.1494 v Pressure -3.1553e+05 1.5826e+05 -79497 -61449 v TurbVisc 1.2474e-19 0.021651 0.00019082 4.476e-05 v CourantNb 1.0329e-07 0.011494 0.00016924 4.958e-06 v FourierNb 1.2427e-07 0.043259 0.00014802 4.3869e-07 v total_pressure -2.142e+05 2.5959e+05 21828 39876 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0291 0.10741 0.0029396 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.566e-07 0.048681 0.00031725 5.3967e-06 INSTANT 0.876211000E-01 TIME STEP NUMBER 56409 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283204749E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.837187498E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.18889E-01 0.20638E+01 Friction velocity uk : 0.18889E-01 0.20638E+01 Dimensionless distance yplus : 0.18314E-01 0.20293E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -2.482411224e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29476E+08 1 0.18386E-09 0.27921E+02 0.20190E+04 c Velocity[X] 0.15404E+02 c Velocity[Y] 0.12516E+02 c Velocity[Z] 0.11803E-05 c Pressure 0.19328E-03 64 0.84206E-04 0.15960E-02 0.15363E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -26.764 41.501 5.6126 8.0055 v Velocity[Y] -29.588 30.941 -0.15226 -0.023979 v Velocity[Z] -2.9795 3.1006 2.4056e-06 -5.3898e-08 v ǁVelocityǁ 0.00060619 41.68 8.3058 8.1495 v Pressure -3.1722e+05 1.5684e+05 -81200 -62509 v TurbVisc 1.3454e-19 0.021668 0.00019089 4.4828e-05 v CourantNb 1.0267e-07 0.011494 0.00016924 4.958e-06 v FourierNb 1.2427e-07 0.043244 0.00014802 4.3915e-07 v total_pressure -2.159e+05 2.5817e+05 20125 38816 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0293 0.10743 0.0029401 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.568e-07 0.048666 0.00031727 5.3972e-06 INSTANT 0.876212000E-01 TIME STEP NUMBER 56410 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283200740E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.837051573E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.17763E-01 0.20639E+01 Friction velocity uk : 0.17763E-01 0.20639E+01 Dimensionless distance yplus : 0.17222E-01 0.20294E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -2.591016652e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29475E+08 1 0.18387E-09 0.27938E+02 0.20196E+04 c Velocity[X] 0.15418E+02 c Velocity[Y] 0.12521E+02 c Velocity[Z] 0.11702E-05 c Pressure 0.19103E-03 333 0.97941E-04 0.15767E-02 0.14135E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -26.779 41.513 5.6125 8.0054 v Velocity[Y] -29.598 30.955 -0.1523 -0.024088 v Velocity[Z] -2.9799 3.1008 2.405e-06 -5.3898e-08 v ǁVelocityǁ 0.00052596 41.693 8.3074 8.1496 v Pressure -3.1896e+05 1.5538e+05 -82844 -63452 v TurbVisc 1.3272e-19 0.021685 0.00019096 4.4896e-05 v CourantNb 1.011e-07 0.011493 0.00016925 4.958e-06 v FourierNb 1.2427e-07 0.04323 0.00014803 4.3961e-07 v total_pressure -2.1763e+05 2.567e+05 18481 37873 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0294 0.10745 0.0029404 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.57e-07 0.048652 0.00031728 5.3977e-06 INSTANT 0.876213000E-01 TIME STEP NUMBER 56411 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283196315E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.836908351E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.16741E-01 0.20640E+01 Friction velocity uk : 0.16741E-01 0.20640E+01 Dimensionless distance yplus : 0.16231E-01 0.20295E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -2.763798302e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29475E+08 1 0.18388E-09 0.27944E+02 0.20197E+04 c Velocity[X] 0.15431E+02 c Velocity[Y] 0.12513E+02 c Velocity[Z] 0.11645E-05 c Pressure 0.18874E-03 164 0.83146E-04 0.15571E-02 0.13570E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -26.794 41.526 5.6125 8.0054 v Velocity[Y] -29.609 30.968 -0.15235 -0.024199 v Velocity[Z] -2.9804 3.101 2.4044e-06 -5.3898e-08 v ǁVelocityǁ 0.00051474 41.706 8.3089 8.1497 v Pressure -3.206e+05 1.5401e+05 -84457 -64458 v TurbVisc 1.3566e-19 0.021702 0.00019102 4.4963e-05 v CourantNb 9.9512e-08 0.011492 0.00016925 4.9581e-06 v FourierNb 1.2427e-07 0.043215 0.00014804 4.4008e-07 v total_pressure -2.1928e+05 2.5533e+05 16868 36867 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0295 0.10748 0.0029408 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.572e-07 0.048637 0.00031729 5.3981e-06 INSTANT 0.876214000E-01 TIME STEP NUMBER 56412 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283191945E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.836754641E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15900E-01 0.20641E+01 Friction velocity uk : 0.15900E-01 0.20641E+01 Dimensionless distance yplus : 0.15416E-01 0.20296E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -2.943402978e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29475E+08 1 0.18389E-09 0.27966E+02 0.20205E+04 c Velocity[X] 0.15443E+02 c Velocity[Y] 0.12523E+02 c Velocity[Z] 0.11782E-05 c Pressure 0.18321E-03 9 0.60232E-04 0.15107E-02 0.11090E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -26.809 41.539 5.6124 8.0053 v Velocity[Y] -29.619 30.982 -0.15239 -0.024311 v Velocity[Z] -2.9808 3.1012 2.4038e-06 -5.3898e-08 v ǁVelocityǁ 0.00092823 41.719 8.3105 8.1498 v Pressure -3.2214e+05 1.5275e+05 -86036 -65318 v TurbVisc 1.2934e-19 0.021719 0.00019109 4.5031e-05 v CourantNb 9.7765e-08 0.011491 0.00016925 4.9581e-06 v FourierNb 1.2427e-07 0.0432 0.00014805 4.4054e-07 v total_pressure -2.2082e+05 2.5407e+05 15289 36007 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0296 0.1075 0.0029412 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.574e-07 0.048623 0.0003173 5.3986e-06 INSTANT 0.876215000E-01 TIME STEP NUMBER 56413 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283187417E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.836590283E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10673E-01 0.20642E+01 Friction velocity uk : 0.10673E-01 0.20642E+01 Dimensionless distance yplus : 0.95094E-02 0.20297E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -3.232573558e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29474E+08 1 0.18390E-09 0.27982E+02 0.20210E+04 c Velocity[X] 0.15462E+02 c Velocity[Y] 0.12521E+02 c Velocity[Z] 0.11638E-05 c Pressure 0.18131E-03 173 0.78797E-04 0.14944E-02 0.13907E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -26.824 41.552 5.6124 8.0052 v Velocity[Y] -29.629 30.996 -0.15243 -0.024421 v Velocity[Z] -2.9812 3.1014 2.4032e-06 -5.3898e-08 v ǁVelocityǁ 0.0014315 41.732 8.3121 8.1499 v Pressure -3.2383e+05 1.5133e+05 -87580 -66294 v TurbVisc 1.1932e-19 0.021736 0.00019116 4.5099e-05 v CourantNb 9.5404e-08 0.01149 0.00016926 4.9581e-06 v FourierNb 1.2427e-07 0.043186 0.00014806 4.4101e-07 v total_pressure -2.225e+05 2.5265e+05 13745 35031 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0297 0.10752 0.0029415 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.576e-07 0.048608 0.00031731 5.3991e-06 INSTANT 0.876216000E-01 TIME STEP NUMBER 56414 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283182729E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.836415829E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.73776E-02 0.20643E+01 Friction velocity uk : 0.73776E-02 0.20643E+01 Dimensionless distance yplus : 0.71882E-02 0.20298E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -3.474377054e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29474E+08 1 0.18391E-09 0.28001E+02 0.20216E+04 c Velocity[X] 0.15475E+02 c Velocity[Y] 0.12526E+02 c Velocity[Z] 0.11511E-05 c Pressure 0.17840E-03 50 0.84229E-04 0.14697E-02 0.13669E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -26.839 41.564 5.6123 8.0051 v Velocity[Y] -29.639 31.009 -0.15248 -0.024534 v Velocity[Z] -2.9816 3.1015 2.4025e-06 -5.3898e-08 v ǁVelocityǁ 0.001779 41.745 8.3136 8.1499 v Pressure -3.2537e+05 1.5006e+05 -89136 -67265 v TurbVisc 1.2627e-19 0.021753 0.00019122 4.5167e-05 v CourantNb 9.4289e-08 0.01149 0.00016926 4.9581e-06 v FourierNb 1.2427e-07 0.043171 0.00014807 4.4147e-07 v total_pressure -2.2404e+05 2.5138e+05 12189 34060 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0298 0.10754 0.0029419 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.578e-07 0.048593 0.00031733 5.3996e-06 INSTANT 0.876217000E-01 TIME STEP NUMBER 56415 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283178076E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.836235242E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.28196E-02 0.20644E+01 Friction velocity uk : 0.28196E-02 0.20644E+01 Dimensionless distance yplus : 0.27472E-02 0.20299E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -3.722952534e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29474E+08 1 0.18392E-09 0.28019E+02 0.20222E+04 c Velocity[X] 0.15489E+02 c Velocity[Y] 0.12530E+02 c Velocity[Z] 0.11465E-05 c Pressure 0.17585E-03 232 0.98138E-04 0.14480E-02 0.12708E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -26.854 41.577 5.6123 8.005 v Velocity[Y] -29.649 31.023 -0.15252 -0.024645 v Velocity[Z] -2.982 3.1017 2.4019e-06 -5.3898e-08 v ǁVelocityǁ 0.0020087 41.757 8.3152 8.15 v Pressure -3.2696e+05 1.4873e+05 -90634 -68133 v TurbVisc 1.2814e-19 0.02177 0.00019129 4.5235e-05 v CourantNb 9.2218e-08 0.011489 0.00016926 4.9581e-06 v FourierNb 1.2427e-07 0.043156 0.00014807 4.4194e-07 v total_pressure -2.2563e+05 2.5006e+05 10691 33192 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0299 0.10756 0.0029422 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.58e-07 0.048579 0.00031734 5.4001e-06 INSTANT 0.876218000E-01 TIME STEP NUMBER 56416 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283173020E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.836047850E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.34178E-02 0.20645E+01 Friction velocity uk : 0.34178E-02 0.20645E+01 Dimensionless distance yplus : 0.33301E-02 0.20300E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -4.015142284e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29473E+08 1 0.18393E-09 0.28023E+02 0.20223E+04 c Velocity[X] 0.15503E+02 c Velocity[Y] 0.12521E+02 c Velocity[Z] 0.11364E-05 c Pressure 0.17329E-03 422 0.83309E-04 0.14262E-02 0.11587E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -26.869 41.589 5.6122 8.0049 v Velocity[Y] -29.659 31.037 -0.15256 -0.024757 v Velocity[Z] -2.9825 3.1019 2.4013e-06 -5.3898e-08 v ǁVelocityǁ 0.0023379 41.77 8.3167 8.1501 v Pressure -3.2842e+05 1.4755e+05 -92092 -69021 v TurbVisc 1.2605e-19 0.021787 0.00019136 4.5303e-05 v CourantNb 9.0045e-08 0.011488 0.00016927 4.9581e-06 v FourierNb 1.2427e-07 0.043141 0.00014808 4.424e-07 v total_pressure -2.2709e+05 2.4887e+05 9232.5 32304 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.03 0.10758 0.0029425 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.582e-07 0.048564 0.00031735 5.4005e-06 INSTANT 0.876219000E-01 TIME STEP NUMBER 56417 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283168048E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.835850611E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10049E-01 0.20646E+01 Friction velocity uk : 0.10049E-01 0.20646E+01 Dimensionless distance yplus : 0.97914E-02 0.20301E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -4.322228410e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29473E+08 1 0.18394E-09 0.28045E+02 0.20230E+04 c Velocity[X] 0.15514E+02 c Velocity[Y] 0.12532E+02 c Velocity[Z] 0.11421E-05 c Pressure 0.16717E-03 9 0.60007E-04 0.13752E-02 0.10252E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -26.883 41.602 5.6122 8.0048 v Velocity[Y] -29.67 31.05 -0.15261 -0.024872 v Velocity[Z] -2.9829 3.1021 2.4007e-06 -5.3898e-08 v ǁVelocityǁ 0.0023925 41.783 8.3183 8.1502 v Pressure -3.2984e+05 1.464e+05 -93530 -69843 v TurbVisc 1.2373e-19 0.021804 0.00019142 4.5372e-05 v CourantNb 8.7729e-08 0.011487 0.00016927 4.9581e-06 v FourierNb 1.2427e-07 0.043126 0.00014809 4.4287e-07 v total_pressure -2.2851e+05 2.4772e+05 7795 31482 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0301 0.10761 0.0029428 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.5841e-07 0.048548 0.00031736 5.401e-06 INSTANT 0.876220000E-01 TIME STEP NUMBER 56418 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283162919E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.835643605E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.14996E-01 0.20646E+01 Friction velocity uk : 0.14996E-01 0.20646E+01 Dimensionless distance yplus : 0.14611E-01 0.20301E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -4.739087780e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29472E+08 1 0.18395E-09 0.28061E+02 0.20235E+04 c Velocity[X] 0.15532E+02 c Velocity[Y] 0.12529E+02 c Velocity[Z] 0.11335E-05 c Pressure 0.16511E-03 168 0.79077E-04 0.13576E-02 0.12238E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -26.898 41.614 5.6121 8.0046 v Velocity[Y] -29.68 31.064 -0.15265 -0.024983 v Velocity[Z] -2.9833 3.1022 2.4001e-06 -5.3898e-08 v ǁVelocityǁ 0.002109 41.795 8.3198 8.1503 v Pressure -3.3136e+05 1.4514e+05 -94911 -70716 v TurbVisc 1.105e-19 0.021821 0.00019149 4.544e-05 v CourantNb 8.486e-08 0.011486 0.00016927 4.9581e-06 v FourierNb 1.2427e-07 0.04311 0.0001481 4.4334e-07 v total_pressure -2.3004e+05 2.4646e+05 6413.7 30609 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0301 0.10763 0.0029431 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.5861e-07 0.048533 0.00031737 5.4015e-06 INSTANT 0.876221000E-01 TIME STEP NUMBER 56419 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283157632E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.835427739E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19227E-01 0.20647E+01 Friction velocity uk : 0.19227E-01 0.20647E+01 Dimensionless distance yplus : 0.18568E-01 0.20302E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -5.016502067e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29472E+08 1 0.18395E-09 0.28080E+02 0.20241E+04 c Velocity[X] 0.15546E+02 c Velocity[Y] 0.12534E+02 c Velocity[Z] 0.11240E-05 c Pressure 0.16194E-03 63 0.84468E-04 0.13310E-02 0.12053E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -26.913 41.626 5.612 8.0045 v Velocity[Y] -29.69 31.077 -0.15269 -0.025098 v Velocity[Z] -2.9837 3.1024 2.3995e-06 -5.3898e-08 v ǁVelocityǁ 0.0019332 41.808 8.3213 8.1503 v Pressure -3.3273e+05 1.4404e+05 -96302 -71584 v TurbVisc 1.2158e-19 0.021838 0.00019155 4.5508e-05 v CourantNb 8.2843e-08 0.011486 0.00016927 4.9582e-06 v FourierNb 1.2427e-07 0.043095 0.00014811 4.438e-07 v total_pressure -2.314e+05 2.4536e+05 5023.4 29741 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0302 0.10765 0.0029435 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.5881e-07 0.048518 0.00031739 5.402e-06 INSTANT 0.876222000E-01 TIME STEP NUMBER 56420 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283152409E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.835206271E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.18667E-01 0.20648E+01 Friction velocity uk : 0.18667E-01 0.20648E+01 Dimensionless distance yplus : 0.17957E-01 0.20303E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -5.383312376e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29471E+08 1 0.18396E-09 0.28097E+02 0.20247E+04 c Velocity[X] 0.15559E+02 c Velocity[Y] 0.12538E+02 c Velocity[Z] 0.11141E-05 c Pressure 0.15920E-03 311 0.98577E-04 0.13078E-02 0.11258E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -26.927 41.638 5.612 8.0044 v Velocity[Y] -29.699 31.09 -0.15273 -0.025211 v Velocity[Z] -2.9841 3.1026 2.3989e-06 -5.3898e-08 v ǁVelocityǁ 0.0018835 41.82 8.3229 8.1504 v Pressure -3.3414e+05 1.4289e+05 -97633 -72343 v TurbVisc 1.1776e-19 0.021855 0.00019162 4.5577e-05 v CourantNb 8.0023e-08 0.011485 0.00016928 4.9582e-06 v FourierNb 1.2427e-07 0.043079 0.00014812 4.4427e-07 v total_pressure -2.3281e+05 2.4421e+05 3691.8 28982 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0303 0.10767 0.0029437 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.5902e-07 0.048502 0.0003174 5.4024e-06 INSTANT 0.876223000E-01 TIME STEP NUMBER 56421 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283146810E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.834978733E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.17967E-01 0.20648E+01 Friction velocity uk : 0.17967E-01 0.20648E+01 Dimensionless distance yplus : 0.17284E-01 0.20303E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -5.761201705e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29471E+08 1 0.18397E-09 0.28101E+02 0.20248E+04 c Velocity[X] 0.15572E+02 c Velocity[Y] 0.12529E+02 c Velocity[Z] 0.11106E-05 c Pressure 0.15648E-03 81 0.83507E-04 0.12848E-02 0.10786E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -26.942 41.65 5.6119 8.0043 v Velocity[Y] -29.709 31.104 -0.15278 -0.025325 v Velocity[Z] -2.9845 3.1028 2.3983e-06 -5.3898e-08 v ǁVelocityǁ 0.0019646 41.832 8.3244 8.1505 v Pressure -3.3546e+05 1.4184e+05 -98935 -73198 v TurbVisc 1.1228e-19 0.021872 0.00019168 4.5645e-05 v CourantNb 7.7011e-08 0.011484 0.00016928 4.9582e-06 v FourierNb 1.2427e-07 0.043064 0.00014813 4.4474e-07 v total_pressure -2.3413e+05 2.4316e+05 2389.8 28127 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0303 0.10769 0.002944 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.5922e-07 0.048487 0.00031741 5.4029e-06 INSTANT 0.876224000E-01 TIME STEP NUMBER 56422 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283141268E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.834742678E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.17208E-01 0.20649E+01 Friction velocity uk : 0.17208E-01 0.20649E+01 Dimensionless distance yplus : 0.16554E-01 0.20303E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -6.125627725e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29471E+08 1 0.18398E-09 0.28122E+02 0.20255E+04 c Velocity[X] 0.15584E+02 c Velocity[Y] 0.12539E+02 c Velocity[Z] 0.11133E-05 c Pressure 0.14981E-03 9 0.58904E-04 0.12295E-02 0.81384E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -26.956 41.663 5.6118 8.0042 v Velocity[Y] -29.719 31.117 -0.15282 -0.025441 v Velocity[Z] -2.985 3.1029 2.3977e-06 -5.3898e-08 v ǁVelocityǁ 0.002152 41.845 8.326 8.1505 v Pressure -3.3668e+05 1.4088e+05 -1.0018e+05 -73867 v TurbVisc 1.1777e-19 0.021889 0.00019175 4.5714e-05 v CourantNb 7.4503e-08 0.011483 0.00016928 4.9582e-06 v FourierNb 1.2427e-07 0.043048 0.00014814 4.4521e-07 v total_pressure -2.3536e+05 2.422e+05 1141.5 27458 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0303 0.1077 0.0029442 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.5943e-07 0.048471 0.00031742 5.4034e-06 INSTANT 0.876225000E-01 TIME STEP NUMBER 56423 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283135644E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.834498129E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.16266E-01 0.20649E+01 Friction velocity uk : 0.16266E-01 0.20649E+01 Dimensionless distance yplus : 0.15648E-01 0.20303E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -6.633805089e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29470E+08 1 0.18398E-09 0.28137E+02 0.20259E+04 c Velocity[X] 0.15600E+02 c Velocity[Y] 0.12537E+02 c Velocity[Z] 0.11039E-05 c Pressure 0.14769E-03 184 0.79370E-04 0.12116E-02 0.10734E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -26.97 41.675 5.6117 8.0041 v Velocity[Y] -29.729 31.13 -0.15286 -0.025555 v Velocity[Z] -2.9854 3.1031 2.3971e-06 -5.3898e-08 v ǁVelocityǁ 0.0024241 41.857 8.3275 8.1506 v Pressure -3.3802e+05 1.3981e+05 -1.0139e+05 -74644 v TurbVisc 1.0276e-19 0.021906 0.00019181 4.5782e-05 v CourantNb 7.4799e-08 0.011483 0.00016929 4.9582e-06 v FourierNb 1.2427e-07 0.043032 0.00014815 4.4567e-07 v total_pressure -2.3669e+05 2.4113e+05 -68.953 26681 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0303 0.10772 0.0029444 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.5963e-07 0.048455 0.00031743 5.4038e-06 INSTANT 0.876226000E-01 TIME STEP NUMBER 56424 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283129830E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.834245658E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11944E-01 0.20649E+01 Friction velocity uk : 0.11944E-01 0.20649E+01 Dimensionless distance yplus : 0.11664E-01 0.20304E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -6.895940242e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29470E+08 1 0.18399E-09 0.28155E+02 0.20265E+04 c Velocity[X] 0.15614E+02 c Velocity[Y] 0.12541E+02 c Velocity[Z] 0.10972E-05 c Pressure 0.14438E-03 62 0.84804E-04 0.11839E-02 0.10677E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -26.985 41.686 5.6117 8.0039 v Velocity[Y] -29.739 31.143 -0.15291 -0.025672 v Velocity[Z] -2.9858 3.1033 2.3965e-06 -5.3898e-08 v ǁVelocityǁ 0.0027455 41.869 8.329 8.1507 v Pressure -3.3921e+05 1.3887e+05 -1.026e+05 -75411 v TurbVisc 1.1582e-19 0.021923 0.00019188 4.5851e-05 v CourantNb 7.5102e-08 0.011482 0.00016929 4.9582e-06 v FourierNb 1.2427e-07 0.043017 0.00014816 4.4614e-07 v total_pressure -2.3789e+05 2.402e+05 -1277.3 25914 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0304 0.10774 0.0029446 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.5984e-07 0.048439 0.00031745 5.4043e-06 INSTANT 0.876227000E-01 TIME STEP NUMBER 56425 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283124116E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.833987945E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.16567E-02 0.20649E+01 Friction velocity uk : 0.16567E-02 0.20649E+01 Dimensionless distance yplus : 0.16179E-02 0.20304E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -7.321097746e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29469E+08 1 0.18400E-09 0.28171E+02 0.20271E+04 c Velocity[X] 0.15626E+02 c Velocity[Y] 0.12545E+02 c Velocity[Z] 0.10883E-05 c Pressure 0.14158E-03 233 0.99161E-04 0.11603E-02 0.10211E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -26.999 41.698 5.6116 8.0038 v Velocity[Y] -29.749 31.156 -0.15295 -0.025786 v Velocity[Z] -2.9862 3.1035 2.3959e-06 -5.3898e-08 v ǁVelocityǁ 0.0030004 41.881 8.3305 8.1507 v Pressure -3.4046e+05 1.3788e+05 -1.0376e+05 -76092 v TurbVisc 1.1168e-19 0.02194 0.00019194 4.592e-05 v CourantNb 7.5369e-08 0.011481 0.00016929 4.9582e-06 v FourierNb 1.2427e-07 0.043001 0.00014817 4.4661e-07 v total_pressure -2.3914e+05 2.3921e+05 -2432.4 25233 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0304 0.10775 0.0029447 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.6004e-07 0.048423 0.00031746 5.4048e-06 INSTANT 0.876228000E-01 TIME STEP NUMBER 56426 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283118027E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.833724997E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.67211E-02 0.20649E+01 Friction velocity uk : 0.67211E-02 0.20649E+01 Dimensionless distance yplus : 0.65637E-02 0.20304E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -7.722282220e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29469E+08 1 0.18400E-09 0.28174E+02 0.20271E+04 c Velocity[X] 0.15639E+02 c Velocity[Y] 0.12535E+02 c Velocity[Z] 0.10832E-05 c Pressure 0.13886E-03 368 0.84116E-04 0.11376E-02 0.86224E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -27.013 41.71 5.6115 8.0037 v Velocity[Y] -29.758 31.169 -0.15299 -0.025902 v Velocity[Z] -2.9866 3.1036 2.3953e-06 -5.3898e-08 v ǁVelocityǁ 0.0029719 41.893 8.332 8.1508 v Pressure -3.4156e+05 1.3705e+05 -1.0486e+05 -76773 v TurbVisc 1.1118e-19 0.021957 0.000192 4.5988e-05 v CourantNb 7.5674e-08 0.01148 0.00016929 4.9582e-06 v FourierNb 1.2427e-07 0.042984 0.00014818 4.4708e-07 v total_pressure -2.4023e+05 2.3837e+05 -3530.9 24552 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0304 0.10777 0.0029449 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.6025e-07 0.048407 0.00031747 5.4053e-06 INSTANT 0.876229000E-01 TIME STEP NUMBER 56427 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283112055E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.833455008E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11979E-01 0.20649E+01 Friction velocity uk : 0.11979E-01 0.20649E+01 Dimensionless distance yplus : 0.11523E-01 0.20304E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -8.104755099e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29468E+08 1 0.18401E-09 0.28195E+02 0.20278E+04 c Velocity[X] 0.15649E+02 c Velocity[Y] 0.12546E+02 c Velocity[Z] 0.10827E-05 c Pressure 0.13161E-03 9 0.59311E-04 0.10776E-02 0.77414E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -27.027 41.722 5.6114 8.0036 v Velocity[Y] -29.768 31.182 -0.15303 -0.026021 v Velocity[Z] -2.987 3.1038 2.3947e-06 -5.3899e-08 v ǁVelocityǁ 0.0030085 41.905 8.3336 8.1508 v Pressure -3.4268e+05 1.3622e+05 -1.0594e+05 -77420 v TurbVisc 1.0863e-19 0.021973 0.00019207 4.6057e-05 v CourantNb 7.5987e-08 0.011479 0.0001693 4.9582e-06 v FourierNb 1.2427e-07 0.042968 0.00014819 4.4755e-07 v total_pressure -2.4136e+05 2.3755e+05 -4612.9 23905 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0304 0.10778 0.0029451 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.6046e-07 0.048391 0.00031748 5.4057e-06 INSTANT 0.876230000E-01 TIME STEP NUMBER 56428 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283105974E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.833177097E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10295E-01 0.20648E+01 Friction velocity uk : 0.10295E-01 0.20648E+01 Dimensionless distance yplus : 0.99036E-02 0.20303E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -8.604324131e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29468E+08 1 0.18401E-09 0.28208E+02 0.20282E+04 c Velocity[X] 0.15666E+02 c Velocity[Y] 0.12542E+02 c Velocity[Z] 0.10782E-05 c Pressure 0.12970E-03 611 0.80227E-04 0.10615E-02 0.91624E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -27.041 41.734 5.6113 8.0034 v Velocity[Y] -29.777 31.195 -0.15307 -0.026136 v Velocity[Z] -2.9875 3.104 2.3941e-06 -5.3899e-08 v ǁVelocityǁ 0.0031133 41.917 8.3351 8.1509 v Pressure -3.4392e+05 1.3535e+05 -1.0695e+05 -78040 v TurbVisc 9.5043e-20 0.02199 0.00019213 4.6126e-05 v CourantNb 7.6329e-08 0.011479 0.0001693 4.9582e-06 v FourierNb 1.2427e-07 0.042952 0.00014819 4.4802e-07 v total_pressure -2.426e+05 2.3667e+05 -5621.6 23285 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0303 0.1078 0.0029452 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.6067e-07 0.048374 0.00031749 5.4062e-06 INSTANT 0.876231000E-01 TIME STEP NUMBER 56429 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283099745E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.832893225E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.85916E-02 0.20648E+01 Friction velocity uk : 0.85916E-02 0.20648E+01 Dimensionless distance yplus : 0.82650E-02 0.20303E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -8.836582039e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29467E+08 1 0.18402E-09 0.28225E+02 0.20288E+04 c Velocity[X] 0.15677E+02 c Velocity[Y] 0.12549E+02 c Velocity[Z] 0.10712E-05 c Pressure 0.12640E-03 388 0.85822E-04 0.10341E-02 0.10250E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -27.055 41.745 5.6112 8.0033 v Velocity[Y] -29.787 31.208 -0.15311 -0.026255 v Velocity[Z] -2.9879 3.1042 2.3935e-06 -5.3899e-08 v ǁVelocityǁ 0.0032671 41.929 8.3366 8.1509 v Pressure -3.4509e+05 1.3455e+05 -1.0798e+05 -78771 v TurbVisc 1.0526e-19 0.022007 0.00019219 4.6195e-05 v CourantNb 7.6654e-08 0.011478 0.0001693 4.9582e-06 v FourierNb 1.2427e-07 0.042935 0.0001482 4.485e-07 v total_pressure -2.4377e+05 2.3587e+05 -6651.8 22554 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0303 0.10781 0.0029453 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.6088e-07 0.048357 0.00031751 5.4067e-06 INSTANT 0.876232000E-01 TIME STEP NUMBER 56430 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283093588E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.832604483E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.61203E-02 0.20648E+01 Friction velocity uk : 0.61203E-02 0.20648E+01 Dimensionless distance yplus : 0.58877E-02 0.20302E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -9.258955538e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29467E+08 1 0.18403E-09 0.28229E+02 0.20288E+04 c Velocity[X] 0.15689E+02 c Velocity[Y] 0.12540E+02 c Velocity[Z] 0.10644E-05 c Pressure 0.12379E-03 254 0.75129E-04 0.10122E-02 0.61594E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -27.069 41.757 5.6111 8.0032 v Velocity[Y] -29.797 31.221 -0.15315 -0.026373 v Velocity[Z] -2.9883 3.1043 2.3929e-06 -5.3899e-08 v ǁVelocityǁ 0.0032071 41.941 8.3381 8.151 v Pressure -3.4609e+05 1.3387e+05 -1.0889e+05 -79212 v TurbVisc 1.0552e-19 0.022024 0.00019226 4.6264e-05 v CourantNb 7.6954e-08 0.011477 0.0001693 4.9582e-06 v FourierNb 1.2427e-07 0.042919 0.00014821 4.4897e-07 v total_pressure -2.4476e+05 2.352e+05 -7566.6 22113 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0302 0.10783 0.0029453 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.6109e-07 0.048341 0.00031752 5.4071e-06 INSTANT 0.876233000E-01 TIME STEP NUMBER 56431 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283087259E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.832312468E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.21211E-02 0.20647E+01 Friction velocity uk : 0.21211E-02 0.20647E+01 Dimensionless distance yplus : 0.20404E-02 0.20302E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -9.603720732e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29466E+08 1 0.18403E-09 0.28247E+02 0.20294E+04 c Velocity[X] 0.15699E+02 c Velocity[Y] 0.12548E+02 c Velocity[Z] 0.10602E-05 c Pressure 0.11695E-03 9 0.55975E-04 0.95592E-03 0.58006E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -27.083 41.769 5.611 8.003 v Velocity[Y] -29.806 31.234 -0.15319 -0.02649 v Velocity[Z] -2.9887 3.1045 2.3923e-06 -5.3899e-08 v ǁVelocityǁ 0.0031381 41.953 8.3396 8.151 v Pressure -3.4711e+05 1.3318e+05 -1.098e+05 -79715 v TurbVisc 1.0242e-19 0.022041 0.00019232 4.6333e-05 v CourantNb 7.8208e-08 0.011476 0.00016931 4.9582e-06 v FourierNb 1.2427e-07 0.042902 0.00014822 4.4944e-07 v total_pressure -2.4579e+05 2.345e+05 -8473.7 21610 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0302 0.10783 0.0029453 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.613e-07 0.048324 0.00031753 5.4076e-06 INSTANT 0.876234000E-01 TIME STEP NUMBER 56432 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283080773E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.832012049E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.26073E-02 0.20646E+01 Friction velocity uk : 0.26073E-02 0.20646E+01 Dimensionless distance yplus : 0.25082E-02 0.20301E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.002436385e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29466E+08 1 0.18404E-09 0.28256E+02 0.20297E+04 c Velocity[X] 0.15713E+02 c Velocity[Y] 0.12543E+02 c Velocity[Z] 0.10535E-05 c Pressure 0.11499E-03 92 0.97207E-04 0.93940E-03 0.81891E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -27.097 41.78 5.6109 8.0029 v Velocity[Y] -29.815 31.247 -0.15323 -0.026608 v Velocity[Z] -2.9891 3.1047 2.3917e-06 -5.3899e-08 v ǁVelocityǁ 0.0030818 41.964 8.3411 8.1511 v Pressure -3.4825e+05 1.3242e+05 -1.1069e+05 -80447 v TurbVisc 9.2759e-20 0.022058 0.00019238 4.6403e-05 v CourantNb 8.3912e-08 0.011476 0.00016931 4.9581e-06 v FourierNb 1.2427e-07 0.042885 0.00014823 4.4991e-07 v total_pressure -2.4692e+05 2.3375e+05 -9360.3 20878 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0301 0.10784 0.0029453 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.6151e-07 0.048306 0.00031754 5.4081e-06 INSTANT 0.876235000E-01 TIME STEP NUMBER 56433 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283074283E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.831705814E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.25482E-02 0.20646E+01 Friction velocity uk : 0.25482E-02 0.20646E+01 Dimensionless distance yplus : 0.24514E-02 0.20300E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.027002010e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29465E+08 1 0.18404E-09 0.28267E+02 0.20300E+04 c Velocity[X] 0.15723E+02 c Velocity[Y] 0.12543E+02 c Velocity[Z] 0.10467E-05 c Pressure 0.11088E-03 328 0.81012E-04 0.90541E-03 0.55851E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -27.111 41.792 5.6108 8.0028 v Velocity[Y] -29.825 31.26 -0.15327 -0.026727 v Velocity[Z] -2.9896 3.1049 2.3911e-06 -5.3899e-08 v ǁVelocityǁ 0.0030204 41.976 8.3426 8.1511 v Pressure -3.4917e+05 1.3182e+05 -1.1152e+05 -80955 v TurbVisc 5.3971e-20 0.022075 0.00019244 4.6472e-05 v CourantNb 8.6097e-08 0.011475 0.00016931 4.9581e-06 v FourierNb 1.2427e-07 0.042868 0.00014824 4.5039e-07 v total_pressure -2.4785e+05 2.3315e+05 -10193 20370 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.03 0.10786 0.0029454 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.6172e-07 0.048289 0.00031756 5.4085e-06 INSTANT 0.876236000E-01 TIME STEP NUMBER 56434 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283067792E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.831395120E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11859E-02 0.20645E+01 Friction velocity uk : 0.11859E-02 0.20645E+01 Dimensionless distance yplus : 0.11467E-02 0.20300E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.067510788e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29465E+08 1 0.18405E-09 0.28284E+02 0.20306E+04 c Velocity[X] 0.15733E+02 c Velocity[Y] 0.12551E+02 c Velocity[Z] 0.10479E-05 c Pressure 0.10629E-03 17 0.52945E-04 0.86757E-03 0.51265E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -27.124 41.803 5.6107 8.0026 v Velocity[Y] -29.834 31.273 -0.15331 -0.026848 v Velocity[Z] -2.99 3.105 2.3905e-06 -5.3899e-08 v ǁVelocityǁ 0.0029639 41.988 8.3441 8.1512 v Pressure -3.5004e+05 1.3129e+05 -1.1231e+05 -81383 v TurbVisc 4.2631e-20 0.022092 0.0001925 4.6541e-05 v CourantNb 8.2196e-08 0.011474 0.00016931 4.9581e-06 v FourierNb 1.2427e-07 0.042851 0.00014825 4.5086e-07 v total_pressure -2.4872e+05 2.3262e+05 -10983 19942 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.03 0.10787 0.0029455 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.6193e-07 0.048272 0.00031757 5.409e-06 INSTANT 0.876237000E-01 TIME STEP NUMBER 56435 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283061281E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.831081639E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.81832E-02 0.20644E+01 Friction velocity uk : 0.81832E-02 0.20644E+01 Dimensionless distance yplus : 0.78722E-02 0.20298E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.090044999e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29464E+08 1 0.18405E-09 0.28292E+02 0.20308E+04 c Velocity[X] 0.15746E+02 c Velocity[Y] 0.12546E+02 c Velocity[Z] 0.10449E-05 c Pressure 0.10479E-03 44 0.98074E-04 0.85491E-03 0.55526E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -27.138 41.814 5.6105 8.0025 v Velocity[Y] -29.843 31.285 -0.15335 -0.026968 v Velocity[Z] -2.9904 3.1052 2.3898e-06 -5.3899e-08 v ǁVelocityǁ 0.0029151 41.999 8.3456 8.1512 v Pressure -3.5098e+05 1.3072e+05 -1.1302e+05 -81868 v TurbVisc 3.9942e-20 0.022109 0.00019257 4.6611e-05 v CourantNb 7.7539e-08 0.011473 0.00016932 4.9581e-06 v FourierNb 1.2427e-07 0.042834 0.00014826 4.5134e-07 v total_pressure -2.4965e+05 2.3205e+05 -11697 19457 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0298 0.10788 0.0029457 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.6214e-07 0.048254 0.00031758 5.4095e-06 INSTANT 0.876238000E-01 TIME STEP NUMBER 56436 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283054656E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.830762860E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10491E-01 0.20643E+01 Friction velocity uk : 0.10491E-01 0.20643E+01 Dimensionless distance yplus : 0.10092E-01 0.20298E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.110781729e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29463E+08 1 0.18406E-09 0.28302E+02 0.20312E+04 c Velocity[X] 0.15757E+02 c Velocity[Y] 0.12546E+02 c Velocity[Z] 0.10349E-05 c Pressure 0.10084E-03 26 0.83552E-04 0.82238E-03 0.48475E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -27.151 41.826 5.6104 8.0024 v Velocity[Y] -29.853 31.298 -0.15339 -0.027088 v Velocity[Z] -2.9908 3.1054 2.3892e-06 -5.3899e-08 v ǁVelocityǁ 0.00287 42.011 8.3471 8.1513 v Pressure -3.518e+05 1.3018e+05 -1.1374e+05 -82310 v TurbVisc 5.0444e-20 0.022126 0.00019263 4.668e-05 v CourantNb 7.4292e-08 0.011473 0.00016932 4.9581e-06 v FourierNb 1.2427e-07 0.042817 0.00014827 4.5181e-07 v total_pressure -2.5047e+05 2.315e+05 -12411 19015 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0298 0.1079 0.0029458 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.6236e-07 0.048237 0.00031759 5.4099e-06 INSTANT 0.876239000E-01 TIME STEP NUMBER 56437 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283047981E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.830437939E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.33898E-02 0.20642E+01 Friction velocity uk : 0.33898E-02 0.20642E+01 Dimensionless distance yplus : 0.33513E-02 0.20297E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.140162126e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29463E+08 1 0.18406E-09 0.28320E+02 0.20317E+04 c Velocity[X] 0.15766E+02 c Velocity[Y] 0.12553E+02 c Velocity[Z] 0.10356E-05 c Pressure 0.96359E-04 12 0.56595E-04 0.78544E-03 0.42653E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -27.165 41.837 5.6103 8.0022 v Velocity[Y] -29.862 31.311 -0.15342 -0.027206 v Velocity[Z] -2.9912 3.1055 2.3886e-06 -5.3899e-08 v ǁVelocityǁ 0.0028317 42.023 8.3485 8.1513 v Pressure -3.5252e+05 1.2971e+05 -1.1439e+05 -82652 v TurbVisc 6.0528e-20 0.022142 0.00019269 4.675e-05 v CourantNb 7.0029e-08 0.011472 0.00016932 4.9581e-06 v FourierNb 1.2427e-07 0.042799 0.00014829 4.5229e-07 v total_pressure -2.5119e+05 2.3103e+05 -13063 18673 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0297 0.1079 0.0029459 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.6257e-07 0.048219 0.00031761 5.4104e-06 INSTANT 0.876240000E-01 TIME STEP NUMBER 56438 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283041234E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.830110951E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.99452E-02 0.20640E+01 Friction velocity uk : 0.99452E-02 0.20640E+01 Dimensionless distance yplus : 0.97641E-02 0.20295E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.172259152e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29462E+08 1 0.18407E-09 0.28331E+02 0.20321E+04 c Velocity[X] 0.15778E+02 c Velocity[Y] 0.12553E+02 c Velocity[Z] 0.10291E-05 c Pressure 0.95557E-04 45 0.77407E-04 0.77856E-03 0.82690E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -27.178 41.848 5.6102 8.0021 v Velocity[Y] -29.871 31.323 -0.15346 -0.027329 v Velocity[Z] -2.9916 3.1057 2.388e-06 -5.3899e-08 v ǁVelocityǁ 0.0028012 42.034 8.35 8.1514 v Pressure -3.5339e+05 1.2924e+05 -1.1502e+05 -83264 v TurbVisc 4.7819e-20 0.022159 0.00019275 4.682e-05 v CourantNb 6.5149e-08 0.011471 0.00016932 4.9581e-06 v FourierNb 1.2427e-07 0.042782 0.0001483 4.5276e-07 v total_pressure -2.5206e+05 2.3057e+05 -13699 18061 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0295 0.10792 0.0029461 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.6278e-07 0.048201 0.00031762 5.4108e-06 INSTANT 0.876241000E-01 TIME STEP NUMBER 56439 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283034555E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.829779559E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.45549E-02 0.20639E+01 Friction velocity uk : 0.45549E-02 0.20639E+01 Dimensionless distance yplus : 0.44719E-02 0.20294E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.180310860e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29462E+08 1 0.18407E-09 0.28343E+02 0.20325E+04 c Velocity[X] 0.15787E+02 c Velocity[Y] 0.12557E+02 c Velocity[Z] 0.10222E-05 c Pressure 0.93050E-04 462 0.82434E-04 0.75779E-03 0.59431E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -27.192 41.86 5.6101 8.0019 v Velocity[Y] -29.88 31.336 -0.1535 -0.027448 v Velocity[Z] -2.992 3.1059 2.3874e-06 -5.3899e-08 v ǁVelocityǁ 0.0027788 42.046 8.3515 8.1514 v Pressure -3.5401e+05 1.2887e+05 -1.1557e+05 -83490 v TurbVisc 8.0051e-20 0.022176 0.00019281 4.689e-05 v CourantNb 6.1646e-08 0.01147 0.00016933 4.9581e-06 v FourierNb 1.2427e-07 0.042764 0.00014831 4.5324e-07 v total_pressure -2.5268e+05 2.3019e+05 -14244 17835 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0294 0.10794 0.0029461 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.6298e-07 0.048183 0.00031763 5.4113e-06 INSTANT 0.876242000E-01 TIME STEP NUMBER 56440 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283027652E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.829445641E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11093E-01 0.20638E+01 Friction velocity uk : 0.11093E-01 0.20638E+01 Dimensionless distance yplus : 0.10685E-01 0.20293E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.202234144e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29461E+08 1 0.18408E-09 0.28356E+02 0.20329E+04 c Velocity[X] 0.15796E+02 c Velocity[Y] 0.12560E+02 c Velocity[Z] 0.10176E-05 c Pressure 0.91455E-04 38 0.96142E-04 0.74447E-03 0.78759E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -27.205 41.871 5.6099 8.0018 v Velocity[Y] -29.889 31.348 -0.15354 -0.027572 v Velocity[Z] -2.9925 3.1061 2.3868e-06 -5.3899e-08 v ǁVelocityǁ 0.0026591 42.057 8.353 8.1515 v Pressure -3.5467e+05 1.2853e+05 -1.161e+05 -83911 v TurbVisc 7.7831e-20 0.022193 0.00019287 4.6959e-05 v CourantNb 5.7259e-08 0.011469 0.00016933 4.9581e-06 v FourierNb 1.2427e-07 0.042747 0.00014832 4.5372e-07 v total_pressure -2.5335e+05 2.2986e+05 -14775 17414 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0293 0.10795 0.0029462 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.6319e-07 0.048165 0.00031764 5.4118e-06 INSTANT 0.876243000E-01 TIME STEP NUMBER 56441 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283020940E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.829108137E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.86274E-02 0.20637E+01 Friction velocity uk : 0.86274E-02 0.20637E+01 Dimensionless distance yplus : 0.83104E-02 0.20292E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.217029856e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29461E+08 1 0.18408E-09 0.28355E+02 0.20328E+04 c Velocity[X] 0.15804E+02 c Velocity[Y] 0.12551E+02 c Velocity[Z] 0.10144E-05 c Pressure 0.90236E-04 700 0.81817E-04 0.73422E-03 0.47671E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -27.218 41.882 5.6098 8.0017 v Velocity[Y] -29.898 31.361 -0.15358 -0.027694 v Velocity[Z] -2.9929 3.1062 2.3862e-06 -5.3899e-08 v ǁVelocityǁ 0.0024405 42.068 8.3545 8.1515 v Pressure -3.553e+05 1.2818e+05 -1.1659e+05 -84210 v TurbVisc 7.8549e-20 0.02221 0.00019293 4.7029e-05 v CourantNb 5.2898e-08 0.011469 0.00016933 4.9581e-06 v FourierNb 1.2427e-07 0.042729 0.00014833 4.5419e-07 v total_pressure -2.5397e+05 2.295e+05 -15260 17115 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0292 0.10797 0.0029463 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.6339e-07 0.048147 0.00031766 5.4122e-06 INSTANT 0.876244000E-01 TIME STEP NUMBER 56442 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283014040E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.828766066E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.53473E-02 0.20635E+01 Friction velocity uk : 0.53473E-02 0.20635E+01 Dimensionless distance yplus : 0.51450E-02 0.20290E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.228917015e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29460E+08 1 0.18409E-09 0.28371E+02 0.20333E+04 c Velocity[X] 0.15813E+02 c Velocity[Y] 0.12557E+02 c Velocity[Z] 0.10124E-05 c Pressure 0.82518E-04 7 0.57632E-04 0.67112E-03 0.29542E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -27.231 41.893 5.6097 8.0015 v Velocity[Y] -29.907 31.373 -0.15361 -0.027814 v Velocity[Z] -2.9933 3.1064 2.3856e-06 -5.3899e-08 v ǁVelocityǁ 0.0017808 42.08 8.3559 8.1515 v Pressure -3.5572e+05 1.2797e+05 -1.1695e+05 -84340 v TurbVisc 7.7143e-20 0.022227 0.00019299 4.7099e-05 v CourantNb 4.8521e-08 0.011468 0.00016933 4.958e-06 v FourierNb 1.2427e-07 0.042711 0.00014834 4.5467e-07 v total_pressure -2.5439e+05 2.293e+05 -15624 16985 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.029 0.10798 0.0029463 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.636e-07 0.048129 0.00031767 5.4127e-06 INSTANT 0.876245000E-01 TIME STEP NUMBER 56443 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283007114E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.828422119E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.70342E-02 0.20634E+01 Friction velocity uk : 0.70342E-02 0.20634E+01 Dimensionless distance yplus : 0.67681E-02 0.20289E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.244555509e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29460E+08 1 0.18409E-09 0.28380E+02 0.20336E+04 c Velocity[X] 0.15823E+02 c Velocity[Y] 0.12558E+02 c Velocity[Z] 0.10082E-05 c Pressure 0.82929E-04 49 0.78251E-04 0.67416E-03 0.74128E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -27.245 41.904 5.6096 8.0014 v Velocity[Y] -29.916 31.386 -0.15365 -0.027938 v Velocity[Z] -2.9937 3.1066 2.385e-06 -5.3899e-08 v ǁVelocityǁ 0.0010784 42.091 8.3574 8.1516 v Pressure -3.5636e+05 1.2767e+05 -1.1744e+05 -84848 v TurbVisc 7.4644e-20 0.022244 0.00019305 4.7169e-05 v CourantNb 4.3737e-08 0.011467 0.00016933 4.958e-06 v FourierNb 1.2427e-07 0.042693 0.00014835 4.5515e-07 v total_pressure -2.5504e+05 2.29e+05 -16114 16477 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0289 0.108 0.0029464 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.6381e-07 0.04811 0.00031768 5.4132e-06 INSTANT 0.876246000E-01 TIME STEP NUMBER 56444 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283000290E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.828070620E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.49302E-02 0.20633E+01 Friction velocity uk : 0.49302E-02 0.20633E+01 Dimensionless distance yplus : 0.47438E-02 0.20288E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.240845689e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29459E+08 1 0.18410E-09 0.28391E+02 0.20339E+04 c Velocity[X] 0.15830E+02 c Velocity[Y] 0.12561E+02 c Velocity[Z] 0.10005E-05 c Pressure 0.81616E-04 70 0.83837E-04 0.66319E-03 0.57127E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -27.258 41.915 5.6094 8.0012 v Velocity[Y] -29.925 31.398 -0.15369 -0.02806 v Velocity[Z] -2.9941 3.1068 2.3844e-06 -5.3899e-08 v ǁVelocityǁ 0.00057419 42.102 8.3589 8.1516 v Pressure -3.5679e+05 1.2746e+05 -1.1774e+05 -84996 v TurbVisc 7.4865e-20 0.02226 0.00019311 4.7239e-05 v CourantNb 3.979e-08 0.011466 0.00016934 4.958e-06 v FourierNb 1.2427e-07 0.042676 0.00014836 4.5563e-07 v total_pressure -2.5546e+05 2.2879e+05 -16418 16329 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0288 0.10801 0.0029464 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.6401e-07 0.048093 0.0003177 5.4136e-06 INSTANT 0.876247000E-01 TIME STEP NUMBER 56445 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282993245E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.827724404E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.50376E-02 0.20631E+01 Friction velocity uk : 0.50376E-02 0.20631E+01 Dimensionless distance yplus : 0.49612E-02 0.20286E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.248524230e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29458E+08 1 0.18410E-09 0.28403E+02 0.20343E+04 c Velocity[X] 0.15839E+02 c Velocity[Y] 0.12564E+02 c Velocity[Z] 0.99280E-06 c Pressure 0.81311E-04 96 0.97542E-04 0.66042E-03 0.71396E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -27.271 41.926 5.6093 8.0011 v Velocity[Y] -29.934 31.41 -0.15372 -0.028186 v Velocity[Z] -2.9945 3.1069 2.3838e-06 -5.3899e-08 v ǁVelocityǁ 0.00049113 42.114 8.3603 8.1517 v Pressure -3.5719e+05 1.2735e+05 -1.1805e+05 -85283 v TurbVisc 7.0739e-20 0.022277 0.00019317 4.731e-05 v CourantNb 3.5367e-08 0.011466 0.00016934 4.958e-06 v FourierNb 1.2427e-07 0.042658 0.00014837 4.5611e-07 v total_pressure -2.5587e+05 2.2867e+05 -16727 16042 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0286 0.10802 0.0029466 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.6422e-07 0.048074 0.00031771 5.4141e-06 INSTANT 0.876248000E-01 TIME STEP NUMBER 56446 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282986431E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.827373790E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10147E-01 0.20630E+01 Friction velocity uk : 0.10147E-01 0.20630E+01 Dimensionless distance yplus : 0.99929E-02 0.20285E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.249678421e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29458E+08 1 0.18411E-09 0.28399E+02 0.20341E+04 c Velocity[X] 0.15846E+02 c Velocity[Y] 0.12554E+02 c Velocity[Z] 0.99042E-06 c Pressure 0.81493E-04 302 0.82736E-04 0.66161E-03 0.40459E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -27.284 41.937 5.6092 8.0009 v Velocity[Y] -29.942 31.423 -0.15376 -0.028309 v Velocity[Z] -2.9949 3.1071 2.3832e-06 -5.39e-08 v ǁVelocityǁ 0.00028101 42.125 8.3618 8.1517 v Pressure -3.5752e+05 1.2722e+05 -1.1829e+05 -85376 v TurbVisc 7.0517e-20 0.022294 0.00019323 4.738e-05 v CourantNb 3.0982e-08 0.011465 0.00016934 4.958e-06 v FourierNb 1.2427e-07 0.04264 0.00014838 4.5659e-07 v total_pressure -2.5619e+05 2.2854e+05 -16963 15949 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0285 0.10804 0.0029468 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.6443e-07 0.048056 0.00031772 5.4146e-06 INSTANT 0.876249000E-01 TIME STEP NUMBER 56447 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282979483E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.827019983E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19458E-01 0.20629E+01 Friction velocity uk : 0.19458E-01 0.20629E+01 Dimensionless distance yplus : 0.18722E-01 0.20284E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.247986132e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29457E+08 1 0.18411E-09 0.28413E+02 0.20345E+04 c Velocity[X] 0.15852E+02 c Velocity[Y] 0.12562E+02 c Velocity[Z] 0.99755E-06 c Pressure 0.74261E-04 15 0.58589E-04 0.60263E-03 0.27790E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -27.297 41.948 5.609 8.0008 v Velocity[Y] -29.951 31.435 -0.1538 -0.028432 v Velocity[Z] -2.9954 3.1073 2.3826e-06 -5.39e-08 v ǁVelocityǁ 0.00071122 42.136 8.3633 8.1517 v Pressure -3.5779e+05 1.2718e+05 -1.1843e+05 -85463 v TurbVisc 6.8182e-20 0.022311 0.00019329 4.745e-05 v CourantNb 2.9297e-08 0.011464 0.00016934 4.958e-06 v FourierNb 1.2427e-07 0.042622 0.00014839 4.5707e-07 v total_pressure -2.5646e+05 2.2851e+05 -17105 15862 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0284 0.10805 0.002947 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.6464e-07 0.048037 0.00031773 5.415e-06 INSTANT 0.876250000E-01 TIME STEP NUMBER 56448 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282972484E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.826663649E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.18995E-01 0.20627E+01 Friction velocity uk : 0.18995E-01 0.20627E+01 Dimensionless distance yplus : 0.18455E-01 0.20282E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.251911526e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29457E+08 1 0.18412E-09 0.28421E+02 0.20348E+04 c Velocity[X] 0.15861E+02 c Velocity[Y] 0.12561E+02 c Velocity[Z] 0.98474E-06 c Pressure 0.76456E-04 31 0.79110E-04 0.62017E-03 0.64389E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -27.309 41.959 5.6089 8.0006 v Velocity[Y] -29.96 31.447 -0.15384 -0.028558 v Velocity[Z] -2.9958 3.1074 2.382e-06 -5.39e-08 v ǁVelocityǁ 0.0005765 42.147 8.3647 8.1518 v Pressure -3.5817e+05 1.2705e+05 -1.1873e+05 -85847 v TurbVisc 2.2512e-20 0.022328 0.00019335 4.752e-05 v CourantNb 2.81e-08 0.011463 0.00016934 4.958e-06 v FourierNb 1.2428e-07 0.042604 0.0001484 4.5755e-07 v total_pressure -2.5684e+05 2.2837e+05 -17409 15478 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0282 0.10807 0.0029472 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.6485e-07 0.048019 0.00031775 5.4155e-06 INSTANT 0.876251000E-01 TIME STEP NUMBER 56449 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282965597E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.826299489E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.14498E-01 0.20626E+01 Friction velocity uk : 0.14498E-01 0.20626E+01 Dimensionless distance yplus : 0.14002E-01 0.20281E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.228445033e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29456E+08 1 0.18413E-09 0.28431E+02 0.20350E+04 c Velocity[X] 0.15866E+02 c Velocity[Y] 0.12564E+02 c Velocity[Z] 0.97634E-06 c Pressure 0.76636E-04 344 0.84822E-04 0.62135E-03 0.57239E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -27.322 41.97 5.6088 8.0005 v Velocity[Y] -29.968 31.459 -0.15387 -0.028682 v Velocity[Z] -2.9962 3.1076 2.3814e-06 -5.39e-08 v ǁVelocityǁ 0.00018923 42.158 8.3662 8.1518 v Pressure -3.5832e+05 1.2709e+05 -1.1878e+05 -85822 v TurbVisc 9.7339e-20 0.022344 0.0001934 4.7591e-05 v CourantNb 2.3565e-08 0.011462 0.00016935 4.9579e-06 v FourierNb 1.2428e-07 0.042586 0.00014842 4.5803e-07 v total_pressure -2.5699e+05 2.2841e+05 -17457 15503 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0281 0.10808 0.0029472 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.6506e-07 0.048 0.00031776 5.416e-06 INSTANT 0.876252000E-01 TIME STEP NUMBER 56450 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282958539E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.825945707E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.97240E-02 0.20625E+01 Friction velocity uk : 0.97240E-02 0.20625E+01 Dimensionless distance yplus : 0.93915E-02 0.20280E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.225882430e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29456E+08 1 0.18413E-09 0.28440E+02 0.20353E+04 c Velocity[X] 0.15873E+02 c Velocity[Y] 0.12568E+02 c Velocity[Z] 0.97362E-06 c Pressure 0.77970E-04 105 0.98404E-04 0.63189E-03 0.68728E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -27.335 41.981 5.6087 8.0004 v Velocity[Y] -29.977 31.472 -0.15391 -0.028809 v Velocity[Z] -2.9966 3.1078 2.3808e-06 -5.39e-08 v ǁVelocityǁ 0.00071857 42.169 8.3677 8.1519 v Pressure -3.5852e+05 1.2715e+05 -1.1886e+05 -85986 v TurbVisc 7.8667e-20 0.022361 0.00019346 4.7661e-05 v CourantNb 2.2231e-08 0.011462 0.00016935 4.9579e-06 v FourierNb 1.2428e-07 0.042568 0.00014843 4.5851e-07 v total_pressure -2.5719e+05 2.2848e+05 -17538 15339 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.028 0.10809 0.0029473 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.6528e-07 0.047982 0.00031777 5.4164e-06 INSTANT 0.876253000E-01 TIME STEP NUMBER 56451 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282951722E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.825586067E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.61857E-02 0.20624E+01 Friction velocity uk : 0.61857E-02 0.20624E+01 Dimensionless distance yplus : 0.60098E-02 0.20279E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.214482187e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29455E+08 1 0.18414E-09 0.28435E+02 0.20351E+04 c Velocity[X] 0.15878E+02 c Velocity[Y] 0.12557E+02 c Velocity[Z] 0.96736E-06 c Pressure 0.79760E-04 461 0.83750E-04 0.64611E-03 0.38654E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -27.348 41.992 5.6085 8.0002 v Velocity[Y] -29.985 31.484 -0.15395 -0.028935 v Velocity[Z] -2.997 3.108 2.3802e-06 -5.39e-08 v ǁVelocityǁ 0.00082602 42.18 8.3691 8.1519 v Pressure -3.5864e+05 1.2719e+05 -1.1889e+05 -86019 v TurbVisc 6.9062e-20 0.022378 0.00019352 4.7732e-05 v CourantNb 2.2221e-08 0.011461 0.00016935 4.9579e-06 v FourierNb 1.2428e-07 0.04255 0.00014844 4.5899e-07 v total_pressure -2.5731e+05 2.2852e+05 -17565 15306 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0279 0.1081 0.0029474 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.6549e-07 0.047963 0.00031779 5.4169e-06 INSTANT 0.876254000E-01 TIME STEP NUMBER 56452 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282944749E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.825224709E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10453E-01 0.20622E+01 Friction velocity uk : 0.10453E-01 0.20622E+01 Dimensionless distance yplus : 0.10298E-01 0.20278E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.200098665e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29454E+08 1 0.18414E-09 0.28448E+02 0.20355E+04 c Velocity[X] 0.15884E+02 c Velocity[Y] 0.12564E+02 c Velocity[Z] 0.96733E-06 c Pressure 0.73896E-04 6 0.58836E-04 0.59835E-03 0.26511E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -27.361 42.002 5.6084 8.0001 v Velocity[Y] -29.994 31.496 -0.15399 -0.02906 v Velocity[Z] -2.9974 3.1081 2.3796e-06 -5.39e-08 v ǁVelocityǁ 0.0010202 42.191 8.3706 8.1519 v Pressure -3.5871e+05 1.2732e+05 -1.1888e+05 -86037 v TurbVisc 6.2577e-20 0.022395 0.00019358 4.7802e-05 v CourantNb 2.2222e-08 0.01146 0.00016935 4.9579e-06 v FourierNb 1.2428e-07 0.042532 0.00014845 4.5947e-07 v total_pressure -2.5738e+05 2.2865e+05 -17553 15288 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0278 0.10811 0.0029474 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.657e-07 0.047945 0.0003178 5.4174e-06 INSTANT 0.876255000E-01 TIME STEP NUMBER 56453 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282937777E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.824863160E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12870E-01 0.20621E+01 Friction velocity uk : 0.12870E-01 0.20621E+01 Dimensionless distance yplus : 0.12679E-01 0.20277E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.182807827e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29454E+08 1 0.18415E-09 0.28454E+02 0.20356E+04 c Velocity[X] 0.15890E+02 c Velocity[Y] 0.12564E+02 c Velocity[Z] 0.96084E-06 c Pressure 0.77839E-04 29 0.79960E-04 0.63000E-03 0.51048E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -27.373 42.013 5.6083 7.9999 v Velocity[Y] -30.002 31.508 -0.15402 -0.029188 v Velocity[Z] -2.9978 3.1083 2.379e-06 -5.39e-08 v ǁVelocityǁ 0.0010968 42.202 8.372 8.152 v Pressure -3.5867e+05 1.2752e+05 -1.1879e+05 -86067 v TurbVisc 5.9654e-20 0.022412 0.00019364 4.7873e-05 v CourantNb 2.2243e-08 0.011459 0.00016935 4.9579e-06 v FourierNb 1.2428e-07 0.042513 0.00014846 4.5996e-07 v total_pressure -2.5734e+05 2.2884e+05 -17467 15258 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0277 0.10812 0.0029474 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.6592e-07 0.047927 0.00031781 5.4178e-06 INSTANT 0.876256000E-01 TIME STEP NUMBER 56454 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282930978E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.824501877E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.57981E-02 0.20620E+01 Friction velocity uk : 0.57981E-02 0.20620E+01 Dimensionless distance yplus : 0.57287E-02 0.20276E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.163031055e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29453E+08 1 0.18416E-09 0.28462E+02 0.20359E+04 c Velocity[X] 0.15894E+02 c Velocity[Y] 0.12568E+02 c Velocity[Z] 0.95544E-06 c Pressure 0.79522E-04 55 0.85755E-04 0.64335E-03 0.56295E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -27.386 42.024 5.6082 7.9998 v Velocity[Y] -30.011 31.52 -0.15406 -0.029313 v Velocity[Z] -2.9983 3.1085 2.3784e-06 -5.39e-08 v ǁVelocityǁ 0.0012083 42.213 8.3735 8.152 v Pressure -3.5871e+05 1.2768e+05 -1.187e+05 -86045 v TurbVisc 5.5204e-20 0.022428 0.0001937 4.7944e-05 v CourantNb 2.2224e-08 0.011458 0.00016936 4.9579e-06 v FourierNb 1.2428e-07 0.042495 0.00014847 4.6044e-07 v total_pressure -2.5738e+05 2.29e+05 -17374 15280 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0276 0.10813 0.0029475 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.6613e-07 0.047908 0.00031783 5.4183e-06 INSTANT 0.876257000E-01 TIME STEP NUMBER 56455 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282923975E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.824137795E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.67476E-02 0.20619E+01 Friction velocity uk : 0.67476E-02 0.20619E+01 Dimensionless distance yplus : 0.66669E-02 0.20275E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.143352465e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29453E+08 1 0.18416E-09 0.28470E+02 0.20361E+04 c Velocity[X] 0.15900E+02 c Velocity[Y] 0.12570E+02 c Velocity[Z] 0.95156E-06 c Pressure 0.82305E-04 109 0.99374E-04 0.66557E-03 0.64926E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -27.399 42.034 5.6081 7.9996 v Velocity[Y] -30.019 31.532 -0.1541 -0.029443 v Velocity[Z] -2.9987 3.1086 2.3778e-06 -5.39e-08 v ǁVelocityǁ 0.0013439 42.224 8.375 8.1521 v Pressure -3.586e+05 1.2798e+05 -1.1854e+05 -86035 v TurbVisc 5.2771e-20 0.022445 0.00019375 4.8015e-05 v CourantNb 2.3374e-08 0.011458 0.00016936 4.9579e-06 v FourierNb 1.2428e-07 0.042477 0.00014848 4.6092e-07 v total_pressure -2.5728e+05 2.293e+05 -17213 15290 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0275 0.10815 0.0029476 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.6635e-07 0.04789 0.00031784 5.4188e-06 INSTANT 0.876258000E-01 TIME STEP NUMBER 56456 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282917266E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.823775009E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.16905E-01 0.20619E+01 Friction velocity uk : 0.16905E-01 0.20619E+01 Dimensionless distance yplus : 0.16703E-01 0.20274E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.120163868e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29452E+08 1 0.18417E-09 0.28463E+02 0.20358E+04 c Velocity[X] 0.15903E+02 c Velocity[Y] 0.12560E+02 c Velocity[Z] 0.95041E-06 c Pressure 0.85452E-04 67 0.84437E-04 0.69072E-03 0.42001E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -27.411 42.045 5.6079 7.9995 v Velocity[Y] -30.027 31.544 -0.15414 -0.02957 v Velocity[Z] -2.9991 3.1088 2.3772e-06 -5.39e-08 v ǁVelocityǁ 0.0014955 42.235 8.3764 8.1521 v Pressure -3.5848e+05 1.2823e+05 -1.1834e+05 -85914 v TurbVisc 4.6648e-20 0.022462 0.00019381 4.8086e-05 v CourantNb 2.4373e-08 0.011457 0.00016936 4.9578e-06 v FourierNb 1.2428e-07 0.042459 0.00014849 4.6141e-07 v total_pressure -2.5715e+05 2.2956e+05 -17011 15411 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0274 0.10817 0.0029476 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.6657e-07 0.047871 0.00031785 5.4192e-06 INSTANT 0.876259000E-01 TIME STEP NUMBER 56457 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282910423E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.823411177E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.24912E-01 0.20618E+01 Friction velocity uk : 0.24912E-01 0.20618E+01 Dimensionless distance yplus : 0.24614E-01 0.20273E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.095080315e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29452E+08 1 0.18418E-09 0.28475E+02 0.20362E+04 c Velocity[X] 0.15908E+02 c Velocity[Y] 0.12567E+02 c Velocity[Z] 0.94873E-06 c Pressure 0.81317E-04 7 0.59310E-04 0.65701E-03 0.27401E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -27.424 42.056 5.6078 7.9993 v Velocity[Y] -30.035 31.556 -0.15418 -0.029697 v Velocity[Z] -2.9995 3.109 2.3766e-06 -5.39e-08 v ǁVelocityǁ 0.0014923 42.246 8.3779 8.1522 v Pressure -3.5839e+05 1.2851e+05 -1.1815e+05 -85906 v TurbVisc 4.7487e-20 0.022479 0.00019387 4.8156e-05 v CourantNb 2.8055e-08 0.011456 0.00016936 4.9578e-06 v FourierNb 1.2428e-07 0.042441 0.00014851 4.6189e-07 v total_pressure -2.5706e+05 2.2983e+05 -16826 15419 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0273 0.10818 0.0029477 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.6678e-07 0.047853 0.00031787 5.4197e-06 INSTANT 0.876260000E-01 TIME STEP NUMBER 56458 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282903564E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.823048002E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.26102E-01 0.20617E+01 Friction velocity uk : 0.26102E-01 0.20617E+01 Dimensionless distance yplus : 0.25163E-01 0.20273E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.060659693e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29451E+08 1 0.18418E-09 0.28479E+02 0.20363E+04 c Velocity[X] 0.15911E+02 c Velocity[Y] 0.12568E+02 c Velocity[Z] 0.94251E-06 c Pressure 0.86251E-04 375 0.80661E-04 0.69657E-03 0.55269E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -27.436 42.066 5.6077 7.9992 v Velocity[Y] -30.044 31.568 -0.15422 -0.029828 v Velocity[Z] -2.9999 3.1092 2.376e-06 -5.39e-08 v ǁVelocityǁ 0.0014052 42.256 8.3793 8.1522 v Pressure -3.5812e+05 1.289e+05 -1.1779e+05 -85789 v TurbVisc 4.8424e-20 0.022496 0.00019393 4.8227e-05 v CourantNb 3.1748e-08 0.011455 0.00016936 4.9578e-06 v FourierNb 1.2428e-07 0.042424 0.00014852 4.6237e-07 v total_pressure -2.568e+05 2.3022e+05 -16464 15536 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0273 0.1082 0.0029477 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.67e-07 0.047835 0.00031788 5.4202e-06 INSTANT 0.876261000E-01 TIME STEP NUMBER 56459 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282896903E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.822689708E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.25529E-01 0.20617E+01 Friction velocity uk : 0.25529E-01 0.20617E+01 Dimensionless distance yplus : 0.24778E-01 0.20272E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.046545869e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29451E+08 1 0.18419E-09 0.28485E+02 0.20365E+04 c Velocity[X] 0.15915E+02 c Velocity[Y] 0.12570E+02 c Velocity[Z] 0.93691E-06 c Pressure 0.89145E-04 370 0.86801E-04 0.71963E-03 0.67244E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -27.449 42.077 5.6076 7.9991 v Velocity[Y] -30.052 31.58 -0.15426 -0.029955 v Velocity[Z] -3.0003 3.1093 2.3754e-06 -5.39e-08 v ǁVelocityǁ 0.0013395 42.267 8.3808 8.1522 v Pressure -3.5781e+05 1.2934e+05 -1.1746e+05 -85525 v TurbVisc 4.0519e-20 0.022512 0.00019398 4.8299e-05 v CourantNb 3.516e-08 0.011454 0.00016937 4.9578e-06 v FourierNb 1.2428e-07 0.042405 0.00014853 4.6286e-07 v total_pressure -2.5649e+05 2.3066e+05 -16139 15800 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0272 0.10821 0.0029478 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.6722e-07 0.047816 0.0003179 5.4207e-06 INSTANT 0.876262000E-01 TIME STEP NUMBER 56460 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282890107E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.822324918E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.22811E-01 0.20616E+01 Friction velocity uk : 0.22811E-01 0.20616E+01 Dimensionless distance yplus : 0.21968E-01 0.20272E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.014865799e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29450E+08 1 0.18420E-09 0.28480E+02 0.20362E+04 c Velocity[X] 0.15917E+02 c Velocity[Y] 0.12563E+02 c Velocity[Z] 0.93306E-06 c Pressure 0.92911E-04 59 0.75575E-04 0.74970E-03 0.40050E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -27.461 42.087 5.6075 7.9989 v Velocity[Y] -30.06 31.592 -0.15431 -0.030085 v Velocity[Z] -3.0007 3.1095 2.3748e-06 -5.39e-08 v ǁVelocityǁ 0.0012901 42.278 8.3823 8.1523 v Pressure -3.5761e+05 1.2973e+05 -1.1713e+05 -85519 v TurbVisc 4.0299e-20 0.022529 0.00019404 4.837e-05 v CourantNb 3.8459e-08 0.011454 0.00016937 4.9578e-06 v FourierNb 1.2428e-07 0.042387 0.00014854 4.6335e-07 v total_pressure -2.5629e+05 2.3105e+05 -15804 15806 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0272 0.10823 0.0029478 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.6744e-07 0.047798 0.00031791 5.4211e-06 INSTANT 0.876263000E-01 TIME STEP NUMBER 56461 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282883451E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.821963200E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19418E-01 0.20616E+01 Friction velocity uk : 0.19418E-01 0.20616E+01 Dimensionless distance yplus : 0.18701E-01 0.20271E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -9.816187217e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29449E+08 1 0.18421E-09 0.28490E+02 0.20365E+04 c Velocity[X] 0.15922E+02 c Velocity[Y] 0.12568E+02 c Velocity[Z] 0.93684E-06 c Pressure 0.91176E-04 7 0.53262E-04 0.73538E-03 0.27989E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -27.474 42.098 5.6074 7.9988 v Velocity[Y] -30.068 31.604 -0.15435 -0.030216 v Velocity[Z] -3.0011 3.1097 2.3742e-06 -5.39e-08 v ǁVelocityǁ 0.0012562 42.289 8.3837 8.1523 v Pressure -3.5732e+05 1.3017e+05 -1.1674e+05 -85402 v TurbVisc 3.8585e-20 0.022546 0.0001941 4.8441e-05 v CourantNb 4.1715e-08 0.011453 0.00016937 4.9578e-06 v FourierNb 1.2428e-07 0.04237 0.00014855 4.6383e-07 v total_pressure -2.5599e+05 2.315e+05 -15420 15923 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0271 0.10824 0.0029478 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.6766e-07 0.04778 0.00031792 5.4216e-06 INSTANT 0.876264000E-01 TIME STEP NUMBER 56462 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282876938E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.821604695E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15284E-01 0.20616E+01 Friction velocity uk : 0.15284E-01 0.20616E+01 Dimensionless distance yplus : 0.14719E-01 0.20272E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -9.437207168e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29449E+08 1 0.18422E-09 0.28488E+02 0.20364E+04 c Velocity[X] 0.15924E+02 c Velocity[Y] 0.12564E+02 c Velocity[Z] 0.92965E-06 c Pressure 0.95995E-04 79 0.97264E-04 0.77392E-03 0.51194E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -27.486 42.108 5.6073 7.9986 v Velocity[Y] -30.076 31.615 -0.15439 -0.030347 v Velocity[Z] -3.0015 3.1098 2.3736e-06 -5.39e-08 v ǁVelocityǁ 0.0012378 42.299 8.3852 8.1524 v Pressure -3.5677e+05 1.308e+05 -1.162e+05 -84986 v TurbVisc 3.6578e-20 0.022563 0.00019415 4.8512e-05 v CourantNb 4.4538e-08 0.011452 0.00016937 4.9578e-06 v FourierNb 1.2428e-07 0.042352 0.00014856 4.6432e-07 v total_pressure -2.5545e+05 2.3213e+05 -14877 16339 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0272 0.10825 0.0029477 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.6788e-07 0.047762 0.00031794 5.4221e-06 INSTANT 0.876265000E-01 TIME STEP NUMBER 56463 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282870414E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.821250495E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.99948E-02 0.20616E+01 Friction velocity uk : 0.99948E-02 0.20616E+01 Dimensionless distance yplus : 0.96736E-02 0.20271E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -9.290381272e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29448E+08 1 0.18422E-09 0.28491E+02 0.20364E+04 c Velocity[X] 0.15926E+02 c Velocity[Y] 0.12564E+02 c Velocity[Z] 0.92264E-06 c Pressure 0.98311E-04 166 0.81618E-04 0.79225E-03 0.29789E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -27.499 42.118 5.6072 7.9985 v Velocity[Y] -30.084 31.627 -0.15443 -0.030477 v Velocity[Z] -3.002 3.11 2.373e-06 -5.39e-08 v ǁVelocityǁ 0.0012345 42.31 8.3866 8.1524 v Pressure -3.5641e+05 1.3133e+05 -1.1572e+05 -84788 v TurbVisc 3.2122e-20 0.022579 0.00019421 4.8583e-05 v CourantNb 4.8072e-08 0.011451 0.00016938 4.9578e-06 v FourierNb 1.2428e-07 0.042334 0.00014858 4.6481e-07 v total_pressure -2.5508e+05 2.3265e+05 -14398 16537 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0271 0.10826 0.0029478 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.681e-07 0.047744 0.00031795 5.4226e-06 INSTANT 0.876266000E-01 TIME STEP NUMBER 56464 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282863892E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.820892495E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.29279E-02 0.20616E+01 Friction velocity uk : 0.29279E-02 0.20616E+01 Dimensionless distance yplus : 0.28339E-02 0.20271E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -8.864653328e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29448E+08 1 0.18423E-09 0.28500E+02 0.20367E+04 c Velocity[X] 0.15929E+02 c Velocity[Y] 0.12570E+02 c Velocity[Z] 0.92627E-06 c Pressure 0.10009E-03 9 0.53584E-04 0.80624E-03 0.34758E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -27.511 42.129 5.6071 7.9984 v Velocity[Y] -30.092 31.639 -0.15448 -0.030607 v Velocity[Z] -3.0024 3.1102 2.3724e-06 -5.3901e-08 v ǁVelocityǁ 0.0012444 42.32 8.3881 8.1525 v Pressure -3.5608e+05 1.3188e+05 -1.1519e+05 -84578 v TurbVisc 3.0147e-20 0.022596 0.00019427 4.8655e-05 v CourantNb 5.0769e-08 0.01145 0.00016938 4.9577e-06 v FourierNb 1.2428e-07 0.042316 0.00014859 4.6529e-07 v total_pressure -2.5475e+05 2.332e+05 -13863 16747 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0271 0.10827 0.0029477 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.6833e-07 0.047726 0.00031797 5.423e-06 INSTANT 0.876267000E-01 TIME STEP NUMBER 56465 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282857422E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.820537286E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.68507E-02 0.20616E+01 Friction velocity uk : 0.68507E-02 0.20616E+01 Dimensionless distance yplus : 0.66308E-02 0.20272E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -8.507983605e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29447E+08 1 0.18424E-09 0.28497E+02 0.20365E+04 c Velocity[X] 0.15931E+02 c Velocity[Y] 0.12566E+02 c Velocity[Z] 0.92061E-06 c Pressure 0.10520E-03 228 0.99455E-04 0.84707E-03 0.44196E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -27.524 42.139 5.607 7.9982 v Velocity[Y] -30.1 31.651 -0.15452 -0.030738 v Velocity[Z] -3.0028 3.1103 2.3718e-06 -5.3901e-08 v ǁVelocityǁ 0.0012675 42.331 8.3895 8.1525 v Pressure -3.5564e+05 1.3256e+05 -1.1459e+05 -84245 v TurbVisc 3.5576e-20 0.022613 0.00019432 4.8726e-05 v CourantNb 5.3192e-08 0.011449 0.00016938 4.9577e-06 v FourierNb 1.2428e-07 0.042299 0.0001486 4.6578e-07 v total_pressure -2.5431e+05 2.3388e+05 -13265 17080 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0272 0.10829 0.0029479 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.6855e-07 0.047708 0.00031798 5.4235e-06 INSTANT 0.876268000E-01 TIME STEP NUMBER 56466 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282851035E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.820185003E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12200E-01 0.20616E+01 Friction velocity uk : 0.12200E-01 0.20616E+01 Dimensionless distance yplus : 0.11808E-01 0.20271E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -8.292904608e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29447E+08 1 0.18425E-09 0.28499E+02 0.20366E+04 c Velocity[X] 0.15933E+02 c Velocity[Y] 0.12567E+02 c Velocity[Z] 0.91594E-06 c Pressure 0.10773E-03 32 0.83947E-04 0.86703E-03 0.30553E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -27.536 42.149 5.6069 7.9981 v Velocity[Y] -30.108 31.662 -0.15457 -0.030871 v Velocity[Z] -3.0032 3.1105 2.3712e-06 -5.3901e-08 v ǁVelocityǁ 0.0013002 42.341 8.391 8.1526 v Pressure -3.5523e+05 1.3321e+05 -1.1399e+05 -84034 v TurbVisc 2.9705e-20 0.022629 0.00019438 4.8798e-05 v CourantNb 5.6281e-08 0.011449 0.00016938 4.9577e-06 v FourierNb 1.2428e-07 0.042281 0.00014861 4.6627e-07 v total_pressure -2.539e+05 2.3453e+05 -12662 17291 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0271 0.10831 0.0029482 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.6878e-07 0.04769 0.000318 5.424e-06 INSTANT 0.876269000E-01 TIME STEP NUMBER 56467 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282844738E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.819835677E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.14637E-01 0.20617E+01 Friction velocity uk : 0.14637E-01 0.20617E+01 Dimensionless distance yplus : 0.14148E-01 0.20272E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -7.944140079e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29446E+08 1 0.18426E-09 0.28509E+02 0.20368E+04 c Velocity[X] 0.15934E+02 c Velocity[Y] 0.12575E+02 c Velocity[Z] 0.93408E-06 c Pressure 0.10969E-03 12 0.55014E-04 0.88246E-03 0.41583E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -27.549 42.16 5.6068 7.998 v Velocity[Y] -30.115 31.674 -0.15461 -0.031005 v Velocity[Z] -3.0036 3.1107 2.3706e-06 -5.3901e-08 v ǁVelocityǁ 0.0013452 42.352 8.3925 8.1527 v Pressure -3.5474e+05 1.3394e+05 -1.1331e+05 -83767 v TurbVisc 2.7253e-20 0.022646 0.00019444 4.8869e-05 v CourantNb 5.8743e-08 0.011448 0.00016939 4.9577e-06 v FourierNb 1.2428e-07 0.042263 0.00014862 4.6676e-07 v total_pressure -2.5342e+05 2.3527e+05 -11986 17558 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0272 0.10833 0.0029484 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.69e-07 0.047673 0.00031801 5.4245e-06 INSTANT 0.876270000E-01 TIME STEP NUMBER 56468 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282838572E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.819489521E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12643E-01 0.20617E+01 Friction velocity uk : 0.12643E-01 0.20617E+01 Dimensionless distance yplus : 0.12221E-01 0.20273E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -7.555048805e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29446E+08 1 0.18427E-09 0.28509E+02 0.20368E+04 c Velocity[X] 0.15936E+02 c Velocity[Y] 0.12573E+02 c Velocity[Z] 0.91578E-06 c Pressure 0.11494E-03 49 0.77602E-04 0.92427E-03 0.87121E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -27.561 42.17 5.6067 7.9978 v Velocity[Y] -30.123 31.686 -0.15466 -0.031136 v Velocity[Z] -3.004 3.1108 2.37e-06 -5.3901e-08 v ǁVelocityǁ 0.0013936 42.362 8.3939 8.1527 v Pressure -3.5417e+05 1.3475e+05 -1.1256e+05 -83170 v TurbVisc 3.2541e-20 0.022663 0.00019449 4.8941e-05 v CourantNb 6.0732e-08 0.011447 0.00016939 4.9577e-06 v FourierNb 1.2428e-07 0.042246 0.00014864 4.6725e-07 v total_pressure -2.5285e+05 2.3607e+05 -11237 18155 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0273 0.10834 0.0029486 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.6923e-07 0.047655 0.00031803 5.425e-06 INSTANT 0.876271000E-01 TIME STEP NUMBER 56469 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282832313E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.819145814E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.79814E-02 0.20618E+01 Friction velocity uk : 0.79814E-02 0.20618E+01 Dimensionless distance yplus : 0.79131E-02 0.20273E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -7.376242298e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29445E+08 1 0.18428E-09 0.28516E+02 0.20370E+04 c Velocity[X] 0.15938E+02 c Velocity[Y] 0.12578E+02 c Velocity[Z] 0.90994E-06 c Pressure 0.11853E-03 272 0.81926E-04 0.95276E-03 0.65671E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -27.573 42.18 5.6067 7.9977 v Velocity[Y] -30.131 31.698 -0.15471 -0.031271 v Velocity[Z] -3.0044 3.111 2.3694e-06 -5.3901e-08 v ǁVelocityǁ 0.0013382 42.373 8.3954 8.1528 v Pressure -3.536e+05 1.3556e+05 -1.1182e+05 -82877 v TurbVisc 1.8738e-20 0.02268 0.00019455 4.9013e-05 v CourantNb 6.3555e-08 0.011446 0.00016939 4.9577e-06 v FourierNb 1.2428e-07 0.042228 0.00014865 4.6774e-07 v total_pressure -2.5228e+05 2.3689e+05 -10493 18448 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0273 0.10836 0.0029488 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.6946e-07 0.047637 0.00031804 5.4254e-06 INSTANT 0.876272000E-01 TIME STEP NUMBER 56470 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282826368E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.818804122E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.40051E-02 0.20618E+01 Friction velocity uk : 0.40051E-02 0.20618E+01 Dimensionless distance yplus : 0.39708E-02 0.20274E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -7.016249997e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29445E+08 1 0.18429E-09 0.28520E+02 0.20371E+04 c Velocity[X] 0.15940E+02 c Velocity[Y] 0.12579E+02 c Velocity[Z] 0.90221E-06 c Pressure 0.12274E-03 107 0.96104E-04 0.98612E-03 0.80065E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -27.586 42.19 5.6066 7.9976 v Velocity[Y] -30.139 31.709 -0.15475 -0.031403 v Velocity[Z] -3.0048 3.1112 2.3688e-06 -5.3901e-08 v ǁVelocityǁ 0.0012326 42.383 8.3969 8.1528 v Pressure -3.5309e+05 1.3631e+05 -1.1104e+05 -82487 v TurbVisc 2.0374e-20 0.022696 0.0001946 4.9085e-05 v CourantNb 6.5641e-08 0.011445 0.0001694 4.9577e-06 v FourierNb 1.2428e-07 0.04221 0.00014866 4.6823e-07 v total_pressure -2.5176e+05 2.3764e+05 -9717.9 18838 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0274 0.10838 0.002949 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.6968e-07 0.047619 0.00031806 5.4259e-06 INSTANT 0.876273000E-01 TIME STEP NUMBER 56471 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282820264E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.818464761E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.17329E-02 0.20619E+01 Friction velocity uk : 0.17329E-02 0.20619E+01 Dimensionless distance yplus : 0.16751E-02 0.20274E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -6.742250272e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29444E+08 1 0.18430E-09 0.28512E+02 0.20367E+04 c Velocity[X] 0.15940E+02 c Velocity[Y] 0.12572E+02 c Velocity[Z] 0.89997E-06 c Pressure 0.12687E-03 318 0.81250E-04 0.10189E-02 0.57624E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -27.598 42.201 5.6065 7.9975 v Velocity[Y] -30.146 31.721 -0.1548 -0.031537 v Velocity[Z] -3.0052 3.1114 2.3682e-06 -5.3901e-08 v ǁVelocityǁ 0.0011362 42.394 8.3983 8.1529 v Pressure -3.5244e+05 1.372e+05 -1.1022e+05 -82144 v TurbVisc 2.0451e-20 0.022713 0.00019466 4.9156e-05 v CourantNb 6.4007e-08 0.011444 0.0001694 4.9577e-06 v FourierNb 1.2428e-07 0.042193 0.00014867 4.6872e-07 v total_pressure -2.5112e+05 2.3853e+05 -8895.6 19181 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0274 0.1084 0.0029492 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.6991e-07 0.047602 0.00031807 5.4264e-06 INSTANT 0.876274000E-01 TIME STEP NUMBER 56472 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282814368E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.818131693E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.26699E-02 0.20620E+01 Friction velocity uk : 0.26699E-02 0.20620E+01 Dimensionless distance yplus : 0.25808E-02 0.20275E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -6.466526750e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29444E+08 1 0.18431E-09 0.28521E+02 0.20370E+04 c Velocity[X] 0.15943E+02 c Velocity[Y] 0.12578E+02 c Velocity[Z] 0.91739E-06 c Pressure 0.12640E-03 15 0.56512E-04 0.10147E-02 0.43590E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -27.61 42.211 5.6064 7.9973 v Velocity[Y] -30.154 31.732 -0.15485 -0.031673 v Velocity[Z] -3.0056 3.1115 2.3676e-06 -5.3901e-08 v ǁVelocityǁ 0.0010621 42.404 8.3998 8.153 v Pressure -3.5182e+05 1.3806e+05 -1.0938e+05 -81824 v TurbVisc 2.0607e-20 0.02273 0.00019472 4.9228e-05 v CourantNb 6.0915e-08 0.011443 0.0001694 4.9577e-06 v FourierNb 1.2428e-07 0.042175 0.00014868 4.6921e-07 v total_pressure -2.505e+05 2.3938e+05 -8053.5 19501 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0275 0.10842 0.0029495 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.7014e-07 0.047584 0.00031808 5.4269e-06 INSTANT 0.876275000E-01 TIME STEP NUMBER 56473 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282808660E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.817802647E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.30648E-02 0.20621E+01 Friction velocity uk : 0.30648E-02 0.20621E+01 Dimensionless distance yplus : 0.29625E-02 0.20277E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -6.126543315e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29443E+08 1 0.18433E-09 0.28521E+02 0.20369E+04 c Velocity[X] 0.15943E+02 c Velocity[Y] 0.12578E+02 c Velocity[Z] 0.90891E-06 c Pressure 0.13137E-03 64 0.77807E-04 0.10541E-02 0.10155E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -27.623 42.221 5.6064 7.9972 v Velocity[Y] -30.162 31.744 -0.1549 -0.031806 v Velocity[Z] -3.0061 3.1117 2.367e-06 -5.3901e-08 v ǁVelocityǁ 0.00098405 42.415 8.4012 8.153 v Pressure -3.5102e+05 1.3911e+05 -1.0842e+05 -81082 v TurbVisc 2.4389e-20 0.022746 0.00019477 4.93e-05 v CourantNb 5.8542e-08 0.011443 0.00016941 4.9577e-06 v FourierNb 1.2428e-07 0.042158 0.00014869 4.697e-07 v total_pressure -2.4969e+05 2.4043e+05 -7090.6 20243 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0277 0.10844 0.0029497 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.7037e-07 0.047567 0.0003181 5.4274e-06 INSTANT 0.876276000E-01 TIME STEP NUMBER 56474 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282802831E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.817479554E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.58103E-02 0.20622E+01 Friction velocity uk : 0.58103E-02 0.20622E+01 Dimensionless distance yplus : 0.56164E-02 0.20277E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -6.005305206e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29443E+08 1 0.18434E-09 0.28528E+02 0.20371E+04 c Velocity[X] 0.15944E+02 c Velocity[Y] 0.12583E+02 c Velocity[Z] 0.90286E-06 c Pressure 0.13499E-03 269 0.83066E-04 0.10827E-02 0.74601E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -27.635 42.231 5.6063 7.9971 v Velocity[Y] -30.169 31.756 -0.15495 -0.031943 v Velocity[Z] -3.0065 3.1119 2.3664e-06 -5.3901e-08 v ǁVelocityǁ 0.00093933 42.425 8.4027 8.1531 v Pressure -3.5025e+05 1.4011e+05 -1.0747e+05 -80664 v TurbVisc 1.2047e-20 0.022763 0.00019483 4.9373e-05 v CourantNb 5.4774e-08 0.011442 0.00016941 4.9577e-06 v FourierNb 1.2428e-07 0.04214 0.00014871 4.7019e-07 v total_pressure -2.4892e+05 2.4144e+05 -6148.2 20661 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0277 0.10847 0.0029501 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.7061e-07 0.047549 0.00031811 5.4279e-06 INSTANT 0.876277000E-01 TIME STEP NUMBER 56475 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282797336E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.817156407E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.77272E-02 0.20623E+01 Friction velocity uk : 0.77272E-02 0.20623E+01 Dimensionless distance yplus : 0.74693E-02 0.20279E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -5.713109500e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29443E+08 1 0.18435E-09 0.28532E+02 0.20372E+04 c Velocity[X] 0.15946E+02 c Velocity[Y] 0.12585E+02 c Velocity[Z] 0.89552E-06 c Pressure 0.13909E-03 41 0.97203E-04 0.11151E-02 0.89427E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -27.648 42.241 5.6062 7.997 v Velocity[Y] -30.177 31.767 -0.155 -0.032077 v Velocity[Z] -3.0069 3.112 2.3658e-06 -5.3901e-08 v ǁVelocityǁ 0.00091892 42.435 8.4042 8.1532 v Pressure -3.4955e+05 1.4105e+05 -1.0651e+05 -80165 v TurbVisc 1.7228e-20 0.02278 0.00019488 4.9445e-05 v CourantNb 5.1591e-08 0.011441 0.00016941 4.9577e-06 v FourierNb 1.2428e-07 0.042123 0.00014872 4.7068e-07 v total_pressure -2.4823e+05 2.4237e+05 -5184.5 21160 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0279 0.10849 0.0029504 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.7084e-07 0.047532 0.00031813 5.4284e-06 INSTANT 0.876278000E-01 TIME STEP NUMBER 56476 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282791699E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.816836778E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.89685E-02 0.20625E+01 Friction velocity uk : 0.89685E-02 0.20625E+01 Dimensionless distance yplus : 0.86692E-02 0.20280E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -5.521317074e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29442E+08 1 0.18436E-09 0.28523E+02 0.20368E+04 c Velocity[X] 0.15946E+02 c Velocity[Y] 0.12577E+02 c Velocity[Z] 0.88986E-06 c Pressure 0.14307E-03 600 0.82529E-04 0.11465E-02 0.70022E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -27.66 42.251 5.6062 7.9969 v Velocity[Y] -30.184 31.779 -0.15505 -0.032213 v Velocity[Z] -3.0073 3.1122 2.3652e-06 -5.3901e-08 v ǁVelocityǁ 0.00092003 42.446 8.4056 8.1532 v Pressure -3.4868e+05 1.4215e+05 -1.0549e+05 -79675 v TurbVisc 1.6066e-20 0.022796 0.00019494 4.9517e-05 v CourantNb 5.0081e-08 0.01144 0.00016941 4.9577e-06 v FourierNb 1.2428e-07 0.042105 0.00014873 4.7118e-07 v total_pressure -2.4736e+05 2.4348e+05 -4160.2 21650 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.028 0.10851 0.0029506 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.7107e-07 0.047515 0.00031814 5.4289e-06 INSTANT 0.876279000E-01 TIME STEP NUMBER 56477 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282786302E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.816525199E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.92669E-02 0.20626E+01 Friction velocity uk : 0.92669E-02 0.20626E+01 Dimensionless distance yplus : 0.89214E-02 0.20281E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -5.320362413e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29442E+08 1 0.18438E-09 0.28533E+02 0.20371E+04 c Velocity[X] 0.15948E+02 c Velocity[Y] 0.12585E+02 c Velocity[Z] 0.90907E-06 c Pressure 0.14286E-03 16 0.57808E-04 0.11444E-02 0.48061E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -27.672 42.261 5.6061 7.9968 v Velocity[Y] -30.192 31.79 -0.1551 -0.032352 v Velocity[Z] -3.0077 3.1124 2.3646e-06 -5.3901e-08 v ǁVelocityǁ 0.00094068 42.456 8.4071 8.1533 v Pressure -3.4794e+05 1.4314e+05 -1.0449e+05 -79346 v TurbVisc 1.5973e-20 0.022813 0.000195 4.9589e-05 v CourantNb 4.9557e-08 0.011439 0.00016942 4.9577e-06 v FourierNb 1.2428e-07 0.042088 0.00014874 4.7167e-07 v total_pressure -2.4661e+05 2.4446e+05 -3164.7 21979 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0281 0.10853 0.0029509 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.7131e-07 0.047497 0.00031816 5.4294e-06 INSTANT 0.876280000E-01 TIME STEP NUMBER 56478 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282781079E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.816218142E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.65162E-02 0.20628E+01 Friction velocity uk : 0.65162E-02 0.20628E+01 Dimensionless distance yplus : 0.62733E-02 0.20283E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -5.061522276e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29441E+08 1 0.18439E-09 0.28533E+02 0.20370E+04 c Velocity[X] 0.15948E+02 c Velocity[Y] 0.12585E+02 c Velocity[Z] 0.89524E-06 c Pressure 0.14750E-03 56 0.79156E-04 0.11810E-02 0.12448E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -27.685 42.271 5.606 7.9966 v Velocity[Y] -30.199 31.802 -0.15515 -0.032487 v Velocity[Z] -3.0081 3.1125 2.364e-06 -5.3901e-08 v ǁVelocityǁ 0.00099212 42.466 8.4086 8.1534 v Pressure -3.4692e+05 1.444e+05 -1.0332e+05 -78392 v TurbVisc 2.5638e-20 0.02283 0.00019505 4.9661e-05 v CourantNb 4.8863e-08 0.011438 0.00016942 4.9577e-06 v FourierNb 1.2428e-07 0.042071 0.00014875 4.7216e-07 v total_pressure -2.4559e+05 2.4572e+05 -1991 22933 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0283 0.10855 0.0029511 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.7154e-07 0.04748 0.00031817 5.4299e-06 INSTANT 0.876281000E-01 TIME STEP NUMBER 56479 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282775801E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.815920380E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.53152E-02 0.20629E+01 Friction velocity uk : 0.53152E-02 0.20629E+01 Dimensionless distance yplus : 0.51171E-02 0.20284E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -5.015048744e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29441E+08 1 0.18440E-09 0.28540E+02 0.20372E+04 c Velocity[X] 0.15949E+02 c Velocity[Y] 0.12591E+02 c Velocity[Z] 0.88697E-06 c Pressure 0.15097E-03 87 0.84434E-04 0.12083E-02 0.76830E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -27.697 42.282 5.606 7.9965 v Velocity[Y] -30.206 31.814 -0.1552 -0.032626 v Velocity[Z] -3.0085 3.1127 2.3634e-06 -5.3901e-08 v ǁVelocityǁ 0.0010649 42.477 8.41 8.1535 v Pressure -3.4602e+05 1.4553e+05 -1.0223e+05 -78024 v TurbVisc 9.9313e-21 0.022846 0.00019511 4.9734e-05 v CourantNb 4.8092e-08 0.011437 0.00016942 4.9577e-06 v FourierNb 1.2428e-07 0.042053 0.00014876 4.7266e-07 v total_pressure -2.447e+05 2.4685e+05 -908.5 23301 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0284 0.10858 0.0029515 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.7178e-07 0.047462 0.00031819 5.4303e-06 INSTANT 0.876282000E-01 TIME STEP NUMBER 56480 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282770793E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.815621470E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.65878E-02 0.20630E+01 Friction velocity uk : 0.65878E-02 0.20630E+01 Dimensionless distance yplus : 0.63422E-02 0.20286E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -4.817429953e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29441E+08 1 0.18442E-09 0.28544E+02 0.20373E+04 c Velocity[X] 0.15951E+02 c Velocity[Y] 0.12593E+02 c Velocity[Z] 0.88156E-06 c Pressure 0.15475E-03 33 0.98845E-04 0.12380E-02 0.11047E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -27.709 42.292 5.6059 7.9964 v Velocity[Y] -30.214 31.825 -0.15525 -0.032762 v Velocity[Z] -3.0089 3.1129 2.3628e-06 -5.3901e-08 v ǁVelocityǁ 0.0011583 42.487 8.4115 8.1535 v Pressure -3.451e+05 1.4669e+05 -1.0106e+05 -77296 v TurbVisc 1.2259e-20 0.022863 0.00019516 4.9806e-05 v CourantNb 4.7784e-08 0.011437 0.00016943 4.9577e-06 v FourierNb 1.2429e-07 0.042036 0.00014877 4.7315e-07 v total_pressure -2.4377e+05 2.4802e+05 265.78 24029 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0286 0.1086 0.0029517 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.7202e-07 0.047445 0.0003182 5.4308e-06 INSTANT 0.876283000E-01 TIME STEP NUMBER 56481 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282765722E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.815329525E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.83891E-02 0.20632E+01 Friction velocity uk : 0.83891E-02 0.20632E+01 Dimensionless distance yplus : 0.80764E-02 0.20287E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -4.714234767e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29440E+08 1 0.18443E-09 0.28536E+02 0.20369E+04 c Velocity[X] 0.15951E+02 c Velocity[Y] 0.12585E+02 c Velocity[Z] 0.88063E-06 c Pressure 0.15851E-03 555 0.83929E-04 0.12676E-02 0.75831E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -27.722 42.302 5.6059 7.9963 v Velocity[Y] -30.221 31.837 -0.1553 -0.032901 v Velocity[Z] -3.0093 3.113 2.3622e-06 -5.3901e-08 v ǁVelocityǁ 0.0012667 42.497 8.4129 8.1536 v Pressure -3.4409e+05 1.4793e+05 -99885 -76775 v TurbVisc 1.2323e-20 0.02288 0.00019522 4.9879e-05 v CourantNb 4.7407e-08 0.011436 0.00016943 4.9577e-06 v FourierNb 1.2429e-07 0.042018 0.00014878 4.7365e-07 v total_pressure -2.4277e+05 2.4925e+05 1440.1 24550 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0287 0.10862 0.002952 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.7225e-07 0.047428 0.00031821 5.4313e-06 INSTANT 0.876284000E-01 TIME STEP NUMBER 56482 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282760876E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.815045071E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10002E-01 0.20634E+01 Friction velocity uk : 0.10002E-01 0.20634E+01 Dimensionless distance yplus : 0.96293E-02 0.20289E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -4.598562855e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29440E+08 1 0.18444E-09 0.28547E+02 0.20373E+04 c Velocity[X] 0.15954E+02 c Velocity[Y] 0.12593E+02 c Velocity[Z] 0.88277E-06 c Pressure 0.15824E-03 9 0.58042E-04 0.12649E-02 0.61302E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -27.734 42.312 5.6058 7.9962 v Velocity[Y] -30.228 31.848 -0.15535 -0.033041 v Velocity[Z] -3.0097 3.1132 2.3616e-06 -5.3902e-08 v ǁVelocityǁ 0.0013866 42.508 8.4144 8.1537 v Pressure -3.4313e+05 1.4912e+05 -98696 -76289 v TurbVisc 1.2609e-20 0.022896 0.00019527 4.9952e-05 v CourantNb 4.6574e-08 0.011435 0.00016943 4.9577e-06 v FourierNb 1.2429e-07 0.042001 0.00014879 4.7414e-07 v total_pressure -2.4181e+05 2.5045e+05 2629.3 25036 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0289 0.10864 0.0029523 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.7249e-07 0.04741 0.00031823 5.4318e-06 INSTANT 0.876285000E-01 TIME STEP NUMBER 56483 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282756268E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.814767387E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10822E-01 0.20636E+01 Friction velocity uk : 0.10822E-01 0.20636E+01 Dimensionless distance yplus : 0.10419E-01 0.20291E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -4.456228829e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29439E+08 1 0.18446E-09 0.28547E+02 0.20372E+04 c Velocity[X] 0.15954E+02 c Velocity[Y] 0.12593E+02 c Velocity[Z] 0.87977E-06 c Pressure 0.16255E-03 32 0.80317E-04 0.12988E-02 0.13256E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -27.747 42.322 5.6057 7.9961 v Velocity[Y] -30.236 31.86 -0.1554 -0.033178 v Velocity[Z] -3.0101 3.1134 2.361e-06 -5.3902e-08 v ǁVelocityǁ 0.0015194 42.518 8.4159 8.1538 v Pressure -3.4197e+05 1.5052e+05 -97391 -75292 v TurbVisc 1.3949e-20 0.022913 0.00019533 5.0024e-05 v CourantNb 4.6412e-08 0.011434 0.00016944 4.9577e-06 v FourierNb 1.2429e-07 0.041984 0.0001488 4.7464e-07 v total_pressure -2.4065e+05 2.5184e+05 3933.5 26033 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0291 0.10867 0.0029525 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.7273e-07 0.047393 0.00031824 5.4324e-06 INSTANT 0.876286000E-01 TIME STEP NUMBER 56484 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282751561E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.814497668E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11444E-01 0.20637E+01 Friction velocity uk : 0.11444E-01 0.20637E+01 Dimensionless distance yplus : 0.11062E-01 0.20292E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -4.447964634e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29439E+08 1 0.18447E-09 0.28555E+02 0.20374E+04 c Velocity[X] 0.15954E+02 c Velocity[Y] 0.12601E+02 c Velocity[Z] 0.87814E-06 c Pressure 0.16568E-03 623 0.85861E-04 0.13232E-02 0.89120E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -27.759 42.332 5.6057 7.996 v Velocity[Y] -30.243 31.872 -0.15545 -0.03332 v Velocity[Z] -3.0105 3.1135 2.3604e-06 -5.3902e-08 v ǁVelocityǁ 0.0016569 42.528 8.4173 8.1539 v Pressure -3.409e+05 1.5183e+05 -96126 -74799 v TurbVisc 1.1568e-20 0.02293 0.00019538 5.0097e-05 v CourantNb 4.6098e-08 0.011433 0.00016944 4.9577e-06 v FourierNb 1.2429e-07 0.041966 0.00014881 4.7514e-07 v total_pressure -2.3958e+05 2.5315e+05 5199.2 26526 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0292 0.10869 0.0029528 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.7298e-07 0.047376 0.00031825 5.4329e-06 INSTANT 0.876287000E-01 TIME STEP NUMBER 56485 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282747156E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.814231210E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11337E-01 0.20639E+01 Friction velocity uk : 0.11337E-01 0.20639E+01 Dimensionless distance yplus : 0.10959E-01 0.20294E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -4.371697404e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29439E+08 1 0.18449E-09 0.28549E+02 0.20371E+04 c Velocity[X] 0.15958E+02 c Velocity[Y] 0.12591E+02 c Velocity[Z] 0.87699E-06 c Pressure 0.16915E-03 54 0.75216E-04 0.13503E-02 0.97940E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -27.771 42.342 5.6056 7.9959 v Velocity[Y] -30.25 31.883 -0.15551 -0.033459 v Velocity[Z] -3.0109 3.1137 2.3598e-06 -5.3902e-08 v ǁVelocityǁ 0.0018011 42.539 8.4188 8.154 v Pressure -3.3979e+05 1.5317e+05 -94810 -74032 v TurbVisc 1.1588e-20 0.022946 0.00019544 5.017e-05 v CourantNb 4.5912e-08 0.011432 0.00016944 4.9577e-06 v FourierNb 1.2429e-07 0.041949 0.00014882 4.7563e-07 v total_pressure -2.3847e+05 2.5449e+05 6515.4 27293 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0294 0.10871 0.0029531 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.7322e-07 0.047358 0.00031826 5.4334e-06 INSTANT 0.876288000E-01 TIME STEP NUMBER 56486 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282742793E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.813970099E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11080E-01 0.20641E+01 Friction velocity uk : 0.11080E-01 0.20641E+01 Dimensionless distance yplus : 0.10882E-01 0.20296E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -4.339594938e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29439E+08 1 0.18450E-09 0.28559E+02 0.20374E+04 c Velocity[X] 0.15960E+02 c Velocity[Y] 0.12599E+02 c Velocity[Z] 0.87869E-06 c Pressure 0.16943E-03 9 0.55490E-04 0.13520E-02 0.73382E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -27.784 42.352 5.6056 7.9958 v Velocity[Y] -30.257 31.895 -0.15556 -0.033599 v Velocity[Z] -3.0114 3.1139 2.3592e-06 -5.3902e-08 v ǁVelocityǁ 0.0019525 42.549 8.4202 8.1541 v Pressure -3.3874e+05 1.5445e+05 -93493 -73458 v TurbVisc 1.1554e-20 0.022963 0.0001955 5.0243e-05 v CourantNb 4.5737e-08 0.011431 0.00016945 4.9577e-06 v FourierNb 1.2429e-07 0.041931 0.00014883 4.7613e-07 v total_pressure -2.3742e+05 2.5578e+05 7831.5 27867 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0296 0.10873 0.0029534 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.7346e-07 0.047341 0.00031828 5.4339e-06 INSTANT 0.876289000E-01 TIME STEP NUMBER 56487 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282738573E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.813718436E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.79071E-02 0.20643E+01 Friction velocity uk : 0.79071E-02 0.20643E+01 Dimensionless distance yplus : 0.77651E-02 0.20298E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -4.283155369e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29438E+08 1 0.18452E-09 0.28557E+02 0.20373E+04 c Velocity[X] 0.15961E+02 c Velocity[Y] 0.12596E+02 c Velocity[Z] 0.87646E-06 c Pressure 0.17313E-03 240 0.97697E-04 0.13809E-02 0.10131E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -27.796 42.362 5.6055 7.9958 v Velocity[Y] -30.264 31.906 -0.15561 -0.033739 v Velocity[Z] -3.0118 3.114 2.3586e-06 -5.3902e-08 v ǁVelocityǁ 0.002102 42.559 8.4217 8.1542 v Pressure -3.3753e+05 1.559e+05 -92132 -72634 v TurbVisc 1.2751e-20 0.02298 0.00019555 5.0316e-05 v CourantNb 4.5604e-08 0.01143 0.00016945 4.9577e-06 v FourierNb 1.2429e-07 0.041914 0.00014884 4.7663e-07 v total_pressure -2.362e+05 2.5722e+05 9192.9 28691 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0298 0.10876 0.0029536 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.737e-07 0.047324 0.00031829 5.4344e-06 INSTANT 0.876290000E-01 TIME STEP NUMBER 56488 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282734489E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.813476390E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.43407E-02 0.20644E+01 Friction velocity uk : 0.43407E-02 0.20644E+01 Dimensionless distance yplus : 0.42628E-02 0.20299E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -4.265494160e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29438E+08 1 0.18453E-09 0.28561E+02 0.20374E+04 c Velocity[X] 0.15962E+02 c Velocity[Y] 0.12599E+02 c Velocity[Z] 0.87192E-06 c Pressure 0.17521E-03 36 0.80888E-04 0.13969E-02 0.84439E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -27.809 42.372 5.6055 7.9957 v Velocity[Y] -30.272 31.918 -0.15566 -0.03388 v Velocity[Z] -3.0122 3.1142 2.358e-06 -5.3902e-08 v ǁVelocityǁ 0.0022577 42.57 8.4232 8.1543 v Pressure -3.3633e+05 1.5733e+05 -90732 -71945 v TurbVisc 9.7535e-21 0.022996 0.00019561 5.0389e-05 v CourantNb 4.538e-08 0.011429 0.00016946 4.9578e-06 v FourierNb 1.2429e-07 0.041896 0.00014884 4.7713e-07 v total_pressure -2.35e+05 2.5866e+05 10593 29380 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0299 0.10878 0.0029539 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.7395e-07 0.047306 0.0003183 5.4349e-06 INSTANT 0.876291000E-01 TIME STEP NUMBER 56489 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282730537E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.813241556E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15126E-02 0.20646E+01 Friction velocity uk : 0.15126E-02 0.20646E+01 Dimensionless distance yplus : 0.14854E-02 0.20301E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -4.322966690e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29438E+08 1 0.18455E-09 0.28572E+02 0.20377E+04 c Velocity[X] 0.15964E+02 c Velocity[Y] 0.12609E+02 c Velocity[Z] 0.87627E-06 c Pressure 0.17690E-03 9 0.52299E-04 0.14097E-02 0.84167E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -27.821 42.383 5.6054 7.9956 v Velocity[Y] -30.279 31.93 -0.15571 -0.034023 v Velocity[Z] -3.0126 3.1144 2.3574e-06 -5.3902e-08 v ǁVelocityǁ 0.0024223 42.58 8.4246 8.1544 v Pressure -3.3509e+05 1.588e+05 -89294 -71272 v TurbVisc 8.3207e-21 0.023013 0.00019566 5.0462e-05 v CourantNb 4.5185e-08 0.011429 0.00016946 4.9578e-06 v FourierNb 1.2429e-07 0.041878 0.00014885 4.7763e-07 v total_pressure -2.3377e+05 2.6013e+05 12031 30053 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0301 0.1088 0.0029541 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.742e-07 0.047288 0.00031831 5.4354e-06 INSTANT 0.876292000E-01 TIME STEP NUMBER 56490 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282726828E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.813012985E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.45923E-02 0.20648E+01 Friction velocity uk : 0.45923E-02 0.20648E+01 Dimensionless distance yplus : 0.45099E-02 0.20303E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -4.230668380e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29437E+08 1 0.18456E-09 0.28571E+02 0.20376E+04 c Velocity[X] 0.15966E+02 c Velocity[Y] 0.12605E+02 c Velocity[Z] 0.87415E-06 c Pressure 0.18042E-03 196 0.97617E-04 0.14372E-02 0.11677E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -27.834 42.393 5.6054 7.9955 v Velocity[Y] -30.286 31.941 -0.15576 -0.034166 v Velocity[Z] -3.013 3.1145 2.3568e-06 -5.3902e-08 v ǁVelocityǁ 0.0025755 42.59 8.4261 8.1545 v Pressure -3.338e+05 1.6033e+05 -87868 -70343 v TurbVisc 1.0416e-20 0.023029 0.00019572 5.0535e-05 v CourantNb 4.5058e-08 0.011428 0.00016946 4.9578e-06 v FourierNb 1.2429e-07 0.041861 0.00014886 4.7813e-07 v total_pressure -2.3247e+05 2.6165e+05 13457 30982 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0303 0.10882 0.0029544 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.7444e-07 0.047271 0.00031832 5.4359e-06 INSTANT 0.876293000E-01 TIME STEP NUMBER 56491 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282723125E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.812791652E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.71703E-02 0.20650E+01 Friction velocity uk : 0.71703E-02 0.20650E+01 Dimensionless distance yplus : 0.70415E-02 0.20305E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -4.297155269e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29437E+08 1 0.18458E-09 0.28576E+02 0.20377E+04 c Velocity[X] 0.15970E+02 c Velocity[Y] 0.12607E+02 c Velocity[Z] 0.86806E-06 c Pressure 0.18231E-03 228 0.83210E-04 0.14516E-02 0.98861E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -27.846 42.403 5.6053 7.9954 v Velocity[Y] -30.293 31.953 -0.15582 -0.034308 v Velocity[Z] -3.0134 3.1147 2.3563e-06 -5.3902e-08 v ǁVelocityǁ 0.0027385 42.601 8.4275 8.1546 v Pressure -3.3253e+05 1.6183e+05 -86363 -69528 v TurbVisc 4.2359e-21 0.023046 0.00019577 5.0608e-05 v CourantNb 4.4791e-08 0.011427 0.00016947 4.9578e-06 v FourierNb 1.2429e-07 0.041843 0.00014887 4.7863e-07 v total_pressure -2.3121e+05 2.6315e+05 14962 31797 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0305 0.10885 0.0029546 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.7469e-07 0.047253 0.00031833 5.4364e-06 INSTANT 0.876294000E-01 TIME STEP NUMBER 56492 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282719598E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.812580260E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.87258E-02 0.20652E+01 Friction velocity uk : 0.87258E-02 0.20652E+01 Dimensionless distance yplus : 0.84143E-02 0.20307E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -4.318039625e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29437E+08 1 0.18460E-09 0.28589E+02 0.20381E+04 c Velocity[X] 0.15974E+02 c Velocity[Y] 0.12615E+02 c Velocity[Z] 0.87736E-06 c Pressure 0.18381E-03 9 0.56593E-04 0.14629E-02 0.90121E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -27.858 42.413 5.6053 7.9954 v Velocity[Y] -30.3 31.964 -0.15587 -0.03445 v Velocity[Z] -3.0138 3.1149 2.3557e-06 -5.3902e-08 v ǁVelocityǁ 0.0029114 42.611 8.429 8.1547 v Pressure -3.3128e+05 1.6331e+05 -84874 -68818 v TurbVisc 9.7172e-21 0.023063 0.00019583 5.0681e-05 v CourantNb 4.4633e-08 0.011426 0.00016947 4.9578e-06 v FourierNb 1.2429e-07 0.041825 0.00014888 4.7913e-07 v total_pressure -2.2995e+05 2.6464e+05 16451 32507 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0307 0.10887 0.0029549 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.7494e-07 0.047236 0.00031834 5.4369e-06 INSTANT 0.876295000E-01 TIME STEP NUMBER 56493 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282716207E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.812373404E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10412E-02 0.20654E+01 Friction velocity uk : 0.10412E-02 0.20654E+01 Dimensionless distance yplus : 0.10014E-02 0.20309E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -4.326888782e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29437E+08 1 0.18461E-09 0.28594E+02 0.20382E+04 c Velocity[X] 0.15975E+02 c Velocity[Y] 0.12619E+02 c Velocity[Z] 0.87475E-06 c Pressure 0.18712E-03 231 0.77024E-04 0.14887E-02 0.11837E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -27.871 42.423 5.6053 7.9953 v Velocity[Y] -30.307 31.976 -0.15592 -0.034594 v Velocity[Z] -3.0142 3.115 2.3551e-06 -5.3902e-08 v ǁVelocityǁ 0.0026947 42.622 8.4305 8.1548 v Pressure -3.2991e+05 1.6491e+05 -83386 -67988 v TurbVisc 6.4665e-21 0.023079 0.00019589 5.0755e-05 v CourantNb 4.4479e-08 0.011425 0.00016947 4.9578e-06 v FourierNb 1.2429e-07 0.041807 0.00014888 4.7963e-07 v total_pressure -2.2858e+05 2.6624e+05 17939 33337 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0309 0.10889 0.002955 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.7519e-07 0.047218 0.00031836 5.4375e-06 INSTANT 0.876296000E-01 TIME STEP NUMBER 56494 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282713000E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.812176903E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.32571E-02 0.20656E+01 Friction velocity uk : 0.32571E-02 0.20656E+01 Dimensionless distance yplus : 0.31408E-02 0.20310E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -4.322455732e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29436E+08 1 0.18463E-09 0.28603E+02 0.20384E+04 c Velocity[X] 0.15979E+02 c Velocity[Y] 0.12624E+02 c Velocity[Z] 0.86567E-06 c Pressure 0.18927E-03 68 0.82108E-04 0.15052E-02 0.12005E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -27.883 42.434 5.6052 7.9952 v Velocity[Y] -30.314 31.988 -0.15597 -0.034736 v Velocity[Z] -3.0146 3.1152 2.3545e-06 -5.3902e-08 v ǁVelocityǁ 0.0024841 42.632 8.4319 8.155 v Pressure -3.286e+05 1.6646e+05 -81829 -67150 v TurbVisc 6.1148e-21 0.023096 0.00019594 5.0828e-05 v CourantNb 4.4254e-08 0.011424 0.00016948 4.9578e-06 v FourierNb 1.2429e-07 0.041789 0.00014889 4.8013e-07 v total_pressure -2.2727e+05 2.6778e+05 19496 34175 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.031 0.10892 0.0029555 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.7544e-07 0.0472 0.00031837 5.438e-06 INSTANT 0.876297000E-01 TIME STEP NUMBER 56495 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282709789E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.811988701E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.66757E-02 0.20657E+01 Friction velocity uk : 0.66757E-02 0.20657E+01 Dimensionless distance yplus : 0.64373E-02 0.20312E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -4.410578829e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29436E+08 1 0.18465E-09 0.28614E+02 0.20387E+04 c Velocity[X] 0.15984E+02 c Velocity[Y] 0.12630E+02 c Velocity[Z] 0.86622E-06 c Pressure 0.19172E-03 148 0.95041E-04 0.15239E-02 0.11776E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -27.896 42.444 5.6052 7.9952 v Velocity[Y] -30.321 32 -0.15602 -0.034882 v Velocity[Z] -3.015 3.1154 2.3539e-06 -5.3902e-08 v ǁVelocityǁ 0.0024608 42.643 8.4334 8.1551 v Pressure -3.2722e+05 1.6807e+05 -80282 -66364 v TurbVisc 6.6304e-21 0.023112 0.000196 5.0902e-05 v CourantNb 4.4093e-08 0.011423 0.00016948 4.9579e-06 v FourierNb 1.2429e-07 0.041771 0.0001489 4.8063e-07 v total_pressure -2.2589e+05 2.6939e+05 21043 34961 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0312 0.10895 0.0029559 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.7569e-07 0.047182 0.00031838 5.4385e-06 INSTANT 0.876298000E-01 TIME STEP NUMBER 56496 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282707024E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.811808524E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.81292E-02 0.20659E+01 Friction velocity uk : 0.81292E-02 0.20659E+01 Dimensionless distance yplus : 0.78390E-02 0.20314E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -4.428743319e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29436E+08 1 0.18467E-09 0.28609E+02 0.20385E+04 c Velocity[X] 0.15987E+02 c Velocity[Y] 0.12622E+02 c Velocity[Z] 0.86808E-06 c Pressure 0.19408E-03 75 0.80742E-04 0.15421E-02 0.12064E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -27.908 42.454 5.6051 7.9951 v Velocity[Y] -30.328 32.011 -0.15607 -0.035026 v Velocity[Z] -3.0154 3.1155 2.3533e-06 -5.3902e-08 v ǁVelocityǁ 0.0026273 42.653 8.4348 8.1552 v Pressure -3.2584e+05 1.6967e+05 -78693 -65460 v TurbVisc 7.5283e-21 0.023129 0.00019605 5.0975e-05 v CourantNb 4.3903e-08 0.011422 0.00016948 4.9579e-06 v FourierNb 1.2429e-07 0.041754 0.0001489 4.8113e-07 v total_pressure -2.2452e+05 2.71e+05 22632 35865 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0314 0.10897 0.0029564 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.7595e-07 0.047165 0.00031839 5.439e-06 INSTANT 0.876299000E-01 TIME STEP NUMBER 56497 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282704223E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.811638988E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11911E-01 0.20661E+01 Friction velocity uk : 0.11911E-01 0.20661E+01 Dimensionless distance yplus : 0.11513E-01 0.20316E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -4.483025062e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29436E+08 1 0.18468E-09 0.28625E+02 0.20390E+04 c Velocity[X] 0.15994E+02 c Velocity[Y] 0.12631E+02 c Velocity[Z] 0.87871E-06 c Pressure 0.19330E-03 9 0.57925E-04 0.15352E-02 0.93682E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -27.921 42.465 5.6051 7.995 v Velocity[Y] -30.335 32.023 -0.15612 -0.03517 v Velocity[Z] -3.0158 3.1157 2.3527e-06 -5.3902e-08 v ǁVelocityǁ 0.0029483 42.664 8.4363 8.1553 v Pressure -3.2455e+05 1.712e+05 -77124 -64745 v TurbVisc 6.7382e-21 0.023145 0.00019611 5.1049e-05 v CourantNb 4.3712e-08 0.011422 0.00016949 4.9579e-06 v FourierNb 1.2429e-07 0.041736 0.00014891 4.8163e-07 v total_pressure -2.2322e+05 2.7252e+05 24201 36580 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0316 0.109 0.0029568 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.762e-07 0.047147 0.0003184 5.4395e-06 INSTANT 0.876300000E-01 TIME STEP NUMBER 56498 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282701612E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.811478153E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12420E-01 0.20663E+01 Friction velocity uk : 0.12420E-01 0.20663E+01 Dimensionless distance yplus : 0.12005E-01 0.20318E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -4.492623844e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29436E+08 1 0.18470E-09 0.28631E+02 0.20391E+04 c Velocity[X] 0.15995E+02 c Velocity[Y] 0.12636E+02 c Velocity[Z] 0.87374E-06 c Pressure 0.19599E-03 162 0.76815E-04 0.15559E-02 0.13585E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -27.934 42.475 5.605 7.995 v Velocity[Y] -30.342 32.035 -0.15617 -0.035317 v Velocity[Z] -3.0162 3.1159 2.3521e-06 -5.3902e-08 v ǁVelocityǁ 0.0030908 42.675 8.4377 8.1555 v Pressure -3.2304e+05 1.7294e+05 -75512 -63793 v TurbVisc 7.401e-21 0.023162 0.00019617 5.1123e-05 v CourantNb 4.3544e-08 0.011421 0.00016949 4.9579e-06 v FourierNb 1.2429e-07 0.041718 0.00014892 4.8214e-07 v total_pressure -2.2171e+05 2.7426e+05 25813 37532 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0318 0.10903 0.0029572 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.7646e-07 0.047129 0.00031841 5.4401e-06 INSTANT 0.876301000E-01 TIME STEP NUMBER 56499 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282699172E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.811327961E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12766E-01 0.20665E+01 Friction velocity uk : 0.12766E-01 0.20665E+01 Dimensionless distance yplus : 0.12340E-01 0.20320E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -4.463806298e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29436E+08 1 0.18472E-09 0.28643E+02 0.20395E+04 c Velocity[X] 0.16001E+02 c Velocity[Y] 0.12642E+02 c Velocity[Z] 0.86771E-06 c Pressure 0.19769E-03 82 0.82676E-04 0.15687E-02 0.13159E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -27.946 42.485 5.605 7.9949 v Velocity[Y] -30.349 32.047 -0.15622 -0.035461 v Velocity[Z] -3.0166 3.116 2.3515e-06 -5.3903e-08 v ǁVelocityǁ 0.0030923 42.685 8.4392 8.1556 v Pressure -3.2163e+05 1.7457e+05 -73864 -62892 v TurbVisc 5.8119e-21 0.023179 0.00019622 5.1196e-05 v CourantNb 4.5721e-08 0.01142 0.00016949 4.9579e-06 v FourierNb 1.2429e-07 0.041699 0.00014893 4.8264e-07 v total_pressure -2.2031e+05 2.759e+05 27461 38433 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.032 0.10906 0.0029576 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.7671e-07 0.047111 0.00031842 5.4406e-06 INSTANT 0.876302000E-01 TIME STEP NUMBER 56500 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282696735E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.811183945E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13256E-01 0.20667E+01 Friction velocity uk : 0.13256E-01 0.20667E+01 Dimensionless distance yplus : 0.12814E-01 0.20322E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -4.535602543e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29435E+08 1 0.18474E-09 0.28656E+02 0.20398E+04 c Velocity[X] 0.16007E+02 c Velocity[Y] 0.12649E+02 c Velocity[Z] 0.86295E-06 c Pressure 0.19962E-03 305 0.95710E-04 0.15833E-02 0.13044E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -27.959 42.496 5.6049 7.9949 v Velocity[Y] -30.356 32.058 -0.15627 -0.035609 v Velocity[Z] -3.017 3.1162 2.3509e-06 -5.3903e-08 v ǁVelocityǁ 0.0030952 42.696 8.4406 8.1558 v Pressure -3.2014e+05 1.7629e+05 -72210 -62027 v TurbVisc 6.4151e-21 0.023195 0.00019628 5.127e-05 v CourantNb 4.8202e-08 0.011419 0.0001695 4.958e-06 v FourierNb 1.2429e-07 0.041681 0.00014893 4.8315e-07 v total_pressure -2.1882e+05 2.7762e+05 29115 39298 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0322 0.10908 0.0029579 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.7697e-07 0.047093 0.00031843 5.4411e-06 INSTANT 0.876303000E-01 TIME STEP NUMBER 56501 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282694750E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.811047945E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13797E-01 0.20669E+01 Friction velocity uk : 0.13797E-01 0.20669E+01 Dimensionless distance yplus : 0.13337E-01 0.20323E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -4.569927406e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29435E+08 1 0.18476E-09 0.28654E+02 0.20397E+04 c Velocity[X] 0.16013E+02 c Velocity[Y] 0.12641E+02 c Velocity[Z] 0.86313E-06 c Pressure 0.20152E-03 124 0.81554E-04 0.15977E-02 0.12505E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -27.971 42.506 5.6049 7.9948 v Velocity[Y] -30.363 32.07 -0.15632 -0.035756 v Velocity[Z] -3.0174 3.1164 2.3503e-06 -5.3903e-08 v ǁVelocityǁ 0.0030956 42.707 8.4421 8.1559 v Pressure -3.1873e+05 1.7794e+05 -70562 -61118 v TurbVisc 5.4856e-21 0.023212 0.00019634 5.1344e-05 v CourantNb 5.0956e-08 0.011418 0.0001695 4.958e-06 v FourierNb 1.2429e-07 0.041663 0.00014894 4.8365e-07 v total_pressure -2.174e+05 2.7926e+05 30763 40207 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0323 0.10911 0.0029583 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.7723e-07 0.047075 0.00031844 5.4416e-06 INSTANT 0.876304000E-01 TIME STEP NUMBER 56502 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282692737E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.810922140E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.14391E-01 0.20671E+01 Friction velocity uk : 0.14391E-01 0.20671E+01 Dimensionless distance yplus : 0.13910E-01 0.20325E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -4.553288842e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29435E+08 1 0.18477E-09 0.28672E+02 0.20403E+04 c Velocity[X] 0.16021E+02 c Velocity[Y] 0.12651E+02 c Velocity[Z] 0.87795E-06 c Pressure 0.20022E-03 9 0.58773E-04 0.15867E-02 0.10335E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -27.984 42.517 5.6048 7.9948 v Velocity[Y] -30.37 32.082 -0.15637 -0.035902 v Velocity[Z] -3.0178 3.1165 2.3497e-06 -5.3903e-08 v ǁVelocityǁ 0.003104 42.717 8.4435 8.156 v Pressure -3.1736e+05 1.7954e+05 -68909 -60346 v TurbVisc 5.6944e-21 0.023228 0.00019639 5.1418e-05 v CourantNb 5.3574e-08 0.011417 0.0001695 4.958e-06 v FourierNb 1.2429e-07 0.041645 0.00014895 4.8416e-07 v total_pressure -2.1603e+05 2.8086e+05 32416 40979 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0325 0.10913 0.0029586 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.7749e-07 0.047057 0.00031845 5.4422e-06 INSTANT 0.876305000E-01 TIME STEP NUMBER 56503 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282690927E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.810808316E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15032E-01 0.20673E+01 Friction velocity uk : 0.15032E-01 0.20673E+01 Dimensionless distance yplus : 0.14530E-01 0.20327E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -4.523288021e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29435E+08 1 0.18479E-09 0.28681E+02 0.20405E+04 c Velocity[X] 0.16024E+02 c Velocity[Y] 0.12657E+02 c Velocity[Z] 0.87495E-06 c Pressure 0.20237E-03 369 0.77619E-04 0.16031E-02 0.14616E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -27.997 42.528 5.6048 7.9947 v Velocity[Y] -30.377 32.094 -0.15642 -0.03605 v Velocity[Z] -3.0182 3.1167 2.3491e-06 -5.3903e-08 v ǁVelocityǁ 0.0030962 42.728 8.445 8.1562 v Pressure -3.1578e+05 1.8135e+05 -67225 -59348 v TurbVisc 6.0757e-21 0.023245 0.00019645 5.1492e-05 v CourantNb 5.6632e-08 0.011416 0.00016951 4.9581e-06 v FourierNb 1.2429e-07 0.041627 0.00014895 4.8466e-07 v total_pressure -2.1445e+05 2.8267e+05 34100 41977 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0327 0.10916 0.002959 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.7775e-07 0.047038 0.00031846 5.4427e-06 INSTANT 0.876306000E-01 TIME STEP NUMBER 56504 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282689285E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.810705755E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13802E-01 0.20675E+01 Friction velocity uk : 0.13802E-01 0.20675E+01 Dimensionless distance yplus : 0.13410E-01 0.20329E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -4.455218334e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29435E+08 1 0.18481E-09 0.28696E+02 0.20409E+04 c Velocity[X] 0.16033E+02 c Velocity[Y] 0.12663E+02 c Velocity[Z] 0.86793E-06 c Pressure 0.20353E-03 63 0.83722E-04 0.16116E-02 0.14597E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -28.009 42.538 5.6048 7.9947 v Velocity[Y] -30.384 32.106 -0.15646 -0.036197 v Velocity[Z] -3.0186 3.1169 2.3485e-06 -5.3903e-08 v ǁVelocityǁ 0.0030969 42.739 8.4465 8.1563 v Pressure -3.143e+05 1.8306e+05 -65495 -58357 v TurbVisc 5.4493e-21 0.023261 0.00019651 5.1566e-05 v CourantNb 5.8863e-08 0.011415 0.00016951 4.9581e-06 v FourierNb 1.2429e-07 0.041609 0.00014896 4.8517e-07 v total_pressure -2.1298e+05 2.8438e+05 35830 42968 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0329 0.10918 0.0029593 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.7799e-07 0.04702 0.00031847 5.4432e-06 INSTANT 0.876307000E-01 TIME STEP NUMBER 56505 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282687687E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.810609944E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12929E-01 0.20677E+01 Friction velocity uk : 0.12929E-01 0.20677E+01 Dimensionless distance yplus : 0.12562E-01 0.20331E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -4.460961954e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29435E+08 1 0.18483E-09 0.28711E+02 0.20414E+04 c Velocity[X] 0.16040E+02 c Velocity[Y] 0.12671E+02 c Velocity[Z] 0.86575E-06 c Pressure 0.20496E-03 228 0.96980E-04 0.16222E-02 0.13161E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -28.022 42.549 5.6047 7.9947 v Velocity[Y] -30.391 32.118 -0.15651 -0.036347 v Velocity[Z] -3.019 3.117 2.3479e-06 -5.3903e-08 v ǁVelocityǁ 0.0030968 42.75 8.4479 8.1565 v Pressure -3.1279e+05 1.8479e+05 -63810 -57558 v TurbVisc 4.72e-21 0.023278 0.00019656 5.1641e-05 v CourantNb 6.123e-08 0.011414 0.00016951 4.9581e-06 v FourierNb 1.243e-07 0.04159 0.00014897 4.8567e-07 v total_pressure -2.1147e+05 2.8612e+05 37515 43767 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0331 0.10921 0.0029596 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.78e-07 0.047002 0.00031848 5.4438e-06 INSTANT 0.876308000E-01 TIME STEP NUMBER 56506 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282686480E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.810521822E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12760E-01 0.20679E+01 Friction velocity uk : 0.12760E-01 0.20679E+01 Dimensionless distance yplus : 0.12397E-01 0.20333E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -4.405421984e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29435E+08 1 0.18485E-09 0.28711E+02 0.20413E+04 c Velocity[X] 0.16048E+02 c Velocity[Y] 0.12664E+02 c Velocity[Z] 0.86348E-06 c Pressure 0.20629E-03 125 0.82492E-04 0.16320E-02 0.13788E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -28.035 42.56 5.6047 7.9946 v Velocity[Y] -30.397 32.13 -0.15656 -0.036495 v Velocity[Z] -3.0195 3.1172 2.3474e-06 -5.3903e-08 v ǁVelocityǁ 0.0030982 42.761 8.4494 8.1567 v Pressure -3.1131e+05 1.865e+05 -62089 -56574 v TurbVisc 4.6096e-21 0.023294 0.00019662 5.1715e-05 v CourantNb 6.3719e-08 0.011413 0.00016952 4.9581e-06 v FourierNb 1.243e-07 0.041572 0.00014897 4.8618e-07 v total_pressure -2.0999e+05 2.8783e+05 39236 44751 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0333 0.10923 0.0029599 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.7801e-07 0.046984 0.00031849 5.4443e-06 INSTANT 0.876309000E-01 TIME STEP NUMBER 56507 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282685283E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.810445979E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13313E-01 0.20681E+01 Friction velocity uk : 0.13313E-01 0.20681E+01 Dimensionless distance yplus : 0.12934E-01 0.20335E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -4.343983461e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29435E+08 1 0.18487E-09 0.28733E+02 0.20420E+04 c Velocity[X] 0.16058E+02 c Velocity[Y] 0.12675E+02 c Velocity[Z] 0.88126E-06 c Pressure 0.20445E-03 9 0.59524E-04 0.16167E-02 0.11020E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -28.047 42.57 5.6046 7.9946 v Velocity[Y] -30.404 32.142 -0.15661 -0.036643 v Velocity[Z] -3.0199 3.1173 2.3468e-06 -5.3903e-08 v ǁVelocityǁ 0.002846 42.772 8.4508 8.1568 v Pressure -3.0991e+05 1.8813e+05 -60387 -55773 v TurbVisc 4.3017e-21 0.023311 0.00019668 5.1789e-05 v CourantNb 6.619e-08 0.011413 0.00016952 4.9582e-06 v FourierNb 1.243e-07 0.041554 0.00014897 4.8669e-07 v total_pressure -2.0859e+05 2.8946e+05 40938 45552 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0335 0.10925 0.0029602 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.7802e-07 0.046966 0.00031849 5.4449e-06 INSTANT 0.876310000E-01 TIME STEP NUMBER 56508 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282684298E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.810381226E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.14290E-01 0.20683E+01 Friction velocity uk : 0.14290E-01 0.20683E+01 Dimensionless distance yplus : 0.13883E-01 0.20338E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -4.218584434e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29435E+08 1 0.18488E-09 0.28745E+02 0.20423E+04 c Velocity[X] 0.16063E+02 c Velocity[Y] 0.12681E+02 c Velocity[Z] 0.87629E-06 c Pressure 0.20607E-03 153 0.78619E-04 0.16288E-02 0.15488E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -28.06 42.581 5.6046 7.9946 v Velocity[Y] -30.411 32.154 -0.15666 -0.036794 v Velocity[Z] -3.0203 3.1175 2.3462e-06 -5.3903e-08 v ǁVelocityǁ 0.0025653 42.783 8.4523 8.157 v Pressure -3.0828e+05 1.8998e+05 -58658 -54746 v TurbVisc 4.7452e-21 0.023327 0.00019673 5.1864e-05 v CourantNb 6.9135e-08 0.011412 0.00016952 4.9582e-06 v FourierNb 1.243e-07 0.041535 0.00014898 4.872e-07 v total_pressure -2.0696e+05 2.9131e+05 42667 46579 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0338 0.10928 0.0029606 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.7803e-07 0.046948 0.0003185 5.4454e-06 INSTANT 0.876311000E-01 TIME STEP NUMBER 56509 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282683479E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.810328365E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15440E-01 0.20685E+01 Friction velocity uk : 0.15440E-01 0.20685E+01 Dimensionless distance yplus : 0.15001E-01 0.20340E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -4.081103932e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29435E+08 1 0.18491E-09 0.28762E+02 0.20429E+04 c Velocity[X] 0.16074E+02 c Velocity[Y] 0.12688E+02 c Velocity[Z] 0.86836E-06 c Pressure 0.20669E-03 64 0.84668E-04 0.16330E-02 0.15410E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -28.073 42.592 5.6046 7.9946 v Velocity[Y] -30.418 32.166 -0.1567 -0.036943 v Velocity[Z] -3.0207 3.1177 2.3456e-06 -5.3903e-08 v ǁVelocityǁ 0.0023522 42.794 8.4537 8.1572 v Pressure -3.0678e+05 1.9172e+05 -56887 -53727 v TurbVisc 3.9035e-21 0.023344 0.00019679 5.1938e-05 v CourantNb 7.1117e-08 0.011411 0.00016953 4.9582e-06 v FourierNb 1.243e-07 0.041517 0.00014898 4.877e-07 v total_pressure -2.0546e+05 2.9304e+05 44438 47598 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.034 0.1093 0.0029608 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.7805e-07 0.046929 0.0003185 5.4459e-06 INSTANT 0.876312000E-01 TIME STEP NUMBER 56510 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282682706E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.810282582E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.16684E-01 0.20688E+01 Friction velocity uk : 0.16684E-01 0.20688E+01 Dimensionless distance yplus : 0.16209E-01 0.20342E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -4.000411206e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29435E+08 1 0.18492E-09 0.28781E+02 0.20435E+04 c Velocity[X] 0.16083E+02 c Velocity[Y] 0.12698E+02 c Velocity[Z] 0.86868E-06 c Pressure 0.20758E-03 114 0.98020E-04 0.16394E-02 0.13510E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -28.086 42.603 5.6045 7.9945 v Velocity[Y] -30.425 32.178 -0.15675 -0.037095 v Velocity[Z] -3.0211 3.1178 2.345e-06 -5.3903e-08 v ǁVelocityǁ 0.0022249 42.805 8.4552 8.1573 v Pressure -3.0527e+05 1.9346e+05 -55177 -52941 v TurbVisc 3.5467e-21 0.02336 0.00019685 5.2013e-05 v CourantNb 7.3224e-08 0.01141 0.00016953 4.9583e-06 v FourierNb 1.243e-07 0.041499 0.00014898 4.8821e-07 v total_pressure -2.0394e+05 2.9479e+05 46148 48384 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0342 0.10933 0.0029611 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.7806e-07 0.046911 0.00031851 5.4465e-06 INSTANT 0.876313000E-01 TIME STEP NUMBER 56511 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282682329E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.810244486E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.17926E-01 0.20690E+01 Friction velocity uk : 0.17926E-01 0.20690E+01 Dimensionless distance yplus : 0.17416E-01 0.20344E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -3.854391393e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29435E+08 1 0.18495E-09 0.28784E+02 0.20435E+04 c Velocity[X] 0.16093E+02 c Velocity[Y] 0.12690E+02 c Velocity[Z] 0.86746E-06 c Pressure 0.20835E-03 124 0.83457E-04 0.16447E-02 0.15076E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -28.099 42.614 5.6045 7.9945 v Velocity[Y] -30.432 32.19 -0.1568 -0.037246 v Velocity[Z] -3.0215 3.118 2.3444e-06 -5.3903e-08 v ǁVelocityǁ 0.0021989 42.816 8.4567 8.1575 v Pressure -3.0375e+05 1.9521e+05 -53411 -51891 v TurbVisc 3.4539e-21 0.023377 0.00019691 5.2087e-05 v CourantNb 7.546e-08 0.011409 0.00016953 4.9583e-06 v FourierNb 1.243e-07 0.04148 0.00014898 4.8872e-07 v total_pressure -2.0242e+05 2.9654e+05 47914 49434 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0344 0.10935 0.0029614 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.7811e-07 0.046893 0.00031851 5.447e-06 INSTANT 0.876314000E-01 TIME STEP NUMBER 56512 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282681968E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.810219628E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.18802E-01 0.20692E+01 Friction velocity uk : 0.18802E-01 0.20692E+01 Dimensionless distance yplus : 0.18175E-01 0.20346E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -3.701558961e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29435E+08 1 0.18497E-09 0.28808E+02 0.20443E+04 c Velocity[X] 0.16106E+02 c Velocity[Y] 0.12702E+02 c Velocity[Z] 0.88867E-06 c Pressure 0.20594E-03 9 0.60141E-04 0.16250E-02 0.11296E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -28.111 42.625 5.6045 7.9945 v Velocity[Y] -30.439 32.202 -0.15685 -0.037396 v Velocity[Z] -3.0219 3.1182 2.3438e-06 -5.3903e-08 v ǁVelocityǁ 0.0019671 42.827 8.4581 8.1577 v Pressure -3.0234e+05 1.9685e+05 -51692 -51096 v TurbVisc 3.3009e-21 0.023393 0.00019697 5.2162e-05 v CourantNb 7.7661e-08 0.011408 0.00016954 4.9584e-06 v FourierNb 1.243e-07 0.041462 0.00014899 4.8923e-07 v total_pressure -2.0101e+05 2.9817e+05 49633 50229 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0346 0.10937 0.0029617 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.7847e-07 0.046875 0.00031852 5.4476e-06 INSTANT 0.876315000E-01 TIME STEP NUMBER 56513 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282681814E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.810205118E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19066E-01 0.20695E+01 Friction velocity uk : 0.19066E-01 0.20695E+01 Dimensionless distance yplus : 0.18429E-01 0.20349E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -3.461095310e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29435E+08 1 0.18498E-09 0.28823E+02 0.20447E+04 c Velocity[X] 0.16114E+02 c Velocity[Y] 0.12710E+02 c Velocity[Z] 0.88273E-06 c Pressure 0.20703E-03 404 0.79309E-04 0.16329E-02 0.16039E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -28.124 42.636 5.6045 7.9945 v Velocity[Y] -30.446 32.215 -0.15689 -0.037549 v Velocity[Z] -3.0223 3.1183 2.3432e-06 -5.3903e-08 v ǁVelocityǁ 0.0017608 42.839 8.4596 8.1579 v Pressure -3.0071e+05 1.987e+05 -49947 -50066 v TurbVisc 3.568e-21 0.02341 0.00019702 5.2237e-05 v CourantNb 8.0332e-08 0.011407 0.00016954 4.9584e-06 v FourierNb 1.243e-07 0.041444 0.00014899 4.8974e-07 v total_pressure -1.9939e+05 3.0002e+05 51378 51259 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0349 0.1094 0.002962 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.7884e-07 0.046857 0.00031853 5.4481e-06 INSTANT 0.876316000E-01 TIME STEP NUMBER 56514 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282681834E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.810202767E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.18923E-01 0.20697E+01 Friction velocity uk : 0.18923E-01 0.20697E+01 Dimensionless distance yplus : 0.18291E-01 0.20351E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -3.256036264e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29435E+08 1 0.18500E-09 0.28844E+02 0.20453E+04 c Velocity[X] 0.16126E+02 c Velocity[Y] 0.12717E+02 c Velocity[Z] 0.87571E-06 c Pressure 0.20710E-03 62 0.85501E-04 0.16327E-02 0.16046E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -28.137 42.647 5.6044 7.9945 v Velocity[Y] -30.453 32.227 -0.15694 -0.0377 v Velocity[Z] -3.0227 3.1185 2.3426e-06 -5.3903e-08 v ǁVelocityǁ 0.0016813 42.85 8.461 8.1581 v Pressure -2.9921e+05 2.0044e+05 -48161 -49036 v TurbVisc 3.1459e-21 0.023426 0.00019708 5.2311e-05 v CourantNb 8.201e-08 0.011406 0.00016954 4.9584e-06 v FourierNb 1.243e-07 0.041426 0.000149 4.9025e-07 v total_pressure -1.9788e+05 3.0176e+05 53164 52289 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0351 0.10942 0.0029623 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.7921e-07 0.046839 0.00031854 5.4487e-06 INSTANT 0.876317000E-01 TIME STEP NUMBER 56515 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282681895E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.810207844E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.18472E-01 0.20700E+01 Friction velocity uk : 0.18472E-01 0.20700E+01 Dimensionless distance yplus : 0.17946E-01 0.20354E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -3.065283849e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29435E+08 1 0.18502E-09 0.28866E+02 0.20460E+04 c Velocity[X] 0.16138E+02 c Velocity[Y] 0.12728E+02 c Velocity[Z] 0.87448E-06 c Pressure 0.20746E-03 235 0.98982E-04 0.16348E-02 0.14250E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -28.15 42.658 5.6044 7.9945 v Velocity[Y] -30.459 32.239 -0.15699 -0.037855 v Velocity[Z] -3.0231 3.1187 2.342e-06 -5.3903e-08 v ǁVelocityǁ 0.0017498 42.861 8.4625 8.1582 v Pressure -2.9768e+05 2.0219e+05 -46436 -48225 v TurbVisc 2.5994e-21 0.023443 0.00019714 5.2386e-05 v CourantNb 8.3807e-08 0.011405 0.00016955 4.9585e-06 v FourierNb 1.243e-07 0.041407 0.00014901 4.9076e-07 v total_pressure -1.9636e+05 3.0351e+05 54889 53100 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0354 0.10944 0.0029626 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.7958e-07 0.046821 0.00031856 5.4493e-06 INSTANT 0.876318000E-01 TIME STEP NUMBER 56516 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282682360E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.810220455E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.18085E-01 0.20703E+01 Friction velocity uk : 0.18085E-01 0.20703E+01 Dimensionless distance yplus : 0.17570E-01 0.20357E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -2.819852068e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29435E+08 1 0.18505E-09 0.28871E+02 0.20461E+04 c Velocity[X] 0.16150E+02 c Velocity[Y] 0.12722E+02 c Velocity[Z] 0.87609E-06 c Pressure 0.20772E-03 391 0.84307E-04 0.16361E-02 0.14690E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -28.163 42.669 5.6044 7.9945 v Velocity[Y] -30.466 32.251 -0.15704 -0.038008 v Velocity[Z] -3.0235 3.1188 2.3415e-06 -5.3903e-08 v ǁVelocityǁ 0.0019565 42.873 8.464 8.1584 v Pressure -2.9621e+05 2.0389e+05 -44690 -47240 v TurbVisc 2.5028e-21 0.023459 0.0001972 5.2461e-05 v CourantNb 8.5732e-08 0.011404 0.00016955 4.9585e-06 v FourierNb 1.243e-07 0.041389 0.00014902 4.9128e-07 v total_pressure -1.9489e+05 3.0521e+05 56635 54085 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0357 0.10946 0.0029629 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.7995e-07 0.046803 0.00031857 5.4498e-06 INSTANT 0.876319000E-01 TIME STEP NUMBER 56517 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282682816E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.810245787E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.17838E-01 0.20706E+01 Friction velocity uk : 0.17838E-01 0.20706E+01 Dimensionless distance yplus : 0.17327E-01 0.20359E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -2.569746708e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29436E+08 1 0.18506E-09 0.28899E+02 0.20470E+04 c Velocity[X] 0.16166E+02 c Velocity[Y] 0.12733E+02 c Velocity[Z] 0.89568E-06 c Pressure 0.20464E-03 9 0.60746E-04 0.16112E-02 0.12352E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -28.176 42.681 5.6044 7.9945 v Velocity[Y] -30.473 32.264 -0.15708 -0.03816 v Velocity[Z] -3.0239 3.119 2.3409e-06 -5.3904e-08 v ǁVelocityǁ 0.0022702 42.884 8.4654 8.1586 v Pressure -2.9479e+05 2.0554e+05 -42954 -46384 v TurbVisc 2.3913e-21 0.023476 0.00019726 5.2536e-05 v CourantNb 8.7612e-08 0.011404 0.00016956 4.9586e-06 v FourierNb 1.243e-07 0.041371 0.00014903 4.9179e-07 v total_pressure -1.9346e+05 3.0686e+05 58371 54941 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0359 0.10949 0.0029632 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.8032e-07 0.046785 0.00031858 5.4504e-06 INSTANT 0.876320000E-01 TIME STEP NUMBER 56518 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282683520E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.810282775E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.16258E-01 0.20709E+01 Friction velocity uk : 0.16258E-01 0.20709E+01 Dimensionless distance yplus : 0.15635E-01 0.20362E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -2.220047820e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29436E+08 1 0.18508E-09 0.28917E+02 0.20476E+04 c Velocity[X] 0.16175E+02 c Velocity[Y] 0.12742E+02 c Velocity[Z] 0.88900E-06 c Pressure 0.20525E-03 158 0.80258E-04 0.16153E-02 0.16346E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -28.189 42.692 5.6044 7.9945 v Velocity[Y] -30.48 32.276 -0.15713 -0.038315 v Velocity[Z] -3.0243 3.1191 2.3403e-06 -5.3904e-08 v ǁVelocityǁ 0.002659 42.896 8.4669 8.1588 v Pressure -2.9317e+05 2.0738e+05 -41224 -45378 v TurbVisc 2.6239e-21 0.023492 0.00019732 5.2611e-05 v CourantNb 9.0054e-08 0.011403 0.00016956 4.9586e-06 v FourierNb 1.243e-07 0.041353 0.00014904 4.923e-07 v total_pressure -1.9184e+05 3.0871e+05 60101 55947 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0362 0.10951 0.0029635 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.8069e-07 0.046767 0.0003186 5.4509e-06 INSTANT 0.876321000E-01 TIME STEP NUMBER 56519 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282684366E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.810330989E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13570E-01 0.20711E+01 Friction velocity uk : 0.13570E-01 0.20711E+01 Dimensionless distance yplus : 0.13050E-01 0.20365E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.952793880e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29436E+08 1 0.18510E-09 0.28941E+02 0.20483E+04 c Velocity[X] 0.16190E+02 c Velocity[Y] 0.12751E+02 c Velocity[Z] 0.88117E-06 c Pressure 0.20479E-03 64 0.86550E-04 0.16109E-02 0.16390E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -28.202 42.703 5.6044 7.9945 v Velocity[Y] -30.487 32.289 -0.15718 -0.038468 v Velocity[Z] -3.0247 3.1193 2.3397e-06 -5.3904e-08 v ǁVelocityǁ 0.0025209 42.907 8.4684 8.159 v Pressure -2.917e+05 2.0908e+05 -39453 -44356 v TurbVisc 2.0437e-21 0.023509 0.00019738 5.2687e-05 v CourantNb 9.1362e-08 0.011402 0.00016956 4.9587e-06 v FourierNb 1.243e-07 0.041335 0.00014905 4.9281e-07 v total_pressure -1.9038e+05 3.104e+05 61872 56969 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0365 0.10954 0.0029638 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.8107e-07 0.046749 0.00031861 5.4515e-06 INSTANT 0.876322000E-01 TIME STEP NUMBER 56520 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282685260E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.810386608E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11035E-01 0.20715E+01 Friction velocity uk : 0.11035E-01 0.20715E+01 Dimensionless distance yplus : 0.10612E-01 0.20368E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.659386012e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29436E+08 1 0.18512E-09 0.28953E+02 0.20486E+04 c Velocity[X] 0.16203E+02 c Velocity[Y] 0.12750E+02 c Velocity[Z] 0.88106E-06 c Pressure 0.20462E-03 172 0.75060E-04 0.16089E-02 0.12537E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -28.216 42.715 5.6044 7.9946 v Velocity[Y] -30.494 32.301 -0.15723 -0.038623 v Velocity[Z] -3.0251 3.1195 2.3391e-06 -5.3904e-08 v ǁVelocityǁ 0.0023789 42.919 8.4699 8.1593 v Pressure -2.9023e+05 2.1078e+05 -37753 -43560 v TurbVisc 1.9287e-21 0.023525 0.00019743 5.2762e-05 v CourantNb 9.2817e-08 0.011401 0.00016957 4.9587e-06 v FourierNb 1.243e-07 0.041317 0.00014906 4.9333e-07 v total_pressure -1.8891e+05 3.121e+05 63572 57765 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0368 0.10956 0.0029642 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.8145e-07 0.046732 0.00031863 5.4521e-06 INSTANT 0.876323000E-01 TIME STEP NUMBER 56521 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282686423E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.810449632E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.89214E-02 0.20718E+01 Friction velocity uk : 0.89214E-02 0.20718E+01 Dimensionless distance yplus : 0.85796E-02 0.20372E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.329884144e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29436E+08 1 0.18514E-09 0.28982E+02 0.20496E+04 c Velocity[X] 0.16219E+02 c Velocity[Y] 0.12762E+02 c Velocity[Z] 0.89642E-06 c Pressure 0.20161E-03 9 0.54417E-04 0.15845E-02 0.11432E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -28.229 42.726 5.6044 7.9946 v Velocity[Y] -30.501 32.313 -0.15728 -0.03878 v Velocity[Z] -3.0255 3.1196 2.3385e-06 -5.3904e-08 v ǁVelocityǁ 0.0022363 42.931 8.4713 8.1595 v Pressure -2.8886e+05 2.1238e+05 -36051 -42763 v TurbVisc 1.8771e-21 0.023542 0.00019749 5.2837e-05 v CourantNb 9.4452e-08 0.0114 0.00016957 4.9588e-06 v FourierNb 1.243e-07 0.041299 0.00014907 4.9384e-07 v total_pressure -1.8753e+05 3.1371e+05 65274 58562 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0372 0.10958 0.0029645 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.8183e-07 0.046714 0.00031864 5.4526e-06 INSTANT 0.876324000E-01 TIME STEP NUMBER 56522 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282687931E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.810525708E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.93271E-02 0.20722E+01 Friction velocity uk : 0.93271E-02 0.20722E+01 Dimensionless distance yplus : 0.89698E-02 0.20375E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -9.096528820e-03 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29437E+08 1 0.18517E-09 0.28997E+02 0.20500E+04 c Velocity[X] 0.16233E+02 c Velocity[Y] 0.12764E+02 c Velocity[Z] 0.89558E-06 c Pressure 0.20150E-03 67 0.95790E-04 0.15829E-02 0.16558E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -28.242 42.738 5.6044 7.9946 v Velocity[Y] -30.508 32.326 -0.15733 -0.038936 v Velocity[Z] -3.0259 3.1198 2.3379e-06 -5.3904e-08 v ǁVelocityǁ 0.0021217 42.942 8.4728 8.1597 v Pressure -2.8731e+05 2.1418e+05 -34336 -41655 v TurbVisc 2.0395e-21 0.023558 0.00019755 5.2913e-05 v CourantNb 9.6564e-08 0.011399 0.00016958 4.9589e-06 v FourierNb 1.243e-07 0.041281 0.00014908 4.9436e-07 v total_pressure -1.8599e+05 3.155e+05 66989 59670 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0375 0.10961 0.0029648 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.8221e-07 0.046696 0.00031866 5.4532e-06 INSTANT 0.876325000E-01 TIME STEP NUMBER 56523 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282689414E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.810614531E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.52072E-02 0.20725E+01 Friction velocity uk : 0.52072E-02 0.20725E+01 Dimensionless distance yplus : 0.50077E-02 0.20379E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -6.544951975e-03 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29437E+08 1 0.18518E-09 0.29020E+02 0.20507E+04 c Velocity[X] 0.16249E+02 c Velocity[Y] 0.12771E+02 c Velocity[Z] 0.88700E-06 c Pressure 0.20001E-03 244 0.80129E-04 0.15705E-02 0.13948E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -28.255 42.749 5.6044 7.9946 v Velocity[Y] -30.515 32.338 -0.15738 -0.039092 v Velocity[Z] -3.0263 3.12 2.3374e-06 -5.3904e-08 v ǁVelocityǁ 0.0020078 42.954 8.4743 8.1599 v Pressure -2.8588e+05 2.1587e+05 -32596 -40703 v TurbVisc 1.727e-21 0.023574 0.00019761 5.2988e-05 v CourantNb 9.7664e-08 0.011398 0.00016958 4.9589e-06 v FourierNb 1.243e-07 0.041263 0.00014909 4.9487e-07 v total_pressure -1.8456e+05 3.1719e+05 68729 60622 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0379 0.10963 0.0029652 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.8259e-07 0.046679 0.00031867 5.4538e-06 INSTANT 0.876326000E-01 TIME STEP NUMBER 56524 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282691049E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.810712469E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.56812E-02 0.20729E+01 Friction velocity uk : 0.56812E-02 0.20729E+01 Dimensionless distance yplus : 0.54636E-02 0.20382E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.996473504e-03 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29437E+08 1 0.18521E-09 0.29051E+02 0.20517E+04 c Velocity[X] 0.16266E+02 c Velocity[Y] 0.12784E+02 c Velocity[Z] 0.90357E-06 c Pressure 0.19818E-03 9 0.54104E-04 0.15555E-02 0.12497E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -28.269 42.761 5.6044 7.9947 v Velocity[Y] -30.522 32.351 -0.15743 -0.039248 v Velocity[Z] -3.0267 3.1201 2.3368e-06 -5.3904e-08 v ǁVelocityǁ 0.0019091 42.966 8.4758 8.1601 v Pressure -2.8452e+05 2.1749e+05 -30900 -39868 v TurbVisc 2.7461e-21 0.023591 0.00019767 5.3064e-05 v CourantNb 9.8479e-08 0.011397 0.00016958 4.959e-06 v FourierNb 1.243e-07 0.041245 0.0001491 4.9539e-07 v total_pressure -1.8319e+05 3.1882e+05 70425 61457 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0382 0.10966 0.0029655 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.8297e-07 0.046661 0.00031869 5.4544e-06 INSTANT 0.876327000E-01 TIME STEP NUMBER 56525 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282692855E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.810815690E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.22424E-02 0.20733E+01 Friction velocity uk : 0.22424E-02 0.20733E+01 Dimensionless distance yplus : 0.21676E-02 0.20386E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 2.276313104e-03 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29437E+08 1 0.18522E-09 0.29069E+02 0.20522E+04 c Velocity[X] 0.16281E+02 c Velocity[Y] 0.12787E+02 c Velocity[Z] 0.90328E-06 c Pressure 0.19794E-03 135 0.97557E-04 0.15529E-02 0.14565E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -28.282 42.772 5.6044 7.9947 v Velocity[Y] -30.529 32.364 -0.15748 -0.039404 v Velocity[Z] -3.0271 3.1203 2.3362e-06 -5.3904e-08 v ǁVelocityǁ 0.0018389 42.978 8.4773 8.1603 v Pressure -2.8309e+05 2.1918e+05 -29257 -38919 v TurbVisc 1.6059e-21 0.023607 0.00019773 5.3139e-05 v CourantNb 9.8511e-08 0.011396 0.00016959 4.959e-06 v FourierNb 1.243e-07 0.041227 0.00014911 4.959e-07 v total_pressure -1.8177e+05 3.205e+05 72068 62406 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0386 0.10968 0.0029659 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.8336e-07 0.046644 0.0003187 5.4549e-06 INSTANT 0.876328000E-01 TIME STEP NUMBER 56526 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282694809E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.810930646E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.17356E-02 0.20736E+01 Friction velocity uk : 0.17356E-02 0.20736E+01 Dimensionless distance yplus : 0.16776E-02 0.20390E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 5.366316719e-03 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29438E+08 1 0.18525E-09 0.29093E+02 0.20530E+04 c Velocity[X] 0.16297E+02 c Velocity[Y] 0.12796E+02 c Velocity[Z] 0.89447E-06 c Pressure 0.19608E-03 35 0.82037E-04 0.15376E-02 0.12317E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -28.295 42.784 5.6044 7.9947 v Velocity[Y] -30.536 32.376 -0.15753 -0.039562 v Velocity[Z] -3.0275 3.1204 2.3356e-06 -5.3904e-08 v ǁVelocityǁ 0.0017854 42.99 8.4788 8.1606 v Pressure -2.8174e+05 2.208e+05 -27583 -38095 v TurbVisc 1.578e-21 0.023624 0.00019779 5.3215e-05 v CourantNb 9.8309e-08 0.011395 0.00016959 4.9591e-06 v FourierNb 1.2431e-07 0.041209 0.00014912 4.9642e-07 v total_pressure -1.8041e+05 3.2212e+05 73742 63230 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.039 0.10971 0.0029662 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.8375e-07 0.046627 0.00031872 5.4555e-06 INSTANT 0.876329000E-01 TIME STEP NUMBER 56527 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282696938E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.811057715E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.70054E-02 0.20740E+01 Friction velocity uk : 0.70054E-02 0.20740E+01 Dimensionless distance yplus : 0.67371E-02 0.20394E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 9.214920767e-03 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29438E+08 1 0.18527E-09 0.29126E+02 0.20540E+04 c Velocity[X] 0.16313E+02 c Velocity[Y] 0.12813E+02 c Velocity[Z] 0.90852E-06 c Pressure 0.19382E-03 9 0.54429E-04 0.15192E-02 0.12098E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -28.309 42.796 5.6044 7.9948 v Velocity[Y] -30.543 32.389 -0.15758 -0.039722 v Velocity[Z] -3.0279 3.1206 2.335e-06 -5.3904e-08 v ǁVelocityǁ 0.0017561 43.002 8.4803 8.1608 v Pressure -2.8035e+05 2.2244e+05 -25909 -37301 v TurbVisc 1.583e-21 0.02364 0.00019785 5.3291e-05 v CourantNb 9.841e-08 0.011394 0.0001696 4.9592e-06 v FourierNb 1.2431e-07 0.041192 0.00014913 4.9694e-07 v total_pressure -1.7902e+05 3.2377e+05 75416 64024 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0394 0.10974 0.0029667 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.8414e-07 0.04661 0.00031873 5.4561e-06 INSTANT 0.876330000E-01 TIME STEP NUMBER 56528 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282699334E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.811192685E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.47853E-02 0.20745E+01 Friction velocity uk : 0.47853E-02 0.20745E+01 Dimensionless distance yplus : 0.46020E-02 0.20398E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.489031620e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29438E+08 1 0.18529E-09 0.29145E+02 0.20546E+04 c Velocity[X] 0.16332E+02 c Velocity[Y] 0.12813E+02 c Velocity[Z] 0.90853E-06 c Pressure 0.19334E-03 28 0.99334E-04 0.15148E-02 0.15918E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -28.322 42.808 5.6045 7.9948 v Velocity[Y] -30.55 32.402 -0.15763 -0.03988 v Velocity[Z] -3.0283 3.1208 2.3344e-06 -5.3904e-08 v ǁVelocityǁ 0.001751 43.014 8.4818 8.161 v Pressure -2.7896e+05 2.2409e+05 -24284 -36264 v TurbVisc 1.642e-21 0.023656 0.00019792 5.3366e-05 v CourantNb 9.8506e-08 0.011393 0.0001696 4.9592e-06 v FourierNb 1.2431e-07 0.041174 0.00014915 4.9745e-07 v total_pressure -1.7764e+05 3.2542e+05 77041 65061 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0398 0.10977 0.0029673 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.8453e-07 0.046593 0.00031875 5.4567e-06 INSTANT 0.876331000E-01 TIME STEP NUMBER 56529 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282701758E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.811336705E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.48354E-02 0.20749E+01 Friction velocity uk : 0.48354E-02 0.20749E+01 Dimensionless distance yplus : 0.46502E-02 0.20402E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.744082438e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29438E+08 1 0.18531E-09 0.29171E+02 0.20554E+04 c Velocity[X] 0.16351E+02 c Velocity[Y] 0.12820E+02 c Velocity[Z] 0.90144E-06 c Pressure 0.19120E-03 67 0.84638E-04 0.14973E-02 0.13612E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -28.336 42.82 5.6045 7.9948 v Velocity[Y] -30.557 32.415 -0.15768 -0.040039 v Velocity[Z] -3.0287 3.1209 2.3338e-06 -5.3904e-08 v ǁVelocityǁ 0.0017563 43.026 8.4833 8.1613 v Pressure -2.776e+05 2.2571e+05 -22644 -35349 v TurbVisc 1.6302e-21 0.023673 0.00019798 5.3442e-05 v CourantNb 9.8237e-08 0.011392 0.0001696 4.9593e-06 v FourierNb 1.2431e-07 0.041156 0.00014916 4.9797e-07 v total_pressure -1.7627e+05 3.2704e+05 78681 65976 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0402 0.10979 0.0029678 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.8489e-07 0.046576 0.00031876 5.4573e-06 INSTANT 0.876332000E-01 TIME STEP NUMBER 56530 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282704371E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.811492388E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.54373E-02 0.20754E+01 Friction velocity uk : 0.54373E-02 0.20754E+01 Dimensionless distance yplus : 0.52290E-02 0.20407E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 2.155699231e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29439E+08 1 0.18533E-09 0.29206E+02 0.20566E+04 c Velocity[X] 0.16370E+02 c Velocity[Y] 0.12836E+02 c Velocity[Z] 0.91729E-06 c Pressure 0.18864E-03 9 0.57689E-04 0.14765E-02 0.11925E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -28.35 42.831 5.6045 7.9949 v Velocity[Y] -30.564 32.427 -0.15774 -0.040197 v Velocity[Z] -3.0291 3.1211 2.3333e-06 -5.3904e-08 v ǁVelocityǁ 0.0017908 43.038 8.4848 8.1615 v Pressure -2.7634e+05 2.2724e+05 -21022 -34589 v TurbVisc 1.6507e-21 0.023689 0.00019804 5.3518e-05 v CourantNb 9.8415e-08 0.011391 0.00016961 4.9594e-06 v FourierNb 1.2431e-07 0.041139 0.00014917 4.9849e-07 v total_pressure -1.7501e+05 3.2856e+05 80303 66736 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0407 0.10982 0.0029683 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.8518e-07 0.046559 0.00031878 5.4578e-06 INSTANT 0.876333000E-01 TIME STEP NUMBER 56531 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282707104E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.811654657E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.63874E-02 0.20758E+01 Friction velocity uk : 0.63874E-02 0.20758E+01 Dimensionless distance yplus : 0.61428E-02 0.20411E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 2.812972983e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29439E+08 1 0.18535E-09 0.29232E+02 0.20574E+04 c Velocity[X] 0.16387E+02 c Velocity[Y] 0.12845E+02 c Velocity[Z] 0.91931E-06 c Pressure 0.18799E-03 648 0.77701E-04 0.14708E-02 0.15580E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -28.363 42.843 5.6046 7.995 v Velocity[Y] -30.571 32.44 -0.15779 -0.040358 v Velocity[Z] -3.0295 3.1213 2.3327e-06 -5.3904e-08 v ǁVelocityǁ 0.001848 43.05 8.4863 8.1618 v Pressure -2.7495e+05 2.2888e+05 -19455 -33685 v TurbVisc 1.6874e-21 0.023706 0.0001981 5.3594e-05 v CourantNb 9.8506e-08 0.01139 0.00016961 4.9594e-06 v FourierNb 1.2431e-07 0.041122 0.00014918 4.9901e-07 v total_pressure -1.7362e+05 3.3021e+05 81870 67640 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0411 0.10985 0.0029689 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.8547e-07 0.046542 0.00031879 5.4584e-06 INSTANT 0.876334000E-01 TIME STEP NUMBER 56532 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282710049E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.811827333E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.88991E-02 0.20763E+01 Friction velocity uk : 0.88991E-02 0.20763E+01 Dimensionless distance yplus : 0.85582E-02 0.20416E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 3.032928432e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29439E+08 1 0.18537E-09 0.29263E+02 0.20584E+04 c Velocity[X] 0.16407E+02 c Velocity[Y] 0.12856E+02 c Velocity[Z] 0.91438E-06 c Pressure 0.18617E-03 82 0.82940E-04 0.14559E-02 0.14349E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -28.377 42.855 5.6046 7.995 v Velocity[Y] -30.578 32.453 -0.15784 -0.040517 v Velocity[Z] -3.0299 3.1214 2.3321e-06 -5.3904e-08 v ǁVelocityǁ 0.0019346 43.062 8.4878 8.162 v Pressure -2.7371e+05 2.3046e+05 -17881 -32882 v TurbVisc 1.7177e-21 0.023722 0.00019816 5.367e-05 v CourantNb 9.8307e-08 0.011389 0.00016962 4.9595e-06 v FourierNb 1.2431e-07 0.041104 0.00014919 4.9953e-07 v total_pressure -1.7238e+05 3.3179e+05 83444 68443 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0416 0.10988 0.0029694 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.8577e-07 0.046526 0.0003188 5.459e-06 INSTANT 0.876335000E-01 TIME STEP NUMBER 56533 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282712964E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.812008863E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10762E-01 0.20768E+01 Friction velocity uk : 0.10762E-01 0.20768E+01 Dimensionless distance yplus : 0.10350E-01 0.20421E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 3.476162300e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29440E+08 1 0.18539E-09 0.29295E+02 0.20594E+04 c Velocity[X] 0.16426E+02 c Velocity[Y] 0.12869E+02 c Velocity[Z] 0.91262E-06 c Pressure 0.18462E-03 303 0.96008E-04 0.14431E-02 0.14798E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -28.391 42.867 5.6047 7.9951 v Velocity[Y] -30.585 32.466 -0.1579 -0.040679 v Velocity[Z] -3.0303 3.1216 2.3315e-06 -5.3904e-08 v ǁVelocityǁ 0.002048 43.074 8.4893 8.1623 v Pressure -2.7239e+05 2.3211e+05 -16317 -32068 v TurbVisc 1.7698e-21 0.023738 0.00019822 5.3747e-05 v CourantNb 9.841e-08 0.011389 0.00016962 4.9596e-06 v FourierNb 1.2431e-07 0.041087 0.0001492 5.0005e-07 v total_pressure -1.7106e+05 3.3343e+05 85008 69257 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0421 0.10991 0.00297 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.8606e-07 0.046509 0.00031882 5.4596e-06 INSTANT 0.876336000E-01 TIME STEP NUMBER 56534 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282716348E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.812200332E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.66560E-02 0.20773E+01 Friction velocity uk : 0.66560E-02 0.20773E+01 Dimensionless distance yplus : 0.64079E-02 0.20426E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 3.883067189e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29440E+08 1 0.18542E-09 0.29312E+02 0.20599E+04 c Velocity[X] 0.16446E+02 c Velocity[Y] 0.12866E+02 c Velocity[Z] 0.91639E-06 c Pressure 0.18310E-03 83 0.81545E-04 0.14306E-02 0.13848E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -28.405 42.879 5.6047 7.9951 v Velocity[Y] -30.593 32.479 -0.15795 -0.04084 v Velocity[Z] -3.0307 3.1217 2.3309e-06 -5.3905e-08 v ǁVelocityǁ 0.0021808 43.087 8.4908 8.1625 v Pressure -2.7116e+05 2.337e+05 -14793 -31225 v TurbVisc 1.8347e-21 0.023755 0.00019828 5.3823e-05 v CourantNb 9.8431e-08 0.011388 0.00016963 4.9596e-06 v FourierNb 1.2431e-07 0.04107 0.00014921 5.0057e-07 v total_pressure -1.6984e+05 3.3502e+05 86532 70100 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0426 0.10994 0.0029705 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.8635e-07 0.046493 0.00031883 5.4602e-06 INSTANT 0.876337000E-01 TIME STEP NUMBER 56535 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282719680E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.812401306E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.86259E-02 0.20778E+01 Friction velocity uk : 0.86259E-02 0.20778E+01 Dimensionless distance yplus : 0.83043E-02 0.20431E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 4.301941620e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29441E+08 1 0.18544E-09 0.29349E+02 0.20611E+04 c Velocity[X] 0.16467E+02 c Velocity[Y] 0.12882E+02 c Velocity[Z] 0.92934E-06 c Pressure 0.17797E-03 9 0.58205E-04 0.13899E-02 0.10998E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -28.419 42.892 5.6048 7.9952 v Velocity[Y] -30.6 32.492 -0.15801 -0.041001 v Velocity[Z] -3.0311 3.1219 2.3304e-06 -5.3905e-08 v ǁVelocityǁ 0.002337 43.099 8.4923 8.1628 v Pressure -2.7002e+05 2.3521e+05 -13301 -30538 v TurbVisc 1.895e-21 0.023771 0.00019835 5.3899e-05 v CourantNb 9.8468e-08 0.011387 0.00016963 4.9597e-06 v FourierNb 1.2431e-07 0.041053 0.00014922 5.0109e-07 v total_pressure -1.6869e+05 3.3654e+05 88024 70787 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0431 0.10997 0.0029711 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.8665e-07 0.046476 0.00031885 5.4608e-06 INSTANT 0.876338000E-01 TIME STEP NUMBER 56536 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282723189E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.812613063E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.76867E-02 0.20784E+01 Friction velocity uk : 0.76867E-02 0.20784E+01 Dimensionless distance yplus : 0.73922E-02 0.20436E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 4.797234140e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29441E+08 1 0.18546E-09 0.29378E+02 0.20620E+04 c Velocity[X] 0.16485E+02 c Velocity[Y] 0.12893E+02 c Velocity[Z] 0.92975E-06 c Pressure 0.17685E-03 477 0.77295E-04 0.13805E-02 0.15362E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -28.433 42.904 5.6048 7.9953 v Velocity[Y] -30.607 32.505 -0.15807 -0.041164 v Velocity[Z] -3.0315 3.1221 2.3298e-06 -5.3905e-08 v ǁVelocityǁ 0.0025 43.111 8.4938 8.163 v Pressure -2.6869e+05 2.3689e+05 -11813 -29668 v TurbVisc 1.9824e-21 0.023787 0.00019841 5.3976e-05 v CourantNb 9.8619e-08 0.011386 0.00016964 4.9598e-06 v FourierNb 1.2431e-07 0.041036 0.00014922 5.0161e-07 v total_pressure -1.6737e+05 3.3822e+05 89512 71657 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0436 0.11 0.0029717 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.8694e-07 0.04646 0.00031886 5.4614e-06 INSTANT 0.876339000E-01 TIME STEP NUMBER 56537 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282726869E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.812834811E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.71538E-02 0.20789E+01 Friction velocity uk : 0.71538E-02 0.20789E+01 Dimensionless distance yplus : 0.68798E-02 0.20442E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 5.095590277e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29441E+08 1 0.18548E-09 0.29411E+02 0.20630E+04 c Velocity[X] 0.16508E+02 c Velocity[Y] 0.12903E+02 c Velocity[Z] 0.92619E-06 c Pressure 0.17462E-03 391 0.83257E-04 0.13625E-02 0.15810E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -28.447 42.916 5.6049 7.9953 v Velocity[Y] -30.614 32.518 -0.15812 -0.041325 v Velocity[Z] -3.0319 3.1222 2.3292e-06 -5.3905e-08 v ǁVelocityǁ 0.0026832 43.124 8.4953 8.1633 v Pressure -2.6747e+05 2.3845e+05 -10301 -28772 v TurbVisc 2.0347e-21 0.023804 0.00019847 5.4052e-05 v CourantNb 9.8445e-08 0.011385 0.00016964 4.9599e-06 v FourierNb 1.2431e-07 0.041019 0.00014923 5.0214e-07 v total_pressure -1.6614e+05 3.3978e+05 91024 72553 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0442 0.11002 0.0029722 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.8724e-07 0.046444 0.00031888 5.462e-06 INSTANT 0.876340000E-01 TIME STEP NUMBER 56538 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282730548E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.813062754E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.39963E-02 0.20795E+01 Friction velocity uk : 0.39963E-02 0.20795E+01 Dimensionless distance yplus : 0.39620E-02 0.20447E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 5.474324681e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29442E+08 1 0.18550E-09 0.29446E+02 0.20641E+04 c Velocity[X] 0.16527E+02 c Velocity[Y] 0.12919E+02 c Velocity[Z] 0.92954E-06 c Pressure 0.17279E-03 239 0.96575E-04 0.13476E-02 0.12718E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -28.461 42.928 5.605 7.9954 v Velocity[Y] -30.621 32.531 -0.15818 -0.04149 v Velocity[Z] -3.0323 3.1224 2.3286e-06 -5.3905e-08 v ǁVelocityǁ 0.0028782 43.136 8.4969 8.1636 v Pressure -2.6634e+05 2.3992e+05 -8909.9 -28216 v TurbVisc 2.1747e-21 0.02382 0.00019854 5.4129e-05 v CourantNb 9.8567e-08 0.011384 0.00016965 4.9599e-06 v FourierNb 1.2431e-07 0.041002 0.00014924 5.0266e-07 v total_pressure -1.6501e+05 3.4124e+05 92415 73109 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0447 0.11005 0.0029728 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.8754e-07 0.046428 0.00031889 5.4626e-06 INSTANT 0.876341000E-01 TIME STEP NUMBER 56539 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282734611E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.813296488E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.80859E-02 0.20801E+01 Friction velocity uk : 0.80859E-02 0.20801E+01 Dimensionless distance yplus : 0.80167E-02 0.20453E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 5.854989363e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29442E+08 1 0.18553E-09 0.29465E+02 0.20647E+04 c Velocity[X] 0.16549E+02 c Velocity[Y] 0.12915E+02 c Velocity[Z] 0.93257E-06 c Pressure 0.17086E-03 127 0.82192E-04 0.13319E-02 0.14494E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -28.475 42.941 5.605 7.9955 v Velocity[Y] -30.629 32.544 -0.15824 -0.041653 v Velocity[Z] -3.0327 3.1225 2.328e-06 -5.3905e-08 v ǁVelocityǁ 0.0030827 43.149 8.4984 8.1638 v Pressure -2.6517e+05 2.4142e+05 -7471.6 -27337 v TurbVisc 2.3837e-21 0.023836 0.0001986 5.4205e-05 v CourantNb 9.8612e-08 0.011383 0.00016965 4.96e-06 v FourierNb 1.2431e-07 0.040985 0.00014925 5.0318e-07 v total_pressure -1.6384e+05 3.4275e+05 93853 73988 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0453 0.11008 0.0029734 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.8784e-07 0.046412 0.00031891 5.4632e-06 INSTANT 0.876342000E-01 TIME STEP NUMBER 56540 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282738651E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.813543237E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.97348E-02 0.20806E+01 Friction velocity uk : 0.97348E-02 0.20806E+01 Dimensionless distance yplus : 0.93619E-02 0.20459E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 6.213744849e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29443E+08 1 0.18555E-09 0.29504E+02 0.20659E+04 c Velocity[X] 0.16572E+02 c Velocity[Y] 0.12933E+02 c Velocity[Z] 0.94139E-06 c Pressure 0.16508E-03 9 0.58351E-04 0.12862E-02 0.10056E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -28.489 42.953 5.6051 7.9955 v Velocity[Y] -30.636 32.558 -0.1583 -0.041816 v Velocity[Z] -3.0331 3.1227 2.3275e-06 -5.3905e-08 v ǁVelocityǁ 0.0032963 43.161 8.4999 8.1641 v Pressure -2.6413e+05 2.4282e+05 -6103.5 -26729 v TurbVisc 2.4676e-21 0.023853 0.00019866 5.4282e-05 v CourantNb 9.8669e-08 0.011382 0.00016966 4.9601e-06 v FourierNb 1.2431e-07 0.040968 0.00014926 5.0371e-07 v total_pressure -1.628e+05 3.4414e+05 95222 74596 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0459 0.11011 0.002974 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.8814e-07 0.046396 0.00031892 5.4638e-06 INSTANT 0.876343000E-01 TIME STEP NUMBER 56541 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282742843E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.813799829E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10595E-01 0.20813E+01 Friction velocity uk : 0.10595E-01 0.20813E+01 Dimensionless distance yplus : 0.10189E-01 0.20465E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 6.648160341e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29443E+08 1 0.18557E-09 0.29535E+02 0.20669E+04 c Velocity[X] 0.16591E+02 c Velocity[Y] 0.12943E+02 c Velocity[Z] 0.94528E-06 c Pressure 0.16369E-03 175 0.78102E-04 0.12748E-02 0.14544E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -28.503 42.965 5.6052 7.9956 v Velocity[Y] -30.643 32.571 -0.15836 -0.041982 v Velocity[Z] -3.0335 3.1229 2.3269e-06 -5.3905e-08 v ǁVelocityǁ 0.0033136 43.174 8.5015 8.1644 v Pressure -2.6292e+05 2.4437e+05 -4741.6 -25932 v TurbVisc 2.4446e-21 0.023869 0.00019873 5.4359e-05 v CourantNb 9.6447e-08 0.011381 0.00016967 4.9602e-06 v FourierNb 1.2431e-07 0.040951 0.00014927 5.0423e-07 v total_pressure -1.6159e+05 3.4569e+05 96583 75393 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0465 0.11014 0.0029745 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.8834e-07 0.04638 0.00031894 5.4644e-06 INSTANT 0.876344000E-01 TIME STEP NUMBER 56542 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282747219E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.814066802E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.42625E-02 0.20818E+01 Friction velocity uk : 0.42625E-02 0.20818E+01 Dimensionless distance yplus : 0.41859E-02 0.20470E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 6.880908995e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29444E+08 1 0.18559E-09 0.29570E+02 0.20680E+04 c Velocity[X] 0.16615E+02 c Velocity[Y] 0.12955E+02 c Velocity[Z] 0.94462E-06 c Pressure 0.16112E-03 101 0.84101E-04 0.12542E-02 0.14478E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -28.518 42.978 5.6053 7.9957 v Velocity[Y] -30.651 32.584 -0.15842 -0.042145 v Velocity[Z] -3.0339 3.123 2.3263e-06 -5.3905e-08 v ǁVelocityǁ 0.0032987 43.187 8.503 8.1647 v Pressure -2.6184e+05 2.4578e+05 -3377.8 -25153 v TurbVisc 2.8447e-21 0.023885 0.00019879 5.4436e-05 v CourantNb 9.3756e-08 0.01138 0.00016967 4.9603e-06 v FourierNb 1.2431e-07 0.040934 0.00014928 5.0475e-07 v total_pressure -1.6052e+05 3.471e+05 97947 76172 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.047 0.11017 0.0029751 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.8849e-07 0.046364 0.00031895 5.465e-06 INSTANT 0.876345000E-01 TIME STEP NUMBER 56543 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282751569E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.814339861E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12156E-01 0.20825E+01 Friction velocity uk : 0.12156E-01 0.20825E+01 Dimensionless distance yplus : 0.11690E-01 0.20476E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 7.203345115e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29444E+08 1 0.18561E-09 0.29607E+02 0.20692E+04 c Velocity[X] 0.16636E+02 c Velocity[Y] 0.12971E+02 c Velocity[Z] 0.94617E-06 c Pressure 0.15897E-03 162 0.97493E-04 0.12369E-02 0.12780E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -28.532 42.99 5.6053 7.9958 v Velocity[Y] -30.658 32.597 -0.15848 -0.042312 v Velocity[Z] -3.0343 3.1232 2.3257e-06 -5.3905e-08 v ǁVelocityǁ 0.0032859 43.199 8.5045 8.1649 v Pressure -2.6077e+05 2.4714e+05 -2097.2 -24600 v TurbVisc 3.212e-21 0.023902 0.00019885 5.4513e-05 v CourantNb 9.101e-08 0.011379 0.00016968 4.9604e-06 v FourierNb 1.2431e-07 0.040917 0.00014929 5.0528e-07 v total_pressure -1.5945e+05 3.4847e+05 99228 76725 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0476 0.11021 0.0029757 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.888e-07 0.046348 0.00031897 5.4657e-06 INSTANT 0.876346000E-01 TIME STEP NUMBER 56544 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282756294E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.814619455E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12820E-01 0.20831E+01 Friction velocity uk : 0.12820E-01 0.20831E+01 Dimensionless distance yplus : 0.12329E-01 0.20483E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 7.508616286e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29445E+08 1 0.18564E-09 0.29627E+02 0.20697E+04 c Velocity[X] 0.16659E+02 c Velocity[Y] 0.12968E+02 c Velocity[Z] 0.95007E-06 c Pressure 0.15683E-03 78 0.82892E-04 0.12196E-02 0.12997E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -28.547 43.003 5.6054 7.9959 v Velocity[Y] -30.665 32.611 -0.15854 -0.042478 v Velocity[Z] -3.0347 3.1233 2.3251e-06 -5.3905e-08 v ǁVelocityǁ 0.0032752 43.212 8.5061 8.1652 v Pressure -2.5974e+05 2.4851e+05 -806.56 -23834 v TurbVisc 3.1906e-21 0.023918 0.00019892 5.459e-05 v CourantNb 8.8097e-08 0.011378 0.00016968 4.9605e-06 v FourierNb 1.2432e-07 0.040901 0.0001493 5.0581e-07 v total_pressure -1.5842e+05 3.4983e+05 1.0052e+05 77491 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0483 0.11024 0.0029762 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.8911e-07 0.046332 0.00031898 5.4663e-06 INSTANT 0.876347000E-01 TIME STEP NUMBER 56545 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282760976E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.814910099E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.94849E-02 0.20837E+01 Friction velocity uk : 0.94849E-02 0.20837E+01 Dimensionless distance yplus : 0.91228E-02 0.20489E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 7.765824022e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29445E+08 1 0.18566E-09 0.29668E+02 0.20711E+04 c Velocity[X] 0.16682E+02 c Velocity[Y] 0.12986E+02 c Velocity[Z] 0.96069E-06 c Pressure 0.15036E-03 9 0.58519E-04 0.11688E-02 0.91505E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -28.561 43.015 5.6055 7.996 v Velocity[Y] -30.673 32.624 -0.1586 -0.042643 v Velocity[Z] -3.0351 3.1235 2.3246e-06 -5.3905e-08 v ǁVelocityǁ 0.0032664 43.225 8.5076 8.1655 v Pressure -2.5883e+05 2.4976e+05 416.3 -23298 v TurbVisc 3.4751e-21 0.023934 0.00019898 5.4667e-05 v CourantNb 8.5094e-08 0.011377 0.00016969 4.9605e-06 v FourierNb 1.2432e-07 0.040884 0.00014931 5.0633e-07 v total_pressure -1.575e+05 3.5108e+05 1.0174e+05 78027 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0489 0.11027 0.0029767 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.8941e-07 0.046317 0.000319 5.4669e-06 INSTANT 0.876348000E-01 TIME STEP NUMBER 56546 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282765797E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.815209663E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.84681E-02 0.20844E+01 Friction velocity uk : 0.84681E-02 0.20844E+01 Dimensionless distance yplus : 0.81448E-02 0.20495E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 8.103066272e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29446E+08 1 0.18568E-09 0.29700E+02 0.20721E+04 c Velocity[X] 0.16703E+02 c Velocity[Y] 0.12998E+02 c Velocity[Z] 0.96288E-06 c Pressure 0.14886E-03 218 0.78875E-04 0.11566E-02 0.13386E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -28.576 43.028 5.6056 7.9961 v Velocity[Y] -30.68 32.638 -0.15866 -0.042811 v Velocity[Z] -3.0355 3.1237 2.324e-06 -5.3905e-08 v ǁVelocityǁ 0.0032627 43.238 8.5092 8.1658 v Pressure -2.5775e+05 2.5115e+05 1630.7 -22598 v TurbVisc 3.2468e-21 0.023951 0.00019905 5.4744e-05 v CourantNb 8.1906e-08 0.011376 0.00016969 4.9606e-06 v FourierNb 1.2432e-07 0.040867 0.00014932 5.0686e-07 v total_pressure -1.5642e+05 3.5248e+05 1.0296e+05 78727 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0495 0.11031 0.0029773 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.8972e-07 0.046301 0.00031901 5.4675e-06 INSTANT 0.876349000E-01 TIME STEP NUMBER 56547 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282770803E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.815519240E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.47226E-02 0.20850E+01 Friction velocity uk : 0.47226E-02 0.20850E+01 Dimensionless distance yplus : 0.45710E-02 0.20501E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 8.244358220e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29446E+08 1 0.18570E-09 0.29737E+02 0.20732E+04 c Velocity[X] 0.16728E+02 c Velocity[Y] 0.13009E+02 c Velocity[Z] 0.96402E-06 c Pressure 0.14604E-03 411 0.84941E-04 0.11342E-02 0.13923E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -28.59 43.041 5.6057 7.9962 v Velocity[Y] -30.688 32.651 -0.15872 -0.042976 v Velocity[Z] -3.0358 3.1238 2.3234e-06 -5.3905e-08 v ǁVelocityǁ 0.0032616 43.251 8.5107 8.1661 v Pressure -2.5678e+05 2.5243e+05 2848.6 -21877 v TurbVisc 3.9486e-21 0.023967 0.00019911 5.4821e-05 v CourantNb 7.152e-08 0.011375 0.0001697 4.9607e-06 v FourierNb 1.2432e-07 0.04085 0.00014933 5.0739e-07 v total_pressure -1.5546e+05 3.5375e+05 1.0417e+05 79448 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0501 0.11034 0.0029781 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.9003e-07 0.046285 0.00031903 5.4681e-06 INSTANT 0.876350000E-01 TIME STEP NUMBER 56548 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282775757E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.815834699E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.76974E-02 0.20856E+01 Friction velocity uk : 0.76974E-02 0.20856E+01 Dimensionless distance yplus : 0.74503E-02 0.20508E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 8.455729538e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29447E+08 1 0.18572E-09 0.29775E+02 0.20745E+04 c Velocity[X] 0.16747E+02 c Velocity[Y] 0.13028E+02 c Velocity[Z] 0.96840E-06 c Pressure 0.14376E-03 236 0.98356E-04 0.11160E-02 0.11821E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -28.605 43.053 5.6058 7.9963 v Velocity[Y] -30.695 32.665 -0.15878 -0.043146 v Velocity[Z] -3.0362 3.124 2.3228e-06 -5.3905e-08 v ǁVelocityǁ 0.003264 43.264 8.5123 8.1664 v Pressure -2.559e+05 2.5363e+05 3954.9 -21476 v TurbVisc 4.4517e-21 0.023983 0.00019918 5.4899e-05 v CourantNb 6.1481e-08 0.011374 0.0001697 4.9608e-06 v FourierNb 1.2432e-07 0.040833 0.00014934 5.0792e-07 v total_pressure -1.5457e+05 3.5495e+05 1.0528e+05 79849 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0508 0.11038 0.0029789 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.9034e-07 0.046269 0.00031904 5.4687e-06 INSTANT 0.876351000E-01 TIME STEP NUMBER 56549 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282781063E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.816155583E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10914E-01 0.20863E+01 Friction velocity uk : 0.10914E-01 0.20863E+01 Dimensionless distance yplus : 0.10499E-01 0.20514E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 8.650164753e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29447E+08 1 0.18575E-09 0.29796E+02 0.20751E+04 c Velocity[X] 0.16773E+02 c Velocity[Y] 0.13023E+02 c Velocity[Z] 0.97272E-06 c Pressure 0.14148E-03 145 0.83776E-04 0.10977E-02 0.12341E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -28.62 43.066 5.6059 7.9964 v Velocity[Y] -30.703 32.678 -0.15884 -0.043314 v Velocity[Z] -3.0366 3.1241 2.3223e-06 -5.3905e-08 v ǁVelocityǁ 0.0032705 43.276 8.5138 8.1667 v Pressure -2.5498e+05 2.5483e+05 5090.8 -20767 v TurbVisc 4.7946e-21 0.023999 0.00019925 5.4976e-05 v CourantNb 5.0785e-08 0.011373 0.00016971 4.9609e-06 v FourierNb 1.2432e-07 0.040817 0.00014935 5.0844e-07 v total_pressure -1.5365e+05 3.5615e+05 1.0642e+05 80558 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0514 0.11041 0.0029798 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.9065e-07 0.046254 0.00031906 5.4694e-06 INSTANT 0.876352000E-01 TIME STEP NUMBER 56550 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282786341E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.816487682E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.78113E-02 0.20869E+01 Friction velocity uk : 0.78113E-02 0.20869E+01 Dimensionless distance yplus : 0.75144E-02 0.20521E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 8.794381869e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29448E+08 1 0.18577E-09 0.29839E+02 0.20764E+04 c Velocity[X] 0.16797E+02 c Velocity[Y] 0.13042E+02 c Velocity[Z] 0.98129E-06 c Pressure 0.13433E-03 9 0.59100E-04 0.10418E-02 0.79488E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -28.634 43.079 5.606 7.9965 v Velocity[Y] -30.713 32.692 -0.15891 -0.043481 v Velocity[Z] -3.037 3.1243 2.3217e-06 -5.3905e-08 v ǁVelocityǁ 0.0032818 43.29 8.5154 8.167 v Pressure -2.5422e+05 2.5591e+05 6151.7 -20326 v TurbVisc 5.0419e-21 0.024016 0.00019931 5.5053e-05 v CourantNb 4.0061e-08 0.011372 0.00016972 4.961e-06 v FourierNb 1.2432e-07 0.0408 0.00014936 5.0897e-07 v total_pressure -1.5289e+05 3.5724e+05 1.0748e+05 80999 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0521 0.11045 0.0029805 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.9097e-07 0.046238 0.00031907 5.47e-06 INSTANT 0.876353000E-01 TIME STEP NUMBER 56551 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282791726E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.816828203E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.26939E-02 0.20876E+01 Friction velocity uk : 0.26939E-02 0.20876E+01 Dimensionless distance yplus : 0.25915E-02 0.20527E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 8.968899445e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29449E+08 1 0.18579E-09 0.29872E+02 0.20775E+04 c Velocity[X] 0.16818E+02 c Velocity[Y] 0.13054E+02 c Velocity[Z] 0.98351E-06 c Pressure 0.13292E-03 264 0.79998E-04 0.10303E-02 0.12590E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -28.649 43.092 5.6061 7.9966 v Velocity[Y] -30.724 32.705 -0.15897 -0.043651 v Velocity[Z] -3.0374 3.1245 2.3211e-06 -5.3906e-08 v ǁVelocityǁ 0.0032956 43.303 8.5169 8.1673 v Pressure -2.5326e+05 2.5716e+05 7209.1 -19697 v TurbVisc 4.7733e-21 0.024032 0.00019938 5.5131e-05 v CourantNb 3.2202e-08 0.011371 0.00016972 4.9611e-06 v FourierNb 1.2432e-07 0.040783 0.00014937 5.095e-07 v total_pressure -1.5194e+05 3.5848e+05 1.0853e+05 81628 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0527 0.11048 0.0029812 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.9128e-07 0.046222 0.00031909 5.4706e-06 INSTANT 0.876354000E-01 TIME STEP NUMBER 56552 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282797291E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.817177493E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.27970E-02 0.20882E+01 Friction velocity uk : 0.27970E-02 0.20882E+01 Dimensionless distance yplus : 0.26907E-02 0.20533E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 9.046636253e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29449E+08 1 0.18582E-09 0.29910E+02 0.20787E+04 c Velocity[X] 0.16843E+02 c Velocity[Y] 0.13066E+02 c Velocity[Z] 0.98679E-06 c Pressure 0.13000E-03 395 0.86295E-04 0.10072E-02 0.12292E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -28.664 43.105 5.6062 7.9967 v Velocity[Y] -30.736 32.719 -0.15903 -0.043819 v Velocity[Z] -3.0378 3.1246 2.3205e-06 -5.3906e-08 v ǁVelocityǁ 0.0033145 43.316 8.5185 8.1676 v Pressure -2.5246e+05 2.5824e+05 8240.8 -19117 v TurbVisc 5.8206e-21 0.024048 0.00019944 5.5209e-05 v CourantNb 3.1707e-08 0.01137 0.00016973 4.9612e-06 v FourierNb 1.2432e-07 0.040766 0.00014938 5.1003e-07 v total_pressure -1.5114e+05 3.5957e+05 1.0957e+05 82208 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0533 0.11052 0.0029821 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.916e-07 0.046206 0.00031911 5.4712e-06 INSTANT 0.876355000E-01 TIME STEP NUMBER 56553 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282802780E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.817531943E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.49017E-02 0.20889E+01 Friction velocity uk : 0.49017E-02 0.20889E+01 Dimensionless distance yplus : 0.47154E-02 0.20540E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 9.116881252e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29450E+08 1 0.18584E-09 0.29935E+02 0.20794E+04 c Velocity[X] 0.16863E+02 c Velocity[Y] 0.13072E+02 c Velocity[Z] 0.98946E-06 c Pressure 0.12774E-03 154 0.74976E-04 0.98921E-03 0.77623E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -28.679 43.118 5.6062 7.9968 v Velocity[Y] -30.748 32.733 -0.15909 -0.043989 v Velocity[Z] -3.0382 3.1248 2.32e-06 -5.3906e-08 v ǁVelocityǁ 0.0033375 43.329 8.52 8.1679 v Pressure -2.5175e+05 2.5927e+05 9175.2 -18776 v TurbVisc 6.3051e-21 0.024064 0.00019951 5.5286e-05 v CourantNb 3.7554e-08 0.011369 0.00016973 4.9613e-06 v FourierNb 1.2432e-07 0.040749 0.00014939 5.1056e-07 v total_pressure -1.5043e+05 3.6059e+05 1.105e+05 82549 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.054 0.11056 0.002983 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.9191e-07 0.04619 0.00031912 5.4719e-06 INSTANT 0.876356000E-01 TIME STEP NUMBER 56554 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282808492E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.817891561E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.90368E-02 0.20896E+01 Friction velocity uk : 0.90368E-02 0.20896E+01 Dimensionless distance yplus : 0.86933E-02 0.20546E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 9.170366761e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29450E+08 1 0.18587E-09 0.29977E+02 0.20807E+04 c Velocity[X] 0.16887E+02 c Velocity[Y] 0.13090E+02 c Velocity[Z] 0.10184E-05 c Pressure 0.12092E-03 16 0.53733E-04 0.93597E-03 0.67461E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -28.694 43.131 5.6063 7.9969 v Velocity[Y] -30.76 32.746 -0.15916 -0.044161 v Velocity[Z] -3.0386 3.1249 2.3194e-06 -5.3906e-08 v ǁVelocityǁ 0.0033663 43.342 8.5216 8.1682 v Pressure -2.5106e+05 2.6023e+05 10098 -18389 v TurbVisc 6.6225e-21 0.024081 0.00019958 5.5364e-05 v CourantNb 4.8563e-08 0.011368 0.00016974 4.9614e-06 v FourierNb 1.2432e-07 0.040732 0.0001494 5.111e-07 v total_pressure -1.4974e+05 3.6156e+05 1.1142e+05 82936 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0546 0.1106 0.0029839 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.9223e-07 0.046174 0.00031914 5.4725e-06 INSTANT 0.876357000E-01 TIME STEP NUMBER 56555 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282814413E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.818261679E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10156E-01 0.20902E+01 Friction velocity uk : 0.10156E-01 0.20902E+01 Dimensionless distance yplus : 0.97833E-02 0.20553E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 9.228002174e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29451E+08 1 0.18589E-09 0.30005E+02 0.20816E+04 c Velocity[X] 0.16911E+02 c Velocity[Y] 0.13094E+02 c Velocity[Z] 0.10035E-05 c Pressure 0.11928E-03 158 0.96569E-04 0.92283E-03 0.11013E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -28.709 43.144 5.6064 7.997 v Velocity[Y] -30.772 32.76 -0.15922 -0.044332 v Velocity[Z] -3.039 3.1251 2.3188e-06 -5.3906e-08 v ǁVelocityǁ 0.0033526 43.355 8.5231 8.1685 v Pressure -2.5023e+05 2.6131e+05 11029 -17709 v TurbVisc 4.9182e-21 0.024097 0.00019964 5.5442e-05 v CourantNb 5.1805e-08 0.011367 0.00016974 4.9615e-06 v FourierNb 1.2432e-07 0.040715 0.00014941 5.1163e-07 v total_pressure -1.4891e+05 3.6263e+05 1.1235e+05 83616 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0553 0.11064 0.0029847 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.9255e-07 0.046159 0.00031916 5.4731e-06 INSTANT 0.876358000E-01 TIME STEP NUMBER 56556 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282820335E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.818641221E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.82050E-02 0.20909E+01 Friction velocity uk : 0.82050E-02 0.20909E+01 Dimensionless distance yplus : 0.79036E-02 0.20559E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 9.169573876e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29452E+08 1 0.18592E-09 0.30040E+02 0.20827E+04 c Velocity[X] 0.16935E+02 c Velocity[Y] 0.13105E+02 c Velocity[Z] 0.10064E-05 c Pressure 0.11539E-03 37 0.80739E-04 0.89225E-03 0.71016E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -28.724 43.157 5.6065 7.9971 v Velocity[Y] -30.784 32.774 -0.15928 -0.044503 v Velocity[Z] -3.0394 3.1253 2.3183e-06 -5.3906e-08 v ǁVelocityǁ 0.0031044 43.369 8.5247 8.1688 v Pressure -2.4958e+05 2.6225e+05 11910 -17288 v TurbVisc 5.2433e-21 0.024113 0.00019971 5.552e-05 v CourantNb 4.9295e-08 0.011366 0.00016975 4.9616e-06 v FourierNb 1.2432e-07 0.040698 0.00014942 5.1216e-07 v total_pressure -1.4826e+05 3.6358e+05 1.1323e+05 84037 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0559 0.11068 0.0029855 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.9287e-07 0.046142 0.00031917 5.4738e-06 INSTANT 0.876359000E-01 TIME STEP NUMBER 56557 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282826299E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.819023797E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13356E-01 0.20915E+01 Friction velocity uk : 0.13356E-01 0.20915E+01 Dimensionless distance yplus : 0.12976E-01 0.20565E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 9.140261662e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29452E+08 1 0.18594E-09 0.30082E+02 0.20840E+04 c Velocity[X] 0.16958E+02 c Velocity[Y] 0.13124E+02 c Velocity[Z] 0.10271E-05 c Pressure 0.11094E-03 16 0.53680E-04 0.85749E-03 0.63119E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -28.74 43.17 5.6066 7.9972 v Velocity[Y] -30.796 32.788 -0.15935 -0.044674 v Velocity[Z] -3.0398 3.1254 2.3177e-06 -5.3906e-08 v ǁVelocityǁ 0.0028758 43.382 8.5263 8.1691 v Pressure -2.49e+05 2.6312e+05 12700 -16967 v TurbVisc 7.3165e-21 0.024129 0.00019978 5.5598e-05 v CourantNb 4.576e-08 0.011365 0.00016976 4.9617e-06 v FourierNb 1.2432e-07 0.040681 0.00014943 5.1269e-07 v total_pressure -1.4767e+05 3.6445e+05 1.1403e+05 84358 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0565 0.11071 0.0029863 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.9319e-07 0.046126 0.00031919 5.4744e-06 INSTANT 0.876360000E-01 TIME STEP NUMBER 56558 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282832313E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.819410824E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13600E-01 0.20922E+01 Friction velocity uk : 0.13600E-01 0.20922E+01 Dimensionless distance yplus : 0.13213E-01 0.20572E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 9.187853651e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29453E+08 1 0.18597E-09 0.30112E+02 0.20849E+04 c Velocity[X] 0.16982E+02 c Velocity[Y] 0.13130E+02 c Velocity[Z] 0.10166E-05 c Pressure 0.10968E-03 140 0.98394E-04 0.84734E-03 0.76797E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -28.755 43.183 5.6067 7.9974 v Velocity[Y] -30.808 32.802 -0.15941 -0.044845 v Velocity[Z] -3.0402 3.1256 2.3171e-06 -5.3906e-08 v ǁVelocityǁ 0.0026244 43.396 8.5278 8.1694 v Pressure -2.4837e+05 2.6404e+05 13489 -16523 v TurbVisc 5.5352e-21 0.024146 0.00019985 5.5676e-05 v CourantNb 4.2009e-08 0.011364 0.00016976 4.9618e-06 v FourierNb 1.2432e-07 0.040664 0.00014944 5.1323e-07 v total_pressure -1.4705e+05 3.6537e+05 1.1481e+05 84802 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0572 0.11075 0.002987 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.9351e-07 0.04611 0.0003192 5.475e-06 INSTANT 0.876361000E-01 TIME STEP NUMBER 56559 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282838452E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.819807801E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.14097E-01 0.20928E+01 Friction velocity uk : 0.14097E-01 0.20928E+01 Dimensionless distance yplus : 0.13696E-01 0.20578E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 9.068313192e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29454E+08 1 0.18599E-09 0.30146E+02 0.20860E+04 c Velocity[X] 0.17003E+02 c Velocity[Y] 0.13143E+02 c Velocity[Z] 0.10185E-05 c Pressure 0.10579E-03 57 0.83159E-04 0.81683E-03 0.55354E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -28.77 43.197 5.6068 7.9975 v Velocity[Y] -30.82 32.816 -0.15947 -0.045018 v Velocity[Z] -3.0406 3.1257 2.3165e-06 -5.3906e-08 v ǁVelocityǁ 0.0023906 43.409 8.5294 8.1697 v Pressure -2.4782e+05 2.6483e+05 14223 -16221 v TurbVisc 9.1506e-21 0.024162 0.00019992 5.5754e-05 v CourantNb 3.9353e-08 0.011363 0.00016977 4.9619e-06 v FourierNb 1.2432e-07 0.040646 0.00014945 5.1376e-07 v total_pressure -1.4649e+05 3.6616e+05 1.1555e+05 85104 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0578 0.11078 0.0029878 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.9383e-07 0.046094 0.00031922 5.4757e-06 INSTANT 0.876362000E-01 TIME STEP NUMBER 56560 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282844672E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.820209799E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12494E-01 0.20934E+01 Friction velocity uk : 0.12494E-01 0.20934E+01 Dimensionless distance yplus : 0.12029E-01 0.20584E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 8.982152995e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29454E+08 1 0.18602E-09 0.30189E+02 0.20873E+04 c Velocity[X] 0.17023E+02 c Velocity[Y] 0.13166E+02 c Velocity[Z] 0.10390E-05 c Pressure 0.10124E-03 12 0.54419E-04 0.78135E-03 0.58115E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -28.785 43.21 5.6069 7.9976 v Velocity[Y] -30.833 32.83 -0.15953 -0.045193 v Velocity[Z] -3.041 3.1259 2.316e-06 -5.3906e-08 v ǁVelocityǁ 0.0021775 43.423 8.531 8.1701 v Pressure -2.4727e+05 2.6563e+05 14923 -15964 v TurbVisc 9.5441e-21 0.024178 0.00019998 5.5833e-05 v CourantNb 3.6029e-08 0.011362 0.00016977 4.962e-06 v FourierNb 1.2433e-07 0.040629 0.00014946 5.1429e-07 v total_pressure -1.4595e+05 3.6696e+05 1.1625e+05 85361 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0584 0.11081 0.0029885 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.9416e-07 0.046078 0.00031924 5.4763e-06 INSTANT 0.876363000E-01 TIME STEP NUMBER 56561 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282851035E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.820617750E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.29658E-02 0.20941E+01 Friction velocity uk : 0.29658E-02 0.20941E+01 Dimensionless distance yplus : 0.28553E-02 0.20591E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 8.881369299e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29455E+08 1 0.18605E-09 0.30222E+02 0.20883E+04 c Velocity[X] 0.17052E+02 c Velocity[Y] 0.13170E+02 c Velocity[Z] 0.10326E-05 c Pressure 0.10050E-03 36 0.76643E-04 0.77525E-03 0.11696E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -28.801 43.224 5.607 7.9977 v Velocity[Y] -30.845 32.844 -0.15959 -0.045365 v Velocity[Z] -3.0414 3.126 2.3154e-06 -5.3906e-08 v ǁVelocityǁ 0.0019404 43.436 8.5325 8.1704 v Pressure -2.4675e+05 2.6643e+05 15617 -15411 v TurbVisc 6.3428e-21 0.024194 0.00020005 5.5911e-05 v CourantNb 3.2484e-08 0.011361 0.00016978 4.9621e-06 v FourierNb 1.2433e-07 0.040612 0.00014947 5.1483e-07 v total_pressure -1.4542e+05 3.6776e+05 1.1694e+05 85914 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0591 0.11084 0.0029892 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.9448e-07 0.046061 0.00031925 5.4769e-06 INSTANT 0.876364000E-01 TIME STEP NUMBER 56562 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282857297E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.821031907E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.62426E-02 0.20947E+01 Friction velocity uk : 0.62426E-02 0.20947E+01 Dimensionless distance yplus : 0.61479E-02 0.20597E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 8.738378399e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29456E+08 1 0.18607E-09 0.30261E+02 0.20896E+04 c Velocity[X] 0.17071E+02 c Velocity[Y] 0.13190E+02 c Velocity[Z] 0.10349E-05 c Pressure 0.97941E-04 710 0.80894E-04 0.75515E-03 0.88684E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -28.816 43.237 5.6071 7.9978 v Velocity[Y] -30.857 32.858 -0.15966 -0.045541 v Velocity[Z] -3.0418 3.1262 2.3148e-06 -5.3906e-08 v ǁVelocityǁ 0.0017316 43.45 8.5341 8.1707 v Pressure -2.4628e+05 2.6716e+05 16227 -15219 v TurbVisc 1.17e-20 0.02421 0.00020012 5.5989e-05 v CourantNb 2.9895e-08 0.01136 0.00016978 4.9622e-06 v FourierNb 1.2433e-07 0.040594 0.00014948 5.1536e-07 v total_pressure -1.4495e+05 3.6848e+05 1.1755e+05 86106 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0597 0.11087 0.0029899 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.9481e-07 0.046045 0.00031927 5.4776e-06 INSTANT 0.876365000E-01 TIME STEP NUMBER 56563 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282863850E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.821449705E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.17216E-01 0.20953E+01 Friction velocity uk : 0.17216E-01 0.20953E+01 Dimensionless distance yplus : 0.16574E-01 0.20603E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 8.601904872e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29456E+08 1 0.18610E-09 0.30298E+02 0.20907E+04 c Velocity[X] 0.17099E+02 c Velocity[Y] 0.13199E+02 c Velocity[Z] 0.10399E-05 c Pressure 0.96336E-04 101 0.94880E-04 0.74241E-03 0.10739E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -28.831 43.251 5.6072 7.998 v Velocity[Y] -30.869 32.872 -0.15972 -0.045713 v Velocity[Z] -3.0422 3.1264 2.3143e-06 -5.3906e-08 v ǁVelocityǁ 0.001537 43.464 8.5357 8.171 v Pressure -2.4591e+05 2.6777e+05 16802 -14903 v TurbVisc 1.1543e-20 0.024227 0.00020019 5.6068e-05 v CourantNb 2.6753e-08 0.011359 0.00016979 4.9623e-06 v FourierNb 1.2433e-07 0.040576 0.0001495 5.159e-07 v total_pressure -1.4459e+05 3.6909e+05 1.1813e+05 86422 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0603 0.11091 0.0029906 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.9513e-07 0.046028 0.00031929 5.4782e-06 INSTANT 0.876366000E-01 TIME STEP NUMBER 56564 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282870253E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.821872073E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.18351E-01 0.20960E+01 Friction velocity uk : 0.18351E-01 0.20960E+01 Dimensionless distance yplus : 0.17830E-01 0.20609E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 8.425575089e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29457E+08 1 0.18613E-09 0.30322E+02 0.20914E+04 c Velocity[X] 0.17116E+02 c Velocity[Y] 0.13206E+02 c Velocity[Z] 0.10454E-05 c Pressure 0.94934E-04 285 0.80116E-04 0.73125E-03 0.66156E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -28.847 43.264 5.6073 7.9981 v Velocity[Y] -30.882 32.886 -0.15978 -0.045889 v Velocity[Z] -3.0426 3.1265 2.3137e-06 -5.3906e-08 v ǁVelocityǁ 0.0013635 43.477 8.5372 8.1713 v Pressure -2.4553e+05 2.6843e+05 17323 -14763 v TurbVisc 1.1975e-20 0.024243 0.00020026 5.6146e-05 v CourantNb 2.3776e-08 0.011359 0.0001698 4.9624e-06 v FourierNb 1.2433e-07 0.040559 0.00014951 5.1644e-07 v total_pressure -1.4421e+05 3.6975e+05 1.1865e+05 86562 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0609 0.11095 0.0029913 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.9546e-07 0.046012 0.0003193 5.4789e-06 INSTANT 0.876367000E-01 TIME STEP NUMBER 56565 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282876817E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.822301514E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.17923E-01 0.20966E+01 Friction velocity uk : 0.17923E-01 0.20966E+01 Dimensionless distance yplus : 0.17348E-01 0.20615E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 8.258579031e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29458E+08 1 0.18615E-09 0.30364E+02 0.20927E+04 c Velocity[X] 0.17138E+02 c Velocity[Y] 0.13227E+02 c Velocity[Z] 0.10598E-05 c Pressure 0.86827E-04 7 0.54941E-04 0.66847E-03 0.41707E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -28.862 43.278 5.6074 7.9982 v Velocity[Y] -30.894 32.901 -0.15984 -0.046066 v Velocity[Z] -3.043 3.1267 2.3131e-06 -5.3906e-08 v ǁVelocityǁ 0.0012384 43.491 8.5388 8.1717 v Pressure -2.4525e+05 2.6893e+05 17761 -14657 v TurbVisc 1.1914e-20 0.024259 0.00020033 5.6225e-05 v CourantNb 2.0883e-08 0.011358 0.0001698 4.9625e-06 v FourierNb 1.2433e-07 0.040541 0.00014952 5.1697e-07 v total_pressure -1.4392e+05 3.7025e+05 1.1909e+05 86668 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0615 0.11098 0.002992 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.9579e-07 0.045995 0.00031932 5.4795e-06 INSTANT 0.876368000E-01 TIME STEP NUMBER 56566 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282883532E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.822736021E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13990E-01 0.20972E+01 Friction velocity uk : 0.13990E-01 0.20972E+01 Dimensionless distance yplus : 0.13541E-01 0.20622E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 8.078760047e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29458E+08 1 0.18618E-09 0.30397E+02 0.20937E+04 c Velocity[X] 0.17165E+02 c Velocity[Y] 0.13232E+02 c Velocity[Z] 0.10570E-05 c Pressure 0.86969E-04 31 0.76363E-04 0.66923E-03 0.10732E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -28.878 43.291 5.6075 7.9983 v Velocity[Y] -30.907 32.915 -0.1599 -0.04624 v Velocity[Z] -3.0434 3.1268 2.3126e-06 -5.3906e-08 v ǁVelocityǁ 0.0011132 43.505 8.5404 8.172 v Pressure -2.4485e+05 2.6958e+05 18321 -14193 v TurbVisc 1.2123e-20 0.024275 0.0002004 5.6304e-05 v CourantNb 1.9866e-08 0.011357 0.00016981 4.9626e-06 v FourierNb 1.2433e-07 0.040524 0.00014953 5.1751e-07 v total_pressure -1.4353e+05 3.7091e+05 1.1965e+05 87132 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0622 0.11101 0.0029925 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.9612e-07 0.045979 0.00031934 5.4801e-06 INSTANT 0.876369000E-01 TIME STEP NUMBER 56567 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282890096E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.823179579E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12481E-01 0.20978E+01 Friction velocity uk : 0.12481E-01 0.20978E+01 Dimensionless distance yplus : 0.12081E-01 0.20627E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 7.872804092e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29459E+08 1 0.18621E-09 0.30436E+02 0.20950E+04 c Velocity[X] 0.17184E+02 c Velocity[Y] 0.13252E+02 c Velocity[Z] 0.10624E-05 c Pressure 0.85296E-04 66 0.81016E-04 0.65604E-03 0.82213E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -28.893 43.305 5.6076 7.9985 v Velocity[Y] -30.919 32.929 -0.15996 -0.046418 v Velocity[Z] -3.0438 3.127 2.312e-06 -5.3906e-08 v ǁVelocityǁ 0.0010594 43.519 8.5419 8.1723 v Pressure -2.4459e+05 2.7006e+05 18688 -14121 v TurbVisc 1.2975e-20 0.024291 0.00020047 5.6383e-05 v CourantNb 1.9302e-08 0.011356 0.00016981 4.9627e-06 v FourierNb 1.2433e-07 0.040505 0.00014954 5.1805e-07 v total_pressure -1.4326e+05 3.7139e+05 1.2001e+05 87204 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0627 0.11104 0.0029932 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.9645e-07 0.045961 0.00031935 5.4808e-06 INSTANT 0.876370000E-01 TIME STEP NUMBER 56568 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282896938E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.823618734E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.14376E-01 0.20984E+01 Friction velocity uk : 0.14376E-01 0.20984E+01 Dimensionless distance yplus : 0.14162E-01 0.20633E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 7.697544525e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29460E+08 1 0.18624E-09 0.30473E+02 0.20961E+04 c Velocity[X] 0.17209E+02 c Velocity[Y] 0.13263E+02 c Velocity[Z] 0.10682E-05 c Pressure 0.84647E-04 282 0.94614E-04 0.65072E-03 0.10070E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -28.909 43.319 5.6077 7.9986 v Velocity[Y] -30.932 32.943 -0.16002 -0.046593 v Velocity[Z] -3.0441 3.1272 2.3114e-06 -5.3907e-08 v ǁVelocityǁ 0.001054 43.533 8.5435 8.1727 v Pressure -2.444e+05 2.7053e+05 19062 -13910 v TurbVisc 1.3469e-20 0.024307 0.00020054 5.6461e-05 v CourantNb 1.9292e-08 0.011355 0.00016982 4.9628e-06 v FourierNb 1.2433e-07 0.040488 0.00014955 5.1859e-07 v total_pressure -1.4307e+05 3.7186e+05 1.2039e+05 87415 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0633 0.11107 0.0029938 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.9678e-07 0.045944 0.00031937 5.4814e-06 INSTANT 0.876371000E-01 TIME STEP NUMBER 56569 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282903573E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.824064193E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.34229E-02 0.20990E+01 Friction velocity uk : 0.34229E-02 0.20990E+01 Dimensionless distance yplus : 0.33720E-02 0.20639E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 7.485963862e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29461E+08 1 0.18627E-09 0.30496E+02 0.20967E+04 c Velocity[X] 0.17226E+02 c Velocity[Y] 0.13270E+02 c Velocity[Z] 0.10757E-05 c Pressure 0.84341E-04 67 0.80154E-04 0.64806E-03 0.59305E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -28.925 43.333 5.6078 7.9987 v Velocity[Y] -30.944 32.958 -0.16008 -0.046771 v Velocity[Z] -3.0445 3.1273 2.3109e-06 -5.3907e-08 v ǁVelocityǁ 0.0010898 43.547 8.5451 8.173 v Pressure -2.4427e+05 2.7093e+05 19347 -13929 v TurbVisc 1.4103e-20 0.024323 0.00020061 5.6541e-05 v CourantNb 1.9247e-08 0.011354 0.00016983 4.9629e-06 v FourierNb 1.2433e-07 0.04047 0.00014956 5.1913e-07 v total_pressure -1.4294e+05 3.7225e+05 1.2067e+05 87396 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0639 0.11109 0.0029943 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.9712e-07 0.045927 0.00031939 5.4821e-06 INSTANT 0.876372000E-01 TIME STEP NUMBER 56570 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282910388E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.824514264E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.73585E-02 0.20996E+01 Friction velocity uk : 0.73585E-02 0.20996E+01 Dimensionless distance yplus : 0.72244E-02 0.20645E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 7.292060200e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29461E+08 1 0.18630E-09 0.30538E+02 0.20980E+04 c Velocity[X] 0.17247E+02 c Velocity[Y] 0.13290E+02 c Velocity[Z] 0.10787E-05 c Pressure 0.76517E-04 7 0.54679E-04 0.58764E-03 0.38416E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -28.94 43.347 5.6078 7.9989 v Velocity[Y] -30.957 32.972 -0.16014 -0.04695 v Velocity[Z] -3.0449 3.1275 2.3103e-06 -5.3907e-08 v ǁVelocityǁ 0.0011677 43.561 8.5466 8.1733 v Pressure -2.4415e+05 2.7125e+05 19576 -13902 v TurbVisc 1.4644e-20 0.02434 0.00020068 5.662e-05 v CourantNb 1.9207e-08 0.011353 0.00016983 4.9631e-06 v FourierNb 1.2433e-07 0.040452 0.00014957 5.1967e-07 v total_pressure -1.4282e+05 3.7258e+05 1.209e+05 87423 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0645 0.11112 0.0029949 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.9745e-07 0.04591 0.00031941 5.4827e-06 INSTANT 0.876373000E-01 TIME STEP NUMBER 56571 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282917311E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.824970302E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.63749E-02 0.21002E+01 Friction velocity uk : 0.63749E-02 0.21002E+01 Dimensionless distance yplus : 0.62588E-02 0.20651E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 7.124723910e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29462E+08 1 0.18633E-09 0.30570E+02 0.20990E+04 c Velocity[X] 0.17273E+02 c Velocity[Y] 0.13297E+02 c Velocity[Z] 0.10790E-05 c Pressure 0.78186E-04 30 0.76575E-04 0.60016E-03 0.93191E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -28.956 43.361 5.6079 7.999 v Velocity[Y] -30.969 32.987 -0.1602 -0.047127 v Velocity[Z] -3.0453 3.1276 2.3098e-06 -5.3907e-08 v ǁVelocityǁ 0.0013072 43.575 8.5482 8.1736 v Pressure -2.4397e+05 2.7167e+05 19927 -13587 v TurbVisc 1.3786e-20 0.024356 0.00020075 5.6699e-05 v CourantNb 1.9215e-08 0.011352 0.00016984 4.9632e-06 v FourierNb 1.2433e-07 0.040434 0.00014959 5.2021e-07 v total_pressure -1.4265e+05 3.73e+05 1.2125e+05 87738 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0651 0.11116 0.0029954 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.9779e-07 0.045894 0.00031942 5.4834e-06 INSTANT 0.876374000E-01 TIME STEP NUMBER 56572 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282924086E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.825434501E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15181E-01 0.21008E+01 Friction velocity uk : 0.15181E-01 0.21008E+01 Dimensionless distance yplus : 0.14662E-01 0.20657E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 6.879727804e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29463E+08 1 0.18635E-09 0.30608E+02 0.21002E+04 c Velocity[X] 0.17291E+02 c Velocity[Y] 0.13317E+02 c Velocity[Z] 0.10867E-05 c Pressure 0.77788E-04 496 0.81544E-04 0.59681E-03 0.83534E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -28.972 43.375 5.608 7.9991 v Velocity[Y] -30.982 33.001 -0.16026 -0.047307 v Velocity[Z] -3.0457 3.1278 2.3092e-06 -5.3907e-08 v ǁVelocityǁ 0.0014664 43.589 8.5498 8.174 v Pressure -2.4394e+05 2.7195e+05 20060 -13665 v TurbVisc 1.643e-20 0.024372 0.00020082 5.6778e-05 v CourantNb 1.9079e-08 0.011351 0.00016984 4.9633e-06 v FourierNb 1.2433e-07 0.040415 0.0001496 5.2075e-07 v total_pressure -1.4261e+05 3.7327e+05 1.2139e+05 87660 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0657 0.11119 0.0029961 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.9812e-07 0.045876 0.00031944 5.484e-06 INSTANT 0.876375000E-01 TIME STEP NUMBER 56573 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282931098E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.825891847E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15577E-01 0.21014E+01 Friction velocity uk : 0.15577E-01 0.21014E+01 Dimensionless distance yplus : 0.15044E-01 0.20663E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 6.733400530e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29463E+08 1 0.18639E-09 0.30643E+02 0.21013E+04 c Velocity[X] 0.17316E+02 c Velocity[Y] 0.13327E+02 c Velocity[Z] 0.10915E-05 c Pressure 0.78611E-04 119 0.95307E-04 0.60282E-03 0.96197E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -28.988 43.389 5.6081 7.9993 v Velocity[Y] -30.995 33.016 -0.16032 -0.047484 v Velocity[Z] -3.0461 3.1279 2.3086e-06 -5.3907e-08 v ǁVelocityǁ 0.0016464 43.604 8.5514 8.1743 v Pressure -2.4397e+05 2.7216e+05 20204 -13586 v TurbVisc 1.6634e-20 0.024388 0.00020089 5.6857e-05 v CourantNb 1.906e-08 0.01135 0.00016985 4.9634e-06 v FourierNb 1.2433e-07 0.040397 0.00014961 5.2129e-07 v total_pressure -1.4264e+05 3.7349e+05 1.2153e+05 87739 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0663 0.11123 0.0029966 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.9846e-07 0.045859 0.00031946 5.4847e-06 INSTANT 0.876376000E-01 TIME STEP NUMBER 56574 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282937901E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.826355773E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.17009E-01 0.21020E+01 Friction velocity uk : 0.17009E-01 0.21020E+01 Dimensionless distance yplus : 0.16428E-01 0.20669E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 6.563975481e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29464E+08 1 0.18641E-09 0.30665E+02 0.21019E+04 c Velocity[X] 0.17334E+02 c Velocity[Y] 0.13331E+02 c Velocity[Z] 0.10927E-05 c Pressure 0.79831E-04 500 0.80765E-04 0.61187E-03 0.55593E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -29.003 43.403 5.6082 7.9994 v Velocity[Y] -31.008 33.03 -0.16038 -0.047664 v Velocity[Z] -3.0465 3.1281 2.3081e-06 -5.3907e-08 v ǁVelocityǁ 0.0015782 43.618 8.5529 8.1746 v Pressure -2.4396e+05 2.7237e+05 20303 -13621 v TurbVisc 1.667e-20 0.024404 0.00020096 5.6937e-05 v CourantNb 1.9022e-08 0.011349 0.00016985 4.9635e-06 v FourierNb 1.2434e-07 0.040379 0.00014962 5.2184e-07 v total_pressure -1.4263e+05 3.737e+05 1.2163e+05 87704 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0669 0.11126 0.0029971 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.988e-07 0.045842 0.00031947 5.4853e-06 INSTANT 0.876377000E-01 TIME STEP NUMBER 56575 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282944890E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.826823797E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.16648E-01 0.21026E+01 Friction velocity uk : 0.16648E-01 0.21026E+01 Dimensionless distance yplus : 0.16012E-01 0.20674E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 6.409994167e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29465E+08 1 0.18645E-09 0.30706E+02 0.21032E+04 c Velocity[X] 0.17351E+02 c Velocity[Y] 0.13354E+02 c Velocity[Z] 0.11030E-05 c Pressure 0.73070E-04 6 0.56167E-04 0.55976E-03 0.42639E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -29.019 43.417 5.6083 7.9995 v Velocity[Y] -31.02 33.045 -0.16044 -0.047846 v Velocity[Z] -3.0469 3.1283 2.3075e-06 -5.3907e-08 v ǁVelocityǁ 0.0015254 43.632 8.5545 8.175 v Pressure -2.4404e+05 2.7253e+05 20332 -13699 v TurbVisc 1.7526e-20 0.02442 0.00020104 5.7016e-05 v CourantNb 2.0431e-08 0.011348 0.00016986 4.9636e-06 v FourierNb 1.2434e-07 0.040361 0.00014963 5.2238e-07 v total_pressure -1.4271e+05 3.7386e+05 1.2166e+05 87626 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0674 0.11129 0.0029976 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.9914e-07 0.045824 0.00031949 5.486e-06 INSTANT 0.876378000E-01 TIME STEP NUMBER 56576 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282951942E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.827293666E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12108E-01 0.21032E+01 Friction velocity uk : 0.12108E-01 0.21032E+01 Dimensionless distance yplus : 0.11646E-01 0.20680E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 6.293934298e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29466E+08 1 0.18648E-09 0.30738E+02 0.21041E+04 c Velocity[X] 0.17375E+02 c Velocity[Y] 0.13362E+02 c Velocity[Z] 0.11035E-05 c Pressure 0.76582E-04 29 0.77155E-04 0.58637E-03 0.75329E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -29.035 43.431 5.6083 7.9997 v Velocity[Y] -31.033 33.06 -0.1605 -0.048025 v Velocity[Z] -3.0473 3.1284 2.3069e-06 -5.3907e-08 v ǁVelocityǁ 0.0015136 43.647 8.5561 8.1753 v Pressure -2.4421e+05 2.7264e+05 20361 -13718 v TurbVisc 1.7023e-20 0.024436 0.00020111 5.7096e-05 v CourantNb 2.245e-08 0.011347 0.00016986 4.9637e-06 v FourierNb 1.2434e-07 0.040342 0.00014964 5.2292e-07 v total_pressure -1.4288e+05 3.7397e+05 1.2169e+05 87607 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.068 0.11132 0.002998 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.9948e-07 0.045807 0.00031951 5.4866e-06 INSTANT 0.876379000E-01 TIME STEP NUMBER 56577 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282958782E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.827767842E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.34722E-02 0.21038E+01 Friction velocity uk : 0.34722E-02 0.21038E+01 Dimensionless distance yplus : 0.33396E-02 0.20686E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 6.119416232e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29466E+08 1 0.18651E-09 0.30775E+02 0.21052E+04 c Velocity[X] 0.17394E+02 c Velocity[Y] 0.13381E+02 c Velocity[Z] 0.11102E-05 c Pressure 0.77698E-04 46 0.82177E-04 0.59462E-03 0.79981E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -29.051 43.445 5.6084 7.9998 v Velocity[Y] -31.046 33.074 -0.16056 -0.048208 v Velocity[Z] -3.0477 3.1286 2.3064e-06 -5.3907e-08 v ǁVelocityǁ 0.0015181 43.661 8.5577 8.1757 v Pressure -2.4433e+05 2.727e+05 20321 -13817 v TurbVisc 1.9014e-20 0.024452 0.00020118 5.7175e-05 v CourantNb 2.4537e-08 0.011347 0.00016987 4.9638e-06 v FourierNb 1.2434e-07 0.040324 0.00014966 5.2347e-07 v total_pressure -1.4301e+05 3.7403e+05 1.2165e+05 87508 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0686 0.11134 0.0029983 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 5.9982e-07 0.04579 0.00031953 5.4873e-06 INSTANT 0.876380000E-01 TIME STEP NUMBER 56578 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282965895E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.828241369E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10803E-01 0.21043E+01 Friction velocity uk : 0.10803E-01 0.21043E+01 Dimensionless distance yplus : 0.10391E-01 0.20692E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 6.028234874e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29467E+08 1 0.18654E-09 0.30809E+02 0.21063E+04 c Velocity[X] 0.17416E+02 c Velocity[Y] 0.13393E+02 c Velocity[Z] 0.11136E-05 c Pressure 0.80098E-04 110 0.95909E-04 0.61268E-03 0.92616E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -29.067 43.459 5.6085 7.9999 v Velocity[Y] -31.059 33.089 -0.16062 -0.048387 v Velocity[Z] -3.0481 3.1287 2.3058e-06 -5.3907e-08 v ǁVelocityǁ 0.0015564 43.675 8.5592 8.176 v Pressure -2.446e+05 2.7273e+05 20227 -13902 v TurbVisc 1.9791e-20 0.024468 0.00020125 5.7255e-05 v CourantNb 2.5771e-08 0.011346 0.00016988 4.9639e-06 v FourierNb 1.2434e-07 0.040305 0.00014967 5.2401e-07 v total_pressure -1.4327e+05 3.7405e+05 1.2155e+05 87423 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0692 0.11137 0.002999 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.0016e-07 0.045772 0.00031954 5.4879e-06 INSTANT 0.876381000E-01 TIME STEP NUMBER 56579 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282972740E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.828717601E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.58654E-02 0.21049E+01 Friction velocity uk : 0.58654E-02 0.21049E+01 Dimensionless distance yplus : 0.56658E-02 0.20697E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 5.946171872e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29468E+08 1 0.18657E-09 0.30829E+02 0.21068E+04 c Velocity[X] 0.17432E+02 c Velocity[Y] 0.13397E+02 c Velocity[Z] 0.11202E-05 c Pressure 0.82834E-04 74 0.81260E-04 0.63329E-03 0.60323E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -29.083 43.474 5.6086 8.0001 v Velocity[Y] -31.072 33.104 -0.16068 -0.04857 v Velocity[Z] -3.0485 3.1289 2.3053e-06 -5.3907e-08 v ǁVelocityǁ 0.0016358 43.69 8.5608 8.1763 v Pressure -2.4482e+05 2.727e+05 20092 -14094 v TurbVisc 2.0251e-20 0.024484 0.00020132 5.7335e-05 v CourantNb 2.6131e-08 0.011346 0.00016988 4.964e-06 v FourierNb 1.2434e-07 0.040287 0.00014968 5.2456e-07 v total_pressure -1.435e+05 3.7403e+05 1.2142e+05 87231 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0697 0.1114 0.0029996 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.0051e-07 0.045755 0.00031956 5.4886e-06 INSTANT 0.876382000E-01 TIME STEP NUMBER 56580 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282979754E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.829196697E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.38289E-02 0.21055E+01 Friction velocity uk : 0.38289E-02 0.21055E+01 Dimensionless distance yplus : 0.36986E-02 0.20703E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 5.877905214e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29469E+08 1 0.18661E-09 0.30868E+02 0.21080E+04 c Velocity[X] 0.17451E+02 c Velocity[Y] 0.13418E+02 c Velocity[Z] 0.11328E-05 c Pressure 0.77842E-04 15 0.56306E-04 0.59481E-03 0.39911E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -29.099 43.488 5.6087 8.0002 v Velocity[Y] -31.085 33.118 -0.16074 -0.048754 v Velocity[Z] -3.0489 3.129 2.3047e-06 -5.3907e-08 v ǁVelocityǁ 0.0017633 43.704 8.5624 8.1767 v Pressure -2.4506e+05 2.7268e+05 19964 -14189 v TurbVisc 2.0774e-20 0.0245 0.0002014 5.7415e-05 v CourantNb 2.6089e-08 0.011347 0.00016989 4.9641e-06 v FourierNb 1.2434e-07 0.040268 0.00014969 5.251e-07 v total_pressure -1.4374e+05 3.7401e+05 1.2129e+05 87136 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0703 0.11143 0.0030003 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.0085e-07 0.045737 0.00031958 5.4892e-06 INSTANT 0.876383000E-01 TIME STEP NUMBER 56581 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282986846E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.829677030E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.59931E-02 0.21061E+01 Friction velocity uk : 0.59931E-02 0.21061E+01 Dimensionless distance yplus : 0.58674E-02 0.20709E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 5.801471448e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29469E+08 1 0.18664E-09 0.30899E+02 0.21090E+04 c Velocity[X] 0.17473E+02 c Velocity[Y] 0.13427E+02 c Velocity[Z] 0.11281E-05 c Pressure 0.82624E-04 64 0.77450E-04 0.63104E-03 0.78888E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -29.115 43.502 5.6088 8.0003 v Velocity[Y] -31.098 33.133 -0.16079 -0.048935 v Velocity[Z] -3.0493 3.1292 2.3041e-06 -5.3907e-08 v ǁVelocityǁ 0.0018931 43.719 8.564 8.177 v Pressure -2.4547e+05 2.7252e+05 19680 -14390 v TurbVisc 2.1977e-20 0.024517 0.00020147 5.7495e-05 v CourantNb 2.7144e-08 0.011348 0.00016989 4.9642e-06 v FourierNb 1.2434e-07 0.04025 0.0001497 5.2565e-07 v total_pressure -1.4415e+05 3.7384e+05 1.21e+05 86935 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0709 0.11147 0.003001 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.012e-07 0.045719 0.0003196 5.4899e-06 INSTANT 0.876384000E-01 TIME STEP NUMBER 56582 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282993690E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.830154469E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11666E-01 0.21067E+01 Friction velocity uk : 0.11666E-01 0.21067E+01 Dimensionless distance yplus : 0.11421E-01 0.20714E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 5.821431197e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29470E+08 1 0.18667E-09 0.30935E+02 0.21100E+04 c Velocity[X] 0.17489E+02 c Velocity[Y] 0.13446E+02 c Velocity[Z] 0.11320E-05 c Pressure 0.85220E-04 77 0.82717E-04 0.65053E-03 0.86640E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -29.131 43.517 5.6088 8.0005 v Velocity[Y] -31.111 33.148 -0.16085 -0.04912 v Velocity[Z] -3.0496 3.1293 2.3036e-06 -5.3907e-08 v ǁVelocityǁ 0.0020584 43.733 8.5656 8.1773 v Pressure -2.4581e+05 2.7237e+05 19437 -14636 v TurbVisc 1.8163e-20 0.024533 0.00020154 5.7575e-05 v CourantNb 2.8826e-08 0.01135 0.0001699 4.9643e-06 v FourierNb 1.2434e-07 0.040231 0.00014971 5.2619e-07 v total_pressure -1.4448e+05 3.7369e+05 1.2076e+05 86689 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0714 0.11151 0.0030017 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.0154e-07 0.045702 0.00031961 5.4905e-06 INSTANT 0.876385000E-01 TIME STEP NUMBER 56583 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283000780E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.830639220E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.18992E-01 0.21072E+01 Friction velocity uk : 0.18992E-01 0.21072E+01 Dimensionless distance yplus : 0.18593E-01 0.20720E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 5.807105037e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29471E+08 1 0.18671E-09 0.30968E+02 0.21110E+04 c Velocity[X] 0.17510E+02 c Velocity[Y] 0.13457E+02 c Velocity[Z] 0.11319E-05 c Pressure 0.88848E-04 121 0.96572E-04 0.67788E-03 0.94924E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -29.147 43.531 5.6089 8.0006 v Velocity[Y] -31.124 33.163 -0.16091 -0.049302 v Velocity[Z] -3.05 3.1295 2.303e-06 -5.3907e-08 v ǁVelocityǁ 0.0022406 43.748 8.5671 8.1777 v Pressure -2.463e+05 2.7219e+05 19127 -14823 v TurbVisc 2.0594e-20 0.024549 0.00020162 5.7655e-05 v CourantNb 3.0719e-08 0.011351 0.0001699 4.9645e-06 v FourierNb 1.2434e-07 0.040213 0.00014973 5.2674e-07 v total_pressure -1.4497e+05 3.7351e+05 1.2045e+05 86502 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.072 0.11155 0.0030023 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.0189e-07 0.045684 0.00031963 5.4912e-06 INSTANT 0.876386000E-01 TIME STEP NUMBER 56584 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283007586E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.831121692E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.22815E-01 0.21078E+01 Friction velocity uk : 0.22815E-01 0.21078E+01 Dimensionless distance yplus : 0.22120E-01 0.20726E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 5.814380078e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29472E+08 1 0.18674E-09 0.30987E+02 0.21115E+04 c Velocity[X] 0.17527E+02 c Velocity[Y] 0.13460E+02 c Velocity[Z] 0.11400E-05 c Pressure 0.92688E-04 436 0.82212E-04 0.70681E-03 0.69014E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -29.163 43.545 5.609 8.0007 v Velocity[Y] -31.137 33.178 -0.16097 -0.049487 v Velocity[Z] -3.0504 3.1297 2.3025e-06 -5.3907e-08 v ǁVelocityǁ 0.0024387 43.763 8.5687 8.178 v Pressure -2.4673e+05 2.7192e+05 18764 -15143 v TurbVisc 2.175e-20 0.024565 0.00020169 5.7735e-05 v CourantNb 3.2631e-08 0.011352 0.00016991 4.9646e-06 v FourierNb 1.2434e-07 0.040194 0.00014974 5.2729e-07 v total_pressure -1.454e+05 3.7324e+05 1.2009e+05 86182 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0726 0.11158 0.003003 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.0224e-07 0.045667 0.00031965 5.4919e-06 INSTANT 0.876387000E-01 TIME STEP NUMBER 56585 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283014555E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.831604934E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.22667E-01 0.21084E+01 Friction velocity uk : 0.22667E-01 0.21084E+01 Dimensionless distance yplus : 0.21919E-01 0.20731E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 5.851438041e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29472E+08 1 0.18677E-09 0.31024E+02 0.21127E+04 c Velocity[X] 0.17540E+02 c Velocity[Y] 0.13484E+02 c Velocity[Z] 0.11519E-05 c Pressure 0.89495E-04 7 0.57741E-04 0.68212E-03 0.54774E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -29.179 43.56 5.6091 8.0009 v Velocity[Y] -31.15 33.193 -0.16103 -0.049673 v Velocity[Z] -3.0508 3.1298 2.3019e-06 -5.3908e-08 v ǁVelocityǁ 0.0024169 43.777 8.5703 8.1783 v Pressure -2.4721e+05 2.7171e+05 18391 -15395 v TurbVisc 2.3554e-20 0.024581 0.00020176 5.7815e-05 v CourantNb 3.4543e-08 0.011353 0.00016992 4.9647e-06 v FourierNb 1.2434e-07 0.040175 0.00014975 5.2784e-07 v total_pressure -1.4588e+05 3.7304e+05 1.1972e+05 85930 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0731 0.11162 0.0030036 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.0259e-07 0.045649 0.00031967 5.4925e-06 INSTANT 0.876388000E-01 TIME STEP NUMBER 56586 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283021536E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.832087655E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.20587E-01 0.21089E+01 Friction velocity uk : 0.20587E-01 0.21089E+01 Dimensionless distance yplus : 0.19908E-01 0.20737E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 5.894484912e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29473E+08 1 0.18681E-09 0.31054E+02 0.21136E+04 c Velocity[X] 0.17564E+02 c Velocity[Y] 0.13490E+02 c Velocity[Z] 0.11569E-05 c Pressure 0.95032E-04 62 0.78593E-04 0.72395E-03 0.87799E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -29.195 43.574 5.6092 8.001 v Velocity[Y] -31.163 33.207 -0.16109 -0.049857 v Velocity[Z] -3.0512 3.13 2.3014e-06 -5.3908e-08 v ǁVelocityǁ 0.0023632 43.792 8.5719 8.1787 v Pressure -2.4784e+05 2.7131e+05 17906 -15718 v TurbVisc 2.4058e-20 0.024597 0.00020184 5.7896e-05 v CourantNb 3.6015e-08 0.011354 0.00016992 4.9648e-06 v FourierNb 1.2434e-07 0.040156 0.00014976 5.2839e-07 v total_pressure -1.4652e+05 3.7263e+05 1.1923e+05 85607 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0737 0.11165 0.0030042 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.0294e-07 0.045631 0.00031968 5.4932e-06 INSTANT 0.876389000E-01 TIME STEP NUMBER 56587 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283028295E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.832567756E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15411E-01 0.21095E+01 Friction velocity uk : 0.15411E-01 0.21095E+01 Dimensionless distance yplus : 0.15050E-01 0.20743E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 5.982492187e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29474E+08 1 0.18685E-09 0.31089E+02 0.21146E+04 c Velocity[X] 0.17578E+02 c Velocity[Y] 0.13510E+02 c Velocity[Z] 0.11544E-05 c Pressure 0.98516E-04 66 0.84055E-04 0.75011E-03 0.96239E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -29.211 43.589 5.6092 8.0011 v Velocity[Y] -31.176 33.222 -0.16115 -0.050045 v Velocity[Z] -3.0516 3.1301 2.3008e-06 -5.3908e-08 v ǁVelocityǁ 0.0023525 43.807 8.5735 8.179 v Pressure -2.4839e+05 2.7093e+05 17425 -16097 v TurbVisc 2.6138e-20 0.024613 0.00020191 5.7976e-05 v CourantNb 3.85e-08 0.011356 0.00016993 4.9649e-06 v FourierNb 1.2435e-07 0.040138 0.00014977 5.2894e-07 v total_pressure -1.4707e+05 3.7226e+05 1.1875e+05 85228 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0743 0.11168 0.0030047 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.0329e-07 0.045613 0.0003197 5.4938e-06 INSTANT 0.876390000E-01 TIME STEP NUMBER 56588 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283035263E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.833051779E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.63653E-02 0.21101E+01 Friction velocity uk : 0.63653E-02 0.21101E+01 Dimensionless distance yplus : 0.62163E-02 0.20748E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 6.074580888e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29474E+08 1 0.18688E-09 0.31120E+02 0.21156E+04 c Velocity[X] 0.17598E+02 c Velocity[Y] 0.13522E+02 c Velocity[Z] 0.11543E-05 c Pressure 0.10285E-03 127 0.98156E-04 0.78270E-03 0.10012E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -29.227 43.603 5.6093 8.0013 v Velocity[Y] -31.189 33.237 -0.16121 -0.050229 v Velocity[Z] -3.052 3.1303 2.3003e-06 -5.3908e-08 v ǁVelocityǁ 0.0023593 43.821 8.5751 8.1793 v Pressure -2.4909e+05 2.7054e+05 16894 -16396 v TurbVisc 2.7672e-20 0.024629 0.00020198 5.8057e-05 v CourantNb 4.0402e-08 0.011357 0.00016993 4.965e-06 v FourierNb 1.2435e-07 0.040119 0.00014978 5.2949e-07 v total_pressure -1.4776e+05 3.7187e+05 1.1822e+05 84929 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0748 0.11171 0.0030053 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.0364e-07 0.045596 0.00031972 5.4945e-06 INSTANT 0.876391000E-01 TIME STEP NUMBER 56589 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283041928E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.833533986E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.14679E-02 0.21107E+01 Friction velocity uk : 0.14679E-02 0.21107E+01 Dimensionless distance yplus : 0.14335E-02 0.20754E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 6.183745092e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29475E+08 1 0.18691E-09 0.31137E+02 0.21160E+04 c Velocity[X] 0.17612E+02 c Velocity[Y] 0.13525E+02 c Velocity[Z] 0.11591E-05 c Pressure 0.10730E-03 88 0.83575E-04 0.81611E-03 0.85994E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -29.243 43.618 5.6094 8.0014 v Velocity[Y] -31.203 33.252 -0.16127 -0.050416 v Velocity[Z] -3.0524 3.1304 2.2997e-06 -5.3908e-08 v ǁVelocityǁ 0.0024028 43.836 8.5767 8.1797 v Pressure -2.4977e+05 2.7006e+05 16297 -16886 v TurbVisc 2.7551e-20 0.024645 0.00020206 5.8137e-05 v CourantNb 4.2386e-08 0.011358 0.00016994 4.9651e-06 v FourierNb 1.2435e-07 0.0401 0.0001498 5.3004e-07 v total_pressure -1.4844e+05 3.7138e+05 1.1762e+05 84439 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0754 0.11174 0.0030058 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.0399e-07 0.045578 0.00031974 5.4951e-06 INSTANT 0.876392000E-01 TIME STEP NUMBER 56590 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283048720E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.834014757E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.23318E-02 0.21113E+01 Friction velocity uk : 0.23318E-02 0.21113E+01 Dimensionless distance yplus : 0.22521E-02 0.20760E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 6.300523486e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29476E+08 1 0.18695E-09 0.31174E+02 0.21171E+04 c Velocity[X] 0.17627E+02 c Velocity[Y] 0.13547E+02 c Velocity[Z] 0.11822E-05 c Pressure 0.10541E-03 15 0.58523E-04 0.80138E-03 0.58728E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -29.259 43.633 5.6095 8.0015 v Velocity[Y] -31.216 33.267 -0.16133 -0.050605 v Velocity[Z] -3.0528 3.1306 2.2991e-06 -5.3908e-08 v ǁVelocityǁ 0.0024943 43.851 8.5783 8.18 v Pressure -2.5043e+05 2.6962e+05 15694 -17222 v TurbVisc 2.9098e-20 0.024661 0.00020213 5.8218e-05 v CourantNb 4.4416e-08 0.011359 0.00016994 4.9652e-06 v FourierNb 1.2435e-07 0.040081 0.00014981 5.3059e-07 v total_pressure -1.4911e+05 3.7094e+05 1.1702e+05 84103 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.076 0.11178 0.0030063 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.0435e-07 0.04556 0.00031975 5.4958e-06 INSTANT 0.876393000E-01 TIME STEP NUMBER 56591 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283055513E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.834494219E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.29403E-02 0.21118E+01 Friction velocity uk : 0.29403E-02 0.21118E+01 Dimensionless distance yplus : 0.28432E-02 0.20765E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 6.440150561e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29477E+08 1 0.18699E-09 0.31202E+02 0.21179E+04 c Velocity[X] 0.17648E+02 c Velocity[Y] 0.13554E+02 c Velocity[Z] 0.11806E-05 c Pressure 0.11123E-03 260 0.79886E-04 0.84519E-03 0.97832E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -29.275 43.647 5.6096 8.0017 v Velocity[Y] -31.229 33.282 -0.16139 -0.050791 v Velocity[Z] -3.0532 3.1307 2.2986e-06 -5.3908e-08 v ǁVelocityǁ 0.002614 43.866 8.5799 8.1803 v Pressure -2.5128e+05 2.69e+05 15016 -17683 v TurbVisc 3.4671e-20 0.024677 0.00020221 5.8299e-05 v CourantNb 4.5921e-08 0.01136 0.00016995 4.9653e-06 v FourierNb 1.2435e-07 0.040062 0.00014982 5.3114e-07 v total_pressure -1.4995e+05 3.7032e+05 1.1634e+05 83642 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0765 0.11182 0.003007 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.047e-07 0.045542 0.00031977 5.4965e-06 INSTANT 0.876394000E-01 TIME STEP NUMBER 56592 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283062091E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.834970708E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.94196E-02 0.21124E+01 Friction velocity uk : 0.94196E-02 0.21124E+01 Dimensionless distance yplus : 0.91087E-02 0.20771E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 6.555642783e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29477E+08 1 0.18703E-09 0.31235E+02 0.21189E+04 c Velocity[X] 0.17661E+02 c Velocity[Y] 0.13574E+02 c Velocity[Z] 0.11818E-05 c Pressure 0.11511E-03 49 0.85485E-04 0.87420E-03 0.10266E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -29.292 43.662 5.6096 8.0018 v Velocity[Y] -31.242 33.297 -0.16145 -0.050981 v Velocity[Z] -3.0536 3.1309 2.298e-06 -5.3908e-08 v ǁVelocityǁ 0.0027736 43.881 8.5815 8.1807 v Pressure -2.5203e+05 2.6844e+05 14314 -18146 v TurbVisc 2.5584e-20 0.024693 0.00020228 5.838e-05 v CourantNb 4.8706e-08 0.011362 0.00016996 4.9654e-06 v FourierNb 1.2435e-07 0.040044 0.00014983 5.3169e-07 v total_pressure -1.507e+05 3.6977e+05 1.1564e+05 83179 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0771 0.11186 0.0030078 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.0506e-07 0.045524 0.00031979 5.4971e-06 INSTANT 0.876395000E-01 TIME STEP NUMBER 56593 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283068851E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.835447389E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13959E-01 0.21130E+01 Friction velocity uk : 0.13959E-01 0.21130E+01 Dimensionless distance yplus : 0.13498E-01 0.20777E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 6.722555883e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29478E+08 1 0.18707E-09 0.31253E+02 0.21194E+04 c Velocity[X] 0.17678E+02 c Velocity[Y] 0.13575E+02 c Velocity[Z] 0.11722E-05 c Pressure 0.11971E-03 244 0.75031E-04 0.90864E-03 0.80579E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -29.308 43.676 5.6097 8.0019 v Velocity[Y] -31.255 33.312 -0.16151 -0.05117 v Velocity[Z] -3.0539 3.1311 2.2975e-06 -5.3908e-08 v ǁVelocityǁ 0.0029094 43.895 8.583 8.181 v Pressure -2.5293e+05 2.678e+05 13547 -18642 v TurbVisc 2.937e-20 0.024709 0.00020236 5.8461e-05 v CourantNb 5.0794e-08 0.011363 0.00016996 4.9655e-06 v FourierNb 1.2435e-07 0.040025 0.00014984 5.3225e-07 v total_pressure -1.516e+05 3.6912e+05 1.1487e+05 82683 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0777 0.1119 0.0030085 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.0542e-07 0.045506 0.0003198 5.4978e-06 INSTANT 0.876396000E-01 TIME STEP NUMBER 56594 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283075385E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.835920683E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.17417E-01 0.21136E+01 Friction velocity uk : 0.17417E-01 0.21136E+01 Dimensionless distance yplus : 0.16843E-01 0.20783E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 6.883622389e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29479E+08 1 0.18710E-09 0.31287E+02 0.21204E+04 c Velocity[X] 0.17694E+02 c Velocity[Y] 0.13593E+02 c Velocity[Z] 0.11987E-05 c Pressure 0.11958E-03 15 0.56700E-04 0.90722E-03 0.60706E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -29.324 43.691 5.6098 8.002 v Velocity[Y] -31.269 33.327 -0.16157 -0.051358 v Velocity[Z] -3.0543 3.1312 2.2969e-06 -5.3908e-08 v ǁVelocityǁ 0.0028901 43.91 8.5846 8.1813 v Pressure -2.5377e+05 2.6721e+05 12776 -19033 v TurbVisc 3.181e-20 0.024724 0.00020243 5.8542e-05 v CourantNb 5.2975e-08 0.011364 0.00016997 4.9656e-06 v FourierNb 1.2435e-07 0.040006 0.00014985 5.328e-07 v total_pressure -1.5245e+05 3.6853e+05 1.141e+05 82292 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0783 0.11194 0.0030093 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.0577e-07 0.045489 0.00031982 5.4984e-06 INSTANT 0.876397000E-01 TIME STEP NUMBER 56595 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283081819E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.836391765E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.14564E-01 0.21142E+01 Friction velocity uk : 0.14564E-01 0.21142E+01 Dimensionless distance yplus : 0.14191E-01 0.20788E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 7.049530776e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29480E+08 1 0.18714E-09 0.31310E+02 0.21211E+04 c Velocity[X] 0.17709E+02 c Velocity[Y] 0.13602E+02 c Velocity[Z] 0.11919E-05 c Pressure 0.12499E-03 21 0.97828E-04 0.94771E-03 0.10411E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -29.34 43.706 5.6099 8.0022 v Velocity[Y] -31.282 33.342 -0.16164 -0.051547 v Velocity[Z] -3.0547 3.1314 2.2964e-06 -5.3908e-08 v ǁVelocityǁ 0.0028769 43.925 8.5862 8.1817 v Pressure -2.5481e+05 2.664e+05 11888 -19787 v TurbVisc 4.2189e-20 0.02474 0.00020251 5.8623e-05 v CourantNb 5.4624e-08 0.011365 0.00016997 4.9657e-06 v FourierNb 1.2435e-07 0.040063 0.00014986 5.3335e-07 v total_pressure -1.5349e+05 3.6772e+05 1.1321e+05 81538 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0788 0.11197 0.00301 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.0586e-07 0.04547 0.00031984 5.4991e-06 INSTANT 0.876398000E-01 TIME STEP NUMBER 56596 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283088203E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.836857989E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.34797E-02 0.21148E+01 Friction velocity uk : 0.34797E-02 0.21148E+01 Dimensionless distance yplus : 0.33905E-02 0.20794E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 7.235165993e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29480E+08 1 0.18718E-09 0.31336E+02 0.21218E+04 c Velocity[X] 0.17724E+02 c Velocity[Y] 0.13613E+02 c Velocity[Z] 0.11836E-05 c Pressure 0.12803E-03 313 0.81312E-04 0.97029E-03 0.69499E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -29.357 43.72 5.61 8.0023 v Velocity[Y] -31.295 33.357 -0.1617 -0.051737 v Velocity[Z] -3.0551 3.1315 2.2958e-06 -5.3908e-08 v ǁVelocityǁ 0.0028638 43.94 8.5879 8.182 v Pressure -2.5571e+05 2.6565e+05 11040 -20287 v TurbVisc 2.5981e-20 0.024756 0.00020258 5.8704e-05 v CourantNb 5.7563e-08 0.011366 0.00016998 4.9658e-06 v FourierNb 1.2435e-07 0.040117 0.00014988 5.3391e-07 v total_pressure -1.5438e+05 3.6697e+05 1.1236e+05 81038 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0794 0.11201 0.0030106 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.0588e-07 0.045453 0.00031986 5.4998e-06 INSTANT 0.876399000E-01 TIME STEP NUMBER 56597 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283094617E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.837325471E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.64287E-02 0.21154E+01 Friction velocity uk : 0.64287E-02 0.21154E+01 Dimensionless distance yplus : 0.62637E-02 0.20800E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 7.304647657e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29481E+08 1 0.18722E-09 0.31370E+02 0.21228E+04 c Velocity[X] 0.17734E+02 c Velocity[Y] 0.13636E+02 c Velocity[Z] 0.11903E-05 c Pressure 0.13055E-03 9 0.53221E-04 0.98885E-03 0.82728E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -29.373 43.735 5.6101 8.0024 v Velocity[Y] -31.308 33.372 -0.16176 -0.05193 v Velocity[Z] -3.0555 3.1317 2.2953e-06 -5.3908e-08 v ǁVelocityǁ 0.0027985 43.955 8.5895 8.1823 v Pressure -2.5672e+05 2.6492e+05 10086 -20852 v TurbVisc 3.306e-20 0.024772 0.00020266 5.8786e-05 v CourantNb 5.9871e-08 0.011368 0.00016999 4.9659e-06 v FourierNb 1.2435e-07 0.040169 0.00014989 5.3447e-07 v total_pressure -1.5539e+05 3.6625e+05 1.1141e+05 80473 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.08 0.11205 0.0030113 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.059e-07 0.045435 0.00031987 5.5004e-06 INSTANT 0.876400000E-01 TIME STEP NUMBER 56598 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283100973E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.837787628E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.16052E-01 0.21159E+01 Friction velocity uk : 0.16052E-01 0.21159E+01 Dimensionless distance yplus : 0.15640E-01 0.20806E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 7.512308334e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29482E+08 1 0.18725E-09 0.31393E+02 0.21234E+04 c Velocity[X] 0.17753E+02 c Velocity[Y] 0.13639E+02 c Velocity[Z] 0.11915E-05 c Pressure 0.13599E-03 36 0.98166E-04 0.10295E-02 0.84838E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -29.389 43.75 5.6102 8.0025 v Velocity[Y] -31.322 33.387 -0.16183 -0.052122 v Velocity[Z] -3.0559 3.1318 2.2947e-06 -5.3908e-08 v ǁVelocityǁ 0.0026648 43.97 8.5911 8.1826 v Pressure -2.5775e+05 2.6407e+05 9165.5 -21453 v TurbVisc 3.7602e-20 0.024788 0.00020273 5.8867e-05 v CourantNb 6.2371e-08 0.011369 0.00016999 4.966e-06 v FourierNb 1.2435e-07 0.040231 0.0001499 5.3502e-07 v total_pressure -1.5643e+05 3.6539e+05 1.1049e+05 79872 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0806 0.11209 0.0030121 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.0592e-07 0.045417 0.00031989 5.5011e-06 INSTANT 0.876401000E-01 TIME STEP NUMBER 56599 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283107206E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.838248355E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.18959E-01 0.21166E+01 Friction velocity uk : 0.18959E-01 0.21166E+01 Dimensionless distance yplus : 0.18449E-01 0.20812E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 7.651148261e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29482E+08 1 0.18730E-09 0.31418E+02 0.21242E+04 c Velocity[X] 0.17769E+02 c Velocity[Y] 0.13650E+02 c Velocity[Z] 0.11956E-05 c Pressure 0.13902E-03 34 0.83803E-04 0.10519E-02 0.85974E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -29.406 43.764 5.6102 8.0026 v Velocity[Y] -31.335 33.402 -0.16189 -0.052313 v Velocity[Z] -3.0563 3.132 2.2942e-06 -5.3908e-08 v ǁVelocityǁ 0.0025325 43.984 8.5927 8.183 v Pressure -2.5889e+05 2.6317e+05 8133.6 -22091 v TurbVisc 3.3813e-20 0.024804 0.00020281 5.8948e-05 v CourantNb 6.4696e-08 0.01137 0.00017 4.9662e-06 v FourierNb 1.2436e-07 0.040327 0.00014991 5.3558e-07 v total_pressure -1.5756e+05 3.6449e+05 1.0946e+05 79234 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0812 0.11213 0.0030128 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.0595e-07 0.045399 0.00031991 5.5017e-06 INSTANT 0.876402000E-01 TIME STEP NUMBER 56600 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283113352E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.838701138E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15475E-01 0.21171E+01 Friction velocity uk : 0.15475E-01 0.21171E+01 Dimensionless distance yplus : 0.15058E-01 0.20818E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 7.798515434e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29483E+08 1 0.18733E-09 0.31452E+02 0.21252E+04 c Velocity[X] 0.17785E+02 c Velocity[Y] 0.13667E+02 c Velocity[Z] 0.12012E-05 c Pressure 0.14163E-03 9 0.57148E-04 0.10711E-02 0.79372E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -29.422 43.779 5.6103 8.0028 v Velocity[Y] -31.348 33.417 -0.16196 -0.052504 v Velocity[Z] -3.0567 3.1321 2.2936e-06 -5.3908e-08 v ǁVelocityǁ 0.0024145 43.999 8.5943 8.1833 v Pressure -2.6002e+05 2.6227e+05 7083.7 -22652 v TurbVisc 3.9041e-20 0.02482 0.00020288 5.903e-05 v CourantNb 6.7092e-08 0.011371 0.00017001 4.9663e-06 v FourierNb 1.2436e-07 0.040408 0.00014992 5.3613e-07 v total_pressure -1.587e+05 3.636e+05 1.0841e+05 78673 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0818 0.11217 0.0030134 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.0597e-07 0.045381 0.00031993 5.5024e-06 INSTANT 0.876403000E-01 TIME STEP NUMBER 56601 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283119381E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.839153458E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.92067E-02 0.21177E+01 Friction velocity uk : 0.92067E-02 0.21177E+01 Dimensionless distance yplus : 0.89532E-02 0.20823E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 7.902902009e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29484E+08 1 0.18737E-09 0.31480E+02 0.21260E+04 c Velocity[X] 0.17796E+02 c Velocity[Y] 0.13683E+02 c Velocity[Z] 0.12041E-05 c Pressure 0.14707E-03 59 0.77528E-04 0.11117E-02 0.14060E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -29.438 43.794 5.6104 8.0029 v Velocity[Y] -31.361 33.432 -0.16202 -0.052698 v Velocity[Z] -3.0571 3.1323 2.2931e-06 -5.3908e-08 v ǁVelocityǁ 0.0023039 44.014 8.5959 8.1836 v Pressure -2.612e+05 2.6127e+05 5988.1 -23559 v TurbVisc 4.47e-20 0.024836 0.00020296 5.9111e-05 v CourantNb 6.9781e-08 0.011372 0.00017001 4.9664e-06 v FourierNb 1.2436e-07 0.040466 0.00014993 5.3669e-07 v total_pressure -1.5988e+05 3.6259e+05 1.0731e+05 77766 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0823 0.1122 0.0030141 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.0599e-07 0.045363 0.00031994 5.5031e-06 INSTANT 0.876404000E-01 TIME STEP NUMBER 56602 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283125481E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.839602615E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.40094E-02 0.21183E+01 Friction velocity uk : 0.40094E-02 0.21183E+01 Dimensionless distance yplus : 0.38990E-02 0.20829E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 7.987512489e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29484E+08 1 0.18742E-09 0.31508E+02 0.21268E+04 c Velocity[X] 0.17812E+02 c Velocity[Y] 0.13695E+02 c Velocity[Z] 0.12071E-05 c Pressure 0.15091E-03 72 0.82431E-04 0.11401E-02 0.10470E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -29.455 43.808 5.6105 8.003 v Velocity[Y] -31.375 33.448 -0.16209 -0.052889 v Velocity[Z] -3.0574 3.1324 2.2926e-06 -5.3909e-08 v ǁVelocityǁ 0.0022061 44.029 8.5975 8.1839 v Pressure -2.6241e+05 2.6031e+05 4868.5 -24147 v TurbVisc 4.1333e-20 0.024852 0.00020304 5.9193e-05 v CourantNb 7.2156e-08 0.011374 0.00017002 4.9665e-06 v FourierNb 1.2436e-07 0.040514 0.00014994 5.3725e-07 v total_pressure -1.6109e+05 3.6163e+05 1.0619e+05 77178 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0829 0.11224 0.0030147 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.0602e-07 0.045345 0.00031996 5.5037e-06 INSTANT 0.876405000E-01 TIME STEP NUMBER 56603 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283131255E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.840046751E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13502E-01 0.21189E+01 Friction velocity uk : 0.13502E-01 0.21189E+01 Dimensionless distance yplus : 0.13130E-01 0.20835E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 8.117346928e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29485E+08 1 0.18745E-09 0.31537E+02 0.21277E+04 c Velocity[X] 0.17823E+02 c Velocity[Y] 0.13714E+02 c Velocity[Z] 0.12032E-05 c Pressure 0.15525E-03 102 0.96062E-04 0.11723E-02 0.13701E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -29.471 43.823 5.6106 8.0031 v Velocity[Y] -31.388 33.463 -0.16215 -0.053085 v Velocity[Z] -3.0578 3.1326 2.292e-06 -5.3909e-08 v ǁVelocityǁ 0.0021255 44.044 8.5991 8.1842 v Pressure -2.636e+05 2.5928e+05 3696.2 -24946 v TurbVisc 4.6008e-20 0.024868 0.00020311 5.9275e-05 v CourantNb 7.4706e-08 0.011375 0.00017003 4.9666e-06 v FourierNb 1.2436e-07 0.040603 0.00014995 5.3781e-07 v total_pressure -1.6228e+05 3.606e+05 1.0502e+05 76379 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0835 0.11228 0.0030154 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.0604e-07 0.045327 0.00031998 5.5044e-06 INSTANT 0.876406000E-01 TIME STEP NUMBER 56604 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283137174E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.840487057E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12829E-01 0.21195E+01 Friction velocity uk : 0.12829E-01 0.21195E+01 Dimensionless distance yplus : 0.12342E-01 0.20841E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 8.227257571e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29486E+08 1 0.18749E-09 0.31550E+02 0.21280E+04 c Velocity[X] 0.17840E+02 c Velocity[Y] 0.13711E+02 c Velocity[Z] 0.12058E-05 c Pressure 0.15959E-03 190 0.81710E-04 0.12044E-02 0.95062E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -29.487 43.838 5.6107 8.0032 v Velocity[Y] -31.401 33.478 -0.16222 -0.053279 v Velocity[Z] -3.0582 3.1327 2.2915e-06 -5.3909e-08 v ǁVelocityǁ 0.0020624 44.059 8.6007 8.1846 v Pressure -2.6487e+05 2.5822e+05 2519.4 -25558 v TurbVisc 4.5346e-20 0.024884 0.00020319 5.9357e-05 v CourantNb 7.7284e-08 0.011376 0.00017003 4.9667e-06 v FourierNb 1.2436e-07 0.04067 0.00014996 5.3837e-07 v total_pressure -1.6354e+05 3.5955e+05 1.0384e+05 75767 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0841 0.11232 0.003016 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.0606e-07 0.045309 0.00031999 5.505e-06 INSTANT 0.876407000E-01 TIME STEP NUMBER 56605 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283142887E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.840921774E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.40207E-02 0.21201E+01 Friction velocity uk : 0.40207E-02 0.21201E+01 Dimensionless distance yplus : 0.38678E-02 0.20847E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 8.287402598e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29486E+08 1 0.18753E-09 0.31583E+02 0.21289E+04 c Velocity[X] 0.17852E+02 c Velocity[Y] 0.13731E+02 c Velocity[Z] 0.12137E-05 c Pressure 0.15966E-03 9 0.59741E-04 0.12043E-02 0.93537E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -29.504 43.852 5.6108 8.0033 v Velocity[Y] -31.414 33.493 -0.16229 -0.053472 v Velocity[Z] -3.0586 3.1329 2.2909e-06 -5.3909e-08 v ǁVelocityǁ 0.0020214 44.074 8.6023 8.1849 v Pressure -2.6613e+05 2.5721e+05 1281.7 -26257 v TurbVisc 5.0708e-20 0.024899 0.00020326 5.9439e-05 v CourantNb 7.9874e-08 0.011377 0.00017004 4.9668e-06 v FourierNb 1.2436e-07 0.040713 0.00014997 5.3893e-07 v total_pressure -1.6481e+05 3.5853e+05 1.0261e+05 75068 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0847 0.11236 0.0030165 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.0609e-07 0.045291 0.00032001 5.5057e-06 INSTANT 0.876408000E-01 TIME STEP NUMBER 56606 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283148374E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.841350519E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.25544E-02 0.21207E+01 Friction velocity uk : 0.25544E-02 0.21207E+01 Dimensionless distance yplus : 0.24798E-02 0.20853E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 8.315037522e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29487E+08 1 0.18757E-09 0.31610E+02 0.21297E+04 c Velocity[X] 0.17866E+02 c Velocity[Y] 0.13744E+02 c Velocity[Z] 0.12155E-05 c Pressure 0.16468E-03 53 0.77716E-04 0.12415E-02 0.15086E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -29.52 43.867 5.6109 8.0034 v Velocity[Y] -31.428 33.508 -0.16236 -0.053669 v Velocity[Z] -3.059 3.1331 2.2904e-06 -5.3909e-08 v ǁVelocityǁ 0.0019998 44.088 8.604 8.1852 v Pressure -2.6755e+05 2.5596e+05 -10.157 -27260 v TurbVisc 5.8898e-20 0.024915 0.00020334 5.9521e-05 v CourantNb 8.2396e-08 0.011379 0.00017004 4.9669e-06 v FourierNb 1.2436e-07 0.040734 0.00014998 5.3949e-07 v total_pressure -1.6623e+05 3.5728e+05 1.0131e+05 74065 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0853 0.1124 0.0030174 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.0629e-07 0.045273 0.00032003 5.5064e-06 INSTANT 0.876409000E-01 TIME STEP NUMBER 56607 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283154031E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.841774427E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.75504E-02 0.21214E+01 Friction velocity uk : 0.75504E-02 0.21214E+01 Dimensionless distance yplus : 0.73299E-02 0.20859E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 8.347808492e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29487E+08 1 0.18762E-09 0.31638E+02 0.21305E+04 c Velocity[X] 0.17881E+02 c Velocity[Y] 0.13757E+02 c Velocity[Z] 0.12171E-05 c Pressure 0.16835E-03 271 0.83384E-04 0.12685E-02 0.12155E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -29.537 43.881 5.6109 8.0035 v Velocity[Y] -31.441 33.523 -0.16243 -0.053863 v Velocity[Z] -3.0594 3.1332 2.2898e-06 -5.3909e-08 v ǁVelocityǁ 0.0020022 44.103 8.6056 8.1855 v Pressure -2.6895e+05 2.5478e+05 -1339.6 -28030 v TurbVisc 5.1429e-20 0.024931 0.00020342 5.9603e-05 v CourantNb 8.5076e-08 0.01138 0.00017005 4.967e-06 v FourierNb 1.2436e-07 0.040731 0.00014999 5.4005e-07 v total_pressure -1.6763e+05 3.561e+05 99985 73295 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0859 0.11244 0.0030183 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.067e-07 0.045255 0.00032005 5.507e-06 INSTANT 0.876410000E-01 TIME STEP NUMBER 56608 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283159306E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.842194782E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15986E-01 0.21220E+01 Friction velocity uk : 0.15986E-01 0.21220E+01 Dimensionless distance yplus : 0.15519E-01 0.20865E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 8.344258380e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29488E+08 1 0.18766E-09 0.31666E+02 0.21314E+04 c Velocity[X] 0.17891E+02 c Velocity[Y] 0.13775E+02 c Velocity[Z] 0.12140E-05 c Pressure 0.17246E-03 33 0.97013E-04 0.12988E-02 0.13828E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -29.553 43.896 5.611 8.0036 v Velocity[Y] -31.454 33.538 -0.1625 -0.054061 v Velocity[Z] -3.0598 3.1334 2.2893e-06 -5.3909e-08 v ǁVelocityǁ 0.0019869 44.118 8.6072 8.1858 v Pressure -2.7026e+05 2.5362e+05 -2670.3 -28855 v TurbVisc 5.5486e-20 0.024947 0.00020349 5.9685e-05 v CourantNb 8.7665e-08 0.011381 0.00017006 4.9671e-06 v FourierNb 1.2436e-07 0.040706 0.00015001 5.4061e-07 v total_pressure -1.6894e+05 3.5494e+05 98655 72470 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0865 0.11249 0.0030193 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.071e-07 0.045237 0.00032006 5.5077e-06 INSTANT 0.876411000E-01 TIME STEP NUMBER 56609 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283164732E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.842612244E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.17913E-01 0.21226E+01 Friction velocity uk : 0.17913E-01 0.21226E+01 Dimensionless distance yplus : 0.17363E-01 0.20871E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 8.369448175e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29489E+08 1 0.18770E-09 0.31678E+02 0.21316E+04 c Velocity[X] 0.17907E+02 c Velocity[Y] 0.13771E+02 c Velocity[Z] 0.12160E-05 c Pressure 0.17648E-03 338 0.82727E-04 0.13284E-02 0.11088E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -29.569 43.911 5.6111 8.0037 v Velocity[Y] -31.467 33.553 -0.16256 -0.054257 v Velocity[Z] -3.0602 3.1335 2.2887e-06 -5.3909e-08 v ǁVelocityǁ 0.0019862 44.133 8.6088 8.1861 v Pressure -2.7172e+05 2.5236e+05 -4044.8 -29620 v TurbVisc 5.6721e-20 0.024963 0.00020357 5.9767e-05 v CourantNb 9.0247e-08 0.011382 0.00017006 4.9672e-06 v FourierNb 1.2437e-07 0.040659 0.00015002 5.4117e-07 v total_pressure -1.7039e+05 3.5368e+05 97280 71705 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0871 0.11253 0.0030201 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.0751e-07 0.045219 0.00032008 5.5083e-06 INSTANT 0.876412000E-01 TIME STEP NUMBER 56610 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283169920E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.843020558E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11437E-01 0.21232E+01 Friction velocity uk : 0.11437E-01 0.21232E+01 Dimensionless distance yplus : 0.11086E-01 0.20877E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 8.323153007e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29489E+08 1 0.18774E-09 0.31710E+02 0.21326E+04 c Velocity[X] 0.17919E+02 c Velocity[Y] 0.13791E+02 c Velocity[Z] 0.12246E-05 c Pressure 0.17656E-03 9 0.60845E-04 0.13283E-02 0.99078E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -29.586 43.925 5.6112 8.0038 v Velocity[Y] -31.48 33.568 -0.16263 -0.054453 v Velocity[Z] -3.0605 3.1337 2.2882e-06 -5.3909e-08 v ǁVelocityǁ 0.0019836 44.148 8.6104 8.1864 v Pressure -2.7312e+05 2.512e+05 -5448.7 -30380 v TurbVisc 5.8177e-20 0.024979 0.00020364 5.985e-05 v CourantNb 9.2791e-08 0.011384 0.00017007 4.9673e-06 v FourierNb 1.2437e-07 0.04059 0.00015003 5.4174e-07 v total_pressure -1.7179e+05 3.5252e+05 95876 70945 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0877 0.11257 0.0030209 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.0792e-07 0.0452 0.0003201 5.509e-06 INSTANT 0.876413000E-01 TIME STEP NUMBER 56611 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283174866E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.843422185E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.58170E-02 0.21237E+01 Friction velocity uk : 0.58170E-02 0.21237E+01 Dimensionless distance yplus : 0.56384E-02 0.20882E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 8.215955515e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29490E+08 1 0.18778E-09 0.31738E+02 0.21334E+04 c Velocity[X] 0.17932E+02 c Velocity[Y] 0.13805E+02 c Velocity[Z] 0.12226E-05 c Pressure 0.18118E-03 165 0.78887E-04 0.13623E-02 0.17087E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -29.602 43.94 5.6113 8.0039 v Velocity[Y] -31.493 33.583 -0.16271 -0.054652 v Velocity[Z] -3.0609 3.1338 2.2877e-06 -5.3909e-08 v ǁVelocityǁ 0.001981 44.162 8.612 8.1867 v Pressure -2.7473e+05 2.4973e+05 -6933.5 -31576 v TurbVisc 5.5757e-20 0.024995 0.00020372 5.9932e-05 v CourantNb 9.2053e-08 0.011385 0.00017008 4.9673e-06 v FourierNb 1.2437e-07 0.0405 0.00015004 5.423e-07 v total_pressure -1.7341e+05 3.5106e+05 94391 69749 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0882 0.11261 0.0030216 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.0833e-07 0.045182 0.00032011 5.5096e-06 INSTANT 0.876414000E-01 TIME STEP NUMBER 56612 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283179941E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.843816717E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10379E-01 0.21244E+01 Friction velocity uk : 0.10379E-01 0.21244E+01 Dimensionless distance yplus : 0.10060E-01 0.20888E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 8.161336041e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29490E+08 1 0.18783E-09 0.31764E+02 0.21341E+04 c Velocity[X] 0.17950E+02 c Velocity[Y] 0.13815E+02 c Velocity[Z] 0.12185E-05 c Pressure 0.18459E-03 801 0.84767E-04 0.13872E-02 0.11738E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -29.619 43.954 5.6114 8.004 v Velocity[Y] -31.507 33.598 -0.16278 -0.054848 v Velocity[Z] -3.0613 3.134 2.2871e-06 -5.3909e-08 v ǁVelocityǁ 0.0019879 44.177 8.6137 8.187 v Pressure -2.7621e+05 2.4845e+05 -8402.2 -32285 v TurbVisc 2.8087e-20 0.02501 0.0002038 6.0015e-05 v CourantNb 8.0832e-08 0.011386 0.00017008 4.9674e-06 v FourierNb 1.2437e-07 0.040387 0.00015005 5.4286e-07 v total_pressure -1.7489e+05 3.4977e+05 92923 69040 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0888 0.11265 0.0030225 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.0874e-07 0.045164 0.00032013 5.5103e-06 INSTANT 0.876415000E-01 TIME STEP NUMBER 56613 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283184703E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.844208027E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.14774E-01 0.21250E+01 Friction velocity uk : 0.14774E-01 0.21250E+01 Dimensionless distance yplus : 0.14324E-01 0.20894E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 8.043883670e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29491E+08 1 0.18786E-09 0.31793E+02 0.21350E+04 c Velocity[X] 0.17956E+02 c Velocity[Y] 0.13836E+02 c Velocity[Z] 0.12184E-05 c Pressure 0.18832E-03 35 0.98787E-04 0.14145E-02 0.16008E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -29.635 43.969 5.6115 8.0041 v Velocity[Y] -31.52 33.613 -0.16285 -0.055049 v Velocity[Z] -3.0617 3.1341 2.2866e-06 -5.3909e-08 v ǁVelocityǁ 0.0019949 44.192 8.6153 8.1873 v Pressure -2.7773e+05 2.4716e+05 -9921.2 -33321 v TurbVisc 5.1795e-20 0.025026 0.00020387 6.0098e-05 v CourantNb 8.818e-08 0.011387 0.00017009 4.9675e-06 v FourierNb 1.2437e-07 0.040254 0.00015006 5.4343e-07 v total_pressure -1.764e+05 3.4848e+05 91404 68004 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0894 0.1127 0.0030233 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.0915e-07 0.045146 0.00032015 5.511e-06 INSTANT 0.876416000E-01 TIME STEP NUMBER 56614 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283189527E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.844594141E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.14566E-01 0.21255E+01 Friction velocity uk : 0.14566E-01 0.21255E+01 Dimensionless distance yplus : 0.14122E-01 0.20900E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 7.933712805e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29492E+08 1 0.18791E-09 0.31804E+02 0.21352E+04 c Velocity[X] 0.17974E+02 c Velocity[Y] 0.13830E+02 c Velocity[Z] 0.12190E-05 c Pressure 0.19201E-03 288 0.83992E-04 0.14415E-02 0.11732E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -29.652 43.983 5.6115 8.0042 v Velocity[Y] -31.533 33.628 -0.16292 -0.055248 v Velocity[Z] -3.0621 3.1343 2.286e-06 -5.3909e-08 v ǁVelocityǁ 0.0020233 44.206 8.6169 8.1876 v Pressure -2.7931e+05 2.4574e+05 -11454 -34152 v TurbVisc 5.1769e-20 0.025042 0.00020395 6.018e-05 v CourantNb 8.827e-08 0.011389 0.0001701 4.9676e-06 v FourierNb 1.2437e-07 0.040103 0.00015007 5.4399e-07 v total_pressure -1.7798e+05 3.4706e+05 89871 67173 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.09 0.11274 0.0030241 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.0956e-07 0.045127 0.00032017 5.5116e-06 INSTANT 0.876417000E-01 TIME STEP NUMBER 56615 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283194125E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.844970106E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.93934E-02 0.21261E+01 Friction velocity uk : 0.93934E-02 0.21261E+01 Dimensionless distance yplus : 0.90935E-02 0.20906E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 7.775672102e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29492E+08 1 0.18795E-09 0.31836E+02 0.21361E+04 c Velocity[X] 0.17985E+02 c Velocity[Y] 0.13851E+02 c Velocity[Z] 0.12314E-05 c Pressure 0.19188E-03 9 0.62292E-04 0.14397E-02 0.10610E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -29.668 43.998 5.6116 8.0043 v Velocity[Y] -31.546 33.643 -0.16299 -0.055446 v Velocity[Z] -3.0625 3.1344 2.2855e-06 -5.3909e-08 v ǁVelocityǁ 0.002075 44.221 8.6185 8.1879 v Pressure -2.8084e+05 2.4446e+05 -13016 -34991 v TurbVisc 5.1095e-20 0.025058 0.00020403 6.0263e-05 v CourantNb 8.6859e-08 0.01139 0.0001701 4.9677e-06 v FourierNb 1.2437e-07 0.039933 0.00015008 5.4456e-07 v total_pressure -1.7952e+05 3.4579e+05 88309 66334 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0906 0.11278 0.0030248 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.0998e-07 0.045109 0.00032018 5.5123e-06 INSTANT 0.876418000E-01 TIME STEP NUMBER 56616 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283198451E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.845338812E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.34407E-02 0.21267E+01 Friction velocity uk : 0.34407E-02 0.21267E+01 Dimensionless distance yplus : 0.33309E-02 0.20911E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 7.540403004e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29493E+08 1 0.18799E-09 0.31863E+02 0.21369E+04 c Velocity[X] 0.17999E+02 c Velocity[Y] 0.13864E+02 c Velocity[Z] 0.12261E-05 c Pressure 0.19608E-03 33 0.80056E-04 0.14704E-02 0.17986E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -29.684 44.012 5.6117 8.0044 v Velocity[Y] -31.559 33.658 -0.16306 -0.055648 v Velocity[Z] -3.0629 3.1346 2.285e-06 -5.3909e-08 v ǁVelocityǁ 0.0021406 44.236 8.6201 8.1882 v Pressure -2.826e+05 2.4284e+05 -14656 -36293 v TurbVisc 4.8645e-20 0.025074 0.0002041 6.0346e-05 v CourantNb 8.5254e-08 0.011391 0.00017011 4.9678e-06 v FourierNb 1.2437e-07 0.039746 0.00015009 5.4513e-07 v total_pressure -1.8127e+05 3.4416e+05 86669 65032 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0911 0.11282 0.0030255 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.1039e-07 0.04509 0.0003202 5.5129e-06 INSTANT 0.876419000E-01 TIME STEP NUMBER 56617 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283202910E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.845699365E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11711E-01 0.21273E+01 Friction velocity uk : 0.11711E-01 0.21273E+01 Dimensionless distance yplus : 0.11337E-01 0.20917E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 7.380163814e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29493E+08 1 0.18804E-09 0.31890E+02 0.21377E+04 c Velocity[X] 0.18016E+02 c Velocity[Y] 0.13874E+02 c Velocity[Z] 0.12215E-05 c Pressure 0.19912E-03 699 0.86111E-04 0.14924E-02 0.12324E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -29.701 44.026 5.6118 8.0044 v Velocity[Y] -31.572 33.673 -0.16313 -0.055847 v Velocity[Z] -3.0633 3.1347 2.2844e-06 -5.3909e-08 v ǁVelocityǁ 0.0022251 44.25 8.6218 8.1885 v Pressure -2.8422e+05 2.4139e+05 -16278 -37086 v TurbVisc 4.991e-20 0.025089 0.00020418 6.0429e-05 v CourantNb 8.4125e-08 0.011392 0.00017012 4.9679e-06 v FourierNb 1.2437e-07 0.039563 0.0001501 5.4569e-07 v total_pressure -1.8289e+05 3.4272e+05 85047 64239 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0917 0.11287 0.0030263 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.1081e-07 0.045072 0.00032022 5.5136e-06 INSTANT 0.876420000E-01 TIME STEP NUMBER 56618 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283207040E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.846056089E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.17253E-01 0.21279E+01 Friction velocity uk : 0.17253E-01 0.21279E+01 Dimensionless distance yplus : 0.16683E-01 0.20923E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 7.155328267e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29494E+08 1 0.18807E-09 0.31904E+02 0.21380E+04 c Velocity[X] 0.18024E+02 c Velocity[Y] 0.13880E+02 c Velocity[Z] 0.12209E-05 c Pressure 0.20246E-03 57 0.75030E-04 0.15166E-02 0.14386E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -29.717 44.041 5.6119 8.0045 v Velocity[Y] -31.585 33.688 -0.16321 -0.056048 v Velocity[Z] -3.0636 3.1349 2.2839e-06 -5.391e-08 v ǁVelocityǁ 0.0023236 44.265 8.6234 8.1888 v Pressure -2.859e+05 2.3995e+05 -17948 -38192 v TurbVisc 4.7868e-20 0.025105 0.00020426 6.0512e-05 v CourantNb 8.2109e-08 0.011394 0.00017012 4.968e-06 v FourierNb 1.2437e-07 0.039544 0.00015011 5.4626e-07 v total_pressure -1.8457e+05 3.4127e+05 83377 63133 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0923 0.11291 0.0030271 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.1123e-07 0.045053 0.00032023 5.5142e-06 INSTANT 0.876421000E-01 TIME STEP NUMBER 56619 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283211127E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.846407143E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11900E-01 0.21284E+01 Friction velocity uk : 0.11900E-01 0.21284E+01 Dimensionless distance yplus : 0.11507E-01 0.20928E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 6.933581832e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29494E+08 1 0.18812E-09 0.31934E+02 0.21389E+04 c Velocity[X] 0.18035E+02 c Velocity[Y] 0.13899E+02 c Velocity[Z] 0.12403E-05 c Pressure 0.20277E-03 9 0.56845E-04 0.15182E-02 0.11232E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -29.733 44.055 5.6119 8.0046 v Velocity[Y] -31.598 33.702 -0.16328 -0.056251 v Velocity[Z] -3.064 3.135 2.2833e-06 -5.391e-08 v ǁVelocityǁ 0.0023075 44.279 8.625 8.1891 v Pressure -2.875e+05 2.3852e+05 -19619 -39088 v TurbVisc 4.881e-20 0.025121 0.00020433 6.0595e-05 v CourantNb 8.1258e-08 0.011395 0.00017013 4.9681e-06 v FourierNb 1.2437e-07 0.039524 0.00015012 5.4683e-07 v total_pressure -1.8617e+05 3.3985e+05 81706 62237 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0928 0.11295 0.0030278 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.1165e-07 0.045034 0.00032025 5.5149e-06 INSTANT 0.876422000E-01 TIME STEP NUMBER 56620 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283215077E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.846747799E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.56320E-02 0.21290E+01 Friction velocity uk : 0.56320E-02 0.21290E+01 Dimensionless distance yplus : 0.54460E-02 0.20934E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 6.608514648e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29495E+08 1 0.18816E-09 0.31956E+02 0.21395E+04 c Velocity[X] 0.18053E+02 c Velocity[Y] 0.13903E+02 c Velocity[Z] 0.12307E-05 c Pressure 0.20631E-03 66 0.96503E-04 0.15438E-02 0.13642E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -29.75 44.069 5.612 8.0047 v Velocity[Y] -31.611 33.717 -0.16335 -0.056454 v Velocity[Z] -3.0644 3.1352 2.2828e-06 -5.391e-08 v ǁVelocityǁ 0.0020936 44.294 8.6266 8.1893 v Pressure -2.8923e+05 2.3687e+05 -21302 -40177 v TurbVisc 4.5721e-20 0.025137 0.00020441 6.0678e-05 v CourantNb 7.9294e-08 0.011396 0.00017014 4.9682e-06 v FourierNb 1.2438e-07 0.039504 0.00015013 5.474e-07 v total_pressure -1.8791e+05 3.382e+05 80023 61148 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0934 0.11299 0.0030284 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.1207e-07 0.045015 0.00032027 5.5156e-06 INSTANT 0.876423000E-01 TIME STEP NUMBER 56621 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283218878E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.847078457E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.41490E-02 0.21295E+01 Friction velocity uk : 0.41490E-02 0.21295E+01 Dimensionless distance yplus : 0.41020E-02 0.20939E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 6.376727661e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29495E+08 1 0.18820E-09 0.31979E+02 0.21402E+04 c Velocity[X] 0.18067E+02 c Velocity[Y] 0.13912E+02 c Velocity[Z] 0.12206E-05 c Pressure 0.20826E-03 52 0.80572E-04 0.15576E-02 0.12752E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -29.766 44.084 5.6121 8.0047 v Velocity[Y] -31.624 33.732 -0.16343 -0.056656 v Velocity[Z] -3.0648 3.1353 2.2823e-06 -5.391e-08 v ǁVelocityǁ 0.0019146 44.308 8.6282 8.1896 v Pressure -2.91e+05 2.3532e+05 -23072 -41231 v TurbVisc 4.6764e-20 0.025152 0.00020449 6.0762e-05 v CourantNb 7.6963e-08 0.011397 0.00017014 4.9682e-06 v FourierNb 1.2438e-07 0.039484 0.00015014 5.4796e-07 v total_pressure -1.8967e+05 3.3664e+05 78253 60094 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0939 0.11303 0.0030292 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.1249e-07 0.044996 0.00032028 5.5162e-06 INSTANT 0.876424000E-01 TIME STEP NUMBER 56622 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283222535E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.847400304E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13841E-01 0.21301E+01 Friction velocity uk : 0.13841E-01 0.21301E+01 Dimensionless distance yplus : 0.13384E-01 0.20945E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 6.064981140e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29496E+08 1 0.18824E-09 0.32010E+02 0.21411E+04 c Velocity[X] 0.18081E+02 c Velocity[Y] 0.13929E+02 c Velocity[Z] 0.12374E-05 c Pressure 0.20991E-03 9 0.56583E-04 0.15691E-02 0.11821E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -29.782 44.098 5.6121 8.0048 v Velocity[Y] -31.637 33.747 -0.1635 -0.056858 v Velocity[Z] -3.0652 3.1355 2.2817e-06 -5.391e-08 v ǁVelocityǁ 0.0017688 44.323 8.6298 8.1899 v Pressure -2.9277e+05 2.3376e+05 -24851 -42209 v TurbVisc 4.6182e-20 0.025168 0.00020456 6.0845e-05 v CourantNb 7.7427e-08 0.011398 0.00017015 4.9683e-06 v FourierNb 1.2438e-07 0.039464 0.00015015 5.4853e-07 v total_pressure -1.9144e+05 3.3508e+05 76474 59116 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0945 0.11308 0.0030299 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.1291e-07 0.044977 0.0003203 5.5169e-06 INSTANT 0.876425000E-01 TIME STEP NUMBER 56623 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283225978E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.847717734E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.18297E-01 0.21306E+01 Friction velocity uk : 0.18297E-01 0.21306E+01 Dimensionless distance yplus : 0.17725E-01 0.20950E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 5.675600171e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29496E+08 1 0.18828E-09 0.32032E+02 0.21417E+04 c Velocity[X] 0.18095E+02 c Velocity[Y] 0.13936E+02 c Velocity[Z] 0.12310E-05 c Pressure 0.21332E-03 164 0.97716E-04 0.15937E-02 0.15264E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -29.799 44.112 5.6122 8.0049 v Velocity[Y] -31.65 33.762 -0.16357 -0.057061 v Velocity[Z] -3.0656 3.1356 2.2812e-06 -5.391e-08 v ǁVelocityǁ 0.0016532 44.337 8.6314 8.1902 v Pressure -2.9461e+05 2.3205e+05 -26611 -43450 v TurbVisc 4.3816e-20 0.025184 0.00020464 6.0929e-05 v CourantNb 7.4386e-08 0.0114 0.00017016 4.9684e-06 v FourierNb 1.2438e-07 0.039444 0.00015016 5.4911e-07 v total_pressure -1.9328e+05 3.3337e+05 74714 57875 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.095 0.11312 0.0030306 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.1333e-07 0.044958 0.00032031 5.5175e-06 INSTANT 0.876426000E-01 TIME STEP NUMBER 56624 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283229356E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.848027539E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.16087E-01 0.21311E+01 Friction velocity uk : 0.16087E-01 0.21311E+01 Dimensionless distance yplus : 0.15532E-01 0.20955E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 5.377310452e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29497E+08 1 0.18833E-09 0.32055E+02 0.21424E+04 c Velocity[X] 0.18108E+02 c Velocity[Y] 0.13947E+02 c Velocity[Z] 0.12210E-05 c Pressure 0.21501E-03 346 0.82799E-04 0.16056E-02 0.13140E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -29.815 44.126 5.6122 8.0049 v Velocity[Y] -31.663 33.777 -0.16364 -0.057266 v Velocity[Z] -3.066 3.1358 2.2807e-06 -5.391e-08 v ǁVelocityǁ 0.00159 44.352 8.633 8.1904 v Pressure -2.9637e+05 2.3041e+05 -28448 -44560 v TurbVisc 5.7924e-20 0.0252 0.00020471 6.1012e-05 v CourantNb 7.4082e-08 0.011401 0.00017016 4.9685e-06 v FourierNb 1.2438e-07 0.039423 0.00015017 5.4968e-07 v total_pressure -1.9504e+05 3.3173e+05 72877 56765 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0955 0.11317 0.0030313 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.1376e-07 0.044939 0.00032033 5.5182e-06 INSTANT 0.876427000E-01 TIME STEP NUMBER 56625 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283232598E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.848325774E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13878E-01 0.21316E+01 Friction velocity uk : 0.13878E-01 0.21316E+01 Dimensionless distance yplus : 0.13352E-01 0.20960E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 5.172699928e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29497E+08 1 0.18837E-09 0.32086E+02 0.21433E+04 c Velocity[X] 0.18117E+02 c Velocity[Y] 0.13970E+02 c Velocity[Z] 0.12431E-05 c Pressure 0.21638E-03 9 0.58037E-04 0.16149E-02 0.12419E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -29.831 44.141 5.6123 8.005 v Velocity[Y] -31.676 33.792 -0.16372 -0.057472 v Velocity[Z] -3.0663 3.1359 2.2801e-06 -5.391e-08 v ǁVelocityǁ 0.0015708 44.366 8.6346 8.1907 v Pressure -2.9816e+05 2.2886e+05 -30299 -45594 v TurbVisc 4.4637e-20 0.025215 0.00020479 6.1096e-05 v CourantNb 6.6368e-08 0.011402 0.00017017 4.9686e-06 v FourierNb 1.2438e-07 0.039403 0.00015018 5.5025e-07 v total_pressure -1.9683e+05 3.3019e+05 71026 55731 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.096 0.11321 0.0030319 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.1418e-07 0.044919 0.00032035 5.5188e-06 INSTANT 0.876428000E-01 TIME STEP NUMBER 56626 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283235704E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.848619629E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.88142E-02 0.21321E+01 Friction velocity uk : 0.88142E-02 0.21321E+01 Dimensionless distance yplus : 0.84799E-02 0.20965E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 4.580954233e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29497E+08 1 0.18841E-09 0.32113E+02 0.21440E+04 c Velocity[X] 0.18140E+02 c Velocity[Y] 0.13973E+02 c Velocity[Z] 0.12312E-05 c Pressure 0.21952E-03 144 0.75689E-04 0.16374E-02 0.14681E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -29.848 44.155 5.6123 8.005 v Velocity[Y] -31.689 33.806 -0.16379 -0.057676 v Velocity[Z] -3.0667 3.1361 2.2796e-06 -5.391e-08 v ǁVelocityǁ 0.0014464 44.38 8.6363 8.191 v Pressure -3.0004e+05 2.2706e+05 -32097 -46708 v TurbVisc 4.1145e-20 0.025231 0.00020487 6.1179e-05 v CourantNb 7.031e-08 0.011403 0.00017018 4.9686e-06 v FourierNb 1.2438e-07 0.039383 0.00015019 5.5082e-07 v total_pressure -1.9872e+05 3.2839e+05 69228 54617 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0965 0.11324 0.0030324 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.1461e-07 0.0449 0.00032036 5.5195e-06 INSTANT 0.876429000E-01 TIME STEP NUMBER 56627 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283238611E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.848904245E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.56315E-02 0.21326E+01 Friction velocity uk : 0.56315E-02 0.21326E+01 Dimensionless distance yplus : 0.54179E-02 0.20970E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 4.346304405e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29498E+08 1 0.18845E-09 0.32142E+02 0.21449E+04 c Velocity[X] 0.18151E+02 c Velocity[Y] 0.13990E+02 c Velocity[Z] 0.12210E-05 c Pressure 0.22149E-03 50 0.80118E-04 0.16512E-02 0.15031E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -29.864 44.169 5.6124 8.0051 v Velocity[Y] -31.702 33.821 -0.16386 -0.057883 v Velocity[Z] -3.0671 3.1363 2.2791e-06 -5.391e-08 v ǁVelocityǁ 0.0012629 44.395 8.6379 8.1912 v Pressure -3.0186e+05 2.2538e+05 -33998 -47877 v TurbVisc 4.2452e-20 0.025247 0.00020494 6.1263e-05 v CourantNb 6.8067e-08 0.011404 0.00017018 4.9687e-06 v FourierNb 1.2438e-07 0.039362 0.0001502 5.5139e-07 v total_pressure -2.0054e+05 3.267e+05 67327 53448 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.097 0.11328 0.0030329 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.1504e-07 0.04488 0.00032038 5.5201e-06 INSTANT 0.876430000E-01 TIME STEP NUMBER 56628 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283241520E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.849179518E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.97868E-02 0.21331E+01 Friction velocity uk : 0.97868E-02 0.21331E+01 Dimensionless distance yplus : 0.94549E-02 0.20974E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 3.968335868e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29498E+08 1 0.18850E-09 0.32169E+02 0.21457E+04 c Velocity[X] 0.18167E+02 c Velocity[Y] 0.14002E+02 c Velocity[Z] 0.12180E-05 c Pressure 0.22375E-03 423 0.93419E-04 0.16672E-02 0.14393E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -29.88 44.183 5.6124 8.0051 v Velocity[Y] -31.714 33.836 -0.16394 -0.058087 v Velocity[Z] -3.0675 3.1364 2.2785e-06 -5.391e-08 v ǁVelocityǁ 0.001111 44.409 8.6395 8.1915 v Pressure -3.0378e+05 2.2368e+05 -35888 -48982 v TurbVisc 4.2675e-20 0.025262 0.00020502 6.1347e-05 v CourantNb 6.8714e-08 0.011405 0.00017019 4.9688e-06 v FourierNb 1.2438e-07 0.039341 0.00015021 5.5196e-07 v total_pressure -2.0246e+05 3.25e+05 65437 52343 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0974 0.11332 0.0030337 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.1547e-07 0.04486 0.0003204 5.5208e-06 INSTANT 0.876431000E-01 TIME STEP NUMBER 56629 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283243980E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.849447227E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.32056E-02 0.21335E+01 Friction velocity uk : 0.32056E-02 0.21335E+01 Dimensionless distance yplus : 0.30969E-02 0.20979E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 3.597025011e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29499E+08 1 0.18853E-09 0.32183E+02 0.21460E+04 c Velocity[X] 0.18180E+02 c Velocity[Y] 0.14004E+02 c Velocity[Z] 0.12152E-05 c Pressure 0.22593E-03 92 0.79217E-04 0.16826E-02 0.14173E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -29.896 44.197 5.6125 8.0052 v Velocity[Y] -31.727 33.851 -0.16401 -0.058294 v Velocity[Z] -3.0679 3.1366 2.278e-06 -5.391e-08 v ǁVelocityǁ 0.0010034 44.423 8.6411 8.1918 v Pressure -3.0562e+05 2.22e+05 -37787 -50160 v TurbVisc 4.1731e-20 0.025278 0.0002051 6.1431e-05 v CourantNb 6.9387e-08 0.011406 0.00017019 4.9689e-06 v FourierNb 1.2439e-07 0.039321 0.00015022 5.5254e-07 v total_pressure -2.043e+05 3.2332e+05 63538 51165 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0979 0.11336 0.0030344 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.159e-07 0.044841 0.00032041 5.5214e-06 INSTANT 0.876432000E-01 TIME STEP NUMBER 56630 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283246477E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.849705319E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.31358E-02 0.21340E+01 Friction velocity uk : 0.31358E-02 0.21340E+01 Dimensionless distance yplus : 0.30295E-02 0.20983E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 3.197383893e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29499E+08 1 0.18858E-09 0.32216E+02 0.21470E+04 c Velocity[X] 0.18191E+02 c Velocity[Y] 0.14025E+02 c Velocity[Z] 0.12566E-05 c Pressure 0.22509E-03 13 0.58822E-04 0.16754E-02 0.12183E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -29.912 44.211 5.6125 8.0052 v Velocity[Y] -31.74 33.865 -0.16408 -0.058503 v Velocity[Z] -3.0683 3.1367 2.2775e-06 -5.391e-08 v ǁVelocityǁ 0.00095856 44.438 8.6427 8.192 v Pressure -3.0743e+05 2.2041e+05 -39699 -51211 v TurbVisc 4.1859e-20 0.025294 0.00020517 6.1515e-05 v CourantNb 7.1635e-08 0.011407 0.0001702 4.9689e-06 v FourierNb 1.2439e-07 0.0393 0.00015023 5.5311e-07 v total_pressure -2.0611e+05 3.2173e+05 61626 50114 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0983 0.1134 0.0030351 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.1633e-07 0.04482 0.00032043 5.522e-06 INSTANT 0.876433000E-01 TIME STEP NUMBER 56631 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283248783E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.849953026E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.75992E-02 0.21344E+01 Friction velocity uk : 0.75992E-02 0.21344E+01 Dimensionless distance yplus : 0.73416E-02 0.20987E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 2.725256935e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29499E+08 1 0.18862E-09 0.32244E+02 0.21478E+04 c Velocity[X] 0.18214E+02 c Velocity[Y] 0.14029E+02 c Velocity[Z] 0.12261E-05 c Pressure 0.22756E-03 151 0.75139E-04 0.16929E-02 0.15323E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -29.928 44.225 5.6125 8.0052 v Velocity[Y] -31.753 33.88 -0.16415 -0.058709 v Velocity[Z] -3.0687 3.1369 2.2769e-06 -5.391e-08 v ǁVelocityǁ 0.00095553 44.452 8.6443 8.1923 v Pressure -3.0944e+05 2.1863e+05 -41622 -52434 v TurbVisc 4.4178e-20 0.025309 0.00020525 6.1599e-05 v CourantNb 4.4968e-08 0.011409 0.00017021 4.969e-06 v FourierNb 1.2439e-07 0.039279 0.00015024 5.5369e-07 v total_pressure -2.0811e+05 3.1996e+05 59703 48891 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0987 0.11344 0.0030357 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.1676e-07 0.0448 0.00032045 5.5227e-06 INSTANT 0.876434000E-01 TIME STEP NUMBER 56632 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283250916E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.850190919E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.92673E-02 0.21348E+01 Friction velocity uk : 0.92673E-02 0.21348E+01 Dimensionless distance yplus : 0.89376E-02 0.20992E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 2.396225206e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29500E+08 1 0.18866E-09 0.32274E+02 0.21487E+04 c Velocity[X] 0.18227E+02 c Velocity[Y] 0.14047E+02 c Velocity[Z] 0.12131E-05 c Pressure 0.22905E-03 98 0.80408E-04 0.17031E-02 0.15197E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -29.944 44.239 5.6126 8.0053 v Velocity[Y] -31.765 33.895 -0.16422 -0.058918 v Velocity[Z] -3.069 3.137 2.2764e-06 -5.391e-08 v ǁVelocityǁ 0.0010012 44.466 8.6458 8.1925 v Pressure -3.1134e+05 2.1695e+05 -43606 -53663 v TurbVisc 4.1415e-20 0.025325 0.00020532 6.1683e-05 v CourantNb 7.3741e-08 0.01141 0.00017021 4.9691e-06 v FourierNb 1.2439e-07 0.039258 0.00015025 5.5426e-07 v total_pressure -2.1002e+05 3.1828e+05 57719 47662 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0992 0.11347 0.0030364 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.172e-07 0.04478 0.00032047 5.5233e-06 INSTANT 0.876435000E-01 TIME STEP NUMBER 56633 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283253046E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.850424597E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.76346E-02 0.21353E+01 Friction velocity uk : 0.76346E-02 0.21353E+01 Dimensionless distance yplus : 0.73630E-02 0.20996E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 2.014056626e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29500E+08 1 0.18870E-09 0.32302E+02 0.21495E+04 c Velocity[X] 0.18244E+02 c Velocity[Y] 0.14058E+02 c Velocity[Z] 0.12090E-05 c Pressure 0.23078E-03 299 0.93671E-04 0.17150E-02 0.14395E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -29.96 44.253 5.6126 8.0053 v Velocity[Y] -31.778 33.909 -0.1643 -0.059125 v Velocity[Z] -3.0694 3.1372 2.2759e-06 -5.391e-08 v ǁVelocityǁ 0.0011015 44.48 8.6474 8.1928 v Pressure -3.1334e+05 2.1518e+05 -45574 -54812 v TurbVisc 4.139e-20 0.025341 0.0002054 6.1767e-05 v CourantNb 7.5518e-08 0.011411 0.00017022 4.9691e-06 v FourierNb 1.2439e-07 0.039236 0.00015027 5.5484e-07 v total_pressure -2.1201e+05 3.1651e+05 55751 46513 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0996 0.11351 0.003037 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.1763e-07 0.044759 0.00032048 5.524e-06 INSTANT 0.876436000E-01 TIME STEP NUMBER 56634 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283254719E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.850650410E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.67296E-02 0.21356E+01 Friction velocity uk : 0.67296E-02 0.21356E+01 Dimensionless distance yplus : 0.64901E-02 0.20999E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.633385998e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29500E+08 1 0.18874E-09 0.32317E+02 0.21499E+04 c Velocity[X] 0.18257E+02 c Velocity[Y] 0.14059E+02 c Velocity[Z] 0.12074E-05 c Pressure 0.23243E-03 179 0.79600E-04 0.17263E-02 0.14197E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -29.976 44.267 5.6126 8.0053 v Velocity[Y] -31.791 33.924 -0.16437 -0.059335 v Velocity[Z] -3.0698 3.1373 2.2754e-06 -5.391e-08 v ǁVelocityǁ 0.0012426 44.494 8.649 8.193 v Pressure -3.1525e+05 2.135e+05 -47546 -56038 v TurbVisc 4.1237e-20 0.025356 0.00020548 6.1852e-05 v CourantNb 7.601e-08 0.011412 0.00017022 4.9692e-06 v FourierNb 1.2439e-07 0.039215 0.00015028 5.5541e-07 v total_pressure -2.1392e+05 3.1482e+05 53779 45287 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.0999 0.11354 0.0030376 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.1807e-07 0.044739 0.0003205 5.5246e-06 INSTANT 0.876437000E-01 TIME STEP NUMBER 56635 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283256424E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.850865294E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.57177E-02 0.21360E+01 Friction velocity uk : 0.57177E-02 0.21360E+01 Dimensionless distance yplus : 0.55143E-02 0.21003E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.234667969e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29501E+08 1 0.18878E-09 0.32350E+02 0.21509E+04 c Velocity[X] 0.18270E+02 c Velocity[Y] 0.14081E+02 c Velocity[Z] 0.12507E-05 c Pressure 0.23109E-03 13 0.59377E-04 0.17155E-02 0.12123E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -29.992 44.28 5.6126 8.0054 v Velocity[Y] -31.803 33.938 -0.16444 -0.059546 v Velocity[Z] -3.0702 3.1375 2.2748e-06 -5.3911e-08 v ǁVelocityǁ 0.0013939 44.508 8.6506 8.1932 v Pressure -3.1711e+05 2.1186e+05 -49524 -57126 v TurbVisc 4.0989e-20 0.025372 0.00020555 6.1936e-05 v CourantNb 7.4896e-08 0.011413 0.00017023 4.9693e-06 v FourierNb 1.2439e-07 0.039193 0.00015029 5.5599e-07 v total_pressure -2.1579e+05 3.1318e+05 51801 44199 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1003 0.11358 0.0030381 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.1851e-07 0.044718 0.00032052 5.5253e-06 INSTANT 0.876438000E-01 TIME STEP NUMBER 56636 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283257925E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.851068664E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.60220E-02 0.21364E+01 Friction velocity uk : 0.60220E-02 0.21364E+01 Dimensionless distance yplus : 0.58077E-02 0.21007E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 7.502601141e-03 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29501E+08 1 0.18882E-09 0.32379E+02 0.21517E+04 c Velocity[X] 0.18294E+02 c Velocity[Y] 0.14085E+02 c Velocity[Z] 0.12219E-05 c Pressure 0.23298E-03 162 0.75515E-04 0.17286E-02 0.15102E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -30.008 44.294 5.6126 8.0054 v Velocity[Y] -31.816 33.953 -0.16451 -0.059755 v Velocity[Z] -3.0706 3.1376 2.2743e-06 -5.3911e-08 v ǁVelocityǁ 0.0015971 44.522 8.6522 8.1935 v Pressure -3.1918e+05 2.1002e+05 -51507 -58378 v TurbVisc 4.2437e-20 0.025388 0.00020563 6.2021e-05 v CourantNb 4.8379e-08 0.011414 0.00017024 4.9693e-06 v FourierNb 1.2439e-07 0.039172 0.0001503 5.5657e-07 v total_pressure -2.1785e+05 3.1134e+05 49818 42947 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1007 0.11361 0.0030386 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.1894e-07 0.044697 0.00032054 5.5259e-06 INSTANT 0.876439000E-01 TIME STEP NUMBER 56637 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283259259E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.851260843E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.55681E-02 0.21367E+01 Friction velocity uk : 0.55681E-02 0.21367E+01 Dimensionless distance yplus : 0.53700E-02 0.21010E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 4.178928148e-03 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29501E+08 1 0.18886E-09 0.32410E+02 0.21527E+04 c Velocity[X] 0.18308E+02 c Velocity[Y] 0.14102E+02 c Velocity[Z] 0.12159E-05 c Pressure 0.23391E-03 53 0.80702E-04 0.17346E-02 0.15001E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -30.024 44.308 5.6126 8.0054 v Velocity[Y] -31.829 33.968 -0.16458 -0.059967 v Velocity[Z] -3.071 3.1378 2.2738e-06 -5.3911e-08 v ǁVelocityǁ 0.0017928 44.536 8.6538 8.1937 v Pressure -3.2113e+05 2.0829e+05 -53547 -59643 v TurbVisc 4.179e-20 0.025403 0.0002057 6.2105e-05 v CourantNb 7.0662e-08 0.011415 0.00017024 4.9694e-06 v FourierNb 1.2439e-07 0.03915 0.00015031 5.5715e-07 v total_pressure -2.198e+05 3.0961e+05 47778 41682 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.101 0.11364 0.0030391 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.1938e-07 0.044676 0.00032056 5.5265e-06 INSTANT 0.876440000E-01 TIME STEP NUMBER 56638 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283260581E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.851448159E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.29463E-02 0.21371E+01 Friction velocity uk : 0.29463E-02 0.21371E+01 Dimensionless distance yplus : 0.28415E-02 0.21013E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 4.144627868e-04 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29501E+08 1 0.18890E-09 0.32439E+02 0.21535E+04 c Velocity[X] 0.18326E+02 c Velocity[Y] 0.14113E+02 c Velocity[Z] 0.12011E-05 c Pressure 0.23508E-03 215 0.94135E-04 0.17423E-02 0.13972E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -30.039 44.322 5.6126 8.0054 v Velocity[Y] -31.841 33.982 -0.16465 -0.060176 v Velocity[Z] -3.0713 3.1379 2.2733e-06 -5.3911e-08 v ǁVelocityǁ 0.001998 44.55 8.6554 8.1939 v Pressure -3.2316e+05 2.0648e+05 -55560 -60799 v TurbVisc 4.1431e-20 0.025419 0.00020578 6.219e-05 v CourantNb 6.805e-08 0.011416 0.00017025 4.9694e-06 v FourierNb 1.244e-07 0.039128 0.00015033 5.5772e-07 v total_pressure -2.2184e+05 3.078e+05 45765 40526 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1013 0.11367 0.0030396 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.1983e-07 0.044655 0.00032057 5.5272e-06 INSTANT 0.876441000E-01 TIME STEP NUMBER 56639 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283261441E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.851626970E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.65619E-02 0.21374E+01 Friction velocity uk : 0.65619E-02 0.21374E+01 Dimensionless distance yplus : 0.63284E-02 0.21017E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -3.274164652e-03 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29502E+08 1 0.18894E-09 0.32456E+02 0.21539E+04 c Velocity[X] 0.18341E+02 c Velocity[Y] 0.14114E+02 c Velocity[Z] 0.11987E-05 c Pressure 0.23616E-03 88 0.79985E-04 0.17494E-02 0.14357E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -30.055 44.335 5.6126 8.0054 v Velocity[Y] -31.854 33.997 -0.16472 -0.060388 v Velocity[Z] -3.0717 3.1381 2.2727e-06 -5.3911e-08 v ǁVelocityǁ 0.0022073 44.564 8.6569 8.1942 v Pressure -3.2514e+05 2.0473e+05 -57591 -62093 v TurbVisc 4.1991e-20 0.025434 0.00020585 6.2275e-05 v CourantNb 6.5865e-08 0.011416 0.00017025 4.9695e-06 v FourierNb 1.244e-07 0.039106 0.00015034 5.583e-07 v total_pressure -2.2381e+05 3.0605e+05 43734 39232 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1017 0.1137 0.0030401 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.2027e-07 0.044633 0.00032059 5.5278e-06 INSTANT 0.876442000E-01 TIME STEP NUMBER 56640 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283262325E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.851794076E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.88739E-02 0.21377E+01 Friction velocity uk : 0.88739E-02 0.21377E+01 Dimensionless distance yplus : 0.85581E-02 0.21020E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -7.093439562e-03 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29502E+08 1 0.18898E-09 0.32490E+02 0.21550E+04 c Velocity[X] 0.18355E+02 c Velocity[Y] 0.14136E+02 c Velocity[Z] 0.12430E-05 c Pressure 0.23428E-03 13 0.59735E-04 0.17345E-02 0.11692E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -30.071 44.349 5.6126 8.0054 v Velocity[Y] -31.866 34.011 -0.16479 -0.060602 v Velocity[Z] -3.0721 3.1382 2.2722e-06 -5.3911e-08 v ǁVelocityǁ 0.0023971 44.578 8.6585 8.1944 v Pressure -3.2703e+05 2.0305e+05 -59603 -63184 v TurbVisc 4.1698e-20 0.02545 0.00020593 6.236e-05 v CourantNb 6.3602e-08 0.011417 0.00017026 4.9696e-06 v FourierNb 1.244e-07 0.039084 0.00015035 5.5888e-07 v total_pressure -2.2571e+05 3.0437e+05 41722 38141 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.102 0.11373 0.0030405 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.2071e-07 0.044612 0.00032061 5.5284e-06 INSTANT 0.876443000E-01 TIME STEP NUMBER 56641 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283263011E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.851950000E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.91460E-02 0.21380E+01 Friction velocity uk : 0.91460E-02 0.21380E+01 Dimensionless distance yplus : 0.88206E-02 0.21022E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.156842360e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29502E+08 1 0.18902E-09 0.32520E+02 0.21559E+04 c Velocity[X] 0.18381E+02 c Velocity[Y] 0.14140E+02 c Velocity[Z] 0.12104E-05 c Pressure 0.23562E-03 162 0.75839E-04 0.17435E-02 0.14732E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -30.086 44.363 5.6126 8.0054 v Velocity[Y] -31.878 34.025 -0.16486 -0.060813 v Velocity[Z] -3.0725 3.1384 2.2717e-06 -5.3911e-08 v ǁVelocityǁ 0.0026349 44.592 8.6601 8.1946 v Pressure -3.2913e+05 2.012e+05 -61619 -64457 v TurbVisc 4.2069e-20 0.025466 0.000206 6.2444e-05 v CourantNb 5.1475e-08 0.011418 0.00017026 4.9696e-06 v FourierNb 1.244e-07 0.039062 0.00015036 5.5946e-07 v total_pressure -2.2781e+05 3.0252e+05 39706 36868 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1022 0.11375 0.0030409 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.2116e-07 0.04459 0.00032063 5.5291e-06 INSTANT 0.876444000E-01 TIME STEP NUMBER 56642 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283263518E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.852094295E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.80292E-02 0.21383E+01 Friction velocity uk : 0.80292E-02 0.21383E+01 Dimensionless distance yplus : 0.77435E-02 0.21025E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.472610240e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29502E+08 1 0.18906E-09 0.32553E+02 0.21568E+04 c Velocity[X] 0.18396E+02 c Velocity[Y] 0.14157E+02 c Velocity[Z] 0.11959E-05 c Pressure 0.23599E-03 69 0.81167E-04 0.17453E-02 0.14592E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -30.102 44.376 5.6126 8.0054 v Velocity[Y] -31.891 34.04 -0.16493 -0.061028 v Velocity[Z] -3.0729 3.1385 2.2712e-06 -5.3911e-08 v ǁVelocityǁ 0.0028491 44.606 8.6617 8.1948 v Pressure -3.3111e+05 1.9947e+05 -63690 -65739 v TurbVisc 4.3622e-20 0.025481 0.00020608 6.253e-05 v CourantNb 5.9405e-08 0.011419 0.00017027 4.9697e-06 v FourierNb 1.244e-07 0.03904 0.00015038 5.6004e-07 v total_pressure -2.2979e+05 3.0079e+05 37635 35586 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1025 0.11378 0.0030413 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.216e-07 0.044568 0.00032065 5.5297e-06 INSTANT 0.876445000E-01 TIME STEP NUMBER 56643 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283264017E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.852233019E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.87738E-02 0.21386E+01 Friction velocity uk : 0.87738E-02 0.21386E+01 Dimensionless distance yplus : 0.84616E-02 0.21028E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.805939142e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29502E+08 1 0.18910E-09 0.32583E+02 0.21577E+04 c Velocity[X] 0.18415E+02 c Velocity[Y] 0.14168E+02 c Velocity[Z] 0.11867E-05 c Pressure 0.23661E-03 236 0.94674E-04 0.17489E-02 0.13563E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -30.117 44.39 5.6126 8.0054 v Velocity[Y] -31.903 34.054 -0.165 -0.06124 v Velocity[Z] -3.0732 3.1387 2.2706e-06 -5.3911e-08 v ǁVelocityǁ 0.0030654 44.619 8.6632 8.195 v Pressure -3.3318e+05 1.9766e+05 -65727 -66908 v TurbVisc 4.3002e-20 0.025497 0.00020615 6.2614e-05 v CourantNb 5.679e-08 0.01142 0.00017027 4.9697e-06 v FourierNb 1.244e-07 0.039017 0.00015039 5.6062e-07 v total_pressure -2.3186e+05 2.9898e+05 35598 34417 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1028 0.1138 0.0030416 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.2205e-07 0.044546 0.00032066 5.5303e-06 INSTANT 0.876446000E-01 TIME STEP NUMBER 56644 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283264048E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.852362875E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.51530E-02 0.21388E+01 Friction velocity uk : 0.51530E-02 0.21388E+01 Dimensionless distance yplus : 0.50947E-02 0.21031E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -2.123271328e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29503E+08 1 0.18913E-09 0.32600E+02 0.21582E+04 c Velocity[X] 0.18432E+02 c Velocity[Y] 0.14169E+02 c Velocity[Z] 0.11848E-05 c Pressure 0.23714E-03 101 0.80487E-04 0.17519E-02 0.13935E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -30.133 44.403 5.6126 8.0054 v Velocity[Y] -31.915 34.068 -0.16507 -0.061454 v Velocity[Z] -3.0736 3.1388 2.2701e-06 -5.3911e-08 v ǁVelocityǁ 0.0032818 44.633 8.6648 8.1952 v Pressure -3.3518e+05 1.9592e+05 -67775 -68216 v TurbVisc 4.3821e-20 0.025512 0.00020623 6.27e-05 v CourantNb 5.4609e-08 0.011421 0.00017028 4.9698e-06 v FourierNb 1.244e-07 0.038995 0.0001504 5.612e-07 v total_pressure -2.3385e+05 2.9725e+05 33550 33109 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1031 0.11382 0.003042 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.225e-07 0.044524 0.00032068 5.531e-06 INSTANT 0.876447000E-01 TIME STEP NUMBER 56645 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283264102E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.852480546E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.79026E-02 0.21391E+01 Friction velocity uk : 0.79026E-02 0.21391E+01 Dimensionless distance yplus : 0.78130E-02 0.21033E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -2.462657902e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29503E+08 1 0.18917E-09 0.32637E+02 0.21593E+04 c Velocity[X] 0.18447E+02 c Velocity[Y] 0.14190E+02 c Velocity[Z] 0.12277E-05 c Pressure 0.23466E-03 13 0.60060E-04 0.17327E-02 0.11302E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -30.148 44.417 5.6125 8.0054 v Velocity[Y] -31.928 34.083 -0.16514 -0.06167 v Velocity[Z] -3.074 3.139 2.2696e-06 -5.3911e-08 v ǁVelocityǁ 0.0034745 44.647 8.6664 8.1954 v Pressure -3.3709e+05 1.9426e+05 -69802 -69315 v TurbVisc 4.4121e-20 0.025528 0.0002063 6.2785e-05 v CourantNb 5.2362e-08 0.011422 0.00017029 4.9698e-06 v FourierNb 1.244e-07 0.038972 0.00015041 5.6179e-07 v total_pressure -2.3576e+05 2.9559e+05 31523 32010 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1033 0.11385 0.0030423 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.2295e-07 0.044502 0.0003207 5.5316e-06 INSTANT 0.876448000E-01 TIME STEP NUMBER 56646 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283263955E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.852586336E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.99054E-02 0.21393E+01 Friction velocity uk : 0.99054E-02 0.21393E+01 Dimensionless distance yplus : 0.95696E-02 0.21035E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -2.847126291e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29503E+08 1 0.18921E-09 0.32668E+02 0.21602E+04 c Velocity[X] 0.18474E+02 c Velocity[Y] 0.14194E+02 c Velocity[Z] 0.11956E-05 c Pressure 0.23546E-03 279 0.76577E-04 0.17377E-02 0.14176E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -30.164 44.43 5.6125 8.0054 v Velocity[Y] -31.94 34.097 -0.16521 -0.061884 v Velocity[Z] -3.0744 3.1391 2.2691e-06 -5.3911e-08 v ǁVelocityǁ 0.0036451 44.66 8.6679 8.1956 v Pressure -3.3921e+05 1.9241e+05 -71825 -70590 v TurbVisc 4.2596e-20 0.025544 0.00020638 6.287e-05 v CourantNb 4.2809e-08 0.011423 0.00017029 4.9699e-06 v FourierNb 1.2441e-07 0.03895 0.00015043 5.6237e-07 v total_pressure -2.3788e+05 2.9373e+05 29500 30735 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1035 0.11387 0.0030426 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.234e-07 0.04448 0.00032072 5.5322e-06 INSTANT 0.876449000E-01 TIME STEP NUMBER 56647 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283263634E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.852680180E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.53715E-02 0.21395E+01 Friction velocity uk : 0.53715E-02 0.21395E+01 Dimensionless distance yplus : 0.51894E-02 0.21038E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -3.127662294e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29503E+08 1 0.18925E-09 0.32702E+02 0.21612E+04 c Velocity[X] 0.18490E+02 c Velocity[Y] 0.14212E+02 c Velocity[Z] 0.11779E-05 c Pressure 0.23528E-03 110 0.81893E-04 0.17354E-02 0.14529E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -30.179 44.444 5.6125 8.0054 v Velocity[Y] -31.952 34.111 -0.16528 -0.062102 v Velocity[Z] -3.0748 3.1392 2.2685e-06 -5.3911e-08 v ǁVelocityǁ 0.0035596 44.674 8.6695 8.1958 v Pressure -3.4122e+05 1.9064e+05 -73911 -71929 v TurbVisc 5.0316e-20 0.025559 0.00020645 6.2956e-05 v CourantNb 4.8169e-08 0.011423 0.0001703 4.9699e-06 v FourierNb 1.2441e-07 0.038927 0.00015044 5.6295e-07 v total_pressure -2.399e+05 2.9197e+05 27414 29396 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1038 0.1139 0.0030428 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.2385e-07 0.044458 0.00032073 5.5328e-06 INSTANT 0.876450000E-01 TIME STEP NUMBER 56648 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283263271E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.852768335E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.34507E-02 0.21398E+01 Friction velocity uk : 0.34507E-02 0.21398E+01 Dimensionless distance yplus : 0.33337E-02 0.21040E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -3.372878949e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29503E+08 1 0.18928E-09 0.32734E+02 0.21622E+04 c Velocity[X] 0.18512E+02 c Velocity[Y] 0.14222E+02 c Velocity[Z] 0.11684E-05 c Pressure 0.23539E-03 212 0.95598E-04 0.17353E-02 0.12346E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -30.194 44.457 5.6124 8.0054 v Velocity[Y] -31.964 34.125 -0.16535 -0.062316 v Velocity[Z] -3.0752 3.1394 2.268e-06 -5.3911e-08 v ǁVelocityǁ 0.0034811 44.688 8.6711 8.196 v Pressure -3.4324e+05 1.8888e+05 -75919 -72994 v TurbVisc 4.1488e-20 0.025575 0.00020652 6.3041e-05 v CourantNb 4.5492e-08 0.011424 0.0001703 4.9699e-06 v FourierNb 1.2441e-07 0.038904 0.00015045 5.6353e-07 v total_pressure -2.4192e+05 2.9021e+05 25406 28331 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.104 0.11392 0.0030431 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.243e-07 0.044435 0.00032075 5.5335e-06 INSTANT 0.876451000E-01 TIME STEP NUMBER 56649 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283262506E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.852848130E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19254E-02 0.21400E+01 Friction velocity uk : 0.19254E-02 0.21400E+01 Dimensionless distance yplus : 0.18601E-02 0.21042E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -3.651705630e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29503E+08 1 0.18932E-09 0.32752E+02 0.21627E+04 c Velocity[X] 0.18529E+02 c Velocity[Y] 0.14222E+02 c Velocity[Z] 0.11674E-05 c Pressure 0.23534E-03 133 0.81357E-04 0.17340E-02 0.13715E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -30.209 44.47 5.6124 8.0054 v Velocity[Y] -31.976 34.139 -0.16542 -0.062533 v Velocity[Z] -3.0755 3.1395 2.2675e-06 -5.3911e-08 v ǁVelocityǁ 0.0034109 44.701 8.6726 8.1962 v Pressure -3.4526e+05 1.8712e+05 -77971 -74341 v TurbVisc 4.2821e-20 0.02559 0.0002066 6.3127e-05 v CourantNb 4.3323e-08 0.011425 0.00017031 4.97e-06 v FourierNb 1.2441e-07 0.038881 0.00015046 5.6412e-07 v total_pressure -2.4393e+05 2.8844e+05 23354 26984 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1042 0.11394 0.0030433 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.2476e-07 0.044413 0.00032077 5.5341e-06 INSTANT 0.876452000E-01 TIME STEP NUMBER 56650 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283261729E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.852913862E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.64189E-02 0.21402E+01 Friction velocity uk : 0.64189E-02 0.21402E+01 Dimensionless distance yplus : 0.61921E-02 0.21044E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -3.906084643e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29503E+08 1 0.18935E-09 0.32790E+02 0.21638E+04 c Velocity[X] 0.18545E+02 c Velocity[Y] 0.14244E+02 c Velocity[Z] 0.12011E-05 c Pressure 0.23225E-03 15 0.60544E-04 0.17103E-02 0.10840E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -30.224 44.483 5.6124 8.0053 v Velocity[Y] -31.988 34.153 -0.16549 -0.062752 v Velocity[Z] -3.0759 3.1397 2.267e-06 -5.3911e-08 v ǁVelocityǁ 0.0033519 44.715 8.6742 8.1964 v Pressure -3.4717e+05 1.8546e+05 -79986 -75440 v TurbVisc 4.8434e-20 0.025606 0.00020667 6.3212e-05 v CourantNb 4.1059e-08 0.011426 0.00017031 4.97e-06 v FourierNb 1.2441e-07 0.038858 0.00015047 5.647e-07 v total_pressure -2.4585e+05 2.8679e+05 21339 25885 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1044 0.11397 0.0030436 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.2521e-07 0.04439 0.00032078 5.5347e-06 INSTANT 0.876453000E-01 TIME STEP NUMBER 56651 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283260753E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.852968324E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.82881E-02 0.21404E+01 Friction velocity uk : 0.82881E-02 0.21404E+01 Dimensionless distance yplus : 0.79952E-02 0.21046E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -4.199794902e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29503E+08 1 0.18939E-09 0.32822E+02 0.21648E+04 c Velocity[X] 0.18575E+02 c Velocity[Y] 0.14248E+02 c Velocity[Z] 0.11901E-05 c Pressure 0.23253E-03 321 0.77413E-04 0.17114E-02 0.13484E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -30.24 44.497 5.6123 8.0053 v Velocity[Y] -32 34.167 -0.16556 -0.062968 v Velocity[Z] -3.0763 3.1398 2.2665e-06 -5.3912e-08 v ǁVelocityǁ 0.0032962 44.728 8.6757 8.1966 v Pressure -3.4928e+05 1.8362e+05 -81987 -76700 v TurbVisc 5.1245e-20 0.025621 0.00020674 6.3298e-05 v CourantNb 3.9611e-08 0.011427 0.00017032 4.9701e-06 v FourierNb 1.2441e-07 0.038835 0.00015048 5.6529e-07 v total_pressure -2.4795e+05 2.8494e+05 19338 24625 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1046 0.11399 0.0030438 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.2567e-07 0.044367 0.0003208 5.5353e-06 INSTANT 0.876454000E-01 TIME STEP NUMBER 56652 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283259604E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.853010293E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.42522E-02 0.21406E+01 Friction velocity uk : 0.42522E-02 0.21406E+01 Dimensionless distance yplus : 0.41019E-02 0.21048E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -4.432792370e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29504E+08 1 0.18943E-09 0.32858E+02 0.21658E+04 c Velocity[X] 0.18593E+02 c Velocity[Y] 0.14264E+02 c Velocity[Z] 0.11619E-05 c Pressure 0.23183E-03 69 0.82659E-04 0.17054E-02 0.13428E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -30.255 44.51 5.6123 8.0053 v Velocity[Y] -32.012 34.181 -0.16563 -0.063188 v Velocity[Z] -3.0767 3.14 2.2659e-06 -5.3912e-08 v ǁVelocityǁ 0.0032548 44.741 8.6773 8.1968 v Pressure -3.5125e+05 1.819e+05 -84035 -77976 v TurbVisc 1.5472e-20 0.025637 0.00020682 6.3384e-05 v CourantNb 3.6814e-08 0.011428 0.00017032 4.9701e-06 v FourierNb 1.2441e-07 0.038812 0.0001505 5.6587e-07 v total_pressure -2.4993e+05 2.8322e+05 17290 23349 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1048 0.11401 0.0030441 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.2613e-07 0.044344 0.00032082 5.536e-06 INSTANT 0.876455000E-01 TIME STEP NUMBER 56653 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283258449E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.853047002E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.25615E-02 0.21408E+01 Friction velocity uk : 0.25615E-02 0.21408E+01 Dimensionless distance yplus : 0.24710E-02 0.21050E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -4.593215674e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29504E+08 1 0.18946E-09 0.32891E+02 0.21668E+04 c Velocity[X] 0.18614E+02 c Velocity[Y] 0.14276E+02 c Velocity[Z] 0.11558E-05 c Pressure 0.23137E-03 270 0.96465E-04 0.17012E-02 0.12568E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -30.27 44.523 5.6123 8.0052 v Velocity[Y] -32.024 34.195 -0.1657 -0.063405 v Velocity[Z] -3.0771 3.1401 2.2654e-06 -5.3912e-08 v ǁVelocityǁ 0.0032242 44.755 8.6788 8.197 v Pressure -3.5331e+05 1.8009e+05 -86043 -79147 v TurbVisc 4.9289e-20 0.025652 0.00020689 6.3469e-05 v CourantNb 3.415e-08 0.011428 0.00017033 4.9701e-06 v FourierNb 1.2441e-07 0.038789 0.00015051 5.6646e-07 v total_pressure -2.5199e+05 2.8141e+05 15282 22178 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.105 0.11403 0.0030444 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.2659e-07 0.044321 0.00032084 5.5366e-06 INSTANT 0.876456000E-01 TIME STEP NUMBER 56654 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283256819E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.853074325E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.65432E-02 0.21410E+01 Friction velocity uk : 0.65432E-02 0.21410E+01 Dimensionless distance yplus : 0.62932E-02 0.21052E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -4.770600782e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29504E+08 1 0.18949E-09 0.32910E+02 0.21673E+04 c Velocity[X] 0.18635E+02 c Velocity[Y] 0.14275E+02 c Velocity[Z] 0.11491E-05 c Pressure 0.23086E-03 353 0.82093E-04 0.16965E-02 0.12009E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -30.285 44.536 5.6122 8.0052 v Velocity[Y] -32.036 34.209 -0.16577 -0.063624 v Velocity[Z] -3.0774 3.1403 2.2649e-06 -5.3912e-08 v ǁVelocityǁ 0.0032046 44.768 8.6804 8.1972 v Pressure -3.5525e+05 1.7841e+05 -88035 -80363 v TurbVisc 5.0796e-20 0.025668 0.00020696 6.3555e-05 v CourantNb 3.1817e-08 0.011429 0.00017033 4.9702e-06 v FourierNb 1.2441e-07 0.038765 0.00015052 5.6705e-07 v total_pressure -2.5393e+05 2.7973e+05 13290 20962 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1052 0.11405 0.0030446 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.2705e-07 0.044298 0.00032085 5.5372e-06 INSTANT 0.876457000E-01 TIME STEP NUMBER 56655 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283255247E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.853089450E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.67674E-02 0.21412E+01 Friction velocity uk : 0.67674E-02 0.21412E+01 Dimensionless distance yplus : 0.65088E-02 0.21054E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -4.937814803e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29504E+08 1 0.18953E-09 0.32949E+02 0.21685E+04 c Velocity[X] 0.18650E+02 c Velocity[Y] 0.14299E+02 c Velocity[Z] 0.11530E-05 c Pressure 0.22708E-03 10 0.61211E-04 0.16678E-02 0.10845E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -30.299 44.549 5.6122 8.0052 v Velocity[Y] -32.048 34.223 -0.16584 -0.063846 v Velocity[Z] -3.0778 3.1404 2.2644e-06 -5.3912e-08 v ǁVelocityǁ 0.0031964 44.781 8.6819 8.1973 v Pressure -3.5717e+05 1.7674e+05 -90025 -81507 v TurbVisc 5.1658e-20 0.025683 0.00020704 6.3641e-05 v CourantNb 2.9562e-08 0.01143 0.00017034 4.9702e-06 v FourierNb 1.2442e-07 0.038742 0.00015054 5.6763e-07 v total_pressure -2.5584e+05 2.7807e+05 11300 19818 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1054 0.11407 0.0030449 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.2751e-07 0.044275 0.00032087 5.5378e-06 INSTANT 0.876458000E-01 TIME STEP NUMBER 56656 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283253436E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.853092607E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.64257E-02 0.21414E+01 Friction velocity uk : 0.64257E-02 0.21414E+01 Dimensionless distance yplus : 0.61802E-02 0.21056E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -5.108050003e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29504E+08 1 0.18956E-09 0.32983E+02 0.21695E+04 c Velocity[X] 0.18682E+02 c Velocity[Y] 0.14301E+02 c Velocity[Z] 0.11458E-05 c Pressure 0.22688E-03 161 0.78270E-04 0.16655E-02 0.12498E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -30.314 44.562 5.6121 8.0051 v Velocity[Y] -32.06 34.237 -0.16591 -0.064065 v Velocity[Z] -3.0782 3.1406 2.2639e-06 -5.3912e-08 v ǁVelocityǁ 0.0029925 44.794 8.6835 8.1975 v Pressure -3.5923e+05 1.7494e+05 -91970 -82704 v TurbVisc 5.4886e-20 0.025699 0.00020711 6.3727e-05 v CourantNb 2.8147e-08 0.011431 0.00017034 4.9702e-06 v FourierNb 1.2442e-07 0.038719 0.00015055 5.6822e-07 v total_pressure -2.5791e+05 2.7626e+05 9354.7 18621 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1056 0.1141 0.0030452 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.2797e-07 0.044253 0.00032089 5.5384e-06 INSTANT 0.876459000E-01 TIME STEP NUMBER 56657 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283251483E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.853082924E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.86581E-02 0.21415E+01 Friction velocity uk : 0.86581E-02 0.21415E+01 Dimensionless distance yplus : 0.83274E-02 0.21057E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -5.333305851e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29504E+08 1 0.18960E-09 0.33019E+02 0.21706E+04 c Velocity[X] 0.18701E+02 c Velocity[Y] 0.14318E+02 c Velocity[Z] 0.11401E-05 c Pressure 0.22569E-03 65 0.83811E-04 0.16558E-02 0.12727E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -30.329 44.574 5.6121 8.0051 v Velocity[Y] -32.072 34.251 -0.16598 -0.064287 v Velocity[Z] -3.0786 3.1407 2.2633e-06 -5.3912e-08 v ǁVelocityǁ 0.002643 44.807 8.685 8.1977 v Pressure -3.6116e+05 1.7326e+05 -93971 -83959 v TurbVisc 5.355e-20 0.025714 0.00020718 6.3813e-05 v CourantNb 2.5274e-08 0.011431 0.00017035 4.9703e-06 v FourierNb 1.2442e-07 0.038695 0.00015056 5.6881e-07 v total_pressure -2.5984e+05 2.7458e+05 7353.9 17366 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1057 0.11412 0.0030456 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.2844e-07 0.044229 0.00032091 5.5391e-06 INSTANT 0.876460000E-01 TIME STEP NUMBER 56658 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283249523E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.853068375E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12216E-01 0.21417E+01 Friction velocity uk : 0.12216E-01 0.21417E+01 Dimensionless distance yplus : 0.11813E-01 0.21059E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -5.367570998e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29504E+08 1 0.18963E-09 0.33053E+02 0.21717E+04 c Velocity[X] 0.18724E+02 c Velocity[Y] 0.14330E+02 c Velocity[Z] 0.11301E-05 c Pressure 0.22475E-03 219 0.97468E-04 0.16480E-02 0.11672E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -30.344 44.587 5.612 8.005 v Velocity[Y] -32.083 34.264 -0.16605 -0.064507 v Velocity[Z] -3.079 3.1409 2.2628e-06 -5.3912e-08 v ǁVelocityǁ 0.0022918 44.82 8.6865 8.1978 v Pressure -3.6317e+05 1.715e+05 -95918 -85075 v TurbVisc 5.3887e-20 0.02573 0.00020725 6.3899e-05 v CourantNb 2.2593e-08 0.011432 0.00017035 4.9703e-06 v FourierNb 1.2442e-07 0.038672 0.00015058 5.694e-07 v total_pressure -2.6185e+05 2.7283e+05 5407.3 16250 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1059 0.11414 0.003046 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.2891e-07 0.044206 0.00032093 5.5397e-06 INSTANT 0.876461000E-01 TIME STEP NUMBER 56659 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283247095E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.853044780E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.74673E-02 0.21419E+01 Friction velocity uk : 0.74673E-02 0.21419E+01 Dimensionless distance yplus : 0.72207E-02 0.21061E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -5.447086428e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29504E+08 1 0.18966E-09 0.33073E+02 0.21722E+04 c Velocity[X] 0.18744E+02 c Velocity[Y] 0.14329E+02 c Velocity[Z] 0.11266E-05 c Pressure 0.22374E-03 100 0.82740E-04 0.16398E-02 0.11830E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -30.358 44.6 5.612 8.005 v Velocity[Y] -32.095 34.278 -0.16612 -0.064729 v Velocity[Z] -3.0793 3.141 2.2623e-06 -5.3912e-08 v ǁVelocityǁ 0.0019422 44.833 8.6881 8.198 v Pressure -3.6509e+05 1.6983e+05 -97861 -86324 v TurbVisc 5.7634e-20 0.025745 0.00020733 6.3986e-05 v CourantNb 2.0328e-08 0.011433 0.00017036 4.9703e-06 v FourierNb 1.2442e-07 0.038648 0.00015059 5.6999e-07 v total_pressure -2.6377e+05 2.7116e+05 3463.9 15001 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1061 0.11416 0.0030463 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.2937e-07 0.044183 0.00032095 5.5403e-06 INSTANT 0.876462000E-01 TIME STEP NUMBER 56660 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283244709E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.853008992E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.44025E-02 0.21421E+01 Friction velocity uk : 0.44025E-02 0.21421E+01 Dimensionless distance yplus : 0.42571E-02 0.21063E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -5.552978328e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29504E+08 1 0.18969E-09 0.33114E+02 0.21735E+04 c Velocity[X] 0.18763E+02 c Velocity[Y] 0.14351E+02 c Velocity[Z] 0.11512E-05 c Pressure 0.21931E-03 9 0.61146E-04 0.16064E-02 0.94438E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -30.373 44.613 5.6119 8.0049 v Velocity[Y] -32.107 34.292 -0.16619 -0.064953 v Velocity[Z] -3.0797 3.1412 2.2618e-06 -5.3912e-08 v ǁVelocityǁ 0.0016123 44.846 8.6896 8.1982 v Pressure -3.6692e+05 1.6826e+05 -99766 -87357 v TurbVisc 5.645e-20 0.025761 0.0002074 6.4072e-05 v CourantNb 1.7974e-08 0.011434 0.00017036 4.9703e-06 v FourierNb 1.2442e-07 0.038625 0.00015061 5.7058e-07 v total_pressure -2.6559e+05 2.6959e+05 1559.3 13968 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1063 0.11418 0.0030466 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.2984e-07 0.04416 0.00032097 5.5409e-06 INSTANT 0.876463000E-01 TIME STEP NUMBER 56661 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283242141E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.852961480E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.29423E-02 0.21423E+01 Friction velocity uk : 0.29423E-02 0.21423E+01 Dimensionless distance yplus : 0.28451E-02 0.21064E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -5.644237349e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29503E+08 1 0.18972E-09 0.33148E+02 0.21745E+04 c Velocity[X] 0.18795E+02 c Velocity[Y] 0.14353E+02 c Velocity[Z] 0.11362E-05 c Pressure 0.21866E-03 590 0.78806E-04 0.16009E-02 0.11965E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -30.387 44.625 5.6118 8.0048 v Velocity[Y] -32.118 34.305 -0.16626 -0.065174 v Velocity[Z] -3.0801 3.1413 2.2613e-06 -5.3912e-08 v ǁVelocityǁ 0.001256 44.859 8.6912 8.1983 v Pressure -3.6892e+05 1.6652e+05 -1.0165e+05 -88549 v TurbVisc 5.5605e-20 0.025776 0.00020747 6.4158e-05 v CourantNb 1.6735e-08 0.011434 0.00017037 4.9704e-06 v FourierNb 1.2442e-07 0.038601 0.00015063 5.7116e-07 v total_pressure -2.676e+05 2.6784e+05 -328.44 12776 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1064 0.1142 0.0030469 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.3031e-07 0.044136 0.00032099 5.5415e-06 INSTANT 0.876464000E-01 TIME STEP NUMBER 56662 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283239396E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.852902451E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10598E-01 0.21425E+01 Friction velocity uk : 0.10598E-01 0.21425E+01 Dimensionless distance yplus : 0.10248E-01 0.21066E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -5.731255612e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29503E+08 1 0.18976E-09 0.33186E+02 0.21756E+04 c Velocity[X] 0.18814E+02 c Velocity[Y] 0.14372E+02 c Velocity[Z] 0.11224E-05 c Pressure 0.21694E-03 50 0.84213E-04 0.15875E-02 0.11929E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -30.402 44.638 5.6118 8.0048 v Velocity[Y] -32.13 34.319 -0.16633 -0.065399 v Velocity[Z] -3.0805 3.1415 2.2608e-06 -5.3912e-08 v ǁVelocityǁ 0.0009274 44.872 8.6927 8.1985 v Pressure -3.7081e+05 1.6488e+05 -1.0357e+05 -89756 v TurbVisc 6.0037e-20 0.025792 0.00020754 6.4245e-05 v CourantNb 1.5934e-08 0.011435 0.00017037 4.9704e-06 v FourierNb 1.2443e-07 0.038577 0.00015064 5.7176e-07 v total_pressure -2.6948e+05 2.6621e+05 -2244.3 11569 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1066 0.11422 0.0030473 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.3078e-07 0.044113 0.00032101 5.5421e-06 INSTANT 0.876465000E-01 TIME STEP NUMBER 56663 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283236651E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.852836774E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.14324E-01 0.21426E+01 Friction velocity uk : 0.14324E-01 0.21426E+01 Dimensionless distance yplus : 0.13851E-01 0.21068E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -5.734163159e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29503E+08 1 0.18979E-09 0.33221E+02 0.21767E+04 c Velocity[X] 0.18838E+02 c Velocity[Y] 0.14383E+02 c Velocity[Z] 0.11121E-05 c Pressure 0.21554E-03 211 0.98291E-04 0.15763E-02 0.10904E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -30.416 44.65 5.6117 8.0047 v Velocity[Y] -32.141 34.332 -0.16641 -0.065622 v Velocity[Z] -3.0809 3.1416 2.2602e-06 -5.3912e-08 v ǁVelocityǁ 0.00063028 44.884 8.6942 8.1986 v Pressure -3.7274e+05 1.6321e+05 -1.0544e+05 -90820 v TurbVisc 5.9177e-20 0.025807 0.00020761 6.4331e-05 v CourantNb 1.5887e-08 0.011436 0.00017038 4.9704e-06 v FourierNb 1.2443e-07 0.038554 0.00015066 5.7235e-07 v total_pressure -2.7141e+05 2.6453e+05 -4110.5 10505 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1068 0.11425 0.0030477 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.3125e-07 0.04409 0.00032103 5.5428e-06 INSTANT 0.876466000E-01 TIME STEP NUMBER 56664 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283233455E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.852762311E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10054E-01 0.21428E+01 Friction velocity uk : 0.10054E-01 0.21428E+01 Dimensionless distance yplus : 0.97334E-02 0.21070E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -5.738627893e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29503E+08 1 0.18981E-09 0.33242E+02 0.21773E+04 c Velocity[X] 0.18860E+02 c Velocity[Y] 0.14381E+02 c Velocity[Z] 0.11051E-05 c Pressure 0.21408E-03 191 0.83374E-04 0.15649E-02 0.10952E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -30.431 44.662 5.6117 8.0046 v Velocity[Y] -32.152 34.346 -0.16648 -0.065846 v Velocity[Z] -3.0812 3.1418 2.2597e-06 -5.3912e-08 v ǁVelocityǁ 0.00044118 44.897 8.6958 8.1988 v Pressure -3.7459e+05 1.6161e+05 -1.0729e+05 -92016 v TurbVisc 6.2567e-20 0.025822 0.00020768 6.4418e-05 v CourantNb 1.5634e-08 0.011437 0.00017038 4.9704e-06 v FourierNb 1.2443e-07 0.03853 0.00015067 5.7294e-07 v total_pressure -2.7326e+05 2.6293e+05 -5965.7 9308.8 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.107 0.11427 0.003048 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.3173e-07 0.044066 0.00032105 5.5434e-06 INSTANT 0.876467000E-01 TIME STEP NUMBER 56665 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283230314E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.852676442E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.20049E-02 0.21430E+01 Friction velocity uk : 0.20049E-02 0.21430E+01 Dimensionless distance yplus : 0.19409E-02 0.21072E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -5.761928080e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29503E+08 1 0.18984E-09 0.33283E+02 0.21785E+04 c Velocity[X] 0.18879E+02 c Velocity[Y] 0.14404E+02 c Velocity[Z] 0.11251E-05 c Pressure 0.20899E-03 9 0.61409E-04 0.15268E-02 0.87758E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -30.445 44.675 5.6116 8.0046 v Velocity[Y] -32.164 34.359 -0.16655 -0.066073 v Velocity[Z] -3.0816 3.1419 2.2592e-06 -5.3912e-08 v ǁVelocityǁ 0.00037491 44.909 8.6973 8.1989 v Pressure -3.7632e+05 1.6013e+05 -1.0911e+05 -93011 v TurbVisc 6.1937e-20 0.025838 0.00020776 6.4505e-05 v CourantNb 1.5668e-08 0.011437 0.00017039 4.9704e-06 v FourierNb 1.2443e-07 0.038506 0.00015069 5.7353e-07 v total_pressure -2.7499e+05 2.6146e+05 -7782.6 8314.1 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1072 0.11429 0.0030482 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.322e-07 0.044043 0.00032108 5.544e-06 INSTANT 0.876468000E-01 TIME STEP NUMBER 56666 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283226989E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.852579424E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.64502E-02 0.21432E+01 Friction velocity uk : 0.64502E-02 0.21432E+01 Dimensionless distance yplus : 0.62442E-02 0.21073E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -5.784081355e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29503E+08 1 0.18987E-09 0.33318E+02 0.21796E+04 c Velocity[X] 0.18912E+02 c Velocity[Y] 0.14406E+02 c Velocity[Z] 0.11096E-05 c Pressure 0.20796E-03 248 0.79483E-04 0.15185E-02 0.10996E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -30.459 44.687 5.6116 8.0045 v Velocity[Y] -32.175 34.372 -0.16663 -0.066297 v Velocity[Z] -3.082 3.1421 2.2587e-06 -5.3912e-08 v ǁVelocityǁ 0.00044613 44.922 8.6988 8.1991 v Pressure -3.7826e+05 1.5845e+05 -1.109e+05 -94140 v TurbVisc 6.1612e-20 0.025853 0.00020783 6.4592e-05 v CourantNb 1.6347e-08 0.011438 0.00017039 4.9705e-06 v FourierNb 1.2443e-07 0.038483 0.00015071 5.7412e-07 v total_pressure -2.7693e+05 2.5977e+05 -9570.7 7185 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1073 0.11431 0.0030485 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.3268e-07 0.044019 0.0003211 5.5446e-06 INSTANT 0.876469000E-01 TIME STEP NUMBER 56667 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283223493E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.852471023E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.90292E-02 0.21434E+01 Friction velocity uk : 0.90292E-02 0.21434E+01 Dimensionless distance yplus : 0.87409E-02 0.21075E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -5.841877458e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29503E+08 1 0.18991E-09 0.33357E+02 0.21807E+04 c Velocity[X] 0.18933E+02 c Velocity[Y] 0.14423E+02 c Velocity[Z] 0.10935E-05 c Pressure 0.20578E-03 63 0.84899E-04 0.15018E-02 0.10969E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -30.473 44.699 5.6115 8.0044 v Velocity[Y] -32.186 34.386 -0.1667 -0.066525 v Velocity[Z] -3.0824 3.1422 2.2582e-06 -5.3913e-08 v ǁVelocityǁ 0.0006957 44.934 8.7004 8.1992 v Pressure -3.8002e+05 1.5693e+05 -1.1271e+05 -95282 v TurbVisc 6.1044e-20 0.025869 0.0002079 6.4679e-05 v CourantNb 1.6899e-08 0.011439 0.0001704 4.9705e-06 v FourierNb 1.2443e-07 0.038459 0.00015072 5.7472e-07 v total_pressure -2.787e+05 2.5825e+05 -11386 6042.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1075 0.11433 0.0030489 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.3316e-07 0.043996 0.00032112 5.5452e-06 INSTANT 0.876470000E-01 TIME STEP NUMBER 56668 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283220023E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.852355971E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13321E-01 0.21435E+01 Friction velocity uk : 0.13321E-01 0.21435E+01 Dimensionless distance yplus : 0.12895E-01 0.21077E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -5.771009483e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29503E+08 1 0.18994E-09 0.33392E+02 0.21818E+04 c Velocity[X] 0.18957E+02 c Velocity[Y] 0.14435E+02 c Velocity[Z] 0.10862E-05 c Pressure 0.20397E-03 220 0.98961E-04 0.14878E-02 0.10118E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -30.488 44.711 5.6114 8.0043 v Velocity[Y] -32.197 34.399 -0.16678 -0.06675 v Velocity[Z] -3.0827 3.1423 2.2577e-06 -5.3913e-08 v ǁVelocityǁ 0.0010185 44.947 8.7019 8.1993 v Pressure -3.8187e+05 1.5534e+05 -1.1447e+05 -96291 v TurbVisc 6.6875e-20 0.025884 0.00020797 6.4765e-05 v CourantNb 1.7763e-08 0.01144 0.0001704 4.9705e-06 v FourierNb 1.2443e-07 0.038435 0.00015074 5.7531e-07 v total_pressure -2.8054e+05 2.5666e+05 -13145 5034.2 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1077 0.11435 0.0030493 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.3364e-07 0.043972 0.00032114 5.5458e-06 INSTANT 0.876471000E-01 TIME STEP NUMBER 56669 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283216103E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.852232854E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15206E-01 0.21437E+01 Friction velocity uk : 0.15206E-01 0.21437E+01 Dimensionless distance yplus : 0.14693E-01 0.21079E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -5.736203514e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29503E+08 1 0.18996E-09 0.33413E+02 0.21824E+04 c Velocity[X] 0.18979E+02 c Velocity[Y] 0.14434E+02 c Velocity[Z] 0.10863E-05 c Pressure 0.20213E-03 117 0.84112E-04 0.14736E-02 0.10086E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -30.502 44.723 5.6114 8.0042 v Velocity[Y] -32.208 34.412 -0.16685 -0.066977 v Velocity[Z] -3.0831 3.1425 2.2572e-06 -5.3913e-08 v ǁVelocityǁ 0.0013635 44.959 8.7034 8.1995 v Pressure -3.8361e+05 1.5384e+05 -1.1622e+05 -97426 v TurbVisc 7.1846e-20 0.025899 0.00020804 6.4852e-05 v CourantNb 1.8424e-08 0.011441 0.00017041 4.9705e-06 v FourierNb 1.2443e-07 0.038411 0.00015076 5.759e-07 v total_pressure -2.8228e+05 2.5517e+05 -14890 3899 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1079 0.11438 0.0030496 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.3412e-07 0.043949 0.00032117 5.5464e-06 INSTANT 0.876472000E-01 TIME STEP NUMBER 56670 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283212243E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.852098574E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13906E-01 0.21439E+01 Friction velocity uk : 0.13906E-01 0.21439E+01 Dimensionless distance yplus : 0.13479E-01 0.21081E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -5.737708418e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29502E+08 1 0.18999E-09 0.33455E+02 0.21837E+04 c Velocity[X] 0.18999E+02 c Velocity[Y] 0.14456E+02 c Velocity[Z] 0.10963E-05 c Pressure 0.19635E-03 9 0.60899E-04 0.14307E-02 0.78550E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -30.516 44.735 5.6113 8.0041 v Velocity[Y] -32.219 34.425 -0.16693 -0.067207 v Velocity[Z] -3.0835 3.1426 2.2567e-06 -5.3913e-08 v ǁVelocityǁ 0.0017077 44.971 8.7049 8.1996 v Pressure -3.8524e+05 1.5246e+05 -1.1791e+05 -98340 v TurbVisc 6.9127e-20 0.025915 0.00020811 6.494e-05 v CourantNb 1.9132e-08 0.011441 0.00017041 4.9705e-06 v FourierNb 1.2444e-07 0.038387 0.00015078 5.765e-07 v total_pressure -2.8392e+05 2.5378e+05 -16586 2984.9 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1081 0.1144 0.0030499 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.346e-07 0.043925 0.00032119 5.547e-06 INSTANT 0.876473000E-01 TIME STEP NUMBER 56671 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283208242E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.851953440E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.96049E-02 0.21441E+01 Friction velocity uk : 0.96049E-02 0.21441E+01 Dimensionless distance yplus : 0.93100E-02 0.21082E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -5.726886590e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29502E+08 1 0.19002E-09 0.33491E+02 0.21848E+04 c Velocity[X] 0.19032E+02 c Velocity[Y] 0.14459E+02 c Velocity[Z] 0.10826E-05 c Pressure 0.19499E-03 178 0.79932E-04 0.14200E-02 0.10258E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -30.53 44.747 5.6113 8.0041 v Velocity[Y] -32.23 34.438 -0.167 -0.067433 v Velocity[Z] -3.0839 3.1428 2.2562e-06 -5.3913e-08 v ǁVelocityǁ 0.0020774 44.983 8.7065 8.1997 v Pressure -3.8706e+05 1.509e+05 -1.1959e+05 -99427 v TurbVisc 6.9051e-20 0.02593 0.00020818 6.5026e-05 v CourantNb 2.0496e-08 0.011442 0.00017042 4.9705e-06 v FourierNb 1.2444e-07 0.038363 0.00015079 5.7709e-07 v total_pressure -2.8574e+05 2.5222e+05 -18260 1897.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1082 0.11442 0.0030502 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.3508e-07 0.043901 0.00032121 5.5476e-06 INSTANT 0.876474000E-01 TIME STEP NUMBER 56672 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283204026E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.851797201E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.18498E-02 0.21443E+01 Friction velocity uk : 0.18498E-02 0.21443E+01 Dimensionless distance yplus : 0.17930E-02 0.21084E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -5.765539458e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29502E+08 1 0.19005E-09 0.33530E+02 0.21859E+04 c Velocity[X] 0.19053E+02 c Velocity[Y] 0.14477E+02 c Velocity[Z] 0.10724E-05 c Pressure 0.19242E-03 367 0.85518E-04 0.14006E-02 0.10603E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -30.544 44.759 5.6112 8.004 v Velocity[Y] -32.241 34.451 -0.16708 -0.067664 v Velocity[Z] -3.0843 3.1429 2.2556e-06 -5.3913e-08 v ǁVelocityǁ 0.0022801 44.995 8.708 8.1999 v Pressure -3.8876e+05 1.4944e+05 -1.213e+05 -1.0056e+05 v TurbVisc 7.0864e-20 0.025946 0.00020825 6.5114e-05 v CourantNb 2.3897e-08 0.011443 0.00017042 4.9705e-06 v FourierNb 1.2444e-07 0.038339 0.00015081 5.7769e-07 v total_pressure -2.8744e+05 2.5076e+05 -19970 764.98 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1084 0.11444 0.0030505 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.3557e-07 0.043877 0.00032123 5.5482e-06 INSTANT 0.876475000E-01 TIME STEP NUMBER 56673 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283199851E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.851635066E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.28706E-02 0.21444E+01 Friction velocity uk : 0.28706E-02 0.21444E+01 Dimensionless distance yplus : 0.27824E-02 0.21086E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -5.696204910e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29502E+08 1 0.19008E-09 0.33552E+02 0.21866E+04 c Velocity[X] 0.19079E+02 c Velocity[Y] 0.14473E+02 c Velocity[Z] 0.10644E-05 c Pressure 0.19033E-03 145 0.74886E-04 0.13846E-02 0.71576E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -30.558 44.771 5.6111 8.0039 v Velocity[Y] -32.252 34.464 -0.16716 -0.067893 v Velocity[Z] -3.0846 3.1431 2.2551e-06 -5.3913e-08 v ǁVelocityǁ 0.0021624 45.007 8.7095 8.2 v Pressure -3.9035e+05 1.481e+05 -1.2288e+05 -1.0136e+05 v TurbVisc 7.3558e-20 0.025961 0.00020832 6.5201e-05 v CourantNb 2.7466e-08 0.011444 0.00017043 4.9706e-06 v FourierNb 1.2444e-07 0.038315 0.00015083 5.7828e-07 v total_pressure -2.8903e+05 2.4943e+05 -21551 -37.486 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1086 0.11446 0.0030509 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.3606e-07 0.043854 0.00032126 5.5488e-06 INSTANT 0.876476000E-01 TIME STEP NUMBER 56674 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283195426E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.851466736E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.99537E-02 0.21446E+01 Friction velocity uk : 0.99537E-02 0.21446E+01 Dimensionless distance yplus : 0.96482E-02 0.21088E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -5.671882508e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29502E+08 1 0.19010E-09 0.33592E+02 0.21878E+04 c Velocity[X] 0.19098E+02 c Velocity[Y] 0.14495E+02 c Velocity[Z] 0.10716E-05 c Pressure 0.18467E-03 9 0.58583E-04 0.13428E-02 0.73806E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -30.571 44.782 5.6111 8.0038 v Velocity[Y] -32.263 34.477 -0.16724 -0.068121 v Velocity[Z] -3.085 3.1432 2.2546e-06 -5.3913e-08 v ǁVelocityǁ 0.002032 45.019 8.711 8.2001 v Pressure -3.9194e+05 1.4677e+05 -1.2448e+05 -1.0227e+05 v TurbVisc 7.4203e-20 0.025976 0.00020838 6.5288e-05 v CourantNb 3.076e-08 0.011444 0.00017043 4.9706e-06 v FourierNb 1.2444e-07 0.038291 0.00015085 5.7888e-07 v total_pressure -2.9061e+05 2.4809e+05 -23159 -946.23 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1088 0.11448 0.0030512 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.3654e-07 0.04383 0.00032128 5.5494e-06 INSTANT 0.876477000E-01 TIME STEP NUMBER 56675 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283190726E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.851284567E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13779E-01 0.21448E+01 Friction velocity uk : 0.13779E-01 0.21448E+01 Dimensionless distance yplus : 0.13356E-01 0.21089E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -5.685290059e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29501E+08 1 0.19012E-09 0.33624E+02 0.21887E+04 c Velocity[X] 0.19128E+02 c Velocity[Y] 0.14497E+02 c Velocity[Z] 0.10623E-05 c Pressure 0.18285E-03 153 0.96658E-04 0.13288E-02 0.94832E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -30.585 44.794 5.611 8.0037 v Velocity[Y] -32.274 34.49 -0.16731 -0.068352 v Velocity[Z] -3.0854 3.1434 2.2541e-06 -5.3913e-08 v ǁVelocityǁ 0.0019245 45.031 8.7126 8.2002 v Pressure -3.9366e+05 1.4529e+05 -1.2605e+05 -1.0341e+05 v TurbVisc 7.3464e-20 0.025992 0.00020845 6.5376e-05 v CourantNb 3.3794e-08 0.011445 0.00017044 4.9706e-06 v FourierNb 1.2444e-07 0.038267 0.00015087 5.7948e-07 v total_pressure -2.9234e+05 2.4662e+05 -24727 -2089.8 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1089 0.11451 0.0030516 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.3702e-07 0.043806 0.0003213 5.55e-06 INSTANT 0.876478000E-01 TIME STEP NUMBER 56676 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283186049E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.851091826E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.17535E-01 0.21450E+01 Friction velocity uk : 0.17535E-01 0.21450E+01 Dimensionless distance yplus : 0.17023E-01 0.21091E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -5.737650478e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29501E+08 1 0.19016E-09 0.33657E+02 0.21897E+04 c Velocity[X] 0.19150E+02 c Velocity[Y] 0.14507E+02 c Velocity[Z] 0.10552E-05 c Pressure 0.17919E-03 104 0.80525E-04 0.13016E-02 0.79800E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -30.599 44.806 5.6109 8.0036 v Velocity[Y] -32.284 34.503 -0.16739 -0.068583 v Velocity[Z] -3.0858 3.1435 2.2536e-06 -5.3913e-08 v ǁVelocityǁ 0.0018058 45.043 8.7141 8.2003 v Pressure -3.9524e+05 1.4396e+05 -1.2764e+05 -1.0442e+05 v TurbVisc 3.7845e-20 0.026007 0.00020852 6.5463e-05 v CourantNb 3.7357e-08 0.011446 0.00017044 4.9706e-06 v FourierNb 1.2444e-07 0.038242 0.00015088 5.8007e-07 v total_pressure -2.9392e+05 2.4528e+05 -26320 -3090.9 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1091 0.11453 0.0030519 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.3743e-07 0.043782 0.00032133 5.5506e-06 INSTANT 0.876479000E-01 TIME STEP NUMBER 56677 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283181268E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.850891046E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.14077E-01 0.21451E+01 Friction velocity uk : 0.14077E-01 0.21451E+01 Dimensionless distance yplus : 0.13666E-01 0.21093E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -5.678485128e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29501E+08 1 0.19018E-09 0.33698E+02 0.21909E+04 c Velocity[X] 0.19170E+02 c Velocity[Y] 0.14527E+02 c Velocity[Z] 0.10599E-05 c Pressure 0.17518E-03 9 0.53892E-04 0.12718E-02 0.68863E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -30.613 44.817 5.6109 8.0035 v Velocity[Y] -32.295 34.515 -0.16747 -0.068816 v Velocity[Z] -3.0861 3.1437 2.2531e-06 -5.3913e-08 v ǁVelocityǁ 0.0016767 45.055 8.7156 8.2005 v Pressure -3.9671e+05 1.4273e+05 -1.2915e+05 -1.0525e+05 v TurbVisc 8.7632e-20 0.026022 0.00020859 6.5551e-05 v CourantNb 4.0915e-08 0.011446 0.00017045 4.9706e-06 v FourierNb 1.2445e-07 0.038218 0.0001509 5.8067e-07 v total_pressure -2.9539e+05 2.4406e+05 -27828 -3929.4 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1093 0.11455 0.0030522 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.3785e-07 0.043758 0.00032135 5.5512e-06 INSTANT 0.876480000E-01 TIME STEP NUMBER 56678 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283176422E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.850686543E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.90062E-02 0.21453E+01 Friction velocity uk : 0.90062E-02 0.21453E+01 Dimensionless distance yplus : 0.87432E-02 0.21094E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -5.728605050e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29501E+08 1 0.19020E-09 0.33728E+02 0.21919E+04 c Velocity[X] 0.19200E+02 c Velocity[Y] 0.14528E+02 c Velocity[Z] 0.10493E-05 c Pressure 0.17333E-03 150 0.97019E-04 0.12576E-02 0.75711E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -30.626 44.828 5.6108 8.0034 v Velocity[Y] -32.306 34.528 -0.16755 -0.069048 v Velocity[Z] -3.0865 3.1438 2.2526e-06 -5.3913e-08 v ǁVelocityǁ 0.0015708 45.066 8.7171 8.2006 v Pressure -3.9825e+05 1.4145e+05 -1.3059e+05 -1.0618e+05 v TurbVisc 8.1344e-20 0.026038 0.00020866 6.5638e-05 v CourantNb 4.392e-08 0.011447 0.00017045 4.9706e-06 v FourierNb 1.2445e-07 0.038194 0.00015092 5.8127e-07 v total_pressure -2.9692e+05 2.4278e+05 -29268 -4854.7 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1094 0.11457 0.0030525 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.3827e-07 0.043734 0.00032137 5.5518e-06 INSTANT 0.876481000E-01 TIME STEP NUMBER 56679 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283171392E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.850471127E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.17156E-02 0.21455E+01 Friction velocity uk : 0.17156E-02 0.21455E+01 Dimensionless distance yplus : 0.16655E-02 0.21096E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -5.763353753e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29500E+08 1 0.19023E-09 0.33761E+02 0.21928E+04 c Velocity[X] 0.19225E+02 c Velocity[Y] 0.14536E+02 c Velocity[Z] 0.10385E-05 c Pressure 0.16950E-03 37 0.82627E-04 0.12293E-02 0.66555E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -30.64 44.84 5.6107 8.0032 v Velocity[Y] -32.316 34.541 -0.16763 -0.06928 v Velocity[Z] -3.0869 3.1439 2.2521e-06 -5.3913e-08 v ǁVelocityǁ 0.0014562 45.078 8.7186 8.2007 v Pressure -3.9972e+05 1.4022e+05 -1.3205e+05 -1.0703e+05 v TurbVisc 8.3463e-20 0.026053 0.00020873 6.5726e-05 v CourantNb 4.7599e-08 0.011448 0.00017046 4.9706e-06 v FourierNb 1.2445e-07 0.038169 0.00015094 5.8187e-07 v total_pressure -2.984e+05 2.4154e+05 -30728 -5702.7 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1096 0.11459 0.0030528 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.3869e-07 0.04371 0.0003214 5.5524e-06 INSTANT 0.876482000E-01 TIME STEP NUMBER 56680 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283166257E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.850245717E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.33942E-02 0.21457E+01 Friction velocity uk : 0.33942E-02 0.21457E+01 Dimensionless distance yplus : 0.32950E-02 0.21098E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -5.758884907e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29500E+08 1 0.19026E-09 0.33802E+02 0.21941E+04 c Velocity[X] 0.19248E+02 c Velocity[Y] 0.14555E+02 c Velocity[Z] 0.10409E-05 c Pressure 0.16515E-03 9 0.57519E-04 0.11970E-02 0.63999E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -30.653 44.851 5.6107 8.0031 v Velocity[Y] -32.327 34.553 -0.16771 -0.069512 v Velocity[Z] -3.0873 3.1441 2.2516e-06 -5.3913e-08 v ǁVelocityǁ 0.0013282 45.089 8.7201 8.2008 v Pressure -4.012e+05 1.3899e+05 -1.3349e+05 -1.0783e+05 v TurbVisc 8.3823e-20 0.026068 0.00020879 6.5814e-05 v CourantNb 5.0669e-08 0.011449 0.00017046 4.9706e-06 v FourierNb 1.2445e-07 0.038145 0.00015096 5.8246e-07 v total_pressure -2.9987e+05 2.4031e+05 -32166 -6504 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1098 0.11461 0.0030531 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.3912e-07 0.043686 0.00032142 5.553e-06 INSTANT 0.876483000E-01 TIME STEP NUMBER 56681 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283160936E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.850013269E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11025E-01 0.21458E+01 Friction velocity uk : 0.11025E-01 0.21458E+01 Dimensionless distance yplus : 0.10703E-01 0.21099E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -5.940931616e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29500E+08 1 0.19028E-09 0.33839E+02 0.21952E+04 c Velocity[X] 0.19275E+02 c Velocity[Y] 0.14565E+02 c Velocity[Z] 0.10338E-05 c Pressure 0.16341E-03 33 0.76130E-04 0.11838E-02 0.94987E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -30.667 44.862 5.6106 8.003 v Velocity[Y] -32.337 34.566 -0.16779 -0.069747 v Velocity[Z] -3.0876 3.1442 2.2511e-06 -5.3913e-08 v ǁVelocityǁ 0.0012223 45.101 8.7216 8.2009 v Pressure -4.0265e+05 1.3779e+05 -1.3487e+05 -1.089e+05 v TurbVisc 8.0537e-20 0.026084 0.00020886 6.5902e-05 v CourantNb 4.8532e-08 0.011449 0.00017047 4.9706e-06 v FourierNb 1.2445e-07 0.03812 0.00015098 5.8306e-07 v total_pressure -3.0132e+05 2.3911e+05 -33541 -7574.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1099 0.11464 0.0030534 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.3954e-07 0.043661 0.00032144 5.5536e-06 INSTANT 0.876484000E-01 TIME STEP NUMBER 56682 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283155729E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.849774293E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13024E-01 0.21460E+01 Friction velocity uk : 0.13024E-01 0.21460E+01 Dimensionless distance yplus : 0.12595E-01 0.21101E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -5.926080460e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29500E+08 1 0.19031E-09 0.33875E+02 0.21963E+04 c Velocity[X] 0.19298E+02 c Velocity[Y] 0.14577E+02 c Velocity[Z] 0.10239E-05 c Pressure 0.16019E-03 78 0.80919E-04 0.11599E-02 0.70324E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -30.68 44.873 5.6105 8.0029 v Velocity[Y] -32.347 34.578 -0.16788 -0.06998 v Velocity[Z] -3.088 3.1444 2.2506e-06 -5.3913e-08 v ǁVelocityǁ 0.0011116 45.112 8.7231 8.201 v Pressure -4.0404e+05 1.3663e+05 -1.3622e+05 -1.0963e+05 v TurbVisc 8.5096e-20 0.026099 0.00020893 6.5989e-05 v CourantNb 4.6319e-08 0.01145 0.00017047 4.9706e-06 v FourierNb 1.2445e-07 0.038096 0.000151 5.8366e-07 v total_pressure -3.0272e+05 2.3796e+05 -34892 -8307.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1101 0.11466 0.0030536 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.3996e-07 0.043637 0.00032147 5.5543e-06 INSTANT 0.876485000E-01 TIME STEP NUMBER 56683 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283150142E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.849527113E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.84067E-02 0.21462E+01 Friction velocity uk : 0.84067E-02 0.21462E+01 Dimensionless distance yplus : 0.81293E-02 0.21103E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -6.041197637e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29499E+08 1 0.19033E-09 0.33913E+02 0.21974E+04 c Velocity[X] 0.19320E+02 c Velocity[Y] 0.14593E+02 c Velocity[Z] 0.10209E-05 c Pressure 0.15752E-03 102 0.94196E-04 0.11400E-02 0.85865E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -30.694 44.884 5.6104 8.0028 v Velocity[Y] -32.358 34.591 -0.16796 -0.070216 v Velocity[Z] -3.0884 3.1445 2.2501e-06 -5.3914e-08 v ǁVelocityǁ 0.0010027 45.124 8.7247 8.2011 v Pressure -4.0534e+05 1.3558e+05 -1.3754e+05 -1.1052e+05 v TurbVisc 8.3896e-20 0.026114 0.000209 6.6077e-05 v CourantNb 4.4177e-08 0.011451 0.00017048 4.9706e-06 v FourierNb 1.2445e-07 0.038071 0.00015101 5.8427e-07 v total_pressure -3.0402e+05 2.3691e+05 -36211 -9191.8 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1103 0.11468 0.0030539 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.4039e-07 0.043613 0.00032149 5.5548e-06 INSTANT 0.876486000E-01 TIME STEP NUMBER 56684 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283144693E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.849273568E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.22455E-02 0.21463E+01 Friction velocity uk : 0.22455E-02 0.21463E+01 Dimensionless distance yplus : 0.21714E-02 0.21104E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -6.105409201e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29499E+08 1 0.19036E-09 0.33933E+02 0.21980E+04 c Velocity[X] 0.19344E+02 c Velocity[Y] 0.14589E+02 c Velocity[Z] 0.10227E-05 c Pressure 0.15492E-03 436 0.80165E-04 0.11206E-02 0.61117E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -30.707 44.895 5.6104 8.0027 v Velocity[Y] -32.368 34.603 -0.16804 -0.070451 v Velocity[Z] -3.0888 3.1447 2.2496e-06 -5.3914e-08 v ǁVelocityǁ 0.00089953 45.135 8.7262 8.2012 v Pressure -4.0668e+05 1.3449e+05 -1.388e+05 -1.1122e+05 v TurbVisc 9.057e-20 0.02613 0.00020906 6.6165e-05 v CourantNb 4.1972e-08 0.011451 0.00017048 4.9706e-06 v FourierNb 1.2446e-07 0.038047 0.00015103 5.8486e-07 v total_pressure -3.0535e+05 2.3581e+05 -37475 -9893.4 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1104 0.1147 0.003054 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.4081e-07 0.043588 0.00032152 5.5554e-06 INSTANT 0.876487000E-01 TIME STEP NUMBER 56685 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283139017E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.849011572E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.41992E-02 0.21465E+01 Friction velocity uk : 0.41992E-02 0.21465E+01 Dimensionless distance yplus : 0.40836E-02 0.21106E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -6.229251484e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29499E+08 1 0.19038E-09 0.33974E+02 0.21992E+04 c Velocity[X] 0.19367E+02 c Velocity[Y] 0.14607E+02 c Velocity[Z] 0.10219E-05 c Pressure 0.14762E-03 9 0.58052E-04 0.10672E-02 0.47492E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -30.72 44.906 5.6103 8.0025 v Velocity[Y] -32.378 34.616 -0.16812 -0.070685 v Velocity[Z] -3.0891 3.1448 2.2491e-06 -5.3914e-08 v ǁVelocityǁ 0.00079662 45.146 8.7277 8.2013 v Pressure -4.0787e+05 1.3354e+05 -1.4e+05 -1.1181e+05 v TurbVisc 9.0923e-20 0.026145 0.00020913 6.6253e-05 v CourantNb 3.9733e-08 0.011452 0.00017049 4.9706e-06 v FourierNb 1.2446e-07 0.038022 0.00015105 5.8547e-07 v total_pressure -3.0654e+05 2.3487e+05 -38678 -10481 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1106 0.11472 0.0030543 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.4124e-07 0.043564 0.00032154 5.556e-06 INSTANT 0.876488000E-01 TIME STEP NUMBER 56686 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283133185E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.848742192E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.48135E-02 0.21466E+01 Friction velocity uk : 0.48135E-02 0.21466E+01 Dimensionless distance yplus : 0.46318E-02 0.21107E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -6.407208075e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29498E+08 1 0.19040E-09 0.34010E+02 0.22003E+04 c Velocity[X] 0.19393E+02 c Velocity[Y] 0.14617E+02 c Velocity[Z] 0.10103E-05 c Pressure 0.14580E-03 39 0.76471E-04 0.10535E-02 0.90972E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -30.734 44.917 5.6102 8.0024 v Velocity[Y] -32.388 34.628 -0.1682 -0.070923 v Velocity[Z] -3.0895 3.145 2.2486e-06 -5.3914e-08 v ǁVelocityǁ 0.00071784 45.157 8.7292 8.2014 v Pressure -4.092e+05 1.3246e+05 -1.4125e+05 -1.1286e+05 v TurbVisc 9.3435e-20 0.02616 0.0002092 6.6342e-05 v CourantNb 3.75e-08 0.011453 0.00017049 4.9706e-06 v FourierNb 1.2446e-07 0.037997 0.00015107 5.8607e-07 v total_pressure -3.0788e+05 2.3378e+05 -39923 -11531 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1107 0.11474 0.0030546 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.4167e-07 0.043539 0.00032157 5.5566e-06 INSTANT 0.876489000E-01 TIME STEP NUMBER 56687 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283127462E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.848464804E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.38018E-02 0.21468E+01 Friction velocity uk : 0.38018E-02 0.21468E+01 Dimensionless distance yplus : 0.36582E-02 0.21109E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -6.494300370e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29498E+08 1 0.19043E-09 0.34045E+02 0.22014E+04 c Velocity[X] 0.19417E+02 c Velocity[Y] 0.14628E+02 c Velocity[Z] 0.10031E-05 c Pressure 0.14255E-03 559 0.82033E-04 0.10295E-02 0.63010E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -30.747 44.928 5.6101 8.0023 v Velocity[Y] -32.398 34.64 -0.16829 -0.071158 v Velocity[Z] -3.0899 3.1451 2.248e-06 -5.3914e-08 v ǁVelocityǁ 0.00065187 45.168 8.7307 8.2015 v Pressure -4.1042e+05 1.3148e+05 -1.4241e+05 -1.1347e+05 v TurbVisc 9.3722e-20 0.026176 0.00020926 6.643e-05 v CourantNb 3.5131e-08 0.011453 0.0001705 4.9706e-06 v FourierNb 1.2446e-07 0.037972 0.00015109 5.8667e-07 v total_pressure -3.0909e+05 2.3281e+05 -41084 -12148 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1109 0.11477 0.003055 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.421e-07 0.043514 0.00032159 5.5572e-06 INSTANT 0.876490000E-01 TIME STEP NUMBER 56688 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283121423E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.848183833E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.21484E-02 0.21469E+01 Friction velocity uk : 0.21484E-02 0.21469E+01 Dimensionless distance yplus : 0.20673E-02 0.21110E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -6.679436483e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29498E+08 1 0.19045E-09 0.34083E+02 0.22025E+04 c Velocity[X] 0.19437E+02 c Velocity[Y] 0.14645E+02 c Velocity[Z] 0.99882E-06 c Pressure 0.13991E-03 102 0.95382E-04 0.10099E-02 0.80609E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -30.76 44.939 5.6101 8.0022 v Velocity[Y] -32.408 34.652 -0.16837 -0.071398 v Velocity[Z] -3.0903 3.1452 2.2475e-06 -5.3914e-08 v ǁVelocityǁ 0.00060983 45.179 8.7321 8.2016 v Pressure -4.1156e+05 1.3059e+05 -1.4354e+05 -1.1428e+05 v TurbVisc 9.3847e-20 0.026191 0.00020933 6.6518e-05 v CourantNb 3.278e-08 0.011454 0.0001705 4.9706e-06 v FourierNb 1.2446e-07 0.037947 0.00015111 5.8727e-07 v total_pressure -3.1023e+05 2.3191e+05 -42219 -12955 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.111 0.11479 0.0030554 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.4253e-07 0.04349 0.00032162 5.5578e-06 INSTANT 0.876491000E-01 TIME STEP NUMBER 56689 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283115520E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.847898461E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.64344E-02 0.21470E+01 Friction velocity uk : 0.64344E-02 0.21470E+01 Dimensionless distance yplus : 0.61875E-02 0.21112E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -6.830907342e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29497E+08 1 0.19048E-09 0.34101E+02 0.22030E+04 c Velocity[X] 0.19463E+02 c Velocity[Y] 0.14639E+02 c Velocity[Z] 0.99725E-06 c Pressure 0.13740E-03 285 0.81202E-04 0.99127E-03 0.51352E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -30.773 44.95 5.61 8.002 v Velocity[Y] -32.418 34.665 -0.16845 -0.071635 v Velocity[Z] -3.0906 3.1454 2.247e-06 -5.3914e-08 v ǁVelocityǁ 0.00059876 45.19 8.7336 8.2017 v Pressure -4.1267e+05 1.2971e+05 -1.4461e+05 -1.1482e+05 v TurbVisc 9.9166e-20 0.026206 0.00020939 6.6606e-05 v CourantNb 3.0372e-08 0.011455 0.00017051 4.9706e-06 v FourierNb 1.2446e-07 0.037922 0.00015113 5.8787e-07 v total_pressure -3.1135e+05 2.3103e+05 -43282 -13499 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1112 0.11481 0.0030558 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.4296e-07 0.043465 0.00032164 5.5584e-06 INSTANT 0.876492000E-01 TIME STEP NUMBER 56690 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283109434E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.847604822E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.78600E-02 0.21472E+01 Friction velocity uk : 0.78600E-02 0.21472E+01 Dimensionless distance yplus : 0.75584E-02 0.21113E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -7.015092023e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29497E+08 1 0.19050E-09 0.34142E+02 0.22042E+04 c Velocity[X] 0.19482E+02 c Velocity[Y] 0.14660E+02 c Velocity[Z] 0.10114E-05 c Pressure 0.12940E-03 18 0.59769E-04 0.93306E-03 0.44535E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -30.786 44.96 5.6099 8.0019 v Velocity[Y] -32.428 34.677 -0.16854 -0.071872 v Velocity[Z] -3.091 3.1455 2.2465e-06 -5.3914e-08 v ǁVelocityǁ 0.00062359 45.201 8.7351 8.2018 v Pressure -4.1372e+05 1.289e+05 -1.4564e+05 -1.1538e+05 v TurbVisc 1.0016e-19 0.026221 0.00020946 6.6695e-05 v CourantNb 2.7904e-08 0.011455 0.00017051 4.9706e-06 v FourierNb 1.2447e-07 0.037897 0.00015115 5.8848e-07 v total_pressure -3.124e+05 2.3023e+05 -44316 -14059 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1113 0.11484 0.0030563 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.4339e-07 0.04344 0.00032167 5.559e-06 INSTANT 0.876493000E-01 TIME STEP NUMBER 56691 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283103178E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.847304099E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.30417E-02 0.21473E+01 Friction velocity uk : 0.30417E-02 0.21473E+01 Dimensionless distance yplus : 0.29637E-02 0.21114E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -7.289451906e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29497E+08 1 0.19052E-09 0.34177E+02 0.22053E+04 c Velocity[X] 0.19509E+02 c Velocity[Y] 0.14668E+02 c Velocity[Z] 0.99635E-06 c Pressure 0.12795E-03 74 0.77626E-04 0.92216E-03 0.79233E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -30.799 44.971 5.6098 8.0018 v Velocity[Y] -32.438 34.689 -0.16862 -0.072113 v Velocity[Z] -3.0914 3.1457 2.246e-06 -5.3914e-08 v ǁVelocityǁ 0.00067779 45.212 8.7366 8.2019 v Pressure -4.1485e+05 1.2801e+05 -1.4668e+05 -1.1629e+05 v TurbVisc 1.0055e-19 0.026237 0.00020952 6.6783e-05 v CourantNb 2.4929e-08 0.011456 0.00017052 4.9705e-06 v FourierNb 1.2447e-07 0.037872 0.00015117 5.8908e-07 v total_pressure -3.1353e+05 2.2934e+05 -45356 -14966 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1114 0.11486 0.0030569 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.4382e-07 0.043414 0.00032169 5.5596e-06 INSTANT 0.876494000E-01 TIME STEP NUMBER 56692 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283097046E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.846996595E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.45852E-02 0.21474E+01 Friction velocity uk : 0.45852E-02 0.21474E+01 Dimensionless distance yplus : 0.44675E-02 0.21115E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -7.408344285e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29496E+08 1 0.19055E-09 0.34211E+02 0.22063E+04 c Velocity[X] 0.19530E+02 c Velocity[Y] 0.14681E+02 c Velocity[Z] 0.98484E-06 c Pressure 0.12475E-03 73 0.83538E-04 0.89863E-03 0.55873E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -30.812 44.981 5.6097 8.0016 v Velocity[Y] -32.448 34.701 -0.1687 -0.072351 v Velocity[Z] -3.0918 3.1458 2.2455e-06 -5.3914e-08 v ǁVelocityǁ 0.00075976 45.223 8.7381 8.202 v Pressure -4.1588e+05 1.2722e+05 -1.4764e+05 -1.1679e+05 v TurbVisc 1.0373e-19 0.026252 0.00020959 6.6872e-05 v CourantNb 2.3391e-08 0.011457 0.00017052 4.9705e-06 v FourierNb 1.2447e-07 0.037847 0.00015119 5.8969e-07 v total_pressure -3.1456e+05 2.2855e+05 -46315 -15461 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1115 0.11488 0.0030574 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.4426e-07 0.043389 0.00032172 5.5602e-06 INSTANT 0.876495000E-01 TIME STEP NUMBER 56693 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283090614E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.846686473E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.34282E-02 0.21475E+01 Friction velocity uk : 0.34282E-02 0.21475E+01 Dimensionless distance yplus : 0.33773E-02 0.21116E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -7.674806384e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29496E+08 1 0.19057E-09 0.34248E+02 0.22074E+04 c Velocity[X] 0.19552E+02 c Velocity[Y] 0.14696E+02 c Velocity[Z] 0.98048E-06 c Pressure 0.12235E-03 107 0.97209E-04 0.88082E-03 0.72442E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -30.825 44.992 5.6096 8.0015 v Velocity[Y] -32.458 34.713 -0.16879 -0.072593 v Velocity[Z] -3.0921 3.146 2.245e-06 -5.3914e-08 v ǁVelocityǁ 0.00086269 45.233 8.7396 8.202 v Pressure -4.1681e+05 1.2654e+05 -1.4858e+05 -1.1747e+05 v TurbVisc 1.0254e-19 0.026267 0.00020965 6.696e-05 v CourantNb 2.2493e-08 0.011457 0.00017053 4.9705e-06 v FourierNb 1.2447e-07 0.037821 0.00015121 5.9029e-07 v total_pressure -3.1548e+05 2.2786e+05 -47255 -16147 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1116 0.11491 0.003058 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.4469e-07 0.043364 0.00032174 5.5608e-06 INSTANT 0.876496000E-01 TIME STEP NUMBER 56694 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283084371E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.846372025E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11780E-01 0.21477E+01 Friction velocity uk : 0.11780E-01 0.21477E+01 Dimensionless distance yplus : 0.11605E-01 0.21118E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -7.895534319e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29496E+08 1 0.19060E-09 0.34265E+02 0.22079E+04 c Velocity[X] 0.19575E+02 c Velocity[Y] 0.14690E+02 c Velocity[Z] 0.97422E-06 c Pressure 0.12018E-03 274 0.82714E-04 0.86480E-03 0.44203E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -30.838 45.002 5.6095 8.0013 v Velocity[Y] -32.467 34.725 -0.16887 -0.072833 v Velocity[Z] -3.0925 3.1461 2.2445e-06 -5.3914e-08 v ǁVelocityǁ 0.0009804 45.244 8.7411 8.2021 v Pressure -4.1774e+05 1.2584e+05 -1.4944e+05 -1.1791e+05 v TurbVisc 1.0885e-19 0.026282 0.00020972 6.7049e-05 v CourantNb 2.1927e-08 0.011458 0.00017053 4.9705e-06 v FourierNb 1.2447e-07 0.037796 0.00015123 5.909e-07 v total_pressure -3.1642e+05 2.2717e+05 -48115 -16582 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1118 0.11494 0.0030586 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.4513e-07 0.043339 0.00032177 5.5614e-06 INSTANT 0.876497000E-01 TIME STEP NUMBER 56695 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283077941E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.846051195E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.20272E-01 0.21478E+01 Friction velocity uk : 0.20272E-01 0.21478E+01 Dimensionless distance yplus : 0.19970E-01 0.21119E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -8.133644286e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29495E+08 1 0.19062E-09 0.34304E+02 0.22091E+04 c Velocity[X] 0.19593E+02 c Velocity[Y] 0.14711E+02 c Velocity[Z] 0.99727E-06 c Pressure 0.11146E-03 15 0.60472E-04 0.80160E-03 0.37424E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -30.85 45.012 5.6094 8.0012 v Velocity[Y] -32.477 34.737 -0.16895 -0.073072 v Velocity[Z] -3.0929 3.1462 2.244e-06 -5.3914e-08 v ǁVelocityǁ 0.0011142 45.255 8.7425 8.2022 v Pressure -4.1859e+05 1.2523e+05 -1.5027e+05 -1.1836e+05 v TurbVisc 1.1264e-19 0.026298 0.00020978 6.7138e-05 v CourantNb 1.9908e-08 0.011459 0.00017054 4.9705e-06 v FourierNb 1.2447e-07 0.03777 0.00015125 5.915e-07 v total_pressure -3.1727e+05 2.2656e+05 -48941 -17034 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1119 0.11497 0.0030591 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.4516e-07 0.043313 0.00032179 5.562e-06 INSTANT 0.876498000E-01 TIME STEP NUMBER 56696 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283071369E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.845724250E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19178E-01 0.21478E+01 Friction velocity uk : 0.19178E-01 0.21478E+01 Dimensionless distance yplus : 0.18511E-01 0.21119E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -8.457695691e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29495E+08 1 0.19064E-09 0.34339E+02 0.22101E+04 c Velocity[X] 0.19618E+02 c Velocity[Y] 0.14720E+02 c Velocity[Z] 0.98143E-06 c Pressure 0.11064E-03 506 0.79515E-04 0.79532E-03 0.76046E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -30.863 45.023 5.6094 8.0011 v Velocity[Y] -32.487 34.748 -0.16904 -0.073316 v Velocity[Z] -3.0932 3.1464 2.2435e-06 -5.3914e-08 v ǁVelocityǁ 0.0012376 45.265 8.744 8.2023 v Pressure -4.1959e+05 1.2447e+05 -1.5113e+05 -1.1923e+05 v TurbVisc 1.5428e-19 0.026313 0.00020985 6.7226e-05 v CourantNb 1.6971e-08 0.011459 0.00017054 4.9705e-06 v FourierNb 1.2447e-07 0.037744 0.00015127 5.9211e-07 v total_pressure -3.1826e+05 2.258e+05 -49806 -17902 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1119 0.115 0.0030597 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.4519e-07 0.043288 0.00032182 5.5626e-06 INSTANT 0.876499000E-01 TIME STEP NUMBER 56697 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283064895E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.845391173E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19036E-01 0.21480E+01 Friction velocity uk : 0.19036E-01 0.21480E+01 Dimensionless distance yplus : 0.18374E-01 0.21120E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -8.614343174e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29495E+08 1 0.19067E-09 0.34372E+02 0.22111E+04 c Velocity[X] 0.19641E+02 c Velocity[Y] 0.14731E+02 c Velocity[Z] 0.96208E-06 c Pressure 0.10788E-03 204 0.85491E-04 0.77509E-03 0.48841E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -30.876 45.033 5.6093 8.0009 v Velocity[Y] -32.496 34.76 -0.16912 -0.073556 v Velocity[Z] -3.0936 3.1465 2.243e-06 -5.3914e-08 v ǁVelocityǁ 0.00092867 45.276 8.7455 8.2024 v Pressure -4.203e+05 1.24e+05 -1.5183e+05 -1.1944e+05 v TurbVisc 1.1096e-19 0.026328 0.00020991 6.7315e-05 v CourantNb 1.471e-08 0.01146 0.00017055 4.9705e-06 v FourierNb 1.2448e-07 0.037719 0.00015129 5.9271e-07 v total_pressure -3.1897e+05 2.2532e+05 -50507 -18116 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.112 0.11502 0.0030601 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.4521e-07 0.043262 0.00032184 5.5632e-06 INSTANT 0.876500000E-01 TIME STEP NUMBER 56698 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283058210E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.845058540E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.64530E-02 0.21480E+01 Friction velocity uk : 0.64530E-02 0.21480E+01 Dimensionless distance yplus : 0.62324E-02 0.21121E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -8.889840556e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29494E+08 1 0.19069E-09 0.34407E+02 0.22121E+04 c Velocity[X] 0.19660E+02 c Velocity[Y] 0.14748E+02 c Velocity[Z] 0.95665E-06 c Pressure 0.10598E-03 110 0.99587E-04 0.76104E-03 0.71239E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -30.888 45.043 5.6092 8.0008 v Velocity[Y] -32.506 34.772 -0.1692 -0.073801 v Velocity[Z] -3.094 3.1467 2.2425e-06 -5.3914e-08 v ǁVelocityǁ 0.00070424 45.286 8.7469 8.2025 v Pressure -4.2108e+05 1.2346e+05 -1.5258e+05 -1.2008e+05 v TurbVisc 1.1523e-19 0.026343 0.00020997 6.7404e-05 v CourantNb 1.4783e-08 0.01146 0.00017055 4.9705e-06 v FourierNb 1.2448e-07 0.037693 0.00015131 5.9332e-07 v total_pressure -3.1975e+05 2.2478e+05 -51256 -18757 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1121 0.11505 0.0030606 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.4524e-07 0.043236 0.00032187 5.5638e-06 INSTANT 0.876501000E-01 TIME STEP NUMBER 56699 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283051696E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.844719940E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.41398E-02 0.21481E+01 Friction velocity uk : 0.41398E-02 0.21481E+01 Dimensionless distance yplus : 0.40429E-02 0.21122E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -9.176901529e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29494E+08 1 0.19072E-09 0.34422E+02 0.22125E+04 c Velocity[X] 0.19682E+02 c Velocity[Y] 0.14740E+02 c Velocity[Z] 0.95338E-06 c Pressure 0.10451E-03 279 0.84883E-04 0.75005E-03 0.38922E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -30.901 45.053 5.609 8.0006 v Velocity[Y] -32.516 34.784 -0.16928 -0.074044 v Velocity[Z] -3.0944 3.1468 2.242e-06 -5.3915e-08 v ǁVelocityǁ 0.00063942 45.297 8.7484 8.2026 v Pressure -4.2181e+05 1.2296e+05 -1.5323e+05 -1.204e+05 v TurbVisc 1.1923e-19 0.026358 0.00021004 6.7493e-05 v CourantNb 1.4772e-08 0.011461 0.00017056 4.9704e-06 v FourierNb 1.2448e-07 0.037667 0.00015134 5.9393e-07 v total_pressure -3.2049e+05 2.2429e+05 -51904 -19072 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1122 0.11507 0.003061 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.4526e-07 0.04321 0.00032189 5.5644e-06 INSTANT 0.876502000E-01 TIME STEP NUMBER 56700 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283045012E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.844376377E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.65983E-02 0.21482E+01 Friction velocity uk : 0.65983E-02 0.21482E+01 Dimensionless distance yplus : 0.64438E-02 0.21123E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -9.424854464e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29494E+08 1 0.19074E-09 0.34461E+02 0.22137E+04 c Velocity[X] 0.19699E+02 c Velocity[Y] 0.14762E+02 c Velocity[Z] 0.95851E-06 c Pressure 0.95041E-04 12 0.61279E-04 0.68177E-03 0.31688E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -30.913 45.063 5.6089 8.0005 v Velocity[Y] -32.525 34.796 -0.16937 -0.074286 v Velocity[Z] -3.0947 3.147 2.2415e-06 -5.3915e-08 v ǁVelocityǁ 0.00066549 45.307 8.7499 8.2026 v Pressure -4.2247e+05 1.2254e+05 -1.5384e+05 -1.2075e+05 v TurbVisc 1.2228e-19 0.026374 0.0002101 6.7582e-05 v CourantNb 1.4754e-08 0.011461 0.00017056 4.9704e-06 v FourierNb 1.2448e-07 0.037641 0.00015136 5.9453e-07 v total_pressure -3.2115e+05 2.2386e+05 -52519 -19423 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1123 0.11509 0.0030614 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.4529e-07 0.043184 0.00032192 5.565e-06 INSTANT 0.876503000E-01 TIME STEP NUMBER 56701 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283038214E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.844028224E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.17630E-01 0.21482E+01 Friction velocity uk : 0.17630E-01 0.21482E+01 Dimensionless distance yplus : 0.17217E-01 0.21123E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -9.755411305e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29493E+08 1 0.19076E-09 0.34493E+02 0.22146E+04 c Velocity[X] 0.19723E+02 c Velocity[Y] 0.14770E+02 c Velocity[Z] 0.95156E-06 c Pressure 0.95334E-04 65 0.81161E-04 0.68352E-03 0.61934E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -30.926 45.073 5.6088 8.0004 v Velocity[Y] -32.534 34.807 -0.16945 -0.074532 v Velocity[Z] -3.0951 3.1471 2.241e-06 -5.3915e-08 v ǁVelocityǁ 0.0007732 45.317 8.7513 8.2027 v Pressure -4.232e+05 1.2204e+05 -1.5447e+05 -1.2139e+05 v TurbVisc 2.0448e-19 0.026389 0.00021016 6.7671e-05 v CourantNb 1.5034e-08 0.011462 0.00017057 4.9704e-06 v FourierNb 1.2448e-07 0.037615 0.00015138 5.9514e-07 v total_pressure -3.2188e+05 2.2337e+05 -53145 -20061 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1123 0.11512 0.0030619 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.4531e-07 0.043158 0.00032195 5.5656e-06 INSTANT 0.876504000E-01 TIME STEP NUMBER 56702 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283031561E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.843675333E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19325E-01 0.21483E+01 Friction velocity uk : 0.19325E-01 0.21483E+01 Dimensionless distance yplus : 0.18736E-01 0.21124E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -9.905112664e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29493E+08 1 0.19079E-09 0.34525E+02 0.22156E+04 c Velocity[X] 0.19741E+02 c Velocity[Y] 0.14784E+02 c Velocity[Z] 0.94761E-06 c Pressure 0.93216E-04 78 0.87226E-04 0.66799E-03 0.48480E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -30.938 45.083 5.6087 8.0002 v Velocity[Y] -32.544 34.819 -0.16953 -0.074775 v Velocity[Z] -3.0955 3.1472 2.2405e-06 -5.3915e-08 v ǁVelocityǁ 0.0010205 45.328 8.7528 8.2028 v Pressure -4.2381e+05 1.2167e+05 -1.5499e+05 -1.2164e+05 v TurbVisc 1.208e-19 0.026404 0.00021023 6.776e-05 v CourantNb 1.5541e-08 0.011463 0.00017057 4.9704e-06 v FourierNb 1.2448e-07 0.037589 0.0001514 5.9575e-07 v total_pressure -3.2249e+05 2.2299e+05 -53670 -20316 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1124 0.11515 0.0030622 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.4534e-07 0.043132 0.00032197 5.5662e-06 INSTANT 0.876505000E-01 TIME STEP NUMBER 56703 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283024637E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.843321742E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.21004E-01 0.21484E+01 Friction velocity uk : 0.21004E-01 0.21484E+01 Dimensionless distance yplus : 0.20364E-01 0.21125E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.019997887e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29492E+08 1 0.19081E-09 0.34543E+02 0.22161E+04 c Velocity[X] 0.19760E+02 c Velocity[Y] 0.14782E+02 c Velocity[Z] 0.94034E-06 c Pressure 0.92316E-04 53 0.76069E-04 0.66120E-03 0.40259E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -30.951 45.093 5.6086 8.0001 v Velocity[Y] -32.553 34.83 -0.16961 -0.075021 v Velocity[Z] -3.0959 3.1474 2.24e-06 -5.3915e-08 v ǁVelocityǁ 0.00079265 45.338 8.7542 8.2029 v Pressure -4.2437e+05 1.2134e+05 -1.5551e+05 -1.2206e+05 v TurbVisc 1.2232e-19 0.026419 0.00021029 6.785e-05 v CourantNb 1.7482e-08 0.011463 0.00017058 4.9704e-06 v FourierNb 1.2449e-07 0.037562 0.00015142 5.9636e-07 v total_pressure -3.2305e+05 2.2266e+05 -54183 -20734 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1125 0.11517 0.0030625 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.4537e-07 0.043106 0.000322 5.5667e-06 INSTANT 0.876506000E-01 TIME STEP NUMBER 56704 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283017862E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.842965755E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15219E-01 0.21484E+01 Friction velocity uk : 0.15219E-01 0.21484E+01 Dimensionless distance yplus : 0.15077E-01 0.21125E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.043952834e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29492E+08 1 0.19084E-09 0.34579E+02 0.22172E+04 c Velocity[X] 0.19777E+02 c Velocity[Y] 0.14802E+02 c Velocity[Z] 0.94220E-06 c Pressure 0.84129E-04 7 0.54901E-04 0.60225E-03 0.25833E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -30.963 45.103 5.6085 7.9999 v Velocity[Y] -32.563 34.842 -0.16969 -0.075268 v Velocity[Z] -3.0962 3.1475 2.2396e-06 -5.3915e-08 v ǁVelocityǁ 0.00053756 45.348 8.7557 8.2029 v Pressure -4.2483e+05 1.2112e+05 -1.5591e+05 -1.2228e+05 v TurbVisc 1.3244e-19 0.026434 0.00021035 6.7939e-05 v CourantNb 2.0982e-08 0.011464 0.00017058 4.9704e-06 v FourierNb 1.2449e-07 0.037536 0.00015144 5.9697e-07 v total_pressure -3.235e+05 2.2245e+05 -54587 -20958 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1125 0.11519 0.0030628 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.4539e-07 0.043079 0.00032202 5.5673e-06 INSTANT 0.876507000E-01 TIME STEP NUMBER 56705 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283011137E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.842606667E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.61952E-02 0.21485E+01 Friction velocity uk : 0.61952E-02 0.21485E+01 Dimensionless distance yplus : 0.60652E-02 0.21125E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.074991106e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29492E+08 1 0.19086E-09 0.34602E+02 0.22178E+04 c Velocity[X] 0.19799E+02 c Velocity[Y] 0.14804E+02 c Velocity[Z] 0.94021E-06 c Pressure 0.84825E-04 39 0.98299E-04 0.60692E-03 0.28072E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -30.975 45.113 5.6084 7.9998 v Velocity[Y] -32.572 34.853 -0.16978 -0.075515 v Velocity[Z] -3.0966 3.1477 2.2391e-06 -5.3915e-08 v ǁVelocityǁ 0.00036824 45.358 8.7571 8.203 v Pressure -4.2534e+05 1.2085e+05 -1.5636e+05 -1.2263e+05 v TurbVisc 1.3878e-19 0.02645 0.00021042 6.8028e-05 v CourantNb 2.4912e-08 0.011464 0.00017059 4.9704e-06 v FourierNb 1.2449e-07 0.03751 0.00015146 5.9758e-07 v total_pressure -3.2402e+05 2.2217e+05 -55033 -21303 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1125 0.11521 0.0030631 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.4542e-07 0.043052 0.00032205 5.5679e-06 INSTANT 0.876508000E-01 TIME STEP NUMBER 56706 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283004258E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.842240762E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.29434E-02 0.21485E+01 Friction velocity uk : 0.29434E-02 0.21485E+01 Dimensionless distance yplus : 0.28816E-02 0.21126E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.086771760e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29491E+08 1 0.19089E-09 0.34630E+02 0.22186E+04 c Velocity[X] 0.19819E+02 c Velocity[Y] 0.14812E+02 c Velocity[Z] 0.92702E-06 c Pressure 0.81847E-04 20 0.82429E-04 0.58531E-03 0.22061E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -30.987 45.123 5.6083 7.9996 v Velocity[Y] -32.581 34.865 -0.16986 -0.075762 v Velocity[Z] -3.097 3.1478 2.2386e-06 -5.3915e-08 v ǁVelocityǁ 0.00036637 45.368 8.7586 8.2031 v Pressure -4.2582e+05 1.206e+05 -1.5672e+05 -1.2289e+05 v TurbVisc 1.4082e-19 0.026465 0.00021048 6.8118e-05 v CourantNb 2.7924e-08 0.011465 0.00017059 4.9703e-06 v FourierNb 1.2449e-07 0.037483 0.00015148 5.9819e-07 v total_pressure -3.2449e+05 2.2192e+05 -55393 -21566 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1126 0.11522 0.0030631 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.4545e-07 0.043026 0.00032208 5.5685e-06 INSTANT 0.876509000E-01 TIME STEP NUMBER 56707 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282997387E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.841875540E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.45232E-02 0.21486E+01 Friction velocity uk : 0.45232E-02 0.21486E+01 Dimensionless distance yplus : 0.43516E-02 0.21127E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.114450533e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29491E+08 1 0.19091E-09 0.34666E+02 0.22197E+04 c Velocity[X] 0.19837E+02 c Velocity[Y] 0.14829E+02 c Velocity[Z] 0.92762E-06 c Pressure 0.78089E-04 7 0.54669E-04 0.55815E-03 0.21953E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -30.999 45.133 5.6082 7.9995 v Velocity[Y] -32.591 34.876 -0.16994 -0.076008 v Velocity[Z] -3.0973 3.148 2.2381e-06 -5.3915e-08 v ǁVelocityǁ 0.0005238 45.378 8.76 8.2032 v Pressure -4.2622e+05 1.2043e+05 -1.5699e+05 -1.2304e+05 v TurbVisc 1.5472e-19 0.02648 0.00021054 6.8207e-05 v CourantNb 3.1794e-08 0.011465 0.0001706 4.9703e-06 v FourierNb 1.2449e-07 0.037457 0.00015151 5.988e-07 v total_pressure -3.249e+05 2.2176e+05 -55661 -21713 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1127 0.11525 0.0030636 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.4548e-07 0.042999 0.0003221 5.5691e-06 INSTANT 0.876510000E-01 TIME STEP NUMBER 56708 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282990489E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.841508433E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.14313E-01 0.21486E+01 Friction velocity uk : 0.14313E-01 0.21486E+01 Dimensionless distance yplus : 0.13770E-01 0.21127E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.138022269e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29490E+08 1 0.19093E-09 0.34695E+02 0.22206E+04 c Velocity[X] 0.19856E+02 c Velocity[Y] 0.14839E+02 c Velocity[Z] 0.92390E-06 c Pressure 0.80042E-04 30 0.75618E-04 0.57181E-03 0.51719E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -31.011 45.143 5.608 7.9993 v Velocity[Y] -32.6 34.888 -0.17002 -0.076257 v Velocity[Z] -3.0977 3.1481 2.2376e-06 -5.3915e-08 v ǁVelocityǁ 0.00079781 45.388 8.7615 8.2033 v Pressure -4.2664e+05 1.2024e+05 -1.5738e+05 -1.2352e+05 v TurbVisc 1.4323e-19 0.026495 0.0002106 6.8297e-05 v CourantNb 3.5501e-08 0.011466 0.0001706 4.9703e-06 v FourierNb 1.2449e-07 0.03743 0.00015153 5.9941e-07 v total_pressure -3.2531e+05 2.2157e+05 -56051 -22198 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1127 0.11528 0.0030643 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.4551e-07 0.042972 0.00032213 5.5697e-06 INSTANT 0.876511000E-01 TIME STEP NUMBER 56709 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282983684E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.841136080E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.16284E-01 0.21486E+01 Friction velocity uk : 0.16284E-01 0.21486E+01 Dimensionless distance yplus : 0.15686E-01 0.21127E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.144152981e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29490E+08 1 0.19096E-09 0.34725E+02 0.22214E+04 c Velocity[X] 0.19872E+02 c Velocity[Y] 0.14853E+02 c Velocity[Z] 0.91644E-06 c Pressure 0.79456E-04 54 0.80195E-04 0.56733E-03 0.42266E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -31.024 45.152 5.6079 7.9992 v Velocity[Y] -32.609 34.899 -0.1701 -0.076504 v Velocity[Z] -3.0981 3.1482 2.2371e-06 -5.3915e-08 v ǁVelocityǁ 0.0010812 45.398 8.7629 8.2033 v Pressure -4.2696e+05 1.2016e+05 -1.5755e+05 -1.2359e+05 v TurbVisc 1.5392e-19 0.02651 0.00021066 6.8386e-05 v CourantNb 3.9256e-08 0.011466 0.0001706 4.9703e-06 v FourierNb 1.245e-07 0.037403 0.00015155 6.0002e-07 v total_pressure -3.2563e+05 2.2148e+05 -56223 -22261 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1127 0.1153 0.0030646 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.4554e-07 0.042946 0.00032215 5.5703e-06 INSTANT 0.876512000E-01 TIME STEP NUMBER 56710 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282976664E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.840769562E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12983E-01 0.21487E+01 Friction velocity uk : 0.12983E-01 0.21487E+01 Dimensionless distance yplus : 0.12506E-01 0.21128E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.167467634e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29490E+08 1 0.19098E-09 0.34757E+02 0.22224E+04 c Velocity[X] 0.19890E+02 c Velocity[Y] 0.14866E+02 c Velocity[Z] 0.91692E-06 c Pressure 0.80224E-04 120 0.93236E-04 0.57253E-03 0.49929E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -31.036 45.162 5.6078 7.999 v Velocity[Y] -32.618 34.911 -0.17018 -0.076755 v Velocity[Z] -3.0984 3.1484 2.2366e-06 -5.3915e-08 v ǁVelocityǁ 0.0013765 45.408 8.7643 8.2034 v Pressure -4.2717e+05 1.2018e+05 -1.5773e+05 -1.2377e+05 v TurbVisc 1.5491e-19 0.026525 0.00021073 6.8476e-05 v CourantNb 4.3182e-08 0.011467 0.00017061 4.9703e-06 v FourierNb 1.245e-07 0.037376 0.00015157 6.0063e-07 v total_pressure -3.2584e+05 2.2151e+05 -56403 -22446 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1128 0.11533 0.003065 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.4557e-07 0.042919 0.00032218 5.5709e-06 INSTANT 0.876513000E-01 TIME STEP NUMBER 56711 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282969933E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.840398705E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.83971E-02 0.21487E+01 Friction velocity uk : 0.83971E-02 0.21487E+01 Dimensionless distance yplus : 0.80884E-02 0.21128E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.184185868e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29489E+08 1 0.19101E-09 0.34769E+02 0.22227E+04 c Velocity[X] 0.19907E+02 c Velocity[Y] 0.14863E+02 c Velocity[Z] 0.91850E-06 c Pressure 0.81426E-04 95 0.78990E-04 0.58080E-03 0.29602E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -31.048 45.172 5.6077 7.9989 v Velocity[Y] -32.627 34.922 -0.17026 -0.077005 v Velocity[Z] -3.0988 3.1485 2.2361e-06 -5.3915e-08 v ǁVelocityǁ 0.001677 45.418 8.7658 8.2035 v Pressure -4.2744e+05 1.2015e+05 -1.5786e+05 -1.2386e+05 v TurbVisc 1.6416e-19 0.02654 0.00021079 6.8566e-05 v CourantNb 4.7042e-08 0.011467 0.00017061 4.9702e-06 v FourierNb 1.245e-07 0.037349 0.00015159 6.0124e-07 v total_pressure -3.2612e+05 2.2147e+05 -56532 -22535 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1128 0.11535 0.0030654 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.456e-07 0.042892 0.00032221 5.5715e-06 INSTANT 0.876514000E-01 TIME STEP NUMBER 56712 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282963032E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.840025192E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.47617E-02 0.21487E+01 Friction velocity uk : 0.47617E-02 0.21487E+01 Dimensionless distance yplus : 0.45867E-02 0.21128E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.195729505e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29489E+08 1 0.19104E-09 0.34804E+02 0.22237E+04 c Velocity[X] 0.19922E+02 c Velocity[Y] 0.14882E+02 c Velocity[Z] 0.91203E-06 c Pressure 0.73858E-04 6 0.56549E-04 0.52655E-03 0.21000E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -31.059 45.182 5.6075 7.9987 v Velocity[Y] -32.636 34.933 -0.17034 -0.077254 v Velocity[Z] -3.0992 3.1487 2.2356e-06 -5.3915e-08 v ǁVelocityǁ 0.0019662 45.428 8.7672 8.2036 v Pressure -4.2761e+05 1.2043e+05 -1.5791e+05 -1.2393e+05 v TurbVisc 1.6646e-19 0.026556 0.00021085 6.8655e-05 v CourantNb 5.0944e-08 0.011468 0.00017062 4.9702e-06 v FourierNb 1.245e-07 0.037322 0.00015161 6.0186e-07 v total_pressure -3.2629e+05 2.2175e+05 -56589 -22607 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1128 0.11537 0.0030657 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.4605e-07 0.042864 0.00032223 5.5721e-06 INSTANT 0.876515000E-01 TIME STEP NUMBER 56713 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282956108E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.839650476E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.46650E-02 0.21488E+01 Friction velocity uk : 0.46650E-02 0.21488E+01 Dimensionless distance yplus : 0.44936E-02 0.21128E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.212354573e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29489E+08 1 0.19105E-09 0.34832E+02 0.22245E+04 c Velocity[X] 0.19941E+02 c Velocity[Y] 0.14890E+02 c Velocity[Z] 0.90636E-06 c Pressure 0.77494E-04 92 0.75046E-04 0.55218E-03 0.42560E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -31.071 45.191 5.6074 7.9986 v Velocity[Y] -32.645 34.945 -0.17043 -0.077506 v Velocity[Z] -3.0996 3.1488 2.2351e-06 -5.3915e-08 v ǁVelocityǁ 0.0020837 45.438 8.7686 8.2037 v Pressure -4.2788e+05 1.207e+05 -1.5806e+05 -1.2421e+05 v TurbVisc 1.6166e-19 0.026571 0.00021091 6.8745e-05 v CourantNb 5.4772e-08 0.011468 0.00017062 4.9702e-06 v FourierNb 1.245e-07 0.037295 0.00015164 6.0247e-07 v total_pressure -3.2655e+05 2.2203e+05 -56735 -22890 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1128 0.11539 0.0030661 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.4654e-07 0.042837 0.00032226 5.5727e-06 INSTANT 0.876516000E-01 TIME STEP NUMBER 56714 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282949331E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.839271084E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.98220E-02 0.21488E+01 Friction velocity uk : 0.98220E-02 0.21488E+01 Dimensionless distance yplus : 0.96431E-02 0.21129E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.213708332e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29488E+08 1 0.19109E-09 0.34860E+02 0.22253E+04 c Velocity[X] 0.19956E+02 c Velocity[Y] 0.14904E+02 c Velocity[Z] 0.90293E-06 c Pressure 0.78402E-04 42 0.80454E-04 0.55837E-03 0.42111E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -31.083 45.201 5.6073 7.9984 v Velocity[Y] -32.655 34.956 -0.17051 -0.077756 v Velocity[Z] -3.0999 3.1489 2.2346e-06 -5.3916e-08 v ǁVelocityǁ 0.0020896 45.448 8.7701 8.2037 v Pressure -4.2798e+05 1.2098e+05 -1.5803e+05 -1.2421e+05 v TurbVisc 1.7682e-19 0.026586 0.00021097 6.8835e-05 v CourantNb 5.8799e-08 0.011468 0.00017063 4.9702e-06 v FourierNb 1.245e-07 0.037268 0.00015166 6.0308e-07 v total_pressure -3.2665e+05 2.2231e+05 -56706 -22882 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1129 0.11541 0.0030665 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.4703e-07 0.04281 0.00032228 5.5733e-06 INSTANT 0.876517000E-01 TIME STEP NUMBER 56715 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282942352E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.838900498E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.48957E-02 0.21488E+01 Friction velocity uk : 0.48957E-02 0.21488E+01 Dimensionless distance yplus : 0.48065E-02 0.21129E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.222837820e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29488E+08 1 0.19111E-09 0.34890E+02 0.22262E+04 c Velocity[X] 0.19973E+02 c Velocity[Y] 0.14917E+02 c Velocity[Z] 0.90339E-06 c Pressure 0.80670E-04 82 0.93029E-04 0.57423E-03 0.47935E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -31.095 45.21 5.6072 7.9983 v Velocity[Y] -32.664 34.967 -0.17059 -0.078009 v Velocity[Z] -3.1003 3.1491 2.2341e-06 -5.3916e-08 v ǁVelocityǁ 0.0021457 45.458 8.7715 8.2038 v Pressure -4.2801e+05 1.2128e+05 -1.5798e+05 -1.2425e+05 v TurbVisc 1.7996e-19 0.026601 0.00021103 6.8925e-05 v CourantNb 6.2783e-08 0.011469 0.00017063 4.9702e-06 v FourierNb 1.2451e-07 0.037241 0.00015168 6.037e-07 v total_pressure -3.2668e+05 2.226e+05 -56651 -22928 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1129 0.11543 0.0030668 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.4753e-07 0.042783 0.00032231 5.5739e-06 INSTANT 0.876518000E-01 TIME STEP NUMBER 56716 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282935699E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.838526834E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.14963E-01 0.21488E+01 Friction velocity uk : 0.14963E-01 0.21488E+01 Dimensionless distance yplus : 0.14451E-01 0.21129E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.229066939e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29487E+08 1 0.19114E-09 0.34901E+02 0.22265E+04 c Velocity[X] 0.19988E+02 c Velocity[Y] 0.14914E+02 c Velocity[Z] 0.89705E-06 c Pressure 0.83333E-04 103 0.79118E-04 0.59288E-03 0.29627E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -31.107 45.22 5.607 7.9982 v Velocity[Y] -32.673 34.978 -0.17067 -0.078262 v Velocity[Z] -3.1007 3.1492 2.2336e-06 -5.3916e-08 v ǁVelocityǁ 0.0022513 45.468 8.7729 8.2039 v Pressure -4.2807e+05 1.2156e+05 -1.5789e+05 -1.2422e+05 v TurbVisc 1.8468e-19 0.026616 0.00021109 6.9015e-05 v CourantNb 6.6723e-08 0.011469 0.00017064 4.9702e-06 v FourierNb 1.2451e-07 0.037214 0.0001517 6.0431e-07 v total_pressure -3.2674e+05 2.2288e+05 -56565 -22898 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1129 0.11545 0.0030672 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.4802e-07 0.042755 0.00032234 5.5745e-06 INSTANT 0.876519000E-01 TIME STEP NUMBER 56717 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282928876E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.838151644E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.88966E-02 0.21489E+01 Friction velocity uk : 0.88966E-02 0.21489E+01 Dimensionless distance yplus : 0.85924E-02 0.21129E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.231284899e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29487E+08 1 0.19117E-09 0.34935E+02 0.22275E+04 c Velocity[X] 0.20002E+02 c Velocity[Y] 0.14932E+02 c Velocity[Z] 0.90542E-06 c Pressure 0.77466E-04 7 0.56853E-04 0.55085E-03 0.20758E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -31.118 45.229 5.6069 7.998 v Velocity[Y] -32.682 34.989 -0.17075 -0.078513 v Velocity[Z] -3.101 3.1494 2.2331e-06 -5.3916e-08 v ǁVelocityǁ 0.0023985 45.478 8.7743 8.204 v Pressure -4.2811e+05 1.2183e+05 -1.5782e+05 -1.2427e+05 v TurbVisc 1.8717e-19 0.026631 0.00021115 6.9105e-05 v CourantNb 7.0669e-08 0.01147 0.00017064 4.9701e-06 v FourierNb 1.2451e-07 0.037186 0.00015172 6.0492e-07 v total_pressure -3.2679e+05 2.2316e+05 -56499 -22948 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1129 0.11547 0.0030675 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.4852e-07 0.042728 0.00032236 5.5751e-06 INSTANT 0.876520000E-01 TIME STEP NUMBER 56718 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282922032E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.837776602E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.28649E-02 0.21489E+01 Friction velocity uk : 0.28649E-02 0.21489E+01 Dimensionless distance yplus : 0.27670E-02 0.21130E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.221816363e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29487E+08 1 0.19119E-09 0.34961E+02 0.22282E+04 c Velocity[X] 0.20019E+02 c Velocity[Y] 0.14942E+02 c Velocity[Z] 0.89470E-06 c Pressure 0.82347E-04 34 0.75267E-04 0.58526E-03 0.37865E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -31.13 45.239 5.6068 7.9979 v Velocity[Y] -32.691 35.001 -0.17083 -0.078768 v Velocity[Z] -3.1014 3.1495 2.2326e-06 -5.3916e-08 v ǁVelocityǁ 0.0025836 45.487 8.7758 8.2041 v Pressure -4.2806e+05 1.2213e+05 -1.5756e+05 -1.2425e+05 v TurbVisc 1.446e-19 0.026646 0.00021121 6.9195e-05 v CourantNb 7.4754e-08 0.01147 0.00017064 4.9701e-06 v FourierNb 1.2451e-07 0.037159 0.00015174 6.0554e-07 v total_pressure -3.2673e+05 2.2346e+05 -56237 -22923 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.113 0.11549 0.0030678 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.4901e-07 0.0427 0.00032239 5.5757e-06 INSTANT 0.876521000E-01 TIME STEP NUMBER 56719 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282915408E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.837407722E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11018E-01 0.21489E+01 Friction velocity uk : 0.11018E-01 0.21489E+01 Dimensionless distance yplus : 0.10642E-01 0.21130E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.237866137e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29486E+08 1 0.19122E-09 0.34987E+02 0.22290E+04 c Velocity[X] 0.20032E+02 c Velocity[Y] 0.14956E+02 c Velocity[Z] 0.88874E-06 c Pressure 0.84666E-04 47 0.80729E-04 0.60143E-03 0.43132E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -31.142 45.248 5.6067 7.9977 v Velocity[Y] -32.699 35.012 -0.17091 -0.079021 v Velocity[Z] -3.1018 3.1496 2.2321e-06 -5.3916e-08 v ǁVelocityǁ 0.0027949 45.497 8.7772 8.2041 v Pressure -4.2799e+05 1.2241e+05 -1.5738e+05 -1.2415e+05 v TurbVisc 1.8393e-19 0.026661 0.00021127 6.9285e-05 v CourantNb 7.8556e-08 0.011471 0.00017065 4.9701e-06 v FourierNb 1.2451e-07 0.037132 0.00015177 6.0616e-07 v total_pressure -3.2667e+05 2.2374e+05 -56055 -22829 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.113 0.11552 0.0030683 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.4951e-07 0.042673 0.00032242 5.5763e-06 INSTANT 0.876522000E-01 TIME STEP NUMBER 56720 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282908570E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.837029821E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.16158E-01 0.21490E+01 Friction velocity uk : 0.16158E-01 0.21490E+01 Dimensionless distance yplus : 0.15606E-01 0.21130E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.226283720e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29486E+08 1 0.19124E-09 0.35017E+02 0.22298E+04 c Velocity[X] 0.20048E+02 c Velocity[Y] 0.14968E+02 c Velocity[Z] 0.88919E-06 c Pressure 0.88065E-04 92 0.93285E-04 0.62526E-03 0.47992E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -31.153 45.258 5.6065 7.9976 v Velocity[Y] -32.708 35.023 -0.17099 -0.079277 v Velocity[Z] -3.1021 3.1498 2.2317e-06 -5.3916e-08 v ǁVelocityǁ 0.0028727 45.507 8.7786 8.2042 v Pressure -4.2784e+05 1.2271e+05 -1.5712e+05 -1.2411e+05 v TurbVisc 1.9244e-19 0.026676 0.00021133 6.9376e-05 v CourantNb 8.2105e-08 0.011471 0.00017065 4.9701e-06 v FourierNb 1.2451e-07 0.037104 0.00015179 6.0677e-07 v total_pressure -3.2652e+05 2.2404e+05 -55795 -22783 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.113 0.11554 0.0030687 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.5001e-07 0.042645 0.00032244 5.5769e-06 INSTANT 0.876523000E-01 TIME STEP NUMBER 56721 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282902080E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.836657111E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.78975E-02 0.21490E+01 Friction velocity uk : 0.78975E-02 0.21490E+01 Dimensionless distance yplus : 0.76440E-02 0.21131E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.219096911e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29486E+08 1 0.19128E-09 0.35027E+02 0.22301E+04 c Velocity[X] 0.20061E+02 c Velocity[Y] 0.14965E+02 c Velocity[Z] 0.88241E-06 c Pressure 0.91747E-04 105 0.79425E-04 0.65106E-03 0.32924E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -31.165 45.267 5.6064 7.9974 v Velocity[Y] -32.717 35.034 -0.17107 -0.079532 v Velocity[Z] -3.1025 3.1499 2.2312e-06 -5.3916e-08 v ǁVelocityǁ 0.0027981 45.516 8.78 8.2043 v Pressure -4.277e+05 1.23e+05 -1.5681e+05 -1.2393e+05 v TurbVisc 2.044e-19 0.026691 0.00021139 6.9466e-05 v CourantNb 8.2172e-08 0.011472 0.00017066 4.9701e-06 v FourierNb 1.2452e-07 0.037077 0.00015181 6.0739e-07 v total_pressure -3.2637e+05 2.2432e+05 -55482 -22609 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1131 0.11555 0.003069 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.5051e-07 0.042618 0.00032247 5.5775e-06 INSTANT 0.876524000E-01 TIME STEP NUMBER 56722 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282895441E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.836285105E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.50144E-02 0.21490E+01 Friction velocity uk : 0.50144E-02 0.21490E+01 Dimensionless distance yplus : 0.48534E-02 0.21131E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.209812461e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29485E+08 1 0.19130E-09 0.35059E+02 0.22310E+04 c Velocity[X] 0.20076E+02 c Velocity[Y] 0.14983E+02 c Velocity[Z] 0.88338E-06 c Pressure 0.87651E-04 7 0.56680E-04 0.62167E-03 0.21303E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -31.176 45.277 5.6063 7.9973 v Velocity[Y] -32.726 35.045 -0.17115 -0.079787 v Velocity[Z] -3.1029 3.1501 2.2307e-06 -5.3916e-08 v ǁVelocityǁ 0.0027314 45.526 8.7814 8.2044 v Pressure -4.2758e+05 1.2328e+05 -1.5653e+05 -1.2392e+05 v TurbVisc 2.0592e-19 0.026707 0.00021145 6.9556e-05 v CourantNb 8.2234e-08 0.011472 0.00017066 4.9701e-06 v FourierNb 1.2452e-07 0.037049 0.00015183 6.08e-07 v total_pressure -3.2626e+05 2.2461e+05 -55208 -22591 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1131 0.11557 0.0030693 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.5102e-07 0.04259 0.00032249 5.5781e-06 INSTANT 0.876525000E-01 TIME STEP NUMBER 56723 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282888801E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.835914269E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13524E-01 0.21491E+01 Friction velocity uk : 0.13524E-01 0.21491E+01 Dimensionless distance yplus : 0.13319E-01 0.21132E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.191232140e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29485E+08 1 0.19132E-09 0.35084E+02 0.22317E+04 c Velocity[X] 0.20090E+02 c Velocity[Y] 0.14994E+02 c Velocity[Z] 0.87664E-06 c Pressure 0.93122E-04 53 0.75825E-04 0.66014E-03 0.41719E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -31.188 45.286 5.6062 7.9971 v Velocity[Y] -32.735 35.056 -0.17123 -0.080044 v Velocity[Z] -3.1032 3.1502 2.2302e-06 -5.3916e-08 v ǁVelocityǁ 0.0026602 45.536 8.7829 8.2045 v Pressure -4.273e+05 1.2359e+05 -1.5605e+05 -1.2372e+05 v TurbVisc 2.248e-19 0.026722 0.00021151 6.9647e-05 v CourantNb 8.2392e-08 0.011473 0.00017067 4.97e-06 v FourierNb 1.2452e-07 0.037064 0.00015186 6.0862e-07 v total_pressure -3.2597e+05 2.2491e+05 -54728 -22395 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1132 0.1156 0.0030698 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.5152e-07 0.042563 0.00032252 5.5787e-06 INSTANT 0.876526000E-01 TIME STEP NUMBER 56724 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282882394E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.835550425E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.50637E-02 0.21491E+01 Friction velocity uk : 0.50637E-02 0.21491E+01 Dimensionless distance yplus : 0.49869E-02 0.21132E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.190094711e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29485E+08 1 0.19136E-09 0.35109E+02 0.22325E+04 c Velocity[X] 0.20102E+02 c Velocity[Y] 0.15008E+02 c Velocity[Z] 0.87848E-06 c Pressure 0.96322E-04 104 0.81491E-04 0.68247E-03 0.47157E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -31.199 45.296 5.6061 7.997 v Velocity[Y] -32.744 35.067 -0.17131 -0.080299 v Velocity[Z] -3.1036 3.1503 2.2297e-06 -5.3916e-08 v ǁVelocityǁ 0.0025955 45.545 8.7843 8.2046 v Pressure -4.2704e+05 1.2387e+05 -1.5564e+05 -1.2349e+05 v TurbVisc 2.1622e-19 0.026737 0.00021157 6.9737e-05 v CourantNb 8.2233e-08 0.011473 0.00017067 4.97e-06 v FourierNb 1.2452e-07 0.037081 0.00015188 6.0924e-07 v total_pressure -3.2571e+05 2.252e+05 -54320 -22161 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1132 0.11563 0.0030703 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.5203e-07 0.042535 0.00032255 5.5793e-06 INSTANT 0.876527000E-01 TIME STEP NUMBER 56725 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282875797E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.835180064E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13220E-01 0.21492E+01 Friction velocity uk : 0.13220E-01 0.21492E+01 Dimensionless distance yplus : 0.13020E-01 0.21133E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.170580377e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29484E+08 1 0.19138E-09 0.35138E+02 0.22333E+04 c Velocity[X] 0.20117E+02 c Velocity[Y] 0.15021E+02 c Velocity[Z] 0.87307E-06 c Pressure 0.10037E-03 115 0.94374E-04 0.71082E-03 0.49711E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -31.211 45.305 5.6059 7.9969 v Velocity[Y] -32.753 35.078 -0.1714 -0.080559 v Velocity[Z] -3.104 3.1505 2.2292e-06 -5.3916e-08 v ǁVelocityǁ 0.0025347 45.555 8.7857 8.2046 v Pressure -4.2671e+05 1.2418e+05 -1.5518e+05 -1.2336e+05 v TurbVisc 2.2287e-19 0.026752 0.00021163 6.9828e-05 v CourantNb 8.2373e-08 0.011474 0.00017068 4.97e-06 v FourierNb 1.2452e-07 0.037098 0.0001519 6.0986e-07 v total_pressure -3.2539e+05 2.2551e+05 -53859 -22039 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1133 0.11566 0.0030708 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.5254e-07 0.042507 0.00032257 5.5799e-06 INSTANT 0.876528000E-01 TIME STEP NUMBER 56726 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282869562E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.834814052E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.20439E-01 0.21493E+01 Friction velocity uk : 0.20439E-01 0.21493E+01 Dimensionless distance yplus : 0.19673E-01 0.21133E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.152250052e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29484E+08 1 0.19142E-09 0.35147E+02 0.22335E+04 c Velocity[X] 0.20129E+02 c Velocity[Y] 0.15017E+02 c Velocity[Z] 0.86774E-06 c Pressure 0.10460E-03 85 0.80414E-04 0.74033E-03 0.39475E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -31.222 45.314 5.6058 7.9967 v Velocity[Y] -32.761 35.089 -0.17148 -0.080816 v Velocity[Z] -3.1043 3.1506 2.2287e-06 -5.3916e-08 v ǁVelocityǁ 0.0024792 45.565 8.7871 8.2047 v Pressure -4.2637e+05 1.2462e+05 -1.5465e+05 -1.2304e+05 v TurbVisc 2.2578e-19 0.026767 0.00021169 6.9919e-05 v CourantNb 8.2435e-08 0.011474 0.00017068 4.97e-06 v FourierNb 1.2452e-07 0.037115 0.00015192 6.1047e-07 v total_pressure -3.2505e+05 2.2595e+05 -53326 -21714 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1133 0.11569 0.0030713 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.5304e-07 0.042479 0.0003226 5.5805e-06 INSTANT 0.876529000E-01 TIME STEP NUMBER 56727 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282863202E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.834450877E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.22187E-01 0.21493E+01 Friction velocity uk : 0.22187E-01 0.21493E+01 Dimensionless distance yplus : 0.21355E-01 0.21134E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.132413574e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29484E+08 1 0.19144E-09 0.35178E+02 0.22344E+04 c Velocity[X] 0.20143E+02 c Velocity[Y] 0.15036E+02 c Velocity[Z] 0.87552E-06 c Pressure 0.10179E-03 7 0.57559E-04 0.72007E-03 0.23758E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -31.234 45.324 5.6057 7.9966 v Velocity[Y] -32.77 35.1 -0.17156 -0.081074 v Velocity[Z] -3.1047 3.1508 2.2282e-06 -5.3916e-08 v ǁVelocityǁ 0.0024365 45.574 8.7885 8.2048 v Pressure -4.2608e+05 1.2513e+05 -1.5416e+05 -1.2292e+05 v TurbVisc 2.3204e-19 0.026782 0.00021175 7.0009e-05 v CourantNb 8.2479e-08 0.011475 0.00017068 4.97e-06 v FourierNb 1.2453e-07 0.037133 0.00015194 6.1109e-07 v total_pressure -3.2476e+05 2.2646e+05 -52832 -21599 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1134 0.11572 0.0030717 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.5356e-07 0.042452 0.00032263 5.5811e-06 INSTANT 0.876530000E-01 TIME STEP NUMBER 56728 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282856863E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.834090076E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.18884E-01 0.21495E+01 Friction velocity uk : 0.18884E-01 0.21495E+01 Dimensionless distance yplus : 0.18176E-01 0.21135E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.104106971e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29483E+08 1 0.19147E-09 0.35202E+02 0.22351E+04 c Velocity[X] 0.20155E+02 c Velocity[Y] 0.15047E+02 c Velocity[Z] 0.87003E-06 c Pressure 0.10742E-03 110 0.76561E-04 0.75952E-03 0.47330E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -31.245 45.333 5.6056 7.9965 v Velocity[Y] -32.779 35.111 -0.17164 -0.081334 v Velocity[Z] -3.1051 3.1509 2.2277e-06 -5.3916e-08 v ǁVelocityǁ 0.002367 45.584 8.7899 8.2049 v Pressure -4.2559e+05 1.2585e+05 -1.5349e+05 -1.2259e+05 v TurbVisc 2.3304e-19 0.026797 0.00021181 7.01e-05 v CourantNb 8.2632e-08 0.011475 0.00017069 4.97e-06 v FourierNb 1.2453e-07 0.03715 0.00015197 6.1171e-07 v total_pressure -3.2426e+05 2.2718e+05 -52163 -21265 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1135 0.11574 0.003072 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.5407e-07 0.042425 0.00032265 5.5817e-06 INSTANT 0.876531000E-01 TIME STEP NUMBER 56729 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282850764E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.833736297E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.17005E-01 0.21495E+01 Friction velocity uk : 0.17005E-01 0.21495E+01 Dimensionless distance yplus : 0.16368E-01 0.21136E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.091811470e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29483E+08 1 0.19151E-09 0.35227E+02 0.22358E+04 c Velocity[X] 0.20166E+02 c Velocity[Y] 0.15061E+02 c Velocity[Z] 0.86101E-06 c Pressure 0.11099E-03 57 0.82384E-04 0.78438E-03 0.51566E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -31.257 45.342 5.6055 7.9963 v Velocity[Y] -32.788 35.122 -0.17173 -0.081592 v Velocity[Z] -3.1054 3.151 2.2272e-06 -5.3916e-08 v ǁVelocityǁ 0.0022297 45.593 8.7914 8.205 v Pressure -4.2516e+05 1.2651e+05 -1.5287e+05 -1.2225e+05 v TurbVisc 2.5423e-19 0.026812 0.00021187 7.0191e-05 v CourantNb 8.2529e-08 0.011476 0.00017069 4.9699e-06 v FourierNb 1.2453e-07 0.037167 0.00015199 6.1233e-07 v total_pressure -3.2383e+05 2.2783e+05 -51540 -20923 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1136 0.11577 0.0030725 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.5458e-07 0.042396 0.00032268 5.5823e-06 INSTANT 0.876532000E-01 TIME STEP NUMBER 56730 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282844500E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.833378599E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.17804E-01 0.21496E+01 Friction velocity uk : 0.17804E-01 0.21496E+01 Dimensionless distance yplus : 0.17136E-01 0.21137E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.064635142e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29483E+08 1 0.19153E-09 0.35256E+02 0.22366E+04 c Velocity[X] 0.20180E+02 c Velocity[Y] 0.15075E+02 c Velocity[Z] 0.85991E-06 c Pressure 0.11525E-03 228 0.95519E-04 0.81409E-03 0.54288E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -31.268 45.352 5.6054 7.9962 v Velocity[Y] -32.797 35.133 -0.17181 -0.081854 v Velocity[Z] -3.1058 3.1512 2.2268e-06 -5.3917e-08 v ǁVelocityǁ 0.0021546 45.603 8.7928 8.2051 v Pressure -4.2461e+05 1.2727e+05 -1.5218e+05 -1.2196e+05 v TurbVisc 2.4369e-19 0.026827 0.00021193 7.0282e-05 v CourantNb 8.2571e-08 0.011476 0.0001707 4.9699e-06 v FourierNb 1.2453e-07 0.037185 0.00015201 6.1295e-07 v total_pressure -3.2329e+05 2.286e+05 -50855 -20633 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1137 0.11579 0.0030729 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.551e-07 0.042369 0.00032271 5.5829e-06 INSTANT 0.876533000E-01 TIME STEP NUMBER 56731 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282838626E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.833025363E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.16601E-01 0.21497E+01 Friction velocity uk : 0.16601E-01 0.21497E+01 Dimensionless distance yplus : 0.16053E-01 0.21138E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.036282460e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29483E+08 1 0.19157E-09 0.35263E+02 0.22367E+04 c Velocity[X] 0.20192E+02 c Velocity[Y] 0.15071E+02 c Velocity[Z] 0.85657E-06 c Pressure 0.11966E-03 74 0.81255E-04 0.84479E-03 0.40939E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -31.279 45.361 5.6053 7.9961 v Velocity[Y] -32.805 35.144 -0.17189 -0.082115 v Velocity[Z] -3.1062 3.1513 2.2263e-06 -5.3917e-08 v ǁVelocityǁ 0.0021438 45.612 8.7942 8.2052 v Pressure -4.2414e+05 1.2797e+05 -1.5147e+05 -1.2161e+05 v TurbVisc 2.5313e-19 0.026842 0.00021198 7.0373e-05 v CourantNb 8.2614e-08 0.011477 0.0001707 4.9699e-06 v FourierNb 1.2453e-07 0.037203 0.00015203 6.1357e-07 v total_pressure -3.2281e+05 2.293e+05 -50149 -20284 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1138 0.11581 0.0030733 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.5562e-07 0.042341 0.00032273 5.5835e-06 INSTANT 0.876534000E-01 TIME STEP NUMBER 56732 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282832621E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.832675135E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10736E-01 0.21498E+01 Friction velocity uk : 0.10736E-01 0.21498E+01 Dimensionless distance yplus : 0.10334E-01 0.21139E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.010243393e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29482E+08 1 0.19160E-09 0.35295E+02 0.22376E+04 c Velocity[X] 0.20205E+02 c Velocity[Y] 0.15089E+02 c Velocity[Z] 0.87571E-06 c Pressure 0.11764E-03 15 0.58026E-04 0.83006E-03 0.30849E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -31.291 45.37 5.6052 7.9959 v Velocity[Y] -32.814 35.155 -0.17198 -0.082375 v Velocity[Z] -3.1065 3.1514 2.2258e-06 -5.3917e-08 v ǁVelocityǁ 0.0021829 45.622 8.7956 8.2053 v Pressure -4.2365e+05 1.2868e+05 -1.5074e+05 -1.2133e+05 v TurbVisc 2.5529e-19 0.026857 0.00021204 7.0464e-05 v CourantNb 8.2632e-08 0.011477 0.00017071 4.9699e-06 v FourierNb 1.2454e-07 0.037221 0.00015205 6.1419e-07 v total_pressure -3.2233e+05 2.3001e+05 -49414 -20004 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1139 0.11583 0.0030737 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.5614e-07 0.042314 0.00032276 5.5841e-06 INSTANT 0.876535000E-01 TIME STEP NUMBER 56733 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282826698E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.832330069E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.90521E-02 0.21500E+01 Friction velocity uk : 0.90521E-02 0.21500E+01 Dimensionless distance yplus : 0.87129E-02 0.21140E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -9.729402417e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29482E+08 1 0.19162E-09 0.35318E+02 0.22383E+04 c Velocity[X] 0.20216E+02 c Velocity[Y] 0.15102E+02 c Velocity[Z] 0.86265E-06 c Pressure 0.12321E-03 261 0.77647E-04 0.86890E-03 0.53960E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -31.302 45.379 5.6051 7.9958 v Velocity[Y] -32.823 35.166 -0.17206 -0.082638 v Velocity[Z] -3.1069 3.1516 2.2253e-06 -5.3917e-08 v ǁVelocityǁ 0.0022022 45.632 8.797 8.2054 v Pressure -4.2295e+05 1.296e+05 -1.4992e+05 -1.2087e+05 v TurbVisc 2.1866e-19 0.026872 0.0002121 7.0555e-05 v CourantNb 8.2504e-08 0.011478 0.00017071 4.9699e-06 v FourierNb 1.2454e-07 0.037239 0.00015207 6.1482e-07 v total_pressure -3.2163e+05 2.3092e+05 -48591 -19546 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.114 0.11585 0.003074 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.5666e-07 0.042286 0.00032279 5.5847e-06 INSTANT 0.876536000E-01 TIME STEP NUMBER 56734 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282820981E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.831990471E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15068E-01 0.21501E+01 Friction velocity uk : 0.15068E-01 0.21501E+01 Dimensionless distance yplus : 0.14504E-01 0.21142E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -9.548198308e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29482E+08 1 0.19166E-09 0.35343E+02 0.22390E+04 c Velocity[X] 0.20229E+02 c Velocity[Y] 0.15114E+02 c Velocity[Z] 0.85409E-06 c Pressure 0.12680E-03 390 0.83534E-04 0.89377E-03 0.57307E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -31.313 45.388 5.605 7.9957 v Velocity[Y] -32.831 35.177 -0.17215 -0.082898 v Velocity[Z] -3.1073 3.1517 2.2248e-06 -5.3917e-08 v ǁVelocityǁ 0.0019253 45.641 8.7984 8.2055 v Pressure -4.2234e+05 1.3044e+05 -1.4907e+05 -1.204e+05 v TurbVisc 2.8141e-19 0.026887 0.00021216 7.0646e-05 v CourantNb 8.2726e-08 0.011478 0.00017072 4.9699e-06 v FourierNb 1.2454e-07 0.037258 0.0001521 6.1544e-07 v total_pressure -3.2101e+05 2.3176e+05 -47747 -19079 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1142 0.11588 0.0030745 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.5718e-07 0.042259 0.00032281 5.5853e-06 INSTANT 0.876537000E-01 TIME STEP NUMBER 56735 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282815149E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.831651331E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19588E-01 0.21502E+01 Friction velocity uk : 0.19588E-01 0.21502E+01 Dimensionless distance yplus : 0.18854E-01 0.21143E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -9.208377515e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29482E+08 1 0.19169E-09 0.35371E+02 0.22398E+04 c Velocity[X] 0.20238E+02 c Velocity[Y] 0.15133E+02 c Velocity[Z] 0.84893E-06 c Pressure 0.13105E-03 238 0.96681E-04 0.92328E-03 0.57352E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -31.325 45.398 5.6049 7.9956 v Velocity[Y] -32.84 35.187 -0.17224 -0.083164 v Velocity[Z] -3.1076 3.1519 2.2243e-06 -5.3917e-08 v ǁVelocityǁ 0.0016573 45.65 8.7999 8.2056 v Pressure -4.2169e+05 1.313e+05 -1.4823e+05 -1.2014e+05 v TurbVisc 2.774e-19 0.026902 0.00021222 7.0738e-05 v CourantNb 8.2689e-08 0.011479 0.00017072 4.9699e-06 v FourierNb 1.2454e-07 0.037276 0.00015212 6.1606e-07 v total_pressure -3.2037e+05 2.3263e+05 -46908 -18816 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1143 0.11591 0.0030749 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.5771e-07 0.042231 0.00032284 5.5859e-06 INSTANT 0.876538000E-01 TIME STEP NUMBER 56736 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282809666E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.831315915E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15886E-01 0.21504E+01 Friction velocity uk : 0.15886E-01 0.21504E+01 Dimensionless distance yplus : 0.15291E-01 0.21145E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -8.881935932e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29481E+08 1 0.19172E-09 0.35378E+02 0.22399E+04 c Velocity[X] 0.20253E+02 c Velocity[Y] 0.15125E+02 c Velocity[Z] 0.84529E-06 c Pressure 0.13530E-03 96 0.82484E-04 0.95271E-03 0.54819E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -31.336 45.407 5.6048 7.9954 v Velocity[Y] -32.849 35.198 -0.17232 -0.083427 v Velocity[Z] -3.108 3.152 2.2238e-06 -5.3917e-08 v ǁVelocityǁ 0.0014045 45.66 8.8013 8.2057 v Pressure -4.2098e+05 1.3224e+05 -1.473e+05 -1.1955e+05 v TurbVisc 2.7851e-19 0.026917 0.00021228 7.0829e-05 v CourantNb 8.3387e-08 0.011479 0.00017073 4.9699e-06 v FourierNb 1.2454e-07 0.037295 0.00015214 6.1668e-07 v total_pressure -3.1965e+05 2.3356e+05 -45975 -18228 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1145 0.11594 0.0030753 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.5823e-07 0.042204 0.00032287 5.5866e-06 INSTANT 0.876539000E-01 TIME STEP NUMBER 56737 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282804143E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.830986957E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10886E-01 0.21506E+01 Friction velocity uk : 0.10886E-01 0.21506E+01 Dimensionless distance yplus : 0.10478E-01 0.21146E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -8.574340334e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29481E+08 1 0.19175E-09 0.35410E+02 0.22409E+04 c Velocity[X] 0.20265E+02 c Velocity[Y] 0.15145E+02 c Velocity[Z] 0.86366E-06 c Pressure 0.13372E-03 16 0.59451E-04 0.94112E-03 0.34520E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -31.347 45.416 5.6047 7.9953 v Velocity[Y] -32.858 35.209 -0.17241 -0.083689 v Velocity[Z] -3.1084 3.1521 2.2233e-06 -5.3917e-08 v ǁVelocityǁ 0.0011791 45.669 8.8027 8.2058 v Pressure -4.2034e+05 1.3309e+05 -1.4639e+05 -1.1922e+05 v TurbVisc 2.7722e-19 0.026932 0.00021234 7.092e-05 v CourantNb 8.6405e-08 0.01148 0.00017073 4.9699e-06 v FourierNb 1.2455e-07 0.037314 0.00015216 6.1731e-07 v total_pressure -3.1902e+05 2.3442e+05 -45066 -17895 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1146 0.11598 0.0030758 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.5876e-07 0.042177 0.00032289 5.5872e-06 INSTANT 0.876540000E-01 TIME STEP NUMBER 56738 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282798691E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.830663023E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.97840E-02 0.21508E+01 Friction velocity uk : 0.97840E-02 0.21508E+01 Dimensionless distance yplus : 0.94173E-02 0.21148E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -8.154074333e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29481E+08 1 0.19178E-09 0.35433E+02 0.22415E+04 c Velocity[X] 0.20273E+02 c Velocity[Y] 0.15160E+02 c Velocity[Z] 0.85070E-06 c Pressure 0.13902E-03 677 0.79270E-04 0.97790E-03 0.61167E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -31.359 45.425 5.6046 7.9952 v Velocity[Y] -32.866 35.22 -0.1725 -0.083956 v Velocity[Z] -3.1087 3.1523 2.2229e-06 -5.3917e-08 v ǁVelocityǁ 0.00098873 45.679 8.8041 8.2059 v Pressure -4.1949e+05 1.3416e+05 -1.4539e+05 -1.1866e+05 v TurbVisc 2.2504e-19 0.026947 0.0002124 7.1012e-05 v CourantNb 8.9262e-08 0.011481 0.00017074 4.9699e-06 v FourierNb 1.2455e-07 0.037334 0.00015218 6.1793e-07 v total_pressure -3.1816e+05 2.3549e+05 -44062 -17332 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1148 0.11602 0.0030762 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.5929e-07 0.04215 0.00032292 5.5878e-06 INSTANT 0.876541000E-01 TIME STEP NUMBER 56739 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282793443E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.830346071E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.14540E-01 0.21510E+01 Friction velocity uk : 0.14540E-01 0.21510E+01 Dimensionless distance yplus : 0.13995E-01 0.21150E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -7.962180458e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29481E+08 1 0.19182E-09 0.35459E+02 0.22422E+04 c Velocity[X] 0.20289E+02 c Velocity[Y] 0.15169E+02 c Velocity[Z] 0.84735E-06 c Pressure 0.14248E-03 391 0.85392E-04 0.10017E-02 0.66916E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -31.37 45.434 5.6046 7.9951 v Velocity[Y] -32.875 35.231 -0.17259 -0.084219 v Velocity[Z] -3.1091 3.1524 2.2224e-06 -5.3917e-08 v ǁVelocityǁ 0.00087085 45.688 8.8055 8.2061 v Pressure -4.1866e+05 1.3522e+05 -1.4434e+05 -1.1803e+05 v TurbVisc 2.9463e-19 0.026962 0.00021245 7.1103e-05 v CourantNb 8.4735e-08 0.011481 0.00017074 4.9699e-06 v FourierNb 1.2455e-07 0.037353 0.0001522 6.1855e-07 v total_pressure -3.1733e+05 2.3654e+05 -43020 -16704 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.115 0.11606 0.0030767 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.5982e-07 0.042122 0.00032295 5.5884e-06 INSTANT 0.876542000E-01 TIME STEP NUMBER 56740 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282788127E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.830030316E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.16712E-01 0.21512E+01 Friction velocity uk : 0.16712E-01 0.21512E+01 Dimensionless distance yplus : 0.16079E-01 0.21152E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -7.591315621e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29481E+08 1 0.19185E-09 0.35487E+02 0.22430E+04 c Velocity[X] 0.20298E+02 c Velocity[Y] 0.15189E+02 c Velocity[Z] 0.84108E-06 c Pressure 0.14657E-03 139 0.99140E-04 0.10299E-02 0.60739E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -31.381 45.444 5.6045 7.995 v Velocity[Y] -32.884 35.242 -0.17267 -0.084487 v Velocity[Z] -3.1095 3.1525 2.2219e-06 -5.3917e-08 v ǁVelocityǁ 0.00085105 45.698 8.807 8.2062 v Pressure -4.1787e+05 1.3622e+05 -1.4334e+05 -1.177e+05 v TurbVisc 2.9848e-19 0.026977 0.00021251 7.1195e-05 v CourantNb 8.8083e-08 0.011482 0.00017075 4.9699e-06 v FourierNb 1.2455e-07 0.037373 0.00015222 6.1918e-07 v total_pressure -3.1655e+05 2.3754e+05 -42016 -16378 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1152 0.11609 0.0030772 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.6036e-07 0.042095 0.00032297 5.589e-06 INSTANT 0.876543000E-01 TIME STEP NUMBER 56741 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282783183E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.829718938E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11463E-01 0.21514E+01 Friction velocity uk : 0.11463E-01 0.21514E+01 Dimensionless distance yplus : 0.11029E-01 0.21154E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -7.266776744e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29480E+08 1 0.19189E-09 0.35494E+02 0.22431E+04 c Velocity[X] 0.20309E+02 c Velocity[Y] 0.15185E+02 c Velocity[Z] 0.83961E-06 c Pressure 0.15058E-03 354 0.84320E-04 0.10576E-02 0.59141E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -31.393 45.453 5.6044 7.9949 v Velocity[Y] -32.892 35.252 -0.17276 -0.084753 v Velocity[Z] -3.1098 3.1527 2.2214e-06 -5.3917e-08 v ǁVelocityǁ 0.00089815 45.707 8.8084 8.2063 v Pressure -4.1702e+05 1.3729e+05 -1.4224e+05 -1.1706e+05 v TurbVisc 2.9852e-19 0.026992 0.00021257 7.1286e-05 v CourantNb 8.8997e-08 0.011483 0.00017075 4.9699e-06 v FourierNb 1.2455e-07 0.037393 0.00015224 6.198e-07 v total_pressure -3.157e+05 2.3861e+05 -40917 -15731 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1154 0.11613 0.0030776 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.6089e-07 0.042068 0.000323 5.5897e-06 INSTANT 0.876544000E-01 TIME STEP NUMBER 56742 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282778153E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.829415921E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.39731E-02 0.21516E+01 Friction velocity uk : 0.39731E-02 0.21516E+01 Dimensionless distance yplus : 0.38228E-02 0.21157E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -6.950017639e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29480E+08 1 0.19192E-09 0.35527E+02 0.22441E+04 c Velocity[X] 0.20326E+02 c Velocity[Y] 0.15201E+02 c Velocity[Z] 0.83971E-06 c Pressure 0.14904E-03 9 0.59302E-04 0.10462E-02 0.44441E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -31.404 45.462 5.6043 7.9948 v Velocity[Y] -32.901 35.263 -0.17285 -0.085018 v Velocity[Z] -3.1102 3.1528 2.2209e-06 -5.3917e-08 v ǁVelocityǁ 0.00097611 45.717 8.8098 8.2064 v Pressure -4.1619e+05 1.3834e+05 -1.4113e+05 -1.1655e+05 v TurbVisc 2.9787e-19 0.027007 0.00021263 7.1378e-05 v CourantNb 8.9259e-08 0.011483 0.00017076 4.9699e-06 v FourierNb 1.2455e-07 0.037413 0.00015226 6.2043e-07 v total_pressure -3.1486e+05 2.3967e+05 -39809 -15227 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1157 0.11616 0.003078 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.6143e-07 0.042041 0.00032302 5.5903e-06 INSTANT 0.876545000E-01 TIME STEP NUMBER 56743 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282773280E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.829119322E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.45735E-02 0.21519E+01 Friction velocity uk : 0.45735E-02 0.21519E+01 Dimensionless distance yplus : 0.44005E-02 0.21159E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -6.552247023e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29480E+08 1 0.19195E-09 0.35550E+02 0.22447E+04 c Velocity[X] 0.20333E+02 c Velocity[Y] 0.15217E+02 c Velocity[Z] 0.83567E-06 c Pressure 0.15401E-03 330 0.80477E-04 0.10805E-02 0.67136E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -31.415 45.471 5.6043 7.9947 v Velocity[Y] -32.91 35.274 -0.17294 -0.085287 v Velocity[Z] -3.1106 3.153 2.2204e-06 -5.3917e-08 v ǁVelocityǁ 0.0011388 45.726 8.8112 8.2065 v Pressure -4.1515e+05 1.3959e+05 -1.3998e+05 -1.159e+05 v TurbVisc 2.9268e-19 0.027022 0.00021269 7.147e-05 v CourantNb 9.2544e-08 0.011484 0.00017077 4.9699e-06 v FourierNb 1.2456e-07 0.037434 0.00015228 6.2105e-07 v total_pressure -3.1383e+05 2.4092e+05 -38658 -14579 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1159 0.11619 0.0030785 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.6197e-07 0.042014 0.00032305 5.5909e-06 INSTANT 0.876546000E-01 TIME STEP NUMBER 56744 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282768598E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.828828950E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.94093E-02 0.21521E+01 Friction velocity uk : 0.94093E-02 0.21521E+01 Dimensionless distance yplus : 0.90534E-02 0.21161E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -6.332328525e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29480E+08 1 0.19199E-09 0.35576E+02 0.22455E+04 c Velocity[X] 0.20346E+02 c Velocity[Y] 0.15230E+02 c Velocity[Z] 0.83032E-06 c Pressure 0.15719E-03 108 0.86623E-04 0.11022E-02 0.67845E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -31.427 45.48 5.6042 7.9945 v Velocity[Y] -32.918 35.285 -0.17303 -0.085553 v Velocity[Z] -3.1109 3.1531 2.2199e-06 -5.3917e-08 v ǁVelocityǁ 0.0012546 45.735 8.8126 8.2067 v Pressure -4.1425e+05 1.4072e+05 -1.3879e+05 -1.1526e+05 v TurbVisc 3.1427e-19 0.027037 0.00021274 7.1561e-05 v CourantNb 8.8314e-08 0.011485 0.00017077 4.9699e-06 v FourierNb 1.2456e-07 0.037455 0.0001523 6.2168e-07 v total_pressure -3.1292e+05 2.4204e+05 -37469 -13939 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1161 0.11623 0.0030792 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.6251e-07 0.041987 0.00032308 5.5915e-06 INSTANT 0.876547000E-01 TIME STEP NUMBER 56745 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282763843E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.828543110E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11535E-01 0.21524E+01 Friction velocity uk : 0.11535E-01 0.21524E+01 Dimensionless distance yplus : 0.11397E-01 0.21164E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -6.014129844e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29480E+08 1 0.19202E-09 0.35589E+02 0.22458E+04 c Velocity[X] 0.20356E+02 c Velocity[Y] 0.15233E+02 c Velocity[Z] 0.82740E-06 c Pressure 0.16091E-03 159 0.75197E-04 0.11277E-02 0.50538E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -31.438 45.489 5.6041 7.9944 v Velocity[Y] -32.927 35.296 -0.17313 -0.085822 v Velocity[Z] -3.1113 3.1532 2.2195e-06 -5.3918e-08 v ǁVelocityǁ 0.001265 45.745 8.8141 8.2068 v Pressure -4.1327e+05 1.4192e+05 -1.376e+05 -1.1475e+05 v TurbVisc 2.9542e-19 0.027052 0.0002128 7.1653e-05 v CourantNb 8.9062e-08 0.011485 0.00017078 4.9699e-06 v FourierNb 1.2456e-07 0.037475 0.00015232 6.2231e-07 v total_pressure -3.1194e+05 2.4324e+05 -36280 -13427 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1164 0.11627 0.0030798 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.6305e-07 0.04196 0.0003231 5.5922e-06 INSTANT 0.876548000E-01 TIME STEP NUMBER 56746 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282759347E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.828262599E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.70128E-02 0.21526E+01 Friction velocity uk : 0.70128E-02 0.21526E+01 Dimensionless distance yplus : 0.69289E-02 0.21167E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -5.714864346e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29480E+08 1 0.19205E-09 0.35622E+02 0.22467E+04 c Velocity[X] 0.20371E+02 c Velocity[Y] 0.15250E+02 c Velocity[Z] 0.83071E-06 c Pressure 0.16028E-03 9 0.53199E-04 0.11228E-02 0.42440E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -31.45 45.499 5.6041 7.9943 v Velocity[Y] -32.936 35.306 -0.17322 -0.086093 v Velocity[Z] -3.1117 3.1534 2.219e-06 -5.3918e-08 v ǁVelocityǁ 0.001339 45.754 8.8155 8.2069 v Pressure -4.1234e+05 1.4306e+05 -1.3639e+05 -1.1425e+05 v TurbVisc 3.0375e-19 0.027067 0.00021286 7.1745e-05 v CourantNb 8.9419e-08 0.011486 0.00017078 4.9699e-06 v FourierNb 1.2456e-07 0.037497 0.00015234 6.2293e-07 v total_pressure -3.1102e+05 2.4438e+05 -35067 -12924 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1167 0.11631 0.0030805 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.636e-07 0.041933 0.00032313 5.5928e-06 INSTANT 0.876549000E-01 TIME STEP NUMBER 56747 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282755122E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.827990792E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.63041E-02 0.21529E+01 Friction velocity uk : 0.63041E-02 0.21529E+01 Dimensionless distance yplus : 0.62287E-02 0.21169E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -5.357127344e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29480E+08 1 0.19209E-09 0.35637E+02 0.22471E+04 c Velocity[X] 0.20382E+02 c Velocity[Y] 0.15255E+02 c Velocity[Z] 0.82923E-06 c Pressure 0.16441E-03 175 0.96175E-04 0.11511E-02 0.71772E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -31.461 45.508 5.604 7.9943 v Velocity[Y] -32.944 35.317 -0.17331 -0.086363 v Velocity[Z] -3.112 3.1535 2.2185e-06 -5.3918e-08 v ǁVelocityǁ 0.0014815 45.764 8.8169 8.2071 v Pressure -4.1118e+05 1.4443e+05 -1.351e+05 -1.1336e+05 v TurbVisc 2.9964e-19 0.027082 0.00021292 7.1837e-05 v CourantNb 9.1594e-08 0.011487 0.00017079 4.9699e-06 v FourierNb 1.2456e-07 0.037518 0.00015236 6.2356e-07 v total_pressure -3.0986e+05 2.4576e+05 -33776 -12037 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1169 0.11634 0.0030811 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.6414e-07 0.041906 0.00032315 5.5934e-06 INSTANT 0.876550000E-01 TIME STEP NUMBER 56748 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282750897E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.827727906E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.67310E-02 0.21532E+01 Friction velocity uk : 0.67310E-02 0.21532E+01 Dimensionless distance yplus : 0.66505E-02 0.21172E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -5.174978631e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29479E+08 1 0.19213E-09 0.35662E+02 0.22478E+04 c Velocity[X] 0.20396E+02 c Velocity[Y] 0.15267E+02 c Velocity[Z] 0.82358E-06 c Pressure 0.16645E-03 75 0.80789E-04 0.11647E-02 0.54013E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -31.472 45.517 5.604 7.9942 v Velocity[Y] -32.953 35.328 -0.1734 -0.086633 v Velocity[Z] -3.1124 3.1536 2.218e-06 -5.3918e-08 v ǁVelocityǁ 0.0012762 45.773 8.8183 8.2072 v Pressure -4.1013e+05 1.457e+05 -1.3379e+05 -1.1269e+05 v TurbVisc 1.8377e-19 0.027097 0.00021298 7.1929e-05 v CourantNb 9.1496e-08 0.011487 0.00017079 4.9699e-06 v FourierNb 1.2457e-07 0.037539 0.00015238 6.2419e-07 v total_pressure -3.088e+05 2.4703e+05 -32462 -11370 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1172 0.11638 0.0030817 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.6469e-07 0.041879 0.00032318 5.5941e-06 INSTANT 0.876551000E-01 TIME STEP NUMBER 56749 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282746764E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.827471010E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.58436E-02 0.21535E+01 Friction velocity uk : 0.58436E-02 0.21535E+01 Dimensionless distance yplus : 0.57737E-02 0.21175E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -4.984574838e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29479E+08 1 0.19216E-09 0.35696E+02 0.22487E+04 c Velocity[X] 0.20409E+02 c Velocity[Y] 0.15287E+02 c Velocity[Z] 0.82798E-06 c Pressure 0.16802E-03 9 0.53676E-04 0.11751E-02 0.52751E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -31.484 45.526 5.6039 7.9941 v Velocity[Y] -32.962 35.339 -0.1735 -0.086903 v Velocity[Z] -3.1127 3.1538 2.2175e-06 -5.3918e-08 v ǁVelocityǁ 0.0010941 45.783 8.8198 8.2073 v Pressure -4.0909e+05 1.4696e+05 -1.3246e+05 -1.1208e+05 v TurbVisc 3.3293e-19 0.027111 0.00021304 7.2021e-05 v CourantNb 7.5965e-08 0.011488 0.0001708 4.9699e-06 v FourierNb 1.2457e-07 0.037561 0.0001524 6.2482e-07 v total_pressure -3.0777e+05 2.4828e+05 -31135 -10754 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1175 0.11641 0.0030823 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.6524e-07 0.041852 0.0003232 5.5947e-06 INSTANT 0.876552000E-01 TIME STEP NUMBER 56750 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282742751E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.827218390E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.21618E-02 0.21538E+01 Friction velocity uk : 0.21618E-02 0.21538E+01 Dimensionless distance yplus : 0.21359E-02 0.21178E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -4.468485716e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29479E+08 1 0.19219E-09 0.35713E+02 0.22492E+04 c Velocity[X] 0.20421E+02 c Velocity[Y] 0.15292E+02 c Velocity[Z] 0.82725E-06 c Pressure 0.17205E-03 136 0.98338E-04 0.12027E-02 0.61438E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -31.495 45.535 5.6039 7.994 v Velocity[Y] -32.97 35.35 -0.17359 -0.087173 v Velocity[Z] -3.1131 3.1539 2.2171e-06 -5.3918e-08 v ǁVelocityǁ 0.00096514 45.792 8.8212 8.2075 v Pressure -4.0795e+05 1.4831e+05 -1.3115e+05 -1.1134e+05 v TurbVisc 3.3095e-19 0.027126 0.00021309 7.2114e-05 v CourantNb 9.4262e-08 0.011489 0.00017081 4.9699e-06 v FourierNb 1.2457e-07 0.037583 0.00015242 6.2545e-07 v total_pressure -3.0663e+05 2.4963e+05 -29823 -10018 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1178 0.11645 0.003083 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.6579e-07 0.041826 0.00032323 5.5953e-06 INSTANT 0.876553000E-01 TIME STEP NUMBER 56751 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282738889E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.826973536E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.43594E-02 0.21541E+01 Friction velocity uk : 0.43594E-02 0.21541E+01 Dimensionless distance yplus : 0.43073E-02 0.21181E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -4.444104961e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29479E+08 1 0.19223E-09 0.35738E+02 0.22499E+04 c Velocity[X] 0.20432E+02 c Velocity[Y] 0.15306E+02 c Velocity[Z] 0.82344E-06 c Pressure 0.17381E-03 36 0.82587E-04 0.12144E-02 0.52893E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -31.507 45.544 5.6038 7.9939 v Velocity[Y] -32.979 35.361 -0.17368 -0.087446 v Velocity[Z] -3.1135 3.1541 2.2166e-06 -5.3918e-08 v ǁVelocityǁ 0.00090901 45.801 8.8226 8.2076 v Pressure -4.0682e+05 1.4966e+05 -1.2977e+05 -1.107e+05 v TurbVisc 3.3444e-19 0.027141 0.00021315 7.2206e-05 v CourantNb 8.905e-08 0.01149 0.00017081 4.9699e-06 v FourierNb 1.2457e-07 0.037605 0.00015244 6.2608e-07 v total_pressure -3.055e+05 2.5098e+05 -28449 -9376.9 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1181 0.11649 0.0030836 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.6635e-07 0.041799 0.00032326 5.596e-06 INSTANT 0.876554000E-01 TIME STEP NUMBER 56752 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282735180E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.826738943E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.52982E-02 0.21544E+01 Friction velocity uk : 0.52982E-02 0.21544E+01 Dimensionless distance yplus : 0.52348E-02 0.21184E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -4.206679837e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29479E+08 1 0.19227E-09 0.35773E+02 0.22509E+04 c Velocity[X] 0.20443E+02 c Velocity[Y] 0.15330E+02 c Velocity[Z] 0.82593E-06 c Pressure 0.17505E-03 9 0.54058E-04 0.12223E-02 0.54370E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -31.518 45.554 5.6038 7.9938 v Velocity[Y] -32.988 35.371 -0.17378 -0.08772 v Velocity[Z] -3.1138 3.1542 2.2161e-06 -5.3918e-08 v ǁVelocityǁ 0.0009004 45.811 8.824 8.2078 v Pressure -4.0564e+05 1.5106e+05 -1.2836e+05 -1.1007e+05 v TurbVisc 3.1361e-19 0.027156 0.00021321 7.2299e-05 v CourantNb 8.5814e-08 0.01149 0.00017082 4.9699e-06 v FourierNb 1.2457e-07 0.037627 0.00015246 6.2671e-07 v total_pressure -3.0431e+05 2.5238e+05 -27036 -8740.7 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1184 0.11652 0.0030842 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.669e-07 0.041772 0.00032328 5.5966e-06 INSTANT 0.876555000E-01 TIME STEP NUMBER 56753 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282731728E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.826510192E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.76988E-02 0.21548E+01 Friction velocity uk : 0.76988E-02 0.21548E+01 Dimensionless distance yplus : 0.76067E-02 0.21188E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -3.865894107e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29479E+08 1 0.19231E-09 0.35795E+02 0.22515E+04 c Velocity[X] 0.20462E+02 c Velocity[Y] 0.15334E+02 c Velocity[Z] 0.82656E-06 c Pressure 0.17885E-03 80 0.75505E-04 0.12482E-02 0.96309E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -31.53 45.563 5.6037 7.9937 v Velocity[Y] -32.996 35.382 -0.17387 -0.087991 v Velocity[Z] -3.1142 3.1543 2.2156e-06 -5.3918e-08 v ǁVelocityǁ 0.00091913 45.82 8.8255 8.2079 v Pressure -4.0437e+05 1.5253e+05 -1.2692e+05 -1.0901e+05 v TurbVisc 3.2228e-19 0.027171 0.00021327 7.2391e-05 v CourantNb 9.2429e-08 0.011491 0.00017082 4.9699e-06 v FourierNb 1.2457e-07 0.03765 0.00015248 6.2734e-07 v total_pressure -3.0305e+05 2.5386e+05 -25595 -7682.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1188 0.11656 0.0030848 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.6746e-07 0.041745 0.00032331 5.5973e-06 INSTANT 0.876556000E-01 TIME STEP NUMBER 56754 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282728163E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.826288459E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.84171E-02 0.21551E+01 Friction velocity uk : 0.84171E-02 0.21551E+01 Dimensionless distance yplus : 0.83165E-02 0.21191E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -3.816516674e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29479E+08 1 0.19234E-09 0.35828E+02 0.22524E+04 c Velocity[X] 0.20472E+02 c Velocity[Y] 0.15356E+02 c Velocity[Z] 0.82747E-06 c Pressure 0.18118E-03 61 0.79682E-04 0.12638E-02 0.63401E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -31.541 45.572 5.6037 7.9937 v Velocity[Y] -33.005 35.393 -0.17397 -0.088267 v Velocity[Z] -3.1146 3.1545 2.2151e-06 -5.3918e-08 v ǁVelocityǁ 0.00096621 45.83 8.8269 8.2081 v Pressure -4.032e+05 1.5393e+05 -1.255e+05 -1.0849e+05 v TurbVisc 2.9769e-19 0.027186 0.00021333 7.2483e-05 v CourantNb 8.0301e-08 0.011492 0.00017083 4.9699e-06 v FourierNb 1.2457e-07 0.037673 0.0001525 6.2797e-07 v total_pressure -3.0187e+05 2.5525e+05 -24178 -7164.8 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1191 0.1166 0.0030855 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.6802e-07 0.041718 0.00032333 5.5979e-06 INSTANT 0.876557000E-01 TIME STEP NUMBER 56755 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282724976E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.826074252E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.81737E-02 0.21554E+01 Friction velocity uk : 0.81737E-02 0.21554E+01 Dimensionless distance yplus : 0.80759E-02 0.21194E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -3.609742701e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29479E+08 1 0.19238E-09 0.35857E+02 0.22532E+04 c Velocity[X] 0.20490E+02 c Velocity[Y] 0.15367E+02 c Velocity[Z] 0.82530E-06 c Pressure 0.18390E-03 34 0.93385E-04 0.12821E-02 0.88267E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -31.553 45.581 5.6036 7.9936 v Velocity[Y] -33.014 35.404 -0.17406 -0.088539 v Velocity[Z] -3.1149 3.1546 2.2146e-06 -5.3918e-08 v ǁVelocityǁ 0.0010692 45.839 8.8283 8.2082 v Pressure -4.0201e+05 1.5533e+05 -1.2402e+05 -1.076e+05 v TurbVisc 3.3494e-19 0.027201 0.00021338 7.2576e-05 v CourantNb 8.9933e-08 0.011492 0.00017084 4.97e-06 v FourierNb 1.2457e-07 0.037695 0.00015252 6.286e-07 v total_pressure -3.0068e+05 2.5665e+05 -22698 -6275.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1194 0.11664 0.0030861 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.6858e-07 0.041692 0.00032336 5.5986e-06 INSTANT 0.876558000E-01 TIME STEP NUMBER 56756 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282721750E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.825867960E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.81160E-02 0.21558E+01 Friction velocity uk : 0.81160E-02 0.21558E+01 Dimensionless distance yplus : 0.80189E-02 0.21197E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -3.477926648e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29479E+08 1 0.19241E-09 0.35871E+02 0.22535E+04 c Velocity[X] 0.20500E+02 c Velocity[Y] 0.15372E+02 c Velocity[Z] 0.81710E-06 c Pressure 0.18655E-03 792 0.78957E-04 0.12999E-02 0.63310E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -31.564 45.591 5.6036 7.9935 v Velocity[Y] -33.023 35.415 -0.17416 -0.088814 v Velocity[Z] -3.1153 3.1547 2.2142e-06 -5.3918e-08 v ǁVelocityǁ 0.0012376 45.849 8.8298 8.2084 v Pressure -4.0074e+05 1.5681e+05 -1.2255e+05 -1.0694e+05 v TurbVisc 3.3619e-19 0.027216 0.00021344 7.2669e-05 v CourantNb 8.9054e-08 0.011493 0.00017084 4.97e-06 v FourierNb 1.2458e-07 0.037718 0.00015254 6.2923e-07 v total_pressure -2.9941e+05 2.5814e+05 -21229 -5618.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1197 0.11667 0.0030867 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.6914e-07 0.041665 0.00032338 5.5992e-06 INSTANT 0.876559000E-01 TIME STEP NUMBER 56757 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282718771E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.825671623E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.81945E-02 0.21561E+01 Friction velocity uk : 0.81945E-02 0.21561E+01 Dimensionless distance yplus : 0.80964E-02 0.21201E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -3.336223783e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29479E+08 1 0.19245E-09 0.35909E+02 0.22546E+04 c Velocity[X] 0.20517E+02 c Velocity[Y] 0.15392E+02 c Velocity[Z] 0.82322E-06 c Pressure 0.18513E-03 9 0.54767E-04 0.12894E-02 0.52678E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -31.576 45.6 5.6036 7.9934 v Velocity[Y] -33.031 35.426 -0.17425 -0.089091 v Velocity[Z] -3.1156 3.1549 2.2137e-06 -5.3918e-08 v ǁVelocityǁ 0.0014451 45.858 8.8312 8.2085 v Pressure -3.9955e+05 1.5821e+05 -1.2108e+05 -1.0631e+05 v TurbVisc 3.295e-19 0.027231 0.0002135 7.2761e-05 v CourantNb 8.8899e-08 0.011494 0.00017085 4.97e-06 v FourierNb 1.2458e-07 0.037741 0.00015256 6.2986e-07 v total_pressure -2.9823e+05 2.5954e+05 -19752 -4988.7 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1201 0.11671 0.0030873 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.6971e-07 0.041638 0.00032341 5.5999e-06 INSTANT 0.876560000E-01 TIME STEP NUMBER 56758 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282716117E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.825483855E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.85133E-02 0.21565E+01 Friction velocity uk : 0.85133E-02 0.21565E+01 Dimensionless distance yplus : 0.84114E-02 0.21204E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -3.152519536e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29479E+08 1 0.19249E-09 0.35928E+02 0.22551E+04 c Velocity[X] 0.20531E+02 c Velocity[Y] 0.15397E+02 c Velocity[Z] 0.82055E-06 c Pressure 0.18825E-03 18 0.99657E-04 0.13104E-02 0.85055E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -31.588 45.609 5.6035 7.9934 v Velocity[Y] -33.04 35.437 -0.17435 -0.089367 v Velocity[Z] -3.116 3.155 2.2132e-06 -5.3918e-08 v ǁVelocityǁ 0.0016935 45.868 8.8326 8.2087 v Pressure -3.9815e+05 1.5982e+05 -1.1953e+05 -1.053e+05 v TurbVisc 3.3422e-19 0.027245 0.00021356 7.2854e-05 v CourantNb 9.1579e-08 0.011495 0.00017085 4.97e-06 v FourierNb 1.2458e-07 0.037764 0.00015258 6.3049e-07 v total_pressure -2.9683e+05 2.6114e+05 -18202 -3971.1 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1204 0.11675 0.0030879 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.7027e-07 0.041611 0.00032344 5.6005e-06 INSTANT 0.876561000E-01 TIME STEP NUMBER 56759 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282713430E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.825306150E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.91232E-02 0.21568E+01 Friction velocity uk : 0.91232E-02 0.21568E+01 Dimensionless distance yplus : 0.90141E-02 0.21208E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -3.163667139e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29479E+08 1 0.19253E-09 0.35957E+02 0.22559E+04 c Velocity[X] 0.20546E+02 c Velocity[Y] 0.15411E+02 c Velocity[Z] 0.82018E-06 c Pressure 0.18939E-03 254 0.84232E-04 0.13176E-02 0.68816E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -31.599 45.618 5.6035 7.9933 v Velocity[Y] -33.049 35.448 -0.17444 -0.089644 v Velocity[Z] -3.1164 3.1551 2.2127e-06 -5.3918e-08 v ǁVelocityǁ 0.0019655 45.878 8.834 8.2089 v Pressure -3.9683e+05 1.6136e+05 -1.1798e+05 -1.0446e+05 v TurbVisc 3.3397e-19 0.02726 0.00021362 7.2947e-05 v CourantNb 9.3323e-08 0.011496 0.00017086 4.97e-06 v FourierNb 1.2458e-07 0.037787 0.0001526 6.3113e-07 v total_pressure -2.9551e+05 2.6268e+05 -16652 -3135.7 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1208 0.11678 0.0030886 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.7084e-07 0.041584 0.00032346 5.6012e-06 INSTANT 0.876562000E-01 TIME STEP NUMBER 56760 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282710880E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.825134459E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.85163E-02 0.21572E+01 Friction velocity uk : 0.85163E-02 0.21572E+01 Dimensionless distance yplus : 0.84144E-02 0.21211E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -3.040157840e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29479E+08 1 0.19257E-09 0.35996E+02 0.22570E+04 c Velocity[X] 0.20565E+02 c Velocity[Y] 0.15431E+02 c Velocity[Z] 0.82730E-06 c Pressure 0.19000E-03 9 0.56520E-04 0.13212E-02 0.63253E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -31.611 45.628 5.6035 7.9933 v Velocity[Y] -33.058 35.459 -0.17454 -0.08992 v Velocity[Z] -3.1167 3.1553 2.2123e-06 -5.3919e-08 v ǁVelocityǁ 0.0019436 45.887 8.8355 8.2091 v Pressure -3.9556e+05 1.6284e+05 -1.1641e+05 -1.0372e+05 v TurbVisc 3.2432e-19 0.027275 0.00021368 7.304e-05 v CourantNb 8.2227e-08 0.011496 0.00017087 4.97e-06 v FourierNb 1.2458e-07 0.03781 0.00015262 6.3176e-07 v total_pressure -2.9423e+05 2.6417e+05 -15084 -2394.5 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1211 0.11682 0.0030892 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.7141e-07 0.041558 0.00032349 5.6018e-06 INSTANT 0.876563000E-01 TIME STEP NUMBER 56761 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282708488E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.824968603E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.85699E-02 0.21576E+01 Friction velocity uk : 0.85699E-02 0.21576E+01 Dimensionless distance yplus : 0.84674E-02 0.21215E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -2.837285579e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29480E+08 1 0.19260E-09 0.36025E+02 0.22578E+04 c Velocity[X] 0.20576E+02 c Velocity[Y] 0.15448E+02 c Velocity[Z] 0.82538E-06 c Pressure 0.19301E-03 400 0.77099E-04 0.13413E-02 0.85386E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -31.623 45.637 5.6034 7.9932 v Velocity[Y] -33.067 35.47 -0.17463 -0.090198 v Velocity[Z] -3.1171 3.1554 2.2118e-06 -5.3919e-08 v ǁVelocityǁ 0.0019054 45.897 8.8369 8.2092 v Pressure -3.9412e+05 1.6449e+05 -1.1485e+05 -1.0283e+05 v TurbVisc 3.5699e-19 0.02729 0.00021374 7.3133e-05 v CourantNb 9.2448e-08 0.011497 0.00017087 4.9701e-06 v FourierNb 1.2458e-07 0.037834 0.00015264 6.324e-07 v total_pressure -2.928e+05 2.6581e+05 -13524 -1508.3 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1215 0.11686 0.0030898 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.7198e-07 0.041531 0.00032351 5.6025e-06 INSTANT 0.876564000E-01 TIME STEP NUMBER 56762 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282706303E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.824813635E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.81481E-02 0.21579E+01 Friction velocity uk : 0.81481E-02 0.21579E+01 Dimensionless distance yplus : 0.80506E-02 0.21218E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -2.862497057e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29480E+08 1 0.19264E-09 0.36058E+02 0.22587E+04 c Velocity[X] 0.20593E+02 c Velocity[Y] 0.15465E+02 c Velocity[Z] 0.82286E-06 c Pressure 0.19456E-03 80 0.82191E-04 0.13514E-02 0.80707E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -31.634 45.647 5.6034 7.9932 v Velocity[Y] -33.076 35.481 -0.17473 -0.090475 v Velocity[Z] -3.1174 3.1555 2.2113e-06 -5.3919e-08 v ǁVelocityǁ 0.0018607 45.907 8.8383 8.2094 v Pressure -3.9282e+05 1.66e+05 -1.1326e+05 -1.0202e+05 v TurbVisc 3.4475e-19 0.027305 0.00021379 7.3226e-05 v CourantNb 8.7543e-08 0.011498 0.00017088 4.9701e-06 v FourierNb 1.2458e-07 0.037857 0.00015266 6.3303e-07 v total_pressure -2.915e+05 2.6733e+05 -11931 -697.34 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1218 0.11689 0.0030904 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.7256e-07 0.041504 0.00032354 5.6031e-06 INSTANT 0.876565000E-01 TIME STEP NUMBER 56763 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282704087E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.824666855E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.80936E-02 0.21583E+01 Friction velocity uk : 0.80936E-02 0.21583E+01 Dimensionless distance yplus : 0.79968E-02 0.21222E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -2.828881734e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29480E+08 1 0.19268E-09 0.36094E+02 0.22598E+04 c Velocity[X] 0.20612E+02 c Velocity[Y] 0.15482E+02 c Velocity[Z] 0.81552E-06 c Pressure 0.19646E-03 198 0.95215E-04 0.13638E-02 0.81955E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -31.646 45.656 5.6034 7.9931 v Velocity[Y] -33.085 35.492 -0.17483 -0.090756 v Velocity[Z] -3.1178 3.1557 2.2108e-06 -5.3919e-08 v ǁVelocityǁ 0.001814 45.916 8.8398 8.2096 v Pressure -3.9141e+05 1.6762e+05 -1.1165e+05 -1.0123e+05 v TurbVisc 3.6036e-19 0.02732 0.00021385 7.3319e-05 v CourantNb 8.9244e-08 0.011499 0.00017088 4.9701e-06 v FourierNb 1.2458e-07 0.03788 0.00015268 6.3367e-07 v total_pressure -2.9009e+05 2.6895e+05 -10328 93.793 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1222 0.11693 0.0030909 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.7313e-07 0.041495 0.00032357 5.6038e-06 INSTANT 0.876566000E-01 TIME STEP NUMBER 56764 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282702375E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.824530303E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.81881E-02 0.21587E+01 Friction velocity uk : 0.81881E-02 0.21587E+01 Dimensionless distance yplus : 0.80902E-02 0.21226E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -2.795730621e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29480E+08 1 0.19272E-09 0.36109E+02 0.22601E+04 c Velocity[X] 0.20628E+02 c Velocity[Y] 0.15481E+02 c Velocity[Z] 0.81843E-06 c Pressure 0.19833E-03 71 0.80837E-04 0.13761E-02 0.82702E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -31.658 45.666 5.6033 7.9931 v Velocity[Y] -33.093 35.503 -0.17492 -0.091035 v Velocity[Z] -3.1182 3.1558 2.2103e-06 -5.3919e-08 v ǁVelocityǁ 0.0017687 45.926 8.8412 8.2098 v Pressure -3.9005e+05 1.692e+05 -1.1003e+05 -1.003e+05 v TurbVisc 3.3087e-19 0.027335 0.00021391 7.3412e-05 v CourantNb 8.7886e-08 0.011499 0.00017089 4.9701e-06 v FourierNb 1.2459e-07 0.037903 0.0001527 6.343e-07 v total_pressure -2.8872e+05 2.7053e+05 -8705.4 1022.9 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1226 0.11696 0.0030915 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.7371e-07 0.041519 0.00032359 5.6044e-06 INSTANT 0.876567000E-01 TIME STEP NUMBER 56765 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282700608E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.824404298E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.83070E-02 0.21590E+01 Friction velocity uk : 0.83070E-02 0.21590E+01 Dimensionless distance yplus : 0.82077E-02 0.21229E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -2.755626857e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29480E+08 1 0.19276E-09 0.36151E+02 0.22613E+04 c Velocity[X] 0.20647E+02 c Velocity[Y] 0.15503E+02 c Velocity[Z] 0.82781E-06 c Pressure 0.19612E-03 9 0.57807E-04 0.13601E-02 0.61558E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -31.67 45.675 5.6033 7.993 v Velocity[Y] -33.102 35.514 -0.17502 -0.091314 v Velocity[Z] -3.1185 3.1559 2.2099e-06 -5.3919e-08 v ǁVelocityǁ 0.001602 45.936 8.8426 8.21 v Pressure -3.8876e+05 1.707e+05 -1.0843e+05 -99605 v TurbVisc 3.4498e-19 0.027349 0.00021397 7.3505e-05 v CourantNb 8.7652e-08 0.0115 0.0001709 4.9702e-06 v FourierNb 1.2459e-07 0.037926 0.00015272 6.3494e-07 v total_pressure -2.8744e+05 2.7203e+05 -7106.6 1720.2 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1229 0.117 0.0030921 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.7429e-07 0.041543 0.00032362 5.6051e-06 INSTANT 0.876568000E-01 TIME STEP NUMBER 56766 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282699028E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.824288600E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.79614E-02 0.21594E+01 Friction velocity uk : 0.79614E-02 0.21594E+01 Dimensionless distance yplus : 0.78662E-02 0.21234E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -2.692234128e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29480E+08 1 0.19279E-09 0.36182E+02 0.22622E+04 c Velocity[X] 0.20662E+02 c Velocity[Y] 0.15520E+02 c Velocity[Z] 0.82159E-06 c Pressure 0.19845E-03 160 0.76856E-04 0.13755E-02 0.92100E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -31.681 45.685 5.6033 7.993 v Velocity[Y] -33.111 35.525 -0.17511 -0.091595 v Velocity[Z] -3.1189 3.1561 2.2094e-06 -5.3919e-08 v ǁVelocityǁ 0.0014031 45.946 8.8441 8.2102 v Pressure -3.8723e+05 1.7243e+05 -1.0679e+05 -98640 v TurbVisc 3.4974e-19 0.027364 0.00021403 7.3599e-05 v CourantNb 9.2542e-08 0.011501 0.0001709 4.9702e-06 v FourierNb 1.2459e-07 0.03795 0.00015274 6.3557e-07 v total_pressure -2.8591e+05 2.7376e+05 -5465.7 2684.9 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1234 0.11703 0.0030927 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.7488e-07 0.041567 0.00032365 5.6058e-06 INSTANT 0.876569000E-01 TIME STEP NUMBER 56767 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282697656E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.824183744E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.69730E-02 0.21598E+01 Friction velocity uk : 0.69730E-02 0.21598E+01 Dimensionless distance yplus : 0.68896E-02 0.21237E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -2.667484172e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29480E+08 1 0.19284E-09 0.36217E+02 0.22632E+04 c Velocity[X] 0.20680E+02 c Velocity[Y] 0.15537E+02 c Velocity[Z] 0.82051E-06 c Pressure 0.19952E-03 54 0.82496E-04 0.13822E-02 0.88945E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -31.693 45.694 5.6033 7.9929 v Velocity[Y] -33.121 35.536 -0.17521 -0.091875 v Velocity[Z] -3.1192 3.1562 2.2089e-06 -5.3919e-08 v ǁVelocityǁ 0.0012321 45.956 8.8455 8.2103 v Pressure -3.8584e+05 1.7404e+05 -1.0512e+05 -97742 v TurbVisc 3.4229e-19 0.027379 0.00021409 7.3692e-05 v CourantNb 8.7271e-08 0.011502 0.00017091 4.9702e-06 v FourierNb 1.2459e-07 0.037973 0.00015276 6.3621e-07 v total_pressure -2.8451e+05 2.7537e+05 -3795.4 3582.9 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1237 0.11707 0.0030933 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.7546e-07 0.041591 0.00032367 5.6064e-06 INSTANT 0.876570000E-01 TIME STEP NUMBER 56768 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282696247E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.824084742E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.58053E-02 0.21602E+01 Friction velocity uk : 0.58053E-02 0.21602E+01 Dimensionless distance yplus : 0.57359E-02 0.21241E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -2.693997724e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29481E+08 1 0.19287E-09 0.36257E+02 0.22643E+04 c Velocity[X] 0.20700E+02 c Velocity[Y] 0.15557E+02 c Velocity[Z] 0.81884E-06 c Pressure 0.20093E-03 244 0.95432E-04 0.13911E-02 0.86183E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -31.705 45.704 5.6032 7.9929 v Velocity[Y] -33.13 35.547 -0.1753 -0.092158 v Velocity[Z] -3.1196 3.1563 2.2084e-06 -5.3919e-08 v ǁVelocityǁ 0.0011147 45.965 8.8469 8.2105 v Pressure -3.8437e+05 1.7572e+05 -1.0347e+05 -96921 v TurbVisc 3.5744e-19 0.027394 0.00021415 7.3786e-05 v CourantNb 8.6919e-08 0.011503 0.00017092 4.9703e-06 v FourierNb 1.2459e-07 0.037996 0.00015278 6.3685e-07 v total_pressure -2.8304e+05 2.7705e+05 -2143.9 4404.2 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1241 0.1171 0.0030938 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.7605e-07 0.041615 0.0003237 5.6071e-06 INSTANT 0.876571000E-01 TIME STEP NUMBER 56769 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282695345E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.823993591E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19914E-02 0.21606E+01 Friction velocity uk : 0.19914E-02 0.21606E+01 Dimensionless distance yplus : 0.19256E-02 0.21245E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -2.680633856e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29481E+08 1 0.19292E-09 0.36274E+02 0.22647E+04 c Velocity[X] 0.20718E+02 c Velocity[Y] 0.15556E+02 c Velocity[Z] 0.81347E-06 c Pressure 0.20228E-03 125 0.81293E-04 0.13998E-02 0.85544E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -31.717 45.714 5.6032 7.9929 v Velocity[Y] -33.139 35.558 -0.1754 -0.09244 v Velocity[Z] -3.12 3.1565 2.208e-06 -5.3919e-08 v ǁVelocityǁ 0.0010664 45.975 8.8484 8.2107 v Pressure -3.8295e+05 1.7735e+05 -1.018e+05 -95976 v TurbVisc 3.4132e-19 0.027409 0.00021421 7.3879e-05 v CourantNb 8.8726e-08 0.011503 0.00017092 4.9703e-06 v FourierNb 1.2459e-07 0.038019 0.0001528 6.3749e-07 v total_pressure -2.8163e+05 2.7868e+05 -476.22 5348.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1245 0.11714 0.0030944 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.7663e-07 0.041638 0.00032372 5.6078e-06 INSTANT 0.876572000E-01 TIME STEP NUMBER 56770 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282694384E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.823914090E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.58122E-02 0.21610E+01 Friction velocity uk : 0.58122E-02 0.21610E+01 Dimensionless distance yplus : 0.57427E-02 0.21249E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -2.669945326e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29481E+08 1 0.19295E-09 0.36319E+02 0.22660E+04 c Velocity[X] 0.20740E+02 c Velocity[Y] 0.15579E+02 c Velocity[Z] 0.82707E-06 c Pressure 0.19955E-03 9 0.58238E-04 0.13801E-02 0.64858E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -31.729 45.723 5.6032 7.9928 v Velocity[Y] -33.148 35.57 -0.17549 -0.092722 v Velocity[Z] -3.1203 3.1566 2.2075e-06 -5.3919e-08 v ǁVelocityǁ 0.0010682 45.985 8.8498 8.211 v Pressure -3.8165e+05 1.7887e+05 -1.0016e+05 -95246 v TurbVisc 3.5911e-19 0.027423 0.00021427 7.3973e-05 v CourantNb 8.6823e-08 0.011504 0.00017093 4.9703e-06 v FourierNb 1.2459e-07 0.038042 0.00015282 6.3812e-07 v total_pressure -2.8032e+05 2.8019e+05 1168.7 6078.7 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1249 0.11717 0.0030949 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.7722e-07 0.041662 0.00032375 5.6085e-06 INSTANT 0.876573000E-01 TIME STEP NUMBER 56771 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282693629E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.823846085E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.25855E-02 0.21614E+01 Friction velocity uk : 0.25855E-02 0.21614E+01 Dimensionless distance yplus : 0.25546E-02 0.21253E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -2.637316461e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29481E+08 1 0.19299E-09 0.36353E+02 0.22669E+04 c Velocity[X] 0.20756E+02 c Velocity[Y] 0.15597E+02 c Velocity[Z] 0.82711E-06 c Pressure 0.20134E-03 242 0.77243E-04 0.13918E-02 0.95120E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -31.741 45.733 5.6032 7.9928 v Velocity[Y] -33.157 35.581 -0.17559 -0.093006 v Velocity[Z] -3.1207 3.1568 2.207e-06 -5.3919e-08 v ǁVelocityǁ 0.0011232 45.995 8.8512 8.2112 v Pressure -3.8007e+05 1.8065e+05 -98480 -94270 v TurbVisc 3.5317e-19 0.027438 0.00021433 7.4066e-05 v CourantNb 9.0821e-08 0.011505 0.00017093 4.9704e-06 v FourierNb 1.2459e-07 0.038065 0.00015284 6.3876e-07 v total_pressure -2.7874e+05 2.8198e+05 2844.7 7055 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1253 0.11721 0.0030954 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.7782e-07 0.041686 0.00032378 5.6091e-06 INSTANT 0.876574000E-01 TIME STEP NUMBER 56772 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282693073E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.823790500E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.51228E-02 0.21618E+01 Friction velocity uk : 0.51228E-02 0.21618E+01 Dimensionless distance yplus : 0.50615E-02 0.21257E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -2.586344343e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29482E+08 1 0.19303E-09 0.36392E+02 0.22680E+04 c Velocity[X] 0.20777E+02 c Velocity[Y] 0.15615E+02 c Velocity[Z] 0.82376E-06 c Pressure 0.20186E-03 69 0.83072E-04 0.13946E-02 0.92057E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -31.753 45.743 5.6032 7.9928 v Velocity[Y] -33.166 35.592 -0.17569 -0.093289 v Velocity[Z] -3.121 3.1569 2.2065e-06 -5.3919e-08 v ǁVelocityǁ 0.0012465 46.005 8.8527 8.2114 v Pressure -3.7865e+05 1.8229e+05 -96776 -93349 v TurbVisc 3.5081e-19 0.027453 0.00021439 7.416e-05 v CourantNb 8.6663e-08 0.011506 0.00017094 4.9704e-06 v FourierNb 1.246e-07 0.038088 0.00015286 6.394e-07 v total_pressure -2.7732e+05 2.8361e+05 4549 7976.5 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1257 0.11724 0.0030959 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.7841e-07 0.041709 0.0003238 5.6098e-06 INSTANT 0.876575000E-01 TIME STEP NUMBER 56773 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282692489E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.823741324E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.62933E-02 0.21622E+01 Friction velocity uk : 0.62933E-02 0.21622E+01 Dimensionless distance yplus : 0.61165E-02 0.21260E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -2.612653300e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29482E+08 1 0.19307E-09 0.36434E+02 0.22692E+04 c Velocity[X] 0.20799E+02 c Velocity[Y] 0.15635E+02 c Velocity[Z] 0.81825E-06 c Pressure 0.20272E-03 294 0.95987E-04 0.13997E-02 0.88509E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -31.765 45.753 5.6031 7.9928 v Velocity[Y] -33.175 35.604 -0.17578 -0.093575 v Velocity[Z] -3.1214 3.157 2.2061e-06 -5.3919e-08 v ǁVelocityǁ 0.0013661 46.016 8.8541 8.2116 v Pressure -3.7715e+05 1.8399e+05 -95102 -92517 v TurbVisc 3.6848e-19 0.027468 0.00021444 7.4254e-05 v CourantNb 9.1909e-08 0.011507 0.00017095 4.9704e-06 v FourierNb 1.246e-07 0.038111 0.00015288 6.4004e-07 v total_pressure -2.7583e+05 2.8532e+05 6223.5 8808 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.126 0.11727 0.0030965 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.7851e-07 0.041733 0.00032383 5.6105e-06 INSTANT 0.876576000E-01 TIME STEP NUMBER 56774 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282692411E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.823700982E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.55767E-02 0.21626E+01 Friction velocity uk : 0.55767E-02 0.21626E+01 Dimensionless distance yplus : 0.55100E-02 0.21265E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -2.574521568e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29482E+08 1 0.19312E-09 0.36455E+02 0.22697E+04 c Velocity[X] 0.20818E+02 c Velocity[Y] 0.15636E+02 c Velocity[Z] 0.81914E-06 c Pressure 0.20353E-03 407 0.81749E-04 0.14046E-02 0.87110E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -31.777 45.763 5.6031 7.9928 v Velocity[Y] -33.185 35.615 -0.17588 -0.09386 v Velocity[Z] -3.1218 3.1572 2.2056e-06 -5.3919e-08 v ǁVelocityǁ 0.0013224 46.026 8.8555 8.2118 v Pressure -3.7577e+05 1.8561e+05 -93414 -91576 v TurbVisc 3.5738e-19 0.027483 0.0002145 7.4348e-05 v CourantNb 8.7075e-08 0.011508 0.00017095 4.9705e-06 v FourierNb 1.246e-07 0.038134 0.0001529 6.4068e-07 v total_pressure -2.7444e+05 2.8694e+05 7911 9748.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1265 0.11731 0.0030972 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.7853e-07 0.041756 0.00032386 5.6112e-06 INSTANT 0.876577000E-01 TIME STEP NUMBER 56775 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282692266E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.823672576E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.63077E-02 0.21630E+01 Friction velocity uk : 0.63077E-02 0.21630E+01 Dimensionless distance yplus : 0.61773E-02 0.21269E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -2.536278750e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29483E+08 1 0.19315E-09 0.36502E+02 0.22711E+04 c Velocity[X] 0.20846E+02 c Velocity[Y] 0.15657E+02 c Velocity[Z] 0.83139E-06 c Pressure 0.20021E-03 9 0.58529E-04 0.13809E-02 0.69693E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -31.789 45.773 5.6031 7.9928 v Velocity[Y] -33.194 35.626 -0.17597 -0.094144 v Velocity[Z] -3.1221 3.1573 2.2051e-06 -5.392e-08 v ǁVelocityǁ 0.0012691 46.036 8.857 8.212 v Pressure -3.7444e+05 1.8719e+05 -91742 -90792 v TurbVisc 3.6885e-19 0.027497 0.00021456 7.4442e-05 v CourantNb 8.6657e-08 0.011508 0.00017096 4.9705e-06 v FourierNb 1.246e-07 0.038157 0.00015293 6.4132e-07 v total_pressure -2.7312e+05 2.8852e+05 9583.5 10533 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1269 0.11735 0.0030978 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.7855e-07 0.04178 0.00032388 5.6119e-06 INSTANT 0.876578000E-01 TIME STEP NUMBER 56776 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282692355E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.823655900E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13168E-02 0.21635E+01 Friction velocity uk : 0.13168E-02 0.21635E+01 Dimensionless distance yplus : 0.12896E-02 0.21273E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -2.442890518e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29483E+08 1 0.19319E-09 0.36539E+02 0.22721E+04 c Velocity[X] 0.20861E+02 c Velocity[Y] 0.15678E+02 c Velocity[Z] 0.83209E-06 c Pressure 0.20151E-03 327 0.77837E-04 0.13891E-02 0.97637E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -31.801 45.783 5.6031 7.9928 v Velocity[Y] -33.203 35.638 -0.17606 -0.094432 v Velocity[Z] -3.1225 3.1574 2.2046e-06 -5.392e-08 v ǁVelocityǁ 0.0012348 46.046 8.8584 8.2123 v Pressure -3.729e+05 1.8898e+05 -90057 -89815 v TurbVisc 3.7226e-19 0.027512 0.00021462 7.4536e-05 v CourantNb 8.7685e-08 0.011509 0.00017097 4.9706e-06 v FourierNb 1.246e-07 0.038279 0.00015295 6.4197e-07 v total_pressure -2.7157e+05 2.903e+05 11268 11510 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1273 0.11738 0.0030985 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.7857e-07 0.041803 0.00032391 5.6125e-06 INSTANT 0.876579000E-01 TIME STEP NUMBER 56777 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282692628E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.823650773E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.29616E-02 0.21639E+01 Friction velocity uk : 0.29616E-02 0.21639E+01 Dimensionless distance yplus : 0.29004E-02 0.21277E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -2.394540810e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29483E+08 1 0.19323E-09 0.36581E+02 0.22733E+04 c Velocity[X] 0.20887E+02 c Velocity[Y] 0.15694E+02 c Velocity[Z] 0.82661E-06 c Pressure 0.20150E-03 425 0.83858E-04 0.13882E-02 0.98031E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -31.813 45.793 5.6031 7.9928 v Velocity[Y] -33.213 35.649 -0.17616 -0.094717 v Velocity[Z] -3.1228 3.1576 2.2042e-06 -5.392e-08 v ǁVelocityǁ 0.0011957 46.057 8.8598 8.2125 v Pressure -3.7147e+05 1.9065e+05 -88333 -88834 v TurbVisc 3.5932e-19 0.027527 0.00021468 7.463e-05 v CourantNb 8.627e-08 0.01151 0.00017097 4.9706e-06 v FourierNb 1.246e-07 0.038582 0.00015297 6.4261e-07 v total_pressure -2.7014e+05 2.9197e+05 12992 12491 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1277 0.11742 0.0030991 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.7859e-07 0.041827 0.00032394 5.6132e-06 INSTANT 0.876580000E-01 TIME STEP NUMBER 56778 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282692902E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.823652254E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.27549E-02 0.21643E+01 Friction velocity uk : 0.27549E-02 0.21643E+01 Dimensionless distance yplus : 0.26979E-02 0.21281E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -2.352285876e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29484E+08 1 0.19327E-09 0.36627E+02 0.22746E+04 c Velocity[X] 0.20907E+02 c Velocity[Y] 0.15720E+02 c Velocity[Z] 0.82542E-06 c Pressure 0.20189E-03 239 0.97110E-04 0.13902E-02 0.82985E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -31.825 45.803 5.6031 7.9928 v Velocity[Y] -33.222 35.661 -0.17625 -0.095006 v Velocity[Z] -3.1232 3.1577 2.2037e-06 -5.392e-08 v ǁVelocityǁ 0.0011542 46.067 8.8613 8.2127 v Pressure -3.7012e+05 1.9224e+05 -86703 -88170 v TurbVisc 3.6643e-19 0.027542 0.00021474 7.4724e-05 v CourantNb 8.5165e-08 0.011511 0.00017098 4.9707e-06 v FourierNb 1.246e-07 0.038888 0.00015299 6.4325e-07 v total_pressure -2.688e+05 2.9357e+05 14622 13155 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1281 0.11745 0.0030998 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.7871e-07 0.04185 0.00032397 5.6139e-06 INSTANT 0.876581000E-01 TIME STEP NUMBER 56779 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282693615E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.823661501E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.29538E-02 0.21647E+01 Friction velocity uk : 0.29538E-02 0.21647E+01 Dimensionless distance yplus : 0.28927E-02 0.21285E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -2.271435581e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29484E+08 1 0.19332E-09 0.36650E+02 0.22752E+04 c Velocity[X] 0.20933E+02 c Velocity[Y] 0.15717E+02 c Velocity[Z] 0.82445E-06 c Pressure 0.20211E-03 126 0.82479E-04 0.13909E-02 0.96044E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -31.837 45.813 5.603 7.9928 v Velocity[Y] -33.232 35.672 -0.17635 -0.095294 v Velocity[Z] -3.1236 3.1578 2.2032e-06 -5.392e-08 v ǁVelocityǁ 0.0011151 46.077 8.8627 8.213 v Pressure -3.6869e+05 1.9392e+05 -84995 -87129 v TurbVisc 3.6132e-19 0.027556 0.00021481 7.4819e-05 v CourantNb 8.3352e-08 0.011512 0.00017098 4.9707e-06 v FourierNb 1.246e-07 0.039195 0.00015301 6.4389e-07 v total_pressure -2.6736e+05 2.9524e+05 16330 14196 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1285 0.11749 0.0031004 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.7918e-07 0.041874 0.00032399 5.6146e-06 INSTANT 0.876582000E-01 TIME STEP NUMBER 56780 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282694316E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.823685418E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.32468E-02 0.21651E+01 Friction velocity uk : 0.32468E-02 0.21651E+01 Dimensionless distance yplus : 0.31797E-02 0.21289E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -2.160597511e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29484E+08 1 0.19335E-09 0.36701E+02 0.22766E+04 c Velocity[X] 0.20958E+02 c Velocity[Y] 0.15743E+02 c Velocity[Z] 0.83497E-06 c Pressure 0.19815E-03 9 0.59128E-04 0.13629E-02 0.68043E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -31.85 45.823 5.603 7.9928 v Velocity[Y] -33.241 35.684 -0.17644 -0.095581 v Velocity[Z] -3.1239 3.1579 2.2027e-06 -5.392e-08 v ǁVelocityǁ 0.0010683 46.088 8.8641 8.2132 v Pressure -3.674e+05 1.9546e+05 -83345 -86393 v TurbVisc 3.7651e-19 0.027571 0.00021487 7.4913e-05 v CourantNb 8.1167e-08 0.011513 0.00017099 4.9708e-06 v FourierNb 1.246e-07 0.039505 0.00015303 6.4454e-07 v total_pressure -2.6607e+05 2.9679e+05 17980 14932 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1289 0.11753 0.003101 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.7965e-07 0.041897 0.00032402 5.6153e-06 INSTANT 0.876583000E-01 TIME STEP NUMBER 56781 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282695208E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.823720308E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12905E-02 0.21656E+01 Friction velocity uk : 0.12905E-02 0.21656E+01 Dimensionless distance yplus : 0.12638E-02 0.21294E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.991782901e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29485E+08 1 0.19339E-09 0.36741E+02 0.22778E+04 c Velocity[X] 0.20979E+02 c Velocity[Y] 0.15762E+02 c Velocity[Z] 0.83804E-06 c Pressure 0.19894E-03 277 0.78431E-04 0.13676E-02 0.98793E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -31.862 45.834 5.603 7.9928 v Velocity[Y] -33.251 35.696 -0.17654 -0.095871 v Velocity[Z] -3.1243 3.1581 2.2023e-06 -5.392e-08 v ǁVelocityǁ 0.0010414 46.098 8.8656 8.2134 v Pressure -3.6724e+05 1.9722e+05 -81675 -85418 v TurbVisc 3.793e-19 0.027586 0.00021493 7.5007e-05 v CourantNb 7.8537e-08 0.011513 0.000171 4.9708e-06 v FourierNb 1.2461e-07 0.039819 0.00015305 6.4518e-07 v total_pressure -2.6591e+05 2.9854e+05 19650 15907 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1294 0.11756 0.0031016 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.8013e-07 0.041921 0.00032405 5.616e-06 INSTANT 0.876584000E-01 TIME STEP NUMBER 56782 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282696312E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.823766998E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.29856E-02 0.21660E+01 Friction velocity uk : 0.29856E-02 0.21660E+01 Dimensionless distance yplus : 0.29238E-02 0.21298E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.885108939e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29485E+08 1 0.19343E-09 0.36786E+02 0.22790E+04 c Velocity[X] 0.21004E+02 c Velocity[Y] 0.15782E+02 c Velocity[Z] 0.82952E-06 c Pressure 0.19838E-03 67 0.84342E-04 0.13630E-02 0.95439E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -31.874 45.844 5.603 7.9928 v Velocity[Y] -33.261 35.707 -0.17663 -0.096159 v Velocity[Z] -3.1246 3.1582 2.2018e-06 -5.392e-08 v ǁVelocityǁ 0.0010101 46.109 8.867 8.2137 v Pressure -3.6867e+05 1.9883e+05 -79988 -84507 v TurbVisc 3.6453e-19 0.027601 0.00021499 7.5102e-05 v CourantNb 7.6682e-08 0.011514 0.000171 4.9709e-06 v FourierNb 1.2461e-07 0.040133 0.00015307 6.4583e-07 v total_pressure -2.6735e+05 3.0015e+05 21337 16818 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1298 0.1176 0.0031022 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.806e-07 0.041944 0.00032407 5.6167e-06 INSTANT 0.876585000E-01 TIME STEP NUMBER 56783 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282697373E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.823820604E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.28964E-02 0.21665E+01 Friction velocity uk : 0.28964E-02 0.21665E+01 Dimensionless distance yplus : 0.28365E-02 0.21302E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.764757039e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29486E+08 1 0.19347E-09 0.36835E+02 0.22804E+04 c Velocity[X] 0.21031E+02 c Velocity[Y] 0.15804E+02 c Velocity[Z] 0.83028E-06 c Pressure 0.19821E-03 251 0.97458E-04 0.13611E-02 0.91505E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -31.887 45.854 5.603 7.9928 v Velocity[Y] -33.27 35.719 -0.17672 -0.096452 v Velocity[Z] -3.125 3.1583 2.2013e-06 -5.392e-08 v ǁVelocityǁ 0.00097813 46.12 8.8685 8.2139 v Pressure -3.6817e+05 2.005e+05 -78339 -83693 v TurbVisc 3.6665e-19 0.027615 0.00021505 7.5197e-05 v CourantNb 7.4555e-08 0.011515 0.00017101 4.9709e-06 v FourierNb 1.2461e-07 0.04045 0.00015309 6.4647e-07 v total_pressure -2.6685e+05 3.0182e+05 22986 17632 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1302 0.11763 0.0031029 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.8108e-07 0.041968 0.0003241 5.6174e-06 INSTANT 0.876586000E-01 TIME STEP NUMBER 56784 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282698951E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.823882798E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.50266E-02 0.21669E+01 Friction velocity uk : 0.50266E-02 0.21669E+01 Dimensionless distance yplus : 0.49227E-02 0.21307E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.594566136e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29486E+08 1 0.19352E-09 0.36861E+02 0.22811E+04 c Velocity[X] 0.21056E+02 c Velocity[Y] 0.15805E+02 c Velocity[Z] 0.83137E-06 c Pressure 0.19801E-03 125 0.82787E-04 0.13590E-02 0.90075E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -31.899 45.865 5.603 7.9928 v Velocity[Y] -33.28 35.731 -0.17682 -0.096742 v Velocity[Z] -3.1253 3.1585 2.2009e-06 -5.392e-08 v ǁVelocityǁ 0.00094972 46.13 8.8699 8.2142 v Pressure -3.6933e+05 2.0209e+05 -76687 -82753 v TurbVisc 3.8248e-19 0.02763 0.00021511 7.5291e-05 v CourantNb 7.236e-08 0.011516 0.00017102 4.971e-06 v FourierNb 1.2461e-07 0.04077 0.00015311 6.4712e-07 v total_pressure -2.68e+05 3.0341e+05 24638 18572 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1307 0.11767 0.0031035 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.8156e-07 0.041991 0.00032413 5.6181e-06 INSTANT 0.876587000E-01 TIME STEP NUMBER 56785 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282700463E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.823956662E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.61982E-02 0.21674E+01 Friction velocity uk : 0.61982E-02 0.21674E+01 Dimensionless distance yplus : 0.60700E-02 0.21311E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.417187578e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29487E+08 1 0.19356E-09 0.36915E+02 0.22826E+04 c Velocity[X] 0.21084E+02 c Velocity[Y] 0.15831E+02 c Velocity[Z] 0.84094E-06 c Pressure 0.19339E-03 9 0.59213E-04 0.13265E-02 0.67088E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -31.911 45.875 5.603 7.9928 v Velocity[Y] -33.29 35.742 -0.17691 -0.097032 v Velocity[Z] -3.1257 3.1586 2.2004e-06 -5.392e-08 v ǁVelocityǁ 0.00091615 46.141 8.8713 8.2145 v Pressure -3.7019e+05 2.0358e+05 -75077 -82046 v TurbVisc 3.9378e-19 0.027645 0.00021517 7.5386e-05 v CourantNb 7.0193e-08 0.011517 0.00017102 4.971e-06 v FourierNb 1.2461e-07 0.041091 0.00015313 6.4776e-07 v total_pressure -2.6887e+05 3.0491e+05 26248 19279 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1311 0.11771 0.0031041 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.8203e-07 0.042028 0.00032416 5.6188e-06 INSTANT 0.876588000E-01 TIME STEP NUMBER 56786 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282702163E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.824042077E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.68362E-02 0.21679E+01 Friction velocity uk : 0.68362E-02 0.21679E+01 Dimensionless distance yplus : 0.66949E-02 0.21316E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.154915030e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29487E+08 1 0.19359E-09 0.36959E+02 0.22838E+04 c Velocity[X] 0.21108E+02 c Velocity[Y] 0.15851E+02 c Velocity[Z] 0.84156E-06 c Pressure 0.19371E-03 184 0.78592E-04 0.13280E-02 0.98441E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -31.924 45.886 5.603 7.9929 v Velocity[Y] -33.3 35.754 -0.17701 -0.097325 v Velocity[Z] -3.1261 3.1587 2.1999e-06 -5.392e-08 v ǁVelocityǁ 0.00090091 46.152 8.8728 8.2147 v Pressure -3.7012e+05 2.0529e+05 -73451 -81098 v TurbVisc 3.9336e-19 0.027659 0.00021523 7.5481e-05 v CourantNb 6.7577e-08 0.011518 0.00017103 4.9711e-06 v FourierNb 1.2461e-07 0.041417 0.00015315 6.4841e-07 v total_pressure -2.688e+05 3.0661e+05 27874 20227 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1316 0.11774 0.0031047 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.8252e-07 0.042355 0.00032418 5.6195e-06 INSTANT 0.876589000E-01 TIME STEP NUMBER 56787 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282704080E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.824139296E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.65445E-02 0.21683E+01 Friction velocity uk : 0.65445E-02 0.21683E+01 Dimensionless distance yplus : 0.64092E-02 0.21321E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -9.851264246e-03 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29488E+08 1 0.19364E-09 0.37007E+02 0.22852E+04 c Velocity[X] 0.21136E+02 c Velocity[Y] 0.15871E+02 c Velocity[Z] 0.84055E-06 c Pressure 0.19265E-03 145 0.84559E-04 0.13199E-02 0.98455E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -31.936 45.897 5.603 7.9929 v Velocity[Y] -33.309 35.766 -0.1771 -0.097616 v Velocity[Z] -3.1264 3.1589 2.1995e-06 -5.392e-08 v ǁVelocityǁ 0.00088185 46.163 8.8742 8.215 v Pressure -3.7152e+05 2.0686e+05 -71805 -80164 v TurbVisc 3.9303e-19 0.027674 0.00021529 7.5576e-05 v CourantNb 6.5664e-08 0.011519 0.00017104 4.9711e-06 v FourierNb 1.2461e-07 0.041742 0.00015318 6.4906e-07 v total_pressure -2.702e+05 3.0819e+05 29520 21161 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1321 0.11778 0.0031053 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.83e-07 0.042682 0.00032421 5.6202e-06 INSTANT 0.876590000E-01 TIME STEP NUMBER 56788 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282705980E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.824243362E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.61644E-02 0.21688E+01 Friction velocity uk : 0.61644E-02 0.21688E+01 Dimensionless distance yplus : 0.60370E-02 0.21325E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -7.577828364e-03 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29488E+08 1 0.19367E-09 0.37058E+02 0.22866E+04 c Velocity[X] 0.21162E+02 c Velocity[Y] 0.15897E+02 c Velocity[Z] 0.84125E-06 c Pressure 0.19202E-03 177 0.97878E-04 0.13149E-02 0.87970E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -31.949 45.907 5.603 7.9929 v Velocity[Y] -33.319 35.778 -0.1772 -0.097911 v Velocity[Z] -3.1268 3.159 2.199e-06 -5.392e-08 v ǁVelocityǁ 0.00086417 46.174 8.8757 8.2152 v Pressure -3.7111e+05 2.0845e+05 -70226 -79473 v TurbVisc 3.9217e-19 0.027689 0.00021536 7.5671e-05 v CourantNb 6.3539e-08 0.01152 0.00017104 4.9712e-06 v FourierNb 1.2461e-07 0.042071 0.0001532 6.4971e-07 v total_pressure -2.6979e+05 3.0978e+05 31099 21852 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1325 0.11781 0.0031059 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.8348e-07 0.043012 0.00032424 5.6209e-06 INSTANT 0.876591000E-01 TIME STEP NUMBER 56789 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282708316E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.824355409E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.54686E-02 0.21693E+01 Friction velocity uk : 0.54686E-02 0.21693E+01 Dimensionless distance yplus : 0.53555E-02 0.21330E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -5.348831335e-03 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29489E+08 1 0.19372E-09 0.37087E+02 0.22874E+04 c Velocity[X] 0.21191E+02 c Velocity[Y] 0.15896E+02 c Velocity[Z] 0.83943E-06 c Pressure 0.19135E-03 130 0.83106E-04 0.13095E-02 0.91366E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -31.961 45.918 5.603 7.993 v Velocity[Y] -33.329 35.79 -0.17729 -0.098205 v Velocity[Z] -3.1271 3.1591 2.1985e-06 -5.3921e-08 v ǁVelocityǁ 0.0008494 46.185 8.8771 8.2155 v Pressure -3.7224e+05 2.0999e+05 -68624 -78530 v TurbVisc 3.9246e-19 0.027704 0.00021542 7.5766e-05 v CourantNb 6.1279e-08 0.01152 0.00017105 4.9713e-06 v FourierNb 1.2461e-07 0.042401 0.00015322 6.5035e-07 v total_pressure -2.7092e+05 3.1132e+05 32701 22795 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.133 0.11785 0.0031065 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.8396e-07 0.043343 0.00032427 5.6216e-06 INSTANT 0.876592000E-01 TIME STEP NUMBER 56790 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282710622E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.824479547E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.38829E-02 0.21698E+01 Friction velocity uk : 0.38829E-02 0.21698E+01 Dimensionless distance yplus : 0.38026E-02 0.21335E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -2.806672193e-03 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29489E+08 1 0.19376E-09 0.37144E+02 0.22890E+04 c Velocity[X] 0.21220E+02 c Velocity[Y] 0.15924E+02 c Velocity[Z] 0.85003E-06 c Pressure 0.18605E-03 9 0.59392E-04 0.12726E-02 0.66191E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -31.974 45.929 5.6031 7.993 v Velocity[Y] -33.339 35.802 -0.17738 -0.098498 v Velocity[Z] -3.1275 3.1593 2.198e-06 -5.3921e-08 v ǁVelocityǁ 0.00083111 46.196 8.8786 8.2158 v Pressure -3.7311e+05 2.1142e+05 -67077 -77848 v TurbVisc 3.9041e-19 0.027718 0.00021548 7.5861e-05 v CourantNb 5.897e-08 0.011521 0.00017106 4.9713e-06 v FourierNb 1.2461e-07 0.042734 0.00015324 6.51e-07 v total_pressure -2.7179e+05 3.1274e+05 34248 23477 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1335 0.11788 0.0031071 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.8445e-07 0.043677 0.0003243 5.6223e-06 INSTANT 0.876593000E-01 TIME STEP NUMBER 56791 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282713109E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.824614600E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.30483E-02 0.21703E+01 Friction velocity uk : 0.30483E-02 0.21703E+01 Dimensionless distance yplus : 0.29853E-02 0.21340E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 7.728381663e-04 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29490E+08 1 0.19379E-09 0.37191E+02 0.22903E+04 c Velocity[X] 0.21246E+02 c Velocity[Y] 0.15944E+02 c Velocity[Z] 0.85125E-06 c Pressure 0.18597E-03 172 0.79143E-04 0.12713E-02 0.96435E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -31.987 45.94 5.6031 7.993 v Velocity[Y] -33.349 35.814 -0.17748 -0.098794 v Velocity[Z] -3.1278 3.1594 2.1976e-06 -5.3921e-08 v ǁVelocityǁ 0.00083004 46.207 8.88 8.2161 v Pressure -3.7304e+05 2.1305e+05 -65522 -76949 v TurbVisc 3.9629e-19 0.027733 0.00021554 7.5956e-05 v CourantNb 5.6262e-08 0.011522 0.00017106 4.9714e-06 v FourierNb 1.2461e-07 0.043071 0.00015326 6.5165e-07 v total_pressure -2.7172e+05 3.1438e+05 35803 24376 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.134 0.11791 0.0031077 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.8494e-07 0.044015 0.00032432 5.623e-06 INSTANT 0.876594000E-01 TIME STEP NUMBER 56792 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282715808E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.824761465E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.32358E-02 0.21708E+01 Friction velocity uk : 0.32358E-02 0.21708E+01 Dimensionless distance yplus : 0.31689E-02 0.21345E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 2.970423557e-03 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29491E+08 1 0.19384E-09 0.37241E+02 0.22917E+04 c Velocity[X] 0.21277E+02 c Velocity[Y] 0.15965E+02 c Velocity[Z] 0.84878E-06 c Pressure 0.18445E-03 109 0.85053E-04 0.12602E-02 0.97468E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -32 45.951 5.6031 7.9931 v Velocity[Y] -33.359 35.826 -0.17757 -0.099087 v Velocity[Z] -3.1282 3.1595 2.1971e-06 -5.3921e-08 v ǁVelocityǁ 0.00082563 46.218 8.8815 8.2163 v Pressure -3.7446e+05 2.1455e+05 -63947 -76051 v TurbVisc 3.9623e-19 0.027748 0.00021561 7.6051e-05 v CourantNb 5.4246e-08 0.011523 0.00017107 4.9715e-06 v FourierNb 1.2461e-07 0.043408 0.00015328 6.523e-07 v total_pressure -2.7314e+05 3.1588e+05 37378 25274 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1345 0.11795 0.0031083 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.8543e-07 0.044353 0.00032435 5.6238e-06 INSTANT 0.876595000E-01 TIME STEP NUMBER 56793 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282718479E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.824915023E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.30018E-02 0.21713E+01 Friction velocity uk : 0.30018E-02 0.21713E+01 Dimensionless distance yplus : 0.29398E-02 0.21350E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 5.775784276e-03 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29491E+08 1 0.19388E-09 0.37296E+02 0.22933E+04 c Velocity[X] 0.21305E+02 c Velocity[Y] 0.15991E+02 c Velocity[Z] 0.84866E-06 c Pressure 0.18341E-03 177 0.98465E-04 0.12524E-02 0.86482E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -32.012 45.961 5.6031 7.9931 v Velocity[Y] -33.37 35.838 -0.17767 -0.099386 v Velocity[Z] -3.1285 3.1597 2.1966e-06 -5.3921e-08 v ǁVelocityǁ 0.00082329 46.229 8.883 8.2166 v Pressure -3.7405e+05 2.1605e+05 -62453 -75409 v TurbVisc 3.9662e-19 0.027762 0.00021567 7.6147e-05 v CourantNb 5.2665e-08 0.011524 0.00017108 4.9715e-06 v FourierNb 1.2461e-07 0.043748 0.0001533 6.5295e-07 v total_pressure -2.7272e+05 3.1738e+05 38872 25916 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.135 0.11798 0.0031089 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.8592e-07 0.044694 0.00032438 5.6245e-06 INSTANT 0.876596000E-01 TIME STEP NUMBER 56794 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282721589E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.825075704E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.18858E-02 0.21718E+01 Friction velocity uk : 0.18858E-02 0.21718E+01 Dimensionless distance yplus : 0.18468E-02 0.21355E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 9.006229291e-03 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29492E+08 1 0.19393E-09 0.37327E+02 0.22941E+04 c Velocity[X] 0.21335E+02 c Velocity[Y] 0.15992E+02 c Velocity[Z] 0.85391E-06 c Pressure 0.18231E-03 91 0.83706E-04 0.12442E-02 0.88657E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -32.025 45.972 5.6031 7.9932 v Velocity[Y] -33.38 35.85 -0.17777 -0.099682 v Velocity[Z] -3.1289 3.1598 2.1962e-06 -5.3921e-08 v ǁVelocityǁ 0.00082398 46.24 8.8844 8.2169 v Pressure -3.7521e+05 2.176e+05 -60933 -74518 v TurbVisc 3.9898e-19 0.027777 0.00021573 7.6242e-05 v CourantNb 5.2632e-08 0.011525 0.00017108 4.9716e-06 v FourierNb 1.2461e-07 0.044088 0.00015332 6.536e-07 v total_pressure -2.7388e+05 3.1893e+05 40392 26807 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1355 0.11802 0.0031095 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.8641e-07 0.045036 0.00032441 5.6252e-06 INSTANT 0.876597000E-01 TIME STEP NUMBER 56795 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282724649E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.825248850E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.71314E-02 0.21723E+01 Friction velocity uk : 0.71314E-02 0.21723E+01 Dimensionless distance yplus : 0.69840E-02 0.21360E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.195706745e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29492E+08 1 0.19397E-09 0.37387E+02 0.22958E+04 c Velocity[X] 0.21367E+02 c Velocity[Y] 0.16020E+02 c Velocity[Z] 0.86216E-06 c Pressure 0.17631E-03 9 0.59440E-04 0.12025E-02 0.63716E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -32.038 45.984 5.6032 7.9932 v Velocity[Y] -33.39 35.862 -0.17786 -0.099978 v Velocity[Z] -3.1293 3.1599 2.1957e-06 -5.3921e-08 v ǁVelocityǁ 0.0008217 46.252 8.8859 8.2172 v Pressure -3.7608e+05 2.1904e+05 -59475 -73878 v TurbVisc 3.9458e-19 0.027791 0.00021579 7.6337e-05 v CourantNb 5.2407e-08 0.011526 0.00017109 4.9717e-06 v FourierNb 1.2461e-07 0.044432 0.00015335 6.5425e-07 v total_pressure -2.7476e+05 3.2036e+05 41850 27447 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.136 0.11805 0.0031101 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.869e-07 0.045381 0.00032444 5.6259e-06 INSTANT 0.876598000E-01 TIME STEP NUMBER 56796 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282727882E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.825431914E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10714E-01 0.21729E+01 Friction velocity uk : 0.10714E-01 0.21729E+01 Dimensionless distance yplus : 0.10493E-01 0.21366E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.622092393e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29493E+08 1 0.19400E-09 0.37436E+02 0.22971E+04 c Velocity[X] 0.21394E+02 c Velocity[Y] 0.16042E+02 c Velocity[Z] 0.86575E-06 c Pressure 0.17590E-03 151 0.79551E-04 0.11991E-02 0.93058E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -32.051 45.995 5.6032 7.9933 v Velocity[Y] -33.4 35.875 -0.17796 -0.10028 v Velocity[Z] -3.1296 3.1601 2.1952e-06 -5.3921e-08 v ǁVelocityǁ 0.00083652 46.263 8.8873 8.2175 v Pressure -3.7602e+05 2.2069e+05 -58013 -73042 v TurbVisc 4.0039e-19 0.027806 0.00021586 7.6433e-05 v CourantNb 5.2332e-08 0.011527 0.0001711 4.9717e-06 v FourierNb 1.2461e-07 0.044778 0.00015337 6.5491e-07 v total_pressure -2.7469e+05 3.2202e+05 43312 28283 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1366 0.11809 0.0031107 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.874e-07 0.045728 0.00032447 5.6267e-06 INSTANT 0.876599000E-01 TIME STEP NUMBER 56797 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282731327E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.825626366E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13946E-01 0.21734E+01 Friction velocity uk : 0.13946E-01 0.21734E+01 Dimensionless distance yplus : 0.13658E-01 0.21371E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.840364280e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29494E+08 1 0.19405E-09 0.37489E+02 0.22986E+04 c Velocity[X] 0.21427E+02 c Velocity[Y] 0.16063E+02 c Velocity[Z] 0.86438E-06 c Pressure 0.17396E-03 100 0.85491E-04 0.11851E-02 0.94919E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -32.064 46.006 5.6032 7.9934 v Velocity[Y] -33.411 35.887 -0.17806 -0.10057 v Velocity[Z] -3.13 3.1602 2.1948e-06 -5.3921e-08 v ǁVelocityǁ 0.00084924 46.274 8.8888 8.2178 v Pressure -3.7745e+05 2.2219e+05 -56540 -72199 v TurbVisc 3.9246e-19 0.027821 0.00021592 7.6529e-05 v CourantNb 5.2505e-08 0.011528 0.00017111 4.9718e-06 v FourierNb 1.2461e-07 0.045125 0.00015339 6.5556e-07 v total_pressure -2.7613e+05 3.2351e+05 44785 29126 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1371 0.11813 0.0031113 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.879e-07 0.046077 0.0003245 5.6274e-06 INSTANT 0.876600000E-01 TIME STEP NUMBER 56798 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282734729E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.825827374E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.14290E-01 0.21740E+01 Friction velocity uk : 0.14290E-01 0.21740E+01 Dimensionless distance yplus : 0.13872E-01 0.21377E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 2.192492373e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29494E+08 1 0.19409E-09 0.37547E+02 0.23002E+04 c Velocity[X] 0.21456E+02 c Velocity[Y] 0.16091E+02 c Velocity[Z] 0.86316E-06 c Pressure 0.17255E-03 162 0.99051E-04 0.11749E-02 0.84636E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -32.077 46.017 5.6033 7.9934 v Velocity[Y] -33.421 35.899 -0.17815 -0.10087 v Velocity[Z] -3.1303 3.1603 2.1943e-06 -5.3921e-08 v ǁVelocityǁ 0.00086526 46.286 8.8903 8.2181 v Pressure -3.7704e+05 2.2364e+05 -55148 -71616 v TurbVisc 3.9274e-19 0.027835 0.00021599 7.6625e-05 v CourantNb 5.2558e-08 0.011529 0.00017111 4.9719e-06 v FourierNb 1.2461e-07 0.045474 0.00015341 6.5621e-07 v total_pressure -2.7572e+05 3.2496e+05 46177 29709 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1377 0.11816 0.0031119 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.8839e-07 0.046427 0.00032452 5.6281e-06 INSTANT 0.876601000E-01 TIME STEP NUMBER 56799 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282738562E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.826035200E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.14482E-01 0.21746E+01 Friction velocity uk : 0.14482E-01 0.21746E+01 Dimensionless distance yplus : 0.14059E-01 0.21382E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 2.540753039e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29495E+08 1 0.19414E-09 0.37580E+02 0.23011E+04 c Velocity[X] 0.21487E+02 c Velocity[Y] 0.16093E+02 c Velocity[Z] 0.87051E-06 c Pressure 0.17113E-03 356 0.84266E-04 0.11645E-02 0.82834E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -32.09 46.028 5.6033 7.9935 v Velocity[Y] -33.431 35.912 -0.17825 -0.10117 v Velocity[Z] -3.1307 3.1605 2.1938e-06 -5.3921e-08 v ǁVelocityǁ 0.0008857 46.297 8.8918 8.2184 v Pressure -3.7825e+05 2.2512e+05 -53747 -70814 v TurbVisc 4.0498e-19 0.02785 0.00021605 7.672e-05 v CourantNb 5.2629e-08 0.01153 0.00017112 4.972e-06 v FourierNb 1.2461e-07 0.045824 0.00015343 6.5687e-07 v total_pressure -2.7692e+05 3.2645e+05 47578 30511 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1382 0.1182 0.0031126 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.8889e-07 0.046778 0.00032455 5.6288e-06 INSTANT 0.876602000E-01 TIME STEP NUMBER 56800 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282742321E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.826254765E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15763E-01 0.21752E+01 Friction velocity uk : 0.15763E-01 0.21752E+01 Dimensionless distance yplus : 0.15303E-01 0.21388E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 2.863742488e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29496E+08 1 0.19417E-09 0.37642E+02 0.23029E+04 c Velocity[X] 0.21524E+02 c Velocity[Y] 0.16118E+02 c Velocity[Z] 0.87710E-06 c Pressure 0.16436E-03 9 0.59450E-04 0.11178E-02 0.64156E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -32.103 46.04 5.6034 7.9936 v Velocity[Y] -33.442 35.924 -0.17835 -0.10147 v Velocity[Z] -3.131 3.1606 2.1934e-06 -5.3921e-08 v ǁVelocityǁ 0.00089428 46.309 8.8932 8.2187 v Pressure -3.7906e+05 2.2643e+05 -52381 -70172 v TurbVisc 4.0127e-19 0.027865 0.00021611 7.6816e-05 v CourantNb 5.2672e-08 0.011531 0.00017113 4.972e-06 v FourierNb 1.2461e-07 0.046176 0.00015345 6.5752e-07 v total_pressure -2.7773e+05 3.2776e+05 48944 31153 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1388 0.11823 0.0031132 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.8939e-07 0.047132 0.00032458 5.6296e-06 INSTANT 0.876603000E-01 TIME STEP NUMBER 56801 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282746273E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.826484401E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.17905E-01 0.21758E+01 Friction velocity uk : 0.17905E-01 0.21758E+01 Dimensionless distance yplus : 0.17382E-01 0.21394E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 3.311175455e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29497E+08 1 0.19421E-09 0.37693E+02 0.23043E+04 c Velocity[X] 0.21550E+02 c Velocity[Y] 0.16143E+02 c Velocity[Z] 0.87613E-06 c Pressure 0.16378E-03 272 0.80165E-04 0.11132E-02 0.88855E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -32.116 46.051 5.6034 7.9936 v Velocity[Y] -33.452 35.936 -0.17845 -0.10177 v Velocity[Z] -3.1314 3.1607 2.1929e-06 -5.3921e-08 v ǁVelocityǁ 0.00094138 46.321 8.8947 8.219 v Pressure -3.7907e+05 2.2799e+05 -51042 -69423 v TurbVisc 3.9997e-19 0.027879 0.00021618 7.6912e-05 v CourantNb 5.2573e-08 0.011532 0.00017114 4.9721e-06 v FourierNb 1.2461e-07 0.046531 0.00015348 6.5818e-07 v total_pressure -2.7774e+05 3.2931e+05 50283 31902 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1394 0.11827 0.0031138 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.899e-07 0.047488 0.00032461 5.6303e-06 INSTANT 0.876604000E-01 TIME STEP NUMBER 56802 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282750412E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.826723735E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.16434E-01 0.21764E+01 Friction velocity uk : 0.16434E-01 0.21764E+01 Dimensionless distance yplus : 0.15872E-01 0.21400E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 3.528785571e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29497E+08 1 0.19426E-09 0.37749E+02 0.23058E+04 c Velocity[X] 0.21584E+02 c Velocity[Y] 0.16164E+02 c Velocity[Z] 0.87467E-06 c Pressure 0.16149E-03 109 0.86397E-04 0.10970E-02 0.88098E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -32.13 46.063 5.6034 7.9937 v Velocity[Y] -33.463 35.949 -0.17855 -0.10207 v Velocity[Z] -3.1317 3.1608 2.1924e-06 -5.3921e-08 v ǁVelocityǁ 0.00097866 46.332 8.8962 8.2193 v Pressure -3.8051e+05 2.2934e+05 -49705 -68693 v TurbVisc 3.992e-19 0.027894 0.00021624 7.7008e-05 v CourantNb 5.2719e-08 0.011533 0.00017114 4.9722e-06 v FourierNb 1.2461e-07 0.046887 0.0001535 6.5883e-07 v total_pressure -2.7919e+05 3.3066e+05 51620 32632 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.14 0.1183 0.0031143 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.904e-07 0.047845 0.00032464 5.631e-06 INSTANT 0.876605000E-01 TIME STEP NUMBER 56803 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282754489E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.826969310E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12133E-01 0.21770E+01 Friction velocity uk : 0.12133E-01 0.21770E+01 Dimensionless distance yplus : 0.11719E-01 0.21406E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 3.894854918e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29498E+08 1 0.19430E-09 0.37808E+02 0.23075E+04 c Velocity[X] 0.21615E+02 c Velocity[Y] 0.16193E+02 c Velocity[Z] 0.87834E-06 c Pressure 0.15981E-03 144 0.99962E-04 0.10849E-02 0.83107E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -32.143 46.074 5.6035 7.9938 v Velocity[Y] -33.473 35.961 -0.17865 -0.10238 v Velocity[Z] -3.1321 3.161 2.192e-06 -5.3921e-08 v ǁVelocityǁ 0.0010206 46.344 8.8977 8.2196 v Pressure -3.8009e+05 2.3068e+05 -48434 -68160 v TurbVisc 3.8817e-19 0.027908 0.00021631 7.7105e-05 v CourantNb 5.2743e-08 0.011534 0.00017115 4.9723e-06 v FourierNb 1.2461e-07 0.047244 0.00015352 6.5949e-07 v total_pressure -2.7877e+05 3.3201e+05 52891 33165 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1406 0.11834 0.0031148 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.909e-07 0.048203 0.00032467 5.6318e-06 INSTANT 0.876606000E-01 TIME STEP NUMBER 56804 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282758996E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.827221972E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.44803E-02 0.21776E+01 Friction velocity uk : 0.44803E-02 0.21776E+01 Dimensionless distance yplus : 0.43271E-02 0.21412E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 4.239328686e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29499E+08 1 0.19435E-09 0.37843E+02 0.23084E+04 c Velocity[X] 0.21647E+02 c Velocity[Y] 0.16196E+02 c Velocity[Z] 0.88526E-06 c Pressure 0.15816E-03 340 0.85008E-04 0.10732E-02 0.78052E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -32.156 46.086 5.6036 7.9939 v Velocity[Y] -33.484 35.974 -0.17875 -0.10268 v Velocity[Z] -3.1324 3.1611 2.1915e-06 -5.3922e-08 v ǁVelocityǁ 0.0010688 46.356 8.8992 8.2199 v Pressure -3.8133e+05 2.3205e+05 -47162 -67432 v TurbVisc 3.9935e-19 0.027923 0.00021637 7.7201e-05 v CourantNb 5.2784e-08 0.011536 0.00017116 4.9724e-06 v FourierNb 1.2461e-07 0.047602 0.00015354 6.6014e-07 v total_pressure -2.8e+05 3.3337e+05 54163 33893 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1412 0.11837 0.0031153 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.9141e-07 0.048562 0.0003247 5.6325e-06 INSTANT 0.876607000E-01 TIME STEP NUMBER 56805 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282763410E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.827485337E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.53585E-02 0.21783E+01 Friction velocity uk : 0.53585E-02 0.21783E+01 Dimensionless distance yplus : 0.51753E-02 0.21419E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 4.556536616e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29500E+08 1 0.19439E-09 0.37908E+02 0.23102E+04 c Velocity[X] 0.21685E+02 c Velocity[Y] 0.16222E+02 c Velocity[Z] 0.89097E-06 c Pressure 0.15059E-03 9 0.59802E-04 0.10211E-02 0.58293E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -32.17 46.097 5.6036 7.9939 v Velocity[Y] -33.495 35.987 -0.17885 -0.10298 v Velocity[Z] -3.1328 3.1612 2.1911e-06 -5.3922e-08 v ǁVelocityǁ 0.001113 46.368 8.9007 8.2203 v Pressure -3.8216e+05 2.3322e+05 -45937 -66874 v TurbVisc 3.9767e-19 0.027938 0.00021644 7.7297e-05 v CourantNb 5.28e-08 0.011537 0.00017117 4.9725e-06 v FourierNb 1.2461e-07 0.047961 0.00015356 6.608e-07 v total_pressure -2.8084e+05 3.3455e+05 55388 34451 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1419 0.11841 0.003116 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.9192e-07 0.048923 0.00032473 5.6333e-06 INSTANT 0.876608000E-01 TIME STEP NUMBER 56806 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282767997E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.827757900E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.72052E-02 0.21789E+01 Friction velocity uk : 0.72052E-02 0.21789E+01 Dimensionless distance yplus : 0.69305E-02 0.21425E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 4.972945754e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29500E+08 1 0.19442E-09 0.37961E+02 0.23117E+04 c Velocity[X] 0.21713E+02 c Velocity[Y] 0.16248E+02 c Velocity[Z] 0.89173E-06 c Pressure 0.14993E-03 266 0.80831E-04 0.10161E-02 0.84933E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -32.183 46.109 5.6037 7.994 v Velocity[Y] -33.505 35.999 -0.17895 -0.10329 v Velocity[Z] -3.1332 3.1614 2.1906e-06 -5.3922e-08 v ǁVelocityǁ 0.0011838 46.38 8.9022 8.2206 v Pressure -3.8216e+05 2.3464e+05 -44728 -66189 v TurbVisc 3.8449e-19 0.027952 0.0002165 7.7394e-05 v CourantNb 5.2629e-08 0.011538 0.00017117 4.9725e-06 v FourierNb 1.2461e-07 0.048323 0.00015359 6.6146e-07 v total_pressure -2.8084e+05 3.3597e+05 56597 35136 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1425 0.11845 0.003117 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.9243e-07 0.049286 0.00032476 5.634e-06 INSTANT 0.876609000E-01 TIME STEP NUMBER 56807 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282772780E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.828039445E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10027E-01 0.21796E+01 Friction velocity uk : 0.10027E-01 0.21796E+01 Dimensionless distance yplus : 0.96448E-02 0.21432E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 5.192516236e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29501E+08 1 0.19447E-09 0.38018E+02 0.23133E+04 c Velocity[X] 0.21749E+02 c Velocity[Y] 0.16269E+02 c Velocity[Z] 0.89259E-06 c Pressure 0.14738E-03 400 0.87104E-04 0.99825E-03 0.85383E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -32.197 46.121 5.6037 7.9941 v Velocity[Y] -33.516 36.012 -0.17905 -0.10359 v Velocity[Z] -3.1335 3.1615 2.1901e-06 -5.3922e-08 v ǁVelocityǁ 0.0012527 46.392 8.9036 8.2209 v Pressure -3.8362e+05 2.3587e+05 -43529 -65518 v TurbVisc 3.9953e-19 0.027967 0.00021657 7.749e-05 v CourantNb 5.2777e-08 0.011539 0.00017118 4.9726e-06 v FourierNb 1.2461e-07 0.048685 0.00015361 6.6211e-07 v total_pressure -2.8229e+05 3.372e+05 57796 35807 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1432 0.11849 0.0031179 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.9294e-07 0.049649 0.00032479 5.6347e-06 INSTANT 0.876610000E-01 TIME STEP NUMBER 56808 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282777476E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.828326800E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.79963E-02 0.21803E+01 Friction velocity uk : 0.79963E-02 0.21803E+01 Dimensionless distance yplus : 0.76914E-02 0.21438E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 5.521650787e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29502E+08 1 0.19451E-09 0.38060E+02 0.23144E+04 c Velocity[X] 0.21777E+02 c Velocity[Y] 0.16284E+02 c Velocity[Z] 0.89970E-06 c Pressure 0.14559E-03 298 0.75468E-04 0.98549E-03 0.55117E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -32.21 46.132 5.6038 7.9942 v Velocity[Y] -33.527 36.024 -0.17916 -0.10389 v Velocity[Z] -3.1339 3.1616 2.1897e-06 -5.3922e-08 v ǁVelocityǁ 0.0013263 46.404 8.9051 8.2212 v Pressure -3.838e+05 2.3705e+05 -42430 -65115 v TurbVisc 3.9744e-19 0.027981 0.00021663 7.7587e-05 v CourantNb 5.2794e-08 0.01154 0.00017119 4.9727e-06 v FourierNb 1.2461e-07 0.049049 0.00015363 6.6277e-07 v total_pressure -2.8248e+05 3.3838e+05 58895 36210 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1438 0.11853 0.0031188 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.9345e-07 0.050014 0.00032482 5.6355e-06 INSTANT 0.876611000E-01 TIME STEP NUMBER 56809 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282782435E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.828619790E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.58813E-02 0.21809E+01 Friction velocity uk : 0.58813E-02 0.21809E+01 Dimensionless distance yplus : 0.56571E-02 0.21445E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 5.825374131e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29503E+08 1 0.19456E-09 0.38124E+02 0.23162E+04 c Velocity[X] 0.21812E+02 c Velocity[Y] 0.16312E+02 c Velocity[Z] 0.93351E-06 c Pressure 0.13842E-03 16 0.54202E-04 0.93643E-03 0.47188E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -32.224 46.144 5.6039 7.9943 v Velocity[Y] -33.538 36.037 -0.17926 -0.1042 v Velocity[Z] -3.1342 3.1618 2.1892e-06 -5.3922e-08 v ǁVelocityǁ 0.0013952 46.416 8.9066 8.2216 v Pressure -3.8392e+05 2.3814e+05 -41337 -64671 v TurbVisc 3.9139e-19 0.027996 0.0002167 7.7683e-05 v CourantNb 5.2806e-08 0.011541 0.0001712 4.9728e-06 v FourierNb 1.2461e-07 0.049413 0.00015365 6.6343e-07 v total_pressure -2.8259e+05 3.3946e+05 59988 36654 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1445 0.11857 0.0031196 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.9396e-07 0.05038 0.00032485 5.6362e-06 INSTANT 0.876612000E-01 TIME STEP NUMBER 56810 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282787638E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.828924404E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.33355E-02 0.21817E+01 Friction velocity uk : 0.33355E-02 0.21817E+01 Dimensionless distance yplus : 0.32083E-02 0.21452E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 6.210045880e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29504E+08 1 0.19460E-09 0.38170E+02 0.23174E+04 c Velocity[X] 0.21848E+02 c Velocity[Y] 0.16322E+02 c Velocity[Z] 0.90948E-06 c Pressure 0.13725E-03 158 0.97144E-04 0.92795E-03 0.79110E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -32.238 46.156 5.604 7.9944 v Velocity[Y] -33.549 36.05 -0.17936 -0.10451 v Velocity[Z] -3.1346 3.1619 2.1887e-06 -5.3922e-08 v ǁVelocityǁ 0.001497 46.428 8.9081 8.2219 v Pressure -3.8486e+05 2.3942e+05 -40221 -63861 v TurbVisc 3.0219e-19 0.02801 0.00021677 7.778e-05 v CourantNb 5.0742e-08 0.011543 0.00017121 4.9729e-06 v FourierNb 1.2461e-07 0.049779 0.00015367 6.6409e-07 v total_pressure -2.8354e+05 3.4074e+05 61104 37464 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1452 0.11861 0.0031205 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.9448e-07 0.050747 0.00032488 5.637e-06 INSTANT 0.876613000E-01 TIME STEP NUMBER 56811 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282792845E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.829239607E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.27683E-02 0.21823E+01 Friction velocity uk : 0.27683E-02 0.21823E+01 Dimensionless distance yplus : 0.26628E-02 0.21459E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 6.337551021e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29505E+08 1 0.19464E-09 0.38225E+02 0.23189E+04 c Velocity[X] 0.21882E+02 c Velocity[Y] 0.16343E+02 c Velocity[Z] 0.90476E-06 c Pressure 0.13343E-03 79 0.81453E-04 0.90159E-03 0.51945E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -32.252 46.168 5.604 7.9945 v Velocity[Y] -33.559 36.063 -0.17947 -0.10481 v Velocity[Z] -3.1349 3.162 2.1883e-06 -5.3922e-08 v ǁVelocityǁ 0.0015865 46.44 8.9097 8.2222 v Pressure -3.8571e+05 2.4053e+05 -39163 -63353 v TurbVisc 5.383e-19 0.028025 0.00021683 7.7877e-05 v CourantNb 4.7647e-08 0.011544 0.00017121 4.973e-06 v FourierNb 1.2461e-07 0.050146 0.0001537 6.6475e-07 v total_pressure -2.8439e+05 3.4186e+05 62162 37972 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1459 0.11866 0.0031215 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.95e-07 0.051116 0.00032491 5.6378e-06 INSTANT 0.876614000E-01 TIME STEP NUMBER 56812 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282798104E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.829557870E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.76895E-02 0.21830E+01 Friction velocity uk : 0.76895E-02 0.21830E+01 Dimensionless distance yplus : 0.73963E-02 0.21466E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 6.599949675e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29505E+08 1 0.19469E-09 0.38290E+02 0.23207E+04 c Velocity[X] 0.21915E+02 c Velocity[Y] 0.16375E+02 c Velocity[Z] 0.92916E-06 c Pressure 0.12893E-03 16 0.54787E-04 0.87065E-03 0.46503E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -32.265 46.18 5.6041 7.9946 v Velocity[Y] -33.57 36.076 -0.17957 -0.10512 v Velocity[Z] -3.1353 3.1621 2.1878e-06 -5.3922e-08 v ǁVelocityǁ 0.0016796 46.452 8.9112 8.2226 v Pressure -3.8668e+05 2.4155e+05 -38170 -62953 v TurbVisc 3.5017e-19 0.028039 0.0002169 7.7973e-05 v CourantNb 4.4709e-08 0.011545 0.00017122 4.9731e-06 v FourierNb 1.2461e-07 0.050515 0.00015372 6.6541e-07 v total_pressure -2.8535e+05 3.4288e+05 63155 38372 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1466 0.1187 0.0031224 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.9551e-07 0.051485 0.00032494 5.6385e-06 INSTANT 0.876615000E-01 TIME STEP NUMBER 56813 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282803433E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.829881827E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10143E-01 0.21838E+01 Friction velocity uk : 0.10143E-01 0.21838E+01 Dimensionless distance yplus : 0.97564E-02 0.21473E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 7.088920998e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29506E+08 1 0.19473E-09 0.38338E+02 0.23220E+04 c Velocity[X] 0.21951E+02 c Velocity[Y] 0.16388E+02 c Velocity[Z] 0.91839E-06 c Pressure 0.12806E-03 139 0.99555E-04 0.86432E-03 0.57852E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -32.279 46.192 5.6042 7.9947 v Velocity[Y] -33.581 36.089 -0.17968 -0.10543 v Velocity[Z] -3.1356 3.1623 2.1874e-06 -5.3922e-08 v ǁVelocityǁ 0.0017884 46.464 8.9127 8.2229 v Pressure -3.871e+05 2.4268e+05 -37197 -62400 v TurbVisc 2.9085e-19 0.028054 0.00021697 7.8071e-05 v CourantNb 4.4549e-08 0.011546 0.00017123 4.9732e-06 v FourierNb 1.2461e-07 0.050883 0.00015374 6.6608e-07 v total_pressure -2.8578e+05 3.44e+05 64128 38925 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1473 0.11875 0.0031233 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.9603e-07 0.051855 0.00032497 5.6393e-06 INSTANT 0.876616000E-01 TIME STEP NUMBER 56814 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282808911E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.830215877E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12697E-01 0.21845E+01 Friction velocity uk : 0.12697E-01 0.21845E+01 Dimensionless distance yplus : 0.12213E-01 0.21480E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 7.122290352e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29507E+08 1 0.19477E-09 0.38393E+02 0.23235E+04 c Velocity[X] 0.21981E+02 c Velocity[Y] 0.16412E+02 c Velocity[Z] 0.91599E-06 c Pressure 0.12407E-03 56 0.83995E-04 0.83686E-03 0.42289E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -32.293 46.204 5.6043 7.9948 v Velocity[Y] -33.592 36.102 -0.17978 -0.10574 v Velocity[Z] -3.136 3.1624 2.1869e-06 -5.3922e-08 v ǁVelocityǁ 0.0018957 46.476 8.9142 8.2233 v Pressure -3.8761e+05 2.4364e+05 -36268 -62014 v TurbVisc 4.3707e-19 0.028068 0.00021703 7.8168e-05 v CourantNb 4.4169e-08 0.011547 0.00017124 4.9733e-06 v FourierNb 1.2461e-07 0.051254 0.00015376 6.6674e-07 v total_pressure -2.8628e+05 3.4496e+05 65057 39311 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.148 0.11879 0.0031243 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.9655e-07 0.052227 0.000325 5.64e-06 INSTANT 0.876617000E-01 TIME STEP NUMBER 56815 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282814489E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.830555852E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.14816E-01 0.21852E+01 Friction velocity uk : 0.14816E-01 0.21852E+01 Dimensionless distance yplus : 0.14251E-01 0.21487E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 7.391149004e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29508E+08 1 0.19482E-09 0.38458E+02 0.23253E+04 c Velocity[X] 0.22010E+02 c Velocity[Y] 0.16449E+02 c Velocity[Z] 0.94530E-06 c Pressure 0.11927E-03 15 0.55089E-04 0.80399E-03 0.43871E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -32.307 46.216 5.6044 7.9949 v Velocity[Y] -33.603 36.115 -0.17989 -0.10605 v Velocity[Z] -3.1363 3.1625 2.1864e-06 -5.3922e-08 v ǁVelocityǁ 0.0020104 46.489 8.9157 8.2236 v Pressure -3.8792e+05 2.4462e+05 -35366 -61676 v TurbVisc 3.8168e-19 0.028083 0.0002171 7.8265e-05 v CourantNb 4.4343e-08 0.011549 0.00017125 4.9734e-06 v FourierNb 1.2461e-07 0.051624 0.00015379 6.674e-07 v total_pressure -2.866e+05 3.4595e+05 65959 39649 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1487 0.11883 0.0031252 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.9708e-07 0.052599 0.00032503 5.6408e-06 INSTANT 0.876618000E-01 TIME STEP NUMBER 56816 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282820243E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.830902708E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.16622E-01 0.21860E+01 Friction velocity uk : 0.16622E-01 0.21860E+01 Dimensionless distance yplus : 0.15988E-01 0.21494E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 7.694435097e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29509E+08 1 0.19487E-09 0.38511E+02 0.23268E+04 c Velocity[X] 0.22053E+02 c Velocity[Y] 0.16457E+02 c Velocity[Z] 0.93837E-06 c Pressure 0.11873E-03 36 0.77276E-04 0.79988E-03 0.87774E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -32.321 46.228 5.6045 7.995 v Velocity[Y] -33.615 36.128 -0.17999 -0.10635 v Velocity[Z] -3.1367 3.1627 2.186e-06 -5.3922e-08 v ǁVelocityǁ 0.0021249 46.501 8.9172 8.2239 v Pressure -3.8933e+05 2.4565e+05 -34457 -60958 v TurbVisc 2.8632e-19 0.028098 0.00021717 7.8362e-05 v CourantNb 4.4391e-08 0.01155 0.00017126 4.9735e-06 v FourierNb 1.2461e-07 0.051997 0.00015381 6.6806e-07 v total_pressure -2.88e+05 3.4698e+05 66868 40367 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1494 0.11887 0.003126 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.976e-07 0.052973 0.00032506 5.6415e-06 INSTANT 0.876619000E-01 TIME STEP NUMBER 56817 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282825885E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.831256965E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.17416E-01 0.21867E+01 Friction velocity uk : 0.17416E-01 0.21867E+01 Dimensionless distance yplus : 0.16767E-01 0.21501E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 7.753801117e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29510E+08 1 0.19491E-09 0.38574E+02 0.23285E+04 c Velocity[X] 0.22084E+02 c Velocity[Y] 0.16491E+02 c Velocity[Z] 0.93681E-06 c Pressure 0.11603E-03 70 0.81326E-04 0.78123E-03 0.61436E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -32.335 46.24 5.6046 7.9951 v Velocity[Y] -33.626 36.141 -0.1801 -0.10667 v Velocity[Z] -3.137 3.1628 2.1855e-06 -5.3922e-08 v ǁVelocityǁ 0.0021695 46.513 8.9187 8.2243 v Pressure -3.8916e+05 2.4651e+05 -33654 -60714 v TurbVisc 4.394e-19 0.028112 0.00021724 7.8459e-05 v CourantNb 4.4492e-08 0.011551 0.00017126 4.9736e-06 v FourierNb 1.2461e-07 0.052371 0.00015383 6.6873e-07 v total_pressure -2.8784e+05 3.4784e+05 67671 40611 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1501 0.11891 0.0031268 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.9812e-07 0.053349 0.0003251 5.6423e-06 INSTANT 0.876620000E-01 TIME STEP NUMBER 56818 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282831890E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.831614601E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10387E-01 0.21874E+01 Friction velocity uk : 0.10387E-01 0.21874E+01 Dimensionless distance yplus : 0.10000E-01 0.21509E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 7.998672280e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29511E+08 1 0.19496E-09 0.38632E+02 0.23301E+04 c Velocity[X] 0.22122E+02 c Velocity[Y] 0.16510E+02 c Velocity[Z] 0.93908E-06 c Pressure 0.11426E-03 102 0.95283E-04 0.76884E-03 0.78580E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -32.349 46.252 5.6046 7.9952 v Velocity[Y] -33.637 36.154 -0.18021 -0.10698 v Velocity[Z] -3.1374 3.1629 2.1851e-06 -5.3922e-08 v ǁVelocityǁ 0.0020368 46.526 8.9203 8.2246 v Pressure -3.9073e+05 2.4739e+05 -32853 -60262 v TurbVisc 4.2466e-19 0.028126 0.0002173 7.8556e-05 v CourantNb 4.4676e-08 0.011552 0.00017127 4.9737e-06 v FourierNb 1.2462e-07 0.052746 0.00015385 6.6939e-07 v total_pressure -2.8941e+05 3.4872e+05 68472 41063 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1509 0.11895 0.0031275 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.9865e-07 0.053724 0.00032513 5.6431e-06 INSTANT 0.876621000E-01 TIME STEP NUMBER 56819 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282837713E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.831979463E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.38596E-02 0.21882E+01 Friction velocity uk : 0.38596E-02 0.21882E+01 Dimensionless distance yplus : 0.37893E-02 0.21516E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 8.137567473e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29512E+08 1 0.19500E-09 0.38674E+02 0.23312E+04 c Velocity[X] 0.22150E+02 c Velocity[Y] 0.16525E+02 c Velocity[Z] 0.93820E-06 c Pressure 0.11266E-03 271 0.80504E-04 0.75763E-03 0.48311E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -32.364 46.265 5.6047 7.9953 v Velocity[Y] -33.648 36.167 -0.18031 -0.10729 v Velocity[Z] -3.1377 3.163 2.1846e-06 -5.3923e-08 v ǁVelocityǁ 0.0019045 46.538 8.9218 8.225 v Pressure -3.9094e+05 2.4824e+05 -32121 -60033 v TurbVisc 4.017e-19 0.028141 0.00021737 7.8654e-05 v CourantNb 4.4774e-08 0.011554 0.00017128 4.9738e-06 v FourierNb 1.2462e-07 0.053121 0.00015388 6.7006e-07 v total_pressure -2.8962e+05 3.4956e+05 69204 41292 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1516 0.11899 0.0031284 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.9918e-07 0.054101 0.00032516 5.6438e-06 INSTANT 0.876622000E-01 TIME STEP NUMBER 56820 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282843743E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.832351474E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15140E-01 0.21890E+01 Friction velocity uk : 0.15140E-01 0.21890E+01 Dimensionless distance yplus : 0.14864E-01 0.21524E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 8.284193806e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29513E+08 1 0.19505E-09 0.38741E+02 0.23330E+04 c Velocity[X] 0.22184E+02 c Velocity[Y] 0.16557E+02 c Velocity[Z] 0.95113E-06 c Pressure 0.10348E-03 9 0.55296E-04 0.69545E-03 0.33399E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -32.378 46.277 5.6048 7.9954 v Velocity[Y] -33.659 36.18 -0.18042 -0.1076 v Velocity[Z] -3.1381 3.1632 2.1841e-06 -5.3923e-08 v ǁVelocityǁ 0.0017777 46.551 8.9233 8.2253 v Pressure -3.9114e+05 2.4893e+05 -31440 -59819 v TurbVisc 3.9733e-19 0.028155 0.00021744 7.8752e-05 v CourantNb 4.4884e-08 0.011555 0.00017129 4.9739e-06 v FourierNb 1.2462e-07 0.053497 0.0001539 6.7072e-07 v total_pressure -2.8982e+05 3.5025e+05 69885 41506 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1524 0.11904 0.0031295 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 6.9971e-07 0.054478 0.00032519 5.6446e-06 INSTANT 0.876623000E-01 TIME STEP NUMBER 56821 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282849970E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.832730051E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.22133E-01 0.21898E+01 Friction velocity uk : 0.22133E-01 0.21898E+01 Dimensionless distance yplus : 0.21309E-01 0.21532E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 8.461113802e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29514E+08 1 0.19509E-09 0.38793E+02 0.23345E+04 c Velocity[X] 0.22222E+02 c Velocity[Y] 0.16571E+02 c Velocity[Z] 0.94809E-06 c Pressure 0.10338E-03 36 0.76518E-04 0.69438E-03 0.78741E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -32.392 46.289 5.6049 7.9955 v Velocity[Y] -33.671 36.193 -0.18053 -0.10791 v Velocity[Z] -3.1384 3.1633 2.1837e-06 -5.3923e-08 v ǁVelocityǁ 0.0016478 46.563 8.9248 8.2257 v Pressure -3.9269e+05 2.498e+05 -30704 -59237 v TurbVisc 3.1871e-19 0.02817 0.00021751 7.8849e-05 v CourantNb 4.4933e-08 0.011556 0.0001713 4.974e-06 v FourierNb 1.2462e-07 0.053874 0.00015392 6.7139e-07 v total_pressure -2.9136e+05 3.5112e+05 70621 42088 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1532 0.11908 0.0031305 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.0024e-07 0.054856 0.00032522 5.6454e-06 INSTANT 0.876624000E-01 TIME STEP NUMBER 56822 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282856021E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.833116092E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.23719E-01 0.21905E+01 Friction velocity uk : 0.23719E-01 0.21905E+01 Dimensionless distance yplus : 0.22830E-01 0.21539E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 8.474390000e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29515E+08 1 0.19514E-09 0.38857E+02 0.23362E+04 c Velocity[X] 0.22253E+02 c Velocity[Y] 0.16604E+02 c Velocity[Z] 0.95076E-06 c Pressure 0.10107E-03 80 0.81152E-04 0.67844E-03 0.59773E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -32.407 46.302 5.605 7.9957 v Velocity[Y] -33.682 36.207 -0.18064 -0.10823 v Velocity[Z] -3.1388 3.1634 2.1832e-06 -5.3923e-08 v ǁVelocityǁ 0.0015324 46.576 8.9264 8.2261 v Pressure -3.9253e+05 2.5049e+05 -30089 -59056 v TurbVisc 4.0284e-19 0.028184 0.00021758 7.8947e-05 v CourantNb 4.5046e-08 0.011557 0.00017131 4.9741e-06 v FourierNb 1.2462e-07 0.054253 0.00015395 6.7206e-07 v total_pressure -2.912e+05 3.5182e+05 71236 42269 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1539 0.11913 0.0031315 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.0077e-07 0.055237 0.00032525 5.6461e-06 INSTANT 0.876625000E-01 TIME STEP NUMBER 56823 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282862418E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.833503808E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.22839E-01 0.21912E+01 Friction velocity uk : 0.22839E-01 0.21912E+01 Dimensionless distance yplus : 0.21983E-01 0.21546E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 8.611645417e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29516E+08 1 0.19519E-09 0.38915E+02 0.23378E+04 c Velocity[X] 0.22292E+02 c Velocity[Y] 0.16623E+02 c Velocity[Z] 0.95650E-06 c Pressure 0.99827E-04 102 0.94893E-04 0.66969E-03 0.74466E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -32.421 46.314 5.6051 7.9958 v Velocity[Y] -33.693 36.22 -0.18075 -0.10854 v Velocity[Z] -3.1391 3.1636 2.1828e-06 -5.3923e-08 v ǁVelocityǁ 0.0014291 46.589 8.9279 8.2264 v Pressure -3.9414e+05 2.5118e+05 -29485 -58713 v TurbVisc 4.1242e-19 0.028199 0.00021765 7.9045e-05 v CourantNb 4.5197e-08 0.011559 0.00017132 4.9742e-06 v FourierNb 1.2462e-07 0.054632 0.00015397 6.7272e-07 v total_pressure -2.9282e+05 3.5251e+05 71840 42612 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1546 0.11917 0.0031324 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.013e-07 0.055617 0.00032529 5.6469e-06 INSTANT 0.876626000E-01 TIME STEP NUMBER 56824 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282868604E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.833896579E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.20273E-01 0.21920E+01 Friction velocity uk : 0.20273E-01 0.21920E+01 Dimensionless distance yplus : 0.19622E-01 0.21554E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 8.662495624e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29517E+08 1 0.19523E-09 0.38957E+02 0.23389E+04 c Velocity[X] 0.22319E+02 c Velocity[Y] 0.16638E+02 c Velocity[Z] 0.96090E-06 c Pressure 0.98857E-04 284 0.80351E-04 0.66277E-03 0.44177E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -32.435 46.327 5.6052 7.9959 v Velocity[Y] -33.705 36.233 -0.18086 -0.10885 v Velocity[Z] -3.1395 3.1637 2.1823e-06 -5.3923e-08 v ǁVelocityǁ 0.0013438 46.601 8.9294 8.2268 v Pressure -3.9436e+05 2.5183e+05 -28955 -58600 v TurbVisc 3.7782e-19 0.028213 0.00021772 7.9143e-05 v CourantNb 4.5298e-08 0.01156 0.00017132 4.9743e-06 v FourierNb 1.2462e-07 0.055012 0.00015399 6.7339e-07 v total_pressure -2.9303e+05 3.5315e+05 72370 42725 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1554 0.11921 0.0031333 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.0184e-07 0.055999 0.00032532 5.6477e-06 INSTANT 0.876627000E-01 TIME STEP NUMBER 56825 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282874991E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.834295703E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15347E-01 0.21928E+01 Friction velocity uk : 0.15347E-01 0.21928E+01 Dimensionless distance yplus : 0.14855E-01 0.21561E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 8.716639422e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29517E+08 1 0.19528E-09 0.39024E+02 0.23407E+04 c Velocity[X] 0.22351E+02 c Velocity[Y] 0.16673E+02 c Velocity[Z] 0.97242E-06 c Pressure 0.89240E-04 7 0.55171E-04 0.59793E-03 0.28939E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -32.45 46.339 5.6053 7.996 v Velocity[Y] -33.716 36.247 -0.18097 -0.10917 v Velocity[Z] -3.1398 3.1638 2.1819e-06 -5.3923e-08 v ǁVelocityǁ 0.0012806 46.614 8.931 8.2271 v Pressure -3.946e+05 2.5231e+05 -28507 -58509 v TurbVisc 3.8415e-19 0.028228 0.00021779 7.9241e-05 v CourantNb 4.541e-08 0.011561 0.00017133 4.9744e-06 v FourierNb 1.2462e-07 0.055393 0.00015402 6.7406e-07 v total_pressure -2.9327e+05 3.5364e+05 72818 42816 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1561 0.11925 0.0031341 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.0238e-07 0.056381 0.00032535 5.6485e-06 INSTANT 0.876628000E-01 TIME STEP NUMBER 56826 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282881551E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.834701042E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.80406E-02 0.21936E+01 Friction velocity uk : 0.80406E-02 0.21936E+01 Dimensionless distance yplus : 0.77825E-02 0.21569E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 8.789801246e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29518E+08 1 0.19533E-09 0.39077E+02 0.23421E+04 c Velocity[X] 0.22392E+02 c Velocity[Y] 0.16685E+02 c Velocity[Z] 0.96894E-06 c Pressure 0.90129E-04 31 0.76529E-04 0.60352E-03 0.73140E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -32.464 46.352 5.6054 7.9961 v Velocity[Y] -33.728 36.26 -0.18108 -0.10948 v Velocity[Z] -3.1402 3.1639 2.1814e-06 -5.3923e-08 v ǁVelocityǁ 0.0012385 46.627 8.9325 8.2275 v Pressure -3.9613e+05 2.5301e+05 -27915 -58027 v TurbVisc 3.798e-19 0.028242 0.00021786 7.9338e-05 v CourantNb 4.5417e-08 0.011563 0.00017134 4.9745e-06 v FourierNb 1.2462e-07 0.055772 0.00015404 6.7473e-07 v total_pressure -2.948e+05 3.5433e+05 73410 43298 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1569 0.11928 0.0031347 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.0291e-07 0.056762 0.00032538 5.6492e-06 INSTANT 0.876629000E-01 TIME STEP NUMBER 56827 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282887923E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.835116777E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.32322E-02 0.21943E+01 Friction velocity uk : 0.32322E-02 0.21943E+01 Dimensionless distance yplus : 0.31284E-02 0.21576E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 8.729069934e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29519E+08 1 0.19537E-09 0.39140E+02 0.23439E+04 c Velocity[X] 0.22420E+02 c Velocity[Y] 0.16721E+02 c Velocity[Z] 0.97527E-06 c Pressure 0.88596E-04 437 0.81229E-04 0.59289E-03 0.59138E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -32.479 46.364 5.6055 7.9963 v Velocity[Y] -33.739 36.273 -0.18119 -0.1098 v Velocity[Z] -3.1405 3.1641 2.181e-06 -5.3923e-08 v ǁVelocityǁ 0.0012198 46.64 8.934 8.2279 v Pressure -3.9603e+05 2.5351e+05 -27540 -57991 v TurbVisc 3.821e-19 0.028257 0.00021792 7.9437e-05 v CourantNb 4.5511e-08 0.011564 0.00017135 4.9746e-06 v FourierNb 1.2462e-07 0.056159 0.00015406 6.754e-07 v total_pressure -2.947e+05 3.5483e+05 73785 43334 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1576 0.11932 0.0031354 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.0345e-07 0.05715 0.00032541 5.65e-06 INSTANT 0.876630000E-01 TIME STEP NUMBER 56828 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282894609E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.835527268E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.36441E-02 0.21951E+01 Friction velocity uk : 0.36441E-02 0.21951E+01 Dimensionless distance yplus : 0.35677E-02 0.21584E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 8.786721047e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29520E+08 1 0.19543E-09 0.39198E+02 0.23454E+04 c Velocity[X] 0.22460E+02 c Velocity[Y] 0.16738E+02 c Velocity[Z] 0.98171E-06 c Pressure 0.88290E-04 32 0.95167E-04 0.59047E-03 0.70619E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -32.494 46.377 5.6056 7.9964 v Velocity[Y] -33.751 36.287 -0.18129 -0.11012 v Velocity[Z] -3.1409 3.1642 2.1805e-06 -5.3923e-08 v ǁVelocityǁ 0.0012037 46.653 8.9356 8.2282 v Pressure -3.9764e+05 2.5395e+05 -27154 -57779 v TurbVisc 3.6841e-19 0.028271 0.00021799 7.9535e-05 v CourantNb 4.8337e-08 0.011565 0.00017136 4.9747e-06 v FourierNb 1.2462e-07 0.056542 0.00015409 6.7607e-07 v total_pressure -2.9632e+05 3.5527e+05 74171 43546 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1584 0.11936 0.0031366 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.0399e-07 0.057534 0.00032545 5.6508e-06 INSTANT 0.876631000E-01 TIME STEP NUMBER 56829 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282901067E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.835944788E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.26868E-02 0.21958E+01 Friction velocity uk : 0.26868E-02 0.21958E+01 Dimensionless distance yplus : 0.26385E-02 0.21591E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 8.729609781e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29521E+08 1 0.19547E-09 0.39240E+02 0.23465E+04 c Velocity[X] 0.22488E+02 c Velocity[Y] 0.16752E+02 c Velocity[Z] 0.98659E-06 c Pressure 0.88374E-04 78 0.80450E-04 0.59067E-03 0.41252E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -32.508 46.39 5.6057 7.9965 v Velocity[Y] -33.763 36.3 -0.1814 -0.11043 v Velocity[Z] -3.1412 3.1643 2.18e-06 -5.3923e-08 v ǁVelocityǁ 0.001195 46.666 8.9371 8.2286 v Pressure -3.9783e+05 2.5438e+05 -26824 -57751 v TurbVisc 3.7558e-19 0.028285 0.00021807 7.9633e-05 v CourantNb 5.1471e-08 0.011566 0.00017137 4.9748e-06 v FourierNb 1.2462e-07 0.056928 0.00015411 6.7674e-07 v total_pressure -2.9651e+05 3.5571e+05 74501 43574 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1591 0.11941 0.0031376 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.0453e-07 0.057921 0.00032548 5.6516e-06 INSTANT 0.876632000E-01 TIME STEP NUMBER 56830 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282907748E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.836368772E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.14511E-01 0.21966E+01 Friction velocity uk : 0.14511E-01 0.21966E+01 Dimensionless distance yplus : 0.14250E-01 0.21599E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 8.710985433e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29522E+08 1 0.19552E-09 0.39306E+02 0.23483E+04 c Velocity[X] 0.22518E+02 c Velocity[Y] 0.16788E+02 c Velocity[Z] 0.99682E-06 c Pressure 0.78722E-04 6 0.55646E-04 0.52583E-03 0.28269E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -32.523 46.402 5.6058 7.9966 v Velocity[Y] -33.774 36.314 -0.18151 -0.11075 v Velocity[Z] -3.1416 3.1645 2.1796e-06 -5.3923e-08 v ǁVelocityǁ 0.0011911 46.679 8.9386 8.229 v Pressure -3.9814e+05 2.5472e+05 -26587 -57749 v TurbVisc 3.7362e-19 0.0283 0.00021814 7.9732e-05 v CourantNb 5.4718e-08 0.011568 0.00017138 4.9749e-06 v FourierNb 1.2462e-07 0.057314 0.00015414 6.7741e-07 v total_pressure -2.9682e+05 3.5604e+05 74738 43576 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1599 0.11946 0.0031387 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.0508e-07 0.058308 0.00032551 5.6524e-06 INSTANT 0.876633000E-01 TIME STEP NUMBER 56831 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282914536E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.836796927E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15382E-01 0.21974E+01 Friction velocity uk : 0.15382E-01 0.21974E+01 Dimensionless distance yplus : 0.14805E-01 0.21606E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 8.718304301e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29524E+08 1 0.19557E-09 0.39359E+02 0.23497E+04 c Velocity[X] 0.22558E+02 c Velocity[Y] 0.16801E+02 c Velocity[Z] 0.99134E-06 c Pressure 0.81160E-04 30 0.76719E-04 0.54178E-03 0.63793E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -32.538 46.415 5.6059 7.9967 v Velocity[Y] -33.786 36.328 -0.18162 -0.11107 v Velocity[Z] -3.1419 3.1646 2.1791e-06 -5.3923e-08 v ǁVelocityǁ 0.0011812 46.692 8.9402 8.2293 v Pressure -3.9969e+05 2.5517e+05 -26204 -57433 v TurbVisc 3.9727e-19 0.028314 0.00021821 7.983e-05 v CourantNb 5.7152e-08 0.011569 0.00017139 4.9751e-06 v FourierNb 1.2462e-07 0.057699 0.00015416 6.7808e-07 v total_pressure -2.9837e+05 3.5649e+05 75121 43892 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1606 0.11951 0.0031396 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.0562e-07 0.058695 0.00032554 5.6531e-06 INSTANT 0.876634000E-01 TIME STEP NUMBER 56832 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282921146E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.837234223E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10251E-01 0.21981E+01 Friction velocity uk : 0.10251E-01 0.21981E+01 Dimensionless distance yplus : 0.10011E-01 0.21614E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 8.538409291e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29525E+08 1 0.19562E-09 0.39422E+02 0.23514E+04 c Velocity[X] 0.22587E+02 c Velocity[Y] 0.16835E+02 c Velocity[Z] 0.10021E-05 c Pressure 0.80778E-04 45 0.81385E-04 0.53890E-03 0.57735E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -32.553 46.428 5.606 7.9969 v Velocity[Y] -33.798 36.341 -0.18173 -0.11139 v Velocity[Z] -3.1423 3.1647 2.1787e-06 -5.3923e-08 v ǁVelocityǁ 0.0011914 46.705 8.9417 8.2297 v Pressure -3.9956e+05 2.5544e+05 -26046 -57489 v TurbVisc 3.6986e-19 0.028329 0.00021828 7.9928e-05 v CourantNb 6.0968e-08 0.01157 0.00017139 4.9752e-06 v FourierNb 1.2462e-07 0.058089 0.00015418 6.7875e-07 v total_pressure -2.9823e+05 3.5677e+05 75279 43836 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1614 0.11955 0.0031406 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.0617e-07 0.059087 0.00032558 5.6539e-06 INSTANT 0.876635000E-01 TIME STEP NUMBER 56833 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282928055E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.837664201E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.31224E-02 0.21989E+01 Friction velocity uk : 0.31224E-02 0.21989E+01 Dimensionless distance yplus : 0.30087E-02 0.21621E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 8.516298301e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29526E+08 1 0.19567E-09 0.39479E+02 0.23530E+04 c Velocity[X] 0.22623E+02 c Velocity[Y] 0.16856E+02 c Velocity[Z] 0.10036E-05 c Pressure 0.81839E-04 112 0.95230E-04 0.54563E-03 0.66416E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -32.568 46.441 5.6061 7.997 v Velocity[Y] -33.809 36.355 -0.18184 -0.11171 v Velocity[Z] -3.1426 3.1648 2.1782e-06 -5.3924e-08 v ǁVelocityǁ 0.0012195 46.718 8.9433 8.2301 v Pressure -4.0127e+05 2.5569e+05 -25892 -57467 v TurbVisc 3.6094e-19 0.028343 0.00021835 8.0027e-05 v CourantNb 5.8596e-08 0.011571 0.0001714 4.9753e-06 v FourierNb 1.2462e-07 0.058478 0.00015421 6.7942e-07 v total_pressure -2.9995e+05 3.5701e+05 75433 43858 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1621 0.1196 0.0031414 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.0672e-07 0.059477 0.00032561 5.6547e-06 INSTANT 0.876636000E-01 TIME STEP NUMBER 56834 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282934685E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.838101364E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12939E-01 0.21996E+01 Friction velocity uk : 0.12939E-01 0.21996E+01 Dimensionless distance yplus : 0.12467E-01 0.21628E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 8.417534111e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29527E+08 1 0.19572E-09 0.39520E+02 0.23540E+04 c Velocity[X] 0.22651E+02 c Velocity[Y] 0.16869E+02 c Velocity[Z] 0.10044E-05 c Pressure 0.83307E-04 95 0.80484E-04 0.55507E-03 0.39962E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -32.582 46.454 5.6062 7.9971 v Velocity[Y] -33.821 36.369 -0.18195 -0.11203 v Velocity[Z] -3.143 3.165 2.1778e-06 -5.3924e-08 v ǁVelocityǁ 0.0012608 46.731 8.9448 8.2304 v Pressure -4.0145e+05 2.5591e+05 -25774 -57522 v TurbVisc 3.4657e-19 0.028357 0.00021842 8.0126e-05 v CourantNb 5.5387e-08 0.011573 0.00017141 4.9754e-06 v FourierNb 1.2462e-07 0.058868 0.00015423 6.801e-07 v total_pressure -3.0013e+05 3.5724e+05 75551 43803 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1628 0.11965 0.0031426 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.0726e-07 0.059868 0.00032564 5.6555e-06 INSTANT 0.876637000E-01 TIME STEP NUMBER 56835 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282941534E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.838543789E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13828E-01 0.22004E+01 Friction velocity uk : 0.13828E-01 0.22004E+01 Dimensionless distance yplus : 0.13309E-01 0.21636E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 8.321013991e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29528E+08 1 0.19577E-09 0.39585E+02 0.23558E+04 c Velocity[X] 0.22682E+02 c Velocity[Y] 0.16903E+02 c Velocity[Z] 0.10112E-05 c Pressure 0.74477E-04 6 0.55490E-04 0.49593E-03 0.26968E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -32.597 46.467 5.6063 7.9973 v Velocity[Y] -33.833 36.382 -0.18206 -0.11235 v Velocity[Z] -3.1433 3.1651 2.1773e-06 -5.3924e-08 v ǁVelocityǁ 0.0013178 46.744 8.9463 8.2308 v Pressure -4.0175e+05 2.5606e+05 -25727 -57563 v TurbVisc 3.7266e-19 0.028372 0.00021849 8.0225e-05 v CourantNb 5.2235e-08 0.011574 0.00017142 4.9755e-06 v FourierNb 1.2462e-07 0.059259 0.00015426 6.8077e-07 v total_pressure -3.0042e+05 3.5739e+05 75598 43762 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1636 0.1197 0.0031437 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.0781e-07 0.06026 0.00032568 5.6563e-06 INSTANT 0.876638000E-01 TIME STEP NUMBER 56836 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282948499E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.838989503E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11522E-01 0.22011E+01 Friction velocity uk : 0.11522E-01 0.22011E+01 Dimensionless distance yplus : 0.11108E-01 0.21643E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 8.282987270e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29529E+08 1 0.19582E-09 0.39638E+02 0.23572E+04 c Velocity[X] 0.22718E+02 c Velocity[Y] 0.16920E+02 c Velocity[Z] 0.10123E-05 c Pressure 0.78652E-04 95 0.76405E-04 0.52340E-03 0.53688E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -32.612 46.48 5.6064 7.9974 v Velocity[Y] -33.845 36.396 -0.18217 -0.11267 v Velocity[Z] -3.1437 3.1652 2.1769e-06 -5.3924e-08 v ǁVelocityǁ 0.001368 46.757 8.9479 8.2312 v Pressure -4.0339e+05 2.5623e+05 -25621 -57539 v TurbVisc 4.0416e-19 0.028386 0.00021856 8.0323e-05 v CourantNb 4.9217e-08 0.011575 0.00017143 4.9756e-06 v FourierNb 1.2462e-07 0.059649 0.00015428 6.8145e-07 v total_pressure -3.0206e+05 3.5756e+05 75704 43786 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1643 0.11974 0.0031446 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.0837e-07 0.060651 0.00032571 5.6571e-06 INSTANT 0.876639000E-01 TIME STEP NUMBER 56837 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282955207E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.839441576E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13518E-02 0.22018E+01 Friction velocity uk : 0.13518E-02 0.22018E+01 Dimensionless distance yplus : 0.13032E-02 0.21650E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 7.992881137e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29530E+08 1 0.19587E-09 0.39700E+02 0.23589E+04 c Velocity[X] 0.22748E+02 c Velocity[Y] 0.16952E+02 c Velocity[Z] 0.10189E-05 c Pressure 0.79639E-04 46 0.81199E-04 0.52963E-03 0.56471E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -32.627 46.493 5.6065 7.9975 v Velocity[Y] -33.857 36.41 -0.18228 -0.113 v Velocity[Z] -3.144 3.1653 2.1764e-06 -5.3924e-08 v ǁVelocityǁ 0.0014272 46.771 8.9494 8.2315 v Pressure -4.0323e+05 2.5632e+05 -25654 -57642 v TurbVisc 3.5756e-19 0.0284 0.00021863 8.0422e-05 v CourantNb 4.6073e-08 0.011577 0.00017144 4.9757e-06 v FourierNb 1.2462e-07 0.060044 0.00015431 6.8212e-07 v total_pressure -3.019e+05 3.5765e+05 75671 43683 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.165 0.11978 0.0031454 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.0892e-07 0.061048 0.00032574 5.6578e-06 INSTANT 0.876640000E-01 TIME STEP NUMBER 56838 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282962231E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.839888378E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.34274E-02 0.22026E+01 Friction velocity uk : 0.34274E-02 0.22026E+01 Dimensionless distance yplus : 0.33394E-02 0.21657E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 7.932594063e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29531E+08 1 0.19593E-09 0.39756E+02 0.23603E+04 c Velocity[X] 0.22783E+02 c Velocity[Y] 0.16974E+02 c Velocity[Z] 0.10230E-05 c Pressure 0.82173E-04 110 0.94790E-04 0.54614E-03 0.65371E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -32.642 46.506 5.6066 7.9976 v Velocity[Y] -33.869 36.424 -0.18239 -0.11332 v Velocity[Z] -3.1444 3.1655 2.176e-06 -5.3924e-08 v ǁVelocityǁ 0.0014863 46.784 8.951 8.2319 v Pressure -4.0498e+05 2.5635e+05 -25726 -57740 v TurbVisc 3.6041e-19 0.028415 0.00021871 8.0521e-05 v CourantNb 4.3046e-08 0.011578 0.00017145 4.9758e-06 v FourierNb 1.2462e-07 0.060438 0.00015433 6.828e-07 v total_pressure -3.0365e+05 3.5768e+05 75599 43585 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1657 0.11983 0.0031465 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.0947e-07 0.061443 0.00032578 5.6586e-06 INSTANT 0.876641000E-01 TIME STEP NUMBER 56839 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282968950E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.840340095E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.68532E-02 0.22033E+01 Friction velocity uk : 0.68532E-02 0.22033E+01 Dimensionless distance yplus : 0.66105E-02 0.21665E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 7.794366661e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29532E+08 1 0.19597E-09 0.39796E+02 0.23614E+04 c Velocity[X] 0.22810E+02 c Velocity[Y] 0.16986E+02 c Velocity[Z] 0.10255E-05 c Pressure 0.85064E-04 71 0.80305E-04 0.56500E-03 0.42113E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -32.657 46.519 5.6067 7.9978 v Velocity[Y] -33.881 36.437 -0.1825 -0.11364 v Velocity[Z] -3.1447 3.1656 2.1755e-06 -5.3924e-08 v ǁVelocityǁ 0.001543 46.797 8.9525 8.2323 v Pressure -4.0518e+05 2.5635e+05 -25834 -57943 v TurbVisc 3.6776e-19 0.028429 0.00021878 8.062e-05 v CourantNb 4.0125e-08 0.011579 0.00017146 4.9759e-06 v FourierNb 1.2462e-07 0.060832 0.00015436 6.8347e-07 v total_pressure -3.0385e+05 3.5767e+05 75491 43382 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1665 0.11988 0.0031475 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.1003e-07 0.061839 0.00032581 5.6594e-06 INSTANT 0.876642000E-01 TIME STEP NUMBER 56840 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282975871E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.840795411E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.95768E-02 0.22040E+01 Friction velocity uk : 0.95768E-02 0.22040E+01 Dimensionless distance yplus : 0.92377E-02 0.21672E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 7.643972199e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29533E+08 1 0.19603E-09 0.39860E+02 0.23631E+04 c Velocity[X] 0.22839E+02 c Velocity[Y] 0.17020E+02 c Velocity[Z] 0.10347E-05 c Pressure 0.78009E-04 6 0.55792E-04 0.51781E-03 0.27552E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -32.672 46.532 5.6068 7.9979 v Velocity[Y] -33.893 36.451 -0.18261 -0.11396 v Velocity[Z] -3.1451 3.1657 2.1751e-06 -5.3924e-08 v ǁVelocityǁ 0.0015934 46.811 8.9541 8.2327 v Pressure -4.0549e+05 2.5636e+05 -25916 -58015 v TurbVisc 3.5956e-19 0.028443 0.00021885 8.072e-05 v CourantNb 3.7248e-08 0.01158 0.00017146 4.976e-06 v FourierNb 1.2462e-07 0.061228 0.00015438 6.8415e-07 v total_pressure -3.0416e+05 3.5769e+05 75409 43310 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1672 0.11992 0.0031486 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.1059e-07 0.062235 0.00032584 5.6602e-06 INSTANT 0.876643000E-01 TIME STEP NUMBER 56841 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282982902E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.841252493E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.26090E-02 0.22047E+01 Friction velocity uk : 0.26090E-02 0.22047E+01 Dimensionless distance yplus : 0.25184E-02 0.21679E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 7.426108888e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29534E+08 1 0.19608E-09 0.39913E+02 0.23645E+04 c Velocity[X] 0.22875E+02 c Velocity[Y] 0.17037E+02 c Velocity[Z] 0.10354E-05 c Pressure 0.83430E-04 45 0.76525E-04 0.55344E-03 0.55113E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -32.687 46.545 5.6069 7.998 v Velocity[Y] -33.905 36.465 -0.18272 -0.11429 v Velocity[Z] -3.1454 3.1658 2.1746e-06 -5.3924e-08 v ǁVelocityǁ 0.0016447 46.824 8.9556 8.233 v Pressure -4.0715e+05 2.5621e+05 -26195 -58234 v TurbVisc 3.2881e-19 0.028458 0.00021892 8.0819e-05 v CourantNb 3.4289e-08 0.011582 0.00017147 4.9762e-06 v FourierNb 1.2462e-07 0.061626 0.0001544 6.8483e-07 v total_pressure -3.0582e+05 3.5754e+05 75130 43091 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1679 0.11997 0.0031496 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.1114e-07 0.062634 0.00032588 5.661e-06 INSTANT 0.876644000E-01 TIME STEP NUMBER 56842 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282989628E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.841705532E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.61235E-02 0.22054E+01 Friction velocity uk : 0.61235E-02 0.22054E+01 Dimensionless distance yplus : 0.59213E-02 0.21685E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 7.367699986e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29535E+08 1 0.19613E-09 0.39973E+02 0.23661E+04 c Velocity[X] 0.22904E+02 c Velocity[Y] 0.17070E+02 c Velocity[Z] 0.10365E-05 c Pressure 0.85862E-04 87 0.81590E-04 0.56921E-03 0.59404E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -32.703 46.559 5.607 7.9981 v Velocity[Y] -33.917 36.479 -0.18283 -0.11461 v Velocity[Z] -3.1458 3.166 2.1742e-06 -5.3924e-08 v ǁVelocityǁ 0.0016871 46.838 8.9572 8.2334 v Pressure -4.0702e+05 2.5608e+05 -26396 -58467 v TurbVisc 3.684e-19 0.028472 0.000219 8.0918e-05 v CourantNb 3.1668e-08 0.011583 0.00017148 4.9763e-06 v FourierNb 1.2462e-07 0.06202 0.00015443 6.8551e-07 v total_pressure -3.0569e+05 3.5741e+05 74929 42858 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1685 0.12002 0.0031508 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.117e-07 0.06303 0.00032591 5.6618e-06 INSTANT 0.876645000E-01 TIME STEP NUMBER 56843 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282996664E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.842169150E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.49272E-02 0.22061E+01 Friction velocity uk : 0.49272E-02 0.22061E+01 Dimensionless distance yplus : 0.47601E-02 0.21692E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 7.174033921e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29536E+08 1 0.19619E-09 0.40028E+02 0.23675E+04 c Velocity[X] 0.22937E+02 c Velocity[Y] 0.17091E+02 c Velocity[Z] 0.10439E-05 c Pressure 0.89597E-04 118 0.95216E-04 0.59359E-03 0.66225E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -32.718 46.572 5.607 7.9983 v Velocity[Y] -33.929 36.493 -0.18294 -0.11494 v Velocity[Z] -3.1461 3.1661 2.1737e-06 -5.3924e-08 v ǁVelocityǁ 0.0017239 46.851 8.9587 8.2338 v Pressure -4.0879e+05 2.5593e+05 -26675 -58654 v TurbVisc 3.5859e-19 0.028486 0.00021907 8.1018e-05 v CourantNb 2.9037e-08 0.011584 0.00017149 4.9764e-06 v FourierNb 1.2462e-07 0.062418 0.00015445 6.8618e-07 v total_pressure -3.0746e+05 3.5726e+05 74650 42671 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1692 0.12007 0.003152 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.1226e-07 0.063429 0.00032594 5.6626e-06 INSTANT 0.876646000E-01 TIME STEP NUMBER 56844 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283003375E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.842629753E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.18775E-02 0.22068E+01 Friction velocity uk : 0.18775E-02 0.22068E+01 Dimensionless distance yplus : 0.18199E-02 0.21699E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 6.996214757e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29537E+08 1 0.19624E-09 0.40068E+02 0.23685E+04 c Velocity[X] 0.22966E+02 c Velocity[Y] 0.17102E+02 c Velocity[Z] 0.10511E-05 c Pressure 0.93575E-04 415 0.80920E-04 0.61956E-03 0.45768E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -32.733 46.585 5.6071 7.9984 v Velocity[Y] -33.941 36.507 -0.18304 -0.11526 v Velocity[Z] -3.1465 3.1662 2.1733e-06 -5.3924e-08 v ǁVelocityǁ 0.0017531 46.865 8.9602 8.2342 v Pressure -4.0897e+05 2.5569e+05 -27003 -58965 v TurbVisc 3.75e-19 0.028501 0.00021914 8.1117e-05 v CourantNb 2.6416e-08 0.011585 0.0001715 4.9765e-06 v FourierNb 1.2462e-07 0.062816 0.00015448 6.8686e-07 v total_pressure -3.0764e+05 3.5701e+05 74322 42360 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1699 0.12014 0.0031536 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.1283e-07 0.063828 0.00032598 5.6634e-06 INSTANT 0.876647000E-01 TIME STEP NUMBER 56845 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283010285E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.843091608E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.22443E-02 0.22075E+01 Friction velocity uk : 0.22443E-02 0.22075E+01 Dimensionless distance yplus : 0.21726E-02 0.21706E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 6.828437391e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29538E+08 1 0.19630E-09 0.40130E+02 0.23702E+04 c Velocity[X] 0.22987E+02 c Velocity[Y] 0.17143E+02 c Velocity[Z] 0.10605E-05 c Pressure 0.88457E-04 7 0.56866E-04 0.58530E-03 0.37202E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -32.748 46.598 5.6072 7.9985 v Velocity[Y] -33.953 36.521 -0.18315 -0.11559 v Velocity[Z] -3.1468 3.1663 2.1728e-06 -5.3924e-08 v ǁVelocityǁ 0.0017732 46.878 8.9618 8.2345 v Pressure -4.0943e+05 2.5552e+05 -27344 -59222 v TurbVisc 3.6503e-19 0.028515 0.00021922 8.1217e-05 v CourantNb 2.3864e-08 0.011586 0.00017151 4.9766e-06 v FourierNb 1.2462e-07 0.063214 0.0001545 6.8754e-07 v total_pressure -3.0811e+05 3.5685e+05 73981 42103 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1706 0.1202 0.0031551 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.1339e-07 0.064228 0.00032601 5.6641e-06 INSTANT 0.876648000E-01 TIME STEP NUMBER 56846 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283017227E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.843553267E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11858E-01 0.22082E+01 Friction velocity uk : 0.11858E-01 0.22082E+01 Dimensionless distance yplus : 0.11480E-01 0.21713E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 6.615992067e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29539E+08 1 0.19635E-09 0.40183E+02 0.23716E+04 c Velocity[X] 0.23029E+02 c Velocity[Y] 0.17153E+02 c Velocity[Z] 0.10637E-05 c Pressure 0.94583E-04 69 0.77334E-04 0.62543E-03 0.58983E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -32.763 46.612 5.6073 7.9987 v Velocity[Y] -33.965 36.535 -0.18326 -0.11592 v Velocity[Z] -3.1472 3.1665 2.1724e-06 -5.3924e-08 v ǁVelocityǁ 0.0017133 46.892 8.9633 8.2349 v Pressure -4.1096e+05 2.5513e+05 -27795 -59525 v TurbVisc 3.7302e-19 0.028529 0.00021929 8.1316e-05 v CourantNb 2.1544e-08 0.011588 0.00017152 4.9767e-06 v FourierNb 1.2462e-07 0.063615 0.00015453 6.8822e-07 v total_pressure -3.0964e+05 3.5646e+05 73530 41800 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1713 0.12027 0.0031566 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.1395e-07 0.06463 0.00032604 5.6649e-06 INSTANT 0.876649000E-01 TIME STEP NUMBER 56847 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283023912E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.844012534E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.17787E-01 0.22089E+01 Friction velocity uk : 0.17787E-01 0.22089E+01 Dimensionless distance yplus : 0.17121E-01 0.21720E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 6.529342915e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29540E+08 1 0.19641E-09 0.40242E+02 0.23732E+04 c Velocity[X] 0.23054E+02 c Velocity[Y] 0.17188E+02 c Velocity[Z] 0.10731E-05 c Pressure 0.97980E-04 50 0.82712E-04 0.64747E-03 0.65158E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -32.779 46.625 5.6074 7.9988 v Velocity[Y] -33.977 36.549 -0.18337 -0.11625 v Velocity[Z] -3.1475 3.1666 2.1719e-06 -5.3925e-08 v ǁVelocityǁ 0.0013835 46.905 8.9649 8.2353 v Pressure -4.1092e+05 2.5478e+05 -28245 -59911 v TurbVisc 3.5909e-19 0.028543 0.00021936 8.1416e-05 v CourantNb 1.8879e-08 0.011589 0.00017152 4.9768e-06 v FourierNb 1.2462e-07 0.064012 0.00015455 6.889e-07 v total_pressure -3.0959e+05 3.5611e+05 73080 41414 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.172 0.12034 0.0031582 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.1452e-07 0.065028 0.00032608 5.6657e-06 INSTANT 0.876650000E-01 TIME STEP NUMBER 56848 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283030853E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.844476556E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.17937E-01 0.22096E+01 Friction velocity uk : 0.17937E-01 0.22096E+01 Dimensionless distance yplus : 0.17265E-01 0.21726E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 6.342446783e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29541E+08 1 0.19647E-09 0.40296E+02 0.23746E+04 c Velocity[X] 0.23087E+02 c Velocity[Y] 0.17209E+02 c Velocity[Z] 0.10636E-05 c Pressure 0.10247E-03 119 0.96600E-04 0.67669E-03 0.68131E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -32.794 46.639 5.6075 7.9989 v Velocity[Y] -33.99 36.563 -0.18348 -0.11658 v Velocity[Z] -3.1479 3.1667 2.1715e-06 -5.3925e-08 v ǁVelocityǁ 0.0011004 46.919 8.9664 8.2357 v Pressure -4.127e+05 2.5443e+05 -28738 -60189 v TurbVisc 3.6062e-19 0.028558 0.00021944 8.1516e-05 v CourantNb 1.6605e-08 0.01159 0.00017153 4.9769e-06 v FourierNb 1.2462e-07 0.064411 0.00015458 6.8958e-07 v total_pressure -3.1137e+05 3.5576e+05 72587 41136 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1726 0.1204 0.0031597 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.1509e-07 0.065429 0.00032611 5.6665e-06 INSTANT 0.876651000E-01 TIME STEP NUMBER 56849 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283037462E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.844939060E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.18036E-01 0.22102E+01 Friction velocity uk : 0.18036E-01 0.22102E+01 Dimensionless distance yplus : 0.17360E-01 0.21733E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 6.184242395e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29542E+08 1 0.19651E-09 0.40334E+02 0.23755E+04 c Velocity[X] 0.23114E+02 c Velocity[Y] 0.17220E+02 c Velocity[Z] 0.10645E-05 c Pressure 0.10708E-03 488 0.82103E-04 0.70667E-03 0.54217E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -32.809 46.652 5.6075 7.999 v Velocity[Y] -34.002 36.578 -0.18359 -0.1169 v Velocity[Z] -3.1482 3.1669 2.171e-06 -5.3925e-08 v ǁVelocityǁ 0.00090954 46.933 8.968 8.236 v Pressure -4.1291e+05 2.5396e+05 -29296 -60658 v TurbVisc 3.8047e-19 0.028572 0.00021951 8.1616e-05 v CourantNb 1.4333e-08 0.011591 0.00017154 4.977e-06 v FourierNb 1.2462e-07 0.064811 0.0001546 6.9027e-07 v total_pressure -3.1158e+05 3.5529e+05 72029 40667 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1733 0.12046 0.0031611 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.1566e-07 0.06583 0.00032614 5.6673e-06 INSTANT 0.876652000E-01 TIME STEP NUMBER 56850 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283044244E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.845400654E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.18086E-01 0.22109E+01 Friction velocity uk : 0.18086E-01 0.22109E+01 Dimensionless distance yplus : 0.17408E-01 0.21739E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 6.030290340e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29543E+08 1 0.19657E-09 0.40395E+02 0.23771E+04 c Velocity[X] 0.23134E+02 c Velocity[Y] 0.17261E+02 c Velocity[Z] 0.10790E-05 c Pressure 0.10347E-03 12 0.58165E-04 0.68243E-03 0.44405E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -32.824 46.666 5.6076 7.9992 v Velocity[Y] -34.014 36.592 -0.18369 -0.11724 v Velocity[Z] -3.1485 3.167 2.1706e-06 -5.3925e-08 v ǁVelocityǁ 0.00086827 46.946 8.9695 8.2364 v Pressure -4.134e+05 2.5358e+05 -29884 -61056 v TurbVisc 3.6338e-19 0.028586 0.00021958 8.1716e-05 v CourantNb 1.2104e-08 0.011593 0.00017155 4.9772e-06 v FourierNb 1.2462e-07 0.065211 0.00015463 6.9095e-07 v total_pressure -3.1208e+05 3.549e+05 71441 40269 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1739 0.12052 0.0031624 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.1623e-07 0.066231 0.00032618 5.6681e-06 INSTANT 0.876653000E-01 TIME STEP NUMBER 56851 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283051003E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.845860903E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.17648E-01 0.22115E+01 Friction velocity uk : 0.17648E-01 0.22115E+01 Dimensionless distance yplus : 0.17111E-01 0.21746E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 5.850150631e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29544E+08 1 0.19663E-09 0.40447E+02 0.23785E+04 c Velocity[X] 0.23175E+02 c Velocity[Y] 0.17272E+02 c Velocity[Z] 0.10811E-05 c Pressure 0.10991E-03 72 0.78461E-04 0.72446E-03 0.62001E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -32.84 46.679 5.6077 7.9993 v Velocity[Y] -34.026 36.606 -0.1838 -0.11757 v Velocity[Z] -3.1489 3.1671 2.1701e-06 -5.3925e-08 v ǁVelocityǁ 0.00090497 46.96 8.9711 8.2368 v Pressure -4.1493e+05 2.53e+05 -30497 -61423 v TurbVisc 5.8462e-19 0.0286 0.00021966 8.1816e-05 v CourantNb 1.0249e-08 0.011594 0.00017156 4.9773e-06 v FourierNb 1.2462e-07 0.065612 0.00015465 6.9163e-07 v total_pressure -3.1361e+05 3.5432e+05 70828 39902 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1746 0.12058 0.0031637 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.168e-07 0.066632 0.00032621 5.6689e-06 INSTANT 0.876654000E-01 TIME STEP NUMBER 56852 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283057560E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.846319960E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15010E-01 0.22122E+01 Friction velocity uk : 0.15010E-01 0.22122E+01 Dimensionless distance yplus : 0.14553E-01 0.21753E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 5.763728710e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29546E+08 1 0.19669E-09 0.40505E+02 0.23800E+04 c Velocity[X] 0.23198E+02 c Velocity[Y] 0.17307E+02 c Velocity[Z] 0.10876E-05 c Pressure 0.11372E-03 121 0.84227E-04 0.74906E-03 0.73359E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -32.855 46.693 5.6078 7.9994 v Velocity[Y] -34.039 36.62 -0.18391 -0.1179 v Velocity[Z] -3.1492 3.1672 2.1697e-06 -5.3925e-08 v ǁVelocityǁ 0.001086 46.974 8.9726 8.2371 v Pressure -4.1491e+05 2.5242e+05 -31199 -61975 v TurbVisc 3.2893e-19 0.028615 0.00021973 8.1916e-05 v CourantNb 8.7386e-09 0.011595 0.00017157 4.9774e-06 v FourierNb 1.2462e-07 0.066011 0.00015468 6.9232e-07 v total_pressure -3.1358e+05 3.5375e+05 70126 39350 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1753 0.12063 0.003165 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.1737e-07 0.067033 0.00032624 5.6697e-06 INSTANT 0.876655000E-01 TIME STEP NUMBER 56853 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283064311E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.846777701E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13160E-01 0.22129E+01 Friction velocity uk : 0.13160E-01 0.22129E+01 Dimensionless distance yplus : 0.12759E-01 0.21759E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 5.618903365e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29547E+08 1 0.19675E-09 0.40559E+02 0.23814E+04 c Velocity[X] 0.23232E+02 c Velocity[Y] 0.17327E+02 c Velocity[Z] 0.10816E-05 c Pressure 0.11857E-03 114 0.98379E-04 0.78047E-03 0.72090E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -32.87 46.706 5.6078 7.9995 v Velocity[Y] -34.051 36.634 -0.18402 -0.11823 v Velocity[Z] -3.1496 3.1674 2.1692e-06 -5.3925e-08 v ǁVelocityǁ 0.0013621 46.988 8.9742 8.2375 v Pressure -4.1672e+05 2.5185e+05 -31903 -62367 v TurbVisc 3.354e-19 0.028629 0.00021981 8.2016e-05 v CourantNb 8.8496e-09 0.011596 0.00017158 4.9775e-06 v FourierNb 1.2462e-07 0.066411 0.0001547 6.93e-07 v total_pressure -3.154e+05 3.5318e+05 69422 38958 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1759 0.12069 0.0031663 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.1795e-07 0.067434 0.00032628 5.6705e-06 INSTANT 0.876656000E-01 TIME STEP NUMBER 56854 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283070716E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.847235270E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13497E-01 0.22135E+01 Friction velocity uk : 0.13497E-01 0.22135E+01 Dimensionless distance yplus : 0.13086E-01 0.21765E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 5.507722860e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29548E+08 1 0.19680E-09 0.40594E+02 0.23823E+04 c Velocity[X] 0.23256E+02 c Velocity[Y] 0.17338E+02 c Velocity[Z] 0.10834E-05 c Pressure 0.12345E-03 377 0.83534E-04 0.81208E-03 0.62696E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -32.886 46.72 5.6079 7.9996 v Velocity[Y] -34.063 36.648 -0.18413 -0.11856 v Velocity[Z] -3.1499 3.1675 2.1688e-06 -5.3925e-08 v ǁVelocityǁ 0.0016888 47.001 8.9757 8.2379 v Pressure -4.1694e+05 2.5117e+05 -32683 -62972 v TurbVisc 3.6402e-19 0.028643 0.00021988 8.2117e-05 v CourantNb 7.8134e-09 0.011597 0.00017158 4.9776e-06 v FourierNb 1.2462e-07 0.066811 0.00015472 6.9368e-07 v total_pressure -3.1562e+05 3.525e+05 68642 38353 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1765 0.12074 0.0031675 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.1852e-07 0.067835 0.00032631 5.6713e-06 INSTANT 0.876657000E-01 TIME STEP NUMBER 56855 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283077272E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.847690233E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15600E-01 0.22142E+01 Friction velocity uk : 0.15600E-01 0.22142E+01 Dimensionless distance yplus : 0.15125E-01 0.21772E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 5.394317499e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29549E+08 1 0.19686E-09 0.40655E+02 0.23839E+04 c Velocity[X] 0.23275E+02 c Velocity[Y] 0.17380E+02 c Velocity[Z] 0.10968E-05 c Pressure 0.12086E-03 16 0.59376E-04 0.79456E-03 0.49964E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -32.901 46.733 5.608 7.9998 v Velocity[Y] -34.076 36.663 -0.18423 -0.1189 v Velocity[Z] -3.1503 3.1676 2.1683e-06 -5.3925e-08 v ǁVelocityǁ 0.0016597 47.015 8.9773 8.2383 v Pressure -4.1747e+05 2.5063e+05 -33484 -63465 v TurbVisc 3.5787e-19 0.028657 0.00021996 8.2217e-05 v CourantNb 7.7581e-09 0.011599 0.00017159 4.9777e-06 v FourierNb 1.2462e-07 0.067211 0.00015475 6.9437e-07 v total_pressure -3.1615e+05 3.5196e+05 67841 37860 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1772 0.1208 0.0031687 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.191e-07 0.068237 0.00032634 5.6721e-06 INSTANT 0.876658000E-01 TIME STEP NUMBER 56856 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283083780E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.848142877E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.17578E-01 0.22148E+01 Friction velocity uk : 0.17578E-01 0.22148E+01 Dimensionless distance yplus : 0.16919E-01 0.21778E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 5.264628486e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29550E+08 1 0.19691E-09 0.40706E+02 0.23852E+04 c Velocity[X] 0.23319E+02 c Velocity[Y] 0.17388E+02 c Velocity[Z] 0.11034E-05 c Pressure 0.12727E-03 666 0.80166E-04 0.83616E-03 0.70541E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -32.916 46.747 5.608 7.9999 v Velocity[Y] -34.088 36.677 -0.18434 -0.11923 v Velocity[Z] -3.1506 3.1677 2.1679e-06 -5.3925e-08 v ǁVelocityǁ 0.0016232 47.029 8.9788 8.2386 v Pressure -4.1898e+05 2.4978e+05 -34316 -63991 v TurbVisc 4.9364e-19 0.028672 0.00022003 8.2318e-05 v CourantNb 8.0343e-09 0.0116 0.0001716 4.9778e-06 v FourierNb 1.2462e-07 0.06761 0.00015477 6.9505e-07 v total_pressure -3.1766e+05 3.511e+05 67009 37334 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1778 0.12085 0.0031699 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.1968e-07 0.068637 0.00032637 5.6729e-06 INSTANT 0.876659000E-01 TIME STEP NUMBER 56857 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283090088E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.848592930E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.17290E-01 0.22155E+01 Friction velocity uk : 0.17290E-01 0.22155E+01 Dimensionless distance yplus : 0.16642E-01 0.21785E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 5.213428254e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29551E+08 1 0.19698E-09 0.40764E+02 0.23867E+04 c Velocity[X] 0.23337E+02 c Velocity[Y] 0.17427E+02 c Velocity[Z] 0.10949E-05 c Pressure 0.13128E-03 71 0.85735E-04 0.86193E-03 0.80004E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -32.932 46.761 5.6081 8 v Velocity[Y] -34.1 36.691 -0.18445 -0.11956 v Velocity[Z] -3.151 3.1679 2.1674e-06 -5.3925e-08 v ǁVelocityǁ 0.0015848 47.043 8.9804 8.239 v Pressure -4.1902e+05 2.491e+05 -35224 -64648 v TurbVisc 3.5241e-19 0.028686 0.00022011 8.2418e-05 v CourantNb 7.5237e-09 0.011601 0.00017161 4.9779e-06 v FourierNb 1.2462e-07 0.06801 0.0001548 6.9574e-07 v total_pressure -3.1769e+05 3.5043e+05 66101 36677 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1785 0.1209 0.0031711 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.2026e-07 0.069037 0.00032641 5.6737e-06 INSTANT 0.876660000E-01 TIME STEP NUMBER 56858 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283096559E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.849041665E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.17044E-01 0.22162E+01 Friction velocity uk : 0.17044E-01 0.22162E+01 Dimensionless distance yplus : 0.16405E-01 0.21791E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 5.125845651e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29552E+08 1 0.19704E-09 0.40799E+02 0.23876E+04 c Velocity[X] 0.23368E+02 c Velocity[Y] 0.17431E+02 c Velocity[Z] 0.10965E-05 c Pressure 0.13615E-03 245 0.75120E-04 0.89331E-03 0.55562E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -32.947 46.774 5.6082 8.0001 v Velocity[Y] -34.113 36.705 -0.18456 -0.1199 v Velocity[Z] -3.1513 3.168 2.167e-06 -5.3925e-08 v ǁVelocityǁ 0.001547 47.057 8.982 8.2394 v Pressure -4.2033e+05 2.4831e+05 -36149 -65200 v TurbVisc 3.5482e-19 0.0287 0.00022018 8.2519e-05 v CourantNb 8.9191e-09 0.011602 0.00017162 4.978e-06 v FourierNb 1.2462e-07 0.068409 0.00015482 6.9643e-07 v total_pressure -3.19e+05 3.4963e+05 65176 36125 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1791 0.12095 0.0031722 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.2084e-07 0.069437 0.00032644 5.6745e-06 INSTANT 0.876661000E-01 TIME STEP NUMBER 56859 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283102787E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.849487832E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.16784E-01 0.22168E+01 Friction velocity uk : 0.16784E-01 0.22168E+01 Dimensionless distance yplus : 0.16155E-01 0.21798E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 5.070398041e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29553E+08 1 0.19710E-09 0.40857E+02 0.23891E+04 c Velocity[X] 0.23394E+02 c Velocity[Y] 0.17463E+02 c Velocity[Z] 0.11291E-05 c Pressure 0.13535E-03 15 0.57225E-04 0.88746E-03 0.44867E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -32.962 46.788 5.6083 8.0002 v Velocity[Y] -34.125 36.72 -0.18467 -0.12023 v Velocity[Z] -3.1517 3.1681 2.1666e-06 -5.3925e-08 v ǁVelocityǁ 0.0015052 47.071 8.9835 8.2397 v Pressure -4.2156e+05 2.4761e+05 -37092 -65686 v TurbVisc 3.6252e-19 0.028714 0.00022026 8.262e-05 v CourantNb 1.0714e-08 0.011603 0.00017163 4.9781e-06 v FourierNb 1.2462e-07 0.068807 0.00015484 6.9712e-07 v total_pressure -3.2023e+05 3.4893e+05 64233 35639 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1798 0.12101 0.0031734 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.2142e-07 0.069837 0.00032647 5.6753e-06 INSTANT 0.876662000E-01 TIME STEP NUMBER 56860 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283108893E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.849930213E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.16578E-01 0.22174E+01 Friction velocity uk : 0.16578E-01 0.22174E+01 Dimensionless distance yplus : 0.15957E-01 0.21804E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 4.977917698e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29554E+08 1 0.19715E-09 0.40903E+02 0.23903E+04 c Velocity[X] 0.23422E+02 c Velocity[Y] 0.17481E+02 c Velocity[Z] 0.11164E-05 c Pressure 0.14109E-03 96 0.97838E-04 0.92453E-03 0.75762E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -32.978 46.802 5.6083 8.0003 v Velocity[Y] -34.137 36.734 -0.18478 -0.12057 v Velocity[Z] -3.152 3.1682 2.1661e-06 -5.3925e-08 v ǁVelocityǁ 0.0014669 47.085 8.9851 8.2401 v Pressure -4.2215e+05 2.4657e+05 -38143 -66593 v TurbVisc 5.3882e-19 0.028728 0.00022033 8.272e-05 v CourantNb 1.2413e-08 0.011604 0.00017164 4.9782e-06 v FourierNb 1.2462e-07 0.069206 0.00015487 6.978e-07 v total_pressure -3.2082e+05 3.4789e+05 63182 34732 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1804 0.12106 0.0031745 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.22e-07 0.070237 0.0003265 5.6761e-06 INSTANT 0.876663000E-01 TIME STEP NUMBER 56861 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283114943E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.850366782E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.16148E-01 0.22181E+01 Friction velocity uk : 0.16148E-01 0.22181E+01 Dimensionless distance yplus : 0.15543E-01 0.21810E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 4.961809735e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29555E+08 1 0.19722E-09 0.40951E+02 0.23915E+04 c Velocity[X] 0.23449E+02 c Velocity[Y] 0.17502E+02 c Velocity[Z] 0.11077E-05 c Pressure 0.14393E-03 436 0.81412E-04 0.94251E-03 0.50737E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -32.993 46.815 5.6084 8.0005 v Velocity[Y] -34.15 36.748 -0.18489 -0.1209 v Velocity[Z] -3.1524 3.1684 2.1657e-06 -5.3925e-08 v ǁVelocityǁ 0.0014255 47.099 8.9866 8.2404 v Pressure -4.2276e+05 2.4571e+05 -39186 -67197 v TurbVisc 2.457e-19 0.028742 0.00022041 8.2821e-05 v CourantNb 1.4196e-08 0.011606 0.00017164 4.9784e-06 v FourierNb 1.2462e-07 0.069604 0.00015489 6.9849e-07 v total_pressure -3.2143e+05 3.4703e+05 62139 34128 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.181 0.12111 0.0031756 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.2259e-07 0.070635 0.00032654 5.6768e-06 INSTANT 0.876664000E-01 TIME STEP NUMBER 56862 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283121023E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.850803131E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15934E-01 0.22188E+01 Friction velocity uk : 0.15934E-01 0.22188E+01 Dimensionless distance yplus : 0.15337E-01 0.21817E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 4.968168365e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29556E+08 1 0.19728E-09 0.41009E+02 0.23930E+04 c Velocity[X] 0.23466E+02 c Velocity[Y] 0.17543E+02 c Velocity[Z] 0.11116E-05 c Pressure 0.14621E-03 9 0.53492E-04 0.95680E-03 0.58951E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -33.009 46.829 5.6085 8.0006 v Velocity[Y] -34.162 36.763 -0.185 -0.12124 v Velocity[Z] -3.1527 3.1685 2.1652e-06 -5.3926e-08 v ǁVelocityǁ 0.0013814 47.112 8.9882 8.2408 v Pressure -4.234e+05 2.4486e+05 -40301 -67865 v TurbVisc 4.1685e-19 0.028757 0.00022048 8.2922e-05 v CourantNb 1.5154e-08 0.011607 0.00017165 4.9785e-06 v FourierNb 1.2462e-07 0.07 0.00015492 6.9918e-07 v total_pressure -3.2207e+05 3.4619e+05 61024 33460 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1817 0.12116 0.0031767 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.2317e-07 0.071033 0.00032657 5.6776e-06 INSTANT 0.876665000E-01 TIME STEP NUMBER 56863 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283127035E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.851236099E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15764E-01 0.22194E+01 Friction velocity uk : 0.15764E-01 0.22194E+01 Dimensionless distance yplus : 0.15173E-01 0.21823E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 4.881156223e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29557E+08 1 0.19733E-09 0.41054E+02 0.23942E+04 c Velocity[X] 0.23502E+02 c Velocity[Y] 0.17552E+02 c Velocity[Z] 0.11078E-05 c Pressure 0.15193E-03 65 0.98211E-04 0.99357E-03 0.61070E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -33.024 46.843 5.6085 8.0007 v Velocity[Y] -34.175 36.777 -0.18511 -0.12158 v Velocity[Z] -3.153 3.1686 2.1648e-06 -5.3926e-08 v ǁVelocityǁ 0.0013438 47.126 8.9897 8.2412 v Pressure -4.2439e+05 2.4382e+05 -41380 -68581 v TurbVisc 3.8596e-19 0.028771 0.00022056 8.3023e-05 v CourantNb 1.4969e-08 0.011608 0.00017166 4.9786e-06 v FourierNb 1.2462e-07 0.070395 0.00015494 6.9987e-07 v total_pressure -3.2306e+05 3.4515e+05 59945 32744 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1823 0.12121 0.0031778 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.2376e-07 0.071429 0.0003266 5.6784e-06 INSTANT 0.876666000E-01 TIME STEP NUMBER 56864 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283132906E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.851666404E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15278E-01 0.22200E+01 Friction velocity uk : 0.15278E-01 0.22200E+01 Dimensionless distance yplus : 0.14705E-01 0.21829E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 4.910498938e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29558E+08 1 0.19740E-09 0.41103E+02 0.23954E+04 c Velocity[X] 0.23531E+02 c Velocity[Y] 0.17571E+02 c Velocity[Z] 0.11087E-05 c Pressure 0.15472E-03 27 0.83524E-04 0.10111E-02 0.59041E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -33.04 46.856 5.6086 8.0008 v Velocity[Y] -34.187 36.791 -0.18522 -0.12192 v Velocity[Z] -3.1534 3.1687 2.1643e-06 -5.3926e-08 v ǁVelocityǁ 0.0013115 47.14 8.9913 8.2415 v Pressure -4.2542e+05 2.4283e+05 -42570 -69306 v TurbVisc 3.849e-19 0.028785 0.00022063 8.3124e-05 v CourantNb 1.5211e-08 0.011609 0.00017167 4.9787e-06 v FourierNb 1.2462e-07 0.070792 0.00015496 7.0056e-07 v total_pressure -3.241e+05 3.4415e+05 58755 32019 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1829 0.12126 0.0031789 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.2435e-07 0.071827 0.00032663 5.6792e-06 INSTANT 0.876667000E-01 TIME STEP NUMBER 56865 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283138682E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.852087142E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15002E-01 0.22207E+01 Friction velocity uk : 0.15002E-01 0.22207E+01 Dimensionless distance yplus : 0.14440E-01 0.21836E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 4.918102873e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29559E+08 1 0.19746E-09 0.41161E+02 0.23969E+04 c Velocity[X] 0.23559E+02 c Velocity[Y] 0.17602E+02 c Velocity[Z] 0.11157E-05 c Pressure 0.15696E-03 9 0.57488E-04 0.10251E-02 0.56634E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -33.055 46.87 5.6087 8.0009 v Velocity[Y] -34.199 36.805 -0.18533 -0.12226 v Velocity[Z] -3.1537 3.1689 2.1639e-06 -5.3926e-08 v ǁVelocityǁ 0.0012681 47.154 8.9928 8.2419 v Pressure -4.2664e+05 2.418e+05 -43788 -69972 v TurbVisc 4.1778e-19 0.028799 0.00022071 8.3226e-05 v CourantNb 1.5936e-08 0.01161 0.00017168 4.9788e-06 v FourierNb 1.2462e-07 0.071188 0.00015499 7.0125e-07 v total_pressure -3.2532e+05 3.4312e+05 57537 31353 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1836 0.12131 0.00318 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.2494e-07 0.072224 0.00032666 5.68e-06 INSTANT 0.876668000E-01 TIME STEP NUMBER 56866 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283144318E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.852506662E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.14835E-01 0.22213E+01 Friction velocity uk : 0.14835E-01 0.22213E+01 Dimensionless distance yplus : 0.14279E-01 0.21842E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 4.848126282e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29560E+08 1 0.19751E-09 0.41214E+02 0.23983E+04 c Velocity[X] 0.23583E+02 c Velocity[Y] 0.17631E+02 c Velocity[Z] 0.11154E-05 c Pressure 0.16266E-03 47 0.77422E-04 0.10617E-02 0.97256E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -33.07 46.884 5.6087 8.001 v Velocity[Y] -34.212 36.82 -0.18544 -0.1226 v Velocity[Z] -3.1541 3.169 2.1634e-06 -5.3926e-08 v ǁVelocityǁ 0.0012347 47.168 8.9944 8.2422 v Pressure -4.2673e+05 2.4062e+05 -45041 -71015 v TurbVisc 3.8226e-19 0.028813 0.00022078 8.3327e-05 v CourantNb 1.7856e-08 0.011612 0.00017169 4.9789e-06 v FourierNb 1.2462e-07 0.07158 0.00015501 7.0194e-07 v total_pressure -3.254e+05 3.4194e+05 56284 30310 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1842 0.12136 0.0031811 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.2553e-07 0.072617 0.0003267 5.6808e-06 INSTANT 0.876669000E-01 TIME STEP NUMBER 56867 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283150043E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.852922978E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.14450E-01 0.22220E+01 Friction velocity uk : 0.14450E-01 0.22220E+01 Dimensionless distance yplus : 0.13908E-01 0.21848E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 4.902062443e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29561E+08 1 0.19759E-09 0.41265E+02 0.23996E+04 c Velocity[X] 0.23611E+02 c Velocity[Y] 0.17654E+02 c Velocity[Z] 0.11145E-05 c Pressure 0.16636E-03 76 0.82194E-04 0.10851E-02 0.72222E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -33.086 46.897 5.6088 8.0011 v Velocity[Y] -34.224 36.834 -0.18555 -0.12294 v Velocity[Z] -3.1544 3.1691 2.163e-06 -5.3926e-08 v ǁVelocityǁ 0.0012045 47.182 8.996 8.2426 v Pressure -4.2849e+05 2.3955e+05 -46315 -71688 v TurbVisc 3.8174e-19 0.028827 0.00022086 8.3428e-05 v CourantNb 1.9372e-08 0.011613 0.0001717 4.979e-06 v FourierNb 1.2463e-07 0.071974 0.00015503 7.0263e-07 v total_pressure -3.2716e+05 3.4088e+05 55010 29637 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1848 0.1214 0.0031822 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.2612e-07 0.073012 0.00032673 5.6816e-06 INSTANT 0.876670000E-01 TIME STEP NUMBER 56868 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283155392E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.853333069E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.14225E-01 0.22226E+01 Friction velocity uk : 0.14225E-01 0.22226E+01 Dimensionless distance yplus : 0.13692E-01 0.21855E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 4.916118931e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29562E+08 1 0.19764E-09 0.41320E+02 0.24010E+04 c Velocity[X] 0.23632E+02 c Velocity[Y] 0.17688E+02 c Velocity[Z] 0.11181E-05 c Pressure 0.17068E-03 252 0.95704E-04 0.11125E-02 0.95699E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -33.101 46.911 5.6089 8.0012 v Velocity[Y] -34.237 36.848 -0.18566 -0.12328 v Velocity[Z] -3.1548 3.1692 2.1626e-06 -5.3926e-08 v ǁVelocityǁ 0.0011772 47.196 8.9975 8.2429 v Pressure -4.2838e+05 2.3838e+05 -47652 -72616 v TurbVisc 3.6686e-19 0.028841 0.00022094 8.353e-05 v CourantNb 2.1109e-08 0.011614 0.00017171 4.9791e-06 v FourierNb 1.2463e-07 0.072367 0.00015505 7.0333e-07 v total_pressure -3.2705e+05 3.397e+05 53673 28709 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1855 0.12145 0.0031832 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.2671e-07 0.073406 0.00032676 5.6824e-06 INSTANT 0.876671000E-01 TIME STEP NUMBER 56869 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283160925E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.853738976E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.14042E-01 0.22233E+01 Friction velocity uk : 0.14042E-01 0.22233E+01 Dimensionless distance yplus : 0.13516E-01 0.21861E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 4.980801817e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29563E+08 1 0.19771E-09 0.41351E+02 0.24018E+04 c Velocity[X] 0.23665E+02 c Velocity[Y] 0.17687E+02 c Velocity[Z] 0.11192E-05 c Pressure 0.17504E-03 277 0.81362E-04 0.11401E-02 0.63325E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -33.117 46.925 5.6089 8.0013 v Velocity[Y] -34.249 36.863 -0.18577 -0.12362 v Velocity[Z] -3.1551 3.1693 2.1621e-06 -5.3926e-08 v ǁVelocityǁ 0.0011536 47.21 8.9991 8.2433 v Pressure -4.2974e+05 2.3723e+05 -48961 -73285 v TurbVisc 3.9855e-19 0.028856 0.00022101 8.3631e-05 v CourantNb 2.2846e-08 0.011615 0.00017171 4.9792e-06 v FourierNb 1.2463e-07 0.072758 0.00015508 7.0402e-07 v total_pressure -3.2841e+05 3.3855e+05 52364 28040 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1861 0.1215 0.0031843 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.2731e-07 0.073799 0.00032679 5.6832e-06 INSTANT 0.876672000E-01 TIME STEP NUMBER 56870 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283166201E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.854139369E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13904E-01 0.22239E+01 Friction velocity uk : 0.13904E-01 0.22239E+01 Dimensionless distance yplus : 0.13383E-01 0.21867E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 4.974986085e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29564E+08 1 0.19777E-09 0.41409E+02 0.24033E+04 c Velocity[X] 0.23686E+02 c Velocity[Y] 0.17723E+02 c Velocity[Z] 0.11274E-05 c Pressure 0.17411E-03 9 0.59638E-04 0.11333E-02 0.62528E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -33.132 46.938 5.609 8.0014 v Velocity[Y] -34.261 36.877 -0.18589 -0.12396 v Velocity[Z] -3.1554 3.1695 2.1617e-06 -5.3926e-08 v ǁVelocityǁ 0.0011287 47.224 9.0007 8.2436 v Pressure -4.3111e+05 2.3614e+05 -50343 -74051 v TurbVisc 4.0152e-19 0.02887 0.00022109 8.3733e-05 v CourantNb 2.4552e-08 0.011616 0.00017172 4.9793e-06 v FourierNb 1.2463e-07 0.073149 0.0001551 7.0471e-07 v total_pressure -3.2978e+05 3.3746e+05 50982 27274 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1867 0.12155 0.0031853 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.279e-07 0.074191 0.00032682 5.684e-06 INSTANT 0.876673000E-01 TIME STEP NUMBER 56871 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283171253E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.854531691E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13918E-01 0.22245E+01 Friction velocity uk : 0.13918E-01 0.22245E+01 Dimensionless distance yplus : 0.13396E-01 0.21874E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 4.980475412e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29565E+08 1 0.19782E-09 0.41463E+02 0.24047E+04 c Velocity[X] 0.23715E+02 c Velocity[Y] 0.17748E+02 c Velocity[Z] 0.11253E-05 c Pressure 0.17927E-03 57 0.77406E-04 0.11661E-02 0.10515E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -33.148 46.952 5.6091 8.0015 v Velocity[Y] -34.274 36.891 -0.186 -0.1243 v Velocity[Z] -3.1558 3.1696 2.1612e-06 -5.3926e-08 v ǁVelocityǁ 0.0011057 47.237 9.0022 8.244 v Pressure -4.3106e+05 2.3471e+05 -51794 -75220 v TurbVisc 4.111e-19 0.028884 0.00022116 8.3835e-05 v CourantNb 2.6346e-08 0.011618 0.00017173 4.9794e-06 v FourierNb 1.2463e-07 0.073538 0.00015512 7.0541e-07 v total_pressure -3.2974e+05 3.3603e+05 49531 26105 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1874 0.1216 0.0031864 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.285e-07 0.07458 0.00032685 5.6848e-06 INSTANT 0.876674000E-01 TIME STEP NUMBER 56872 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283176469E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.854918533E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13758E-01 0.22252E+01 Friction velocity uk : 0.13758E-01 0.22252E+01 Dimensionless distance yplus : 0.13242E-01 0.21880E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 5.041755671e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29566E+08 1 0.19790E-09 0.41513E+02 0.24059E+04 c Velocity[X] 0.23743E+02 c Velocity[Y] 0.17771E+02 c Velocity[Z] 0.11314E-05 c Pressure 0.18274E-03 266 0.82979E-04 0.11879E-02 0.81485E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -33.163 46.965 5.6091 8.0016 v Velocity[Y] -34.286 36.906 -0.18611 -0.12465 v Velocity[Z] -3.1561 3.1697 2.1608e-06 -5.3926e-08 v ǁVelocityǁ 0.0010891 47.251 9.0038 8.2443 v Pressure -4.3287e+05 2.3342e+05 -53263 -76064 v TurbVisc 4.4297e-19 0.028898 0.00022124 8.3936e-05 v CourantNb 2.8015e-08 0.011619 0.00017174 4.9795e-06 v FourierNb 1.2463e-07 0.073926 0.00015514 7.061e-07 v total_pressure -3.3155e+05 3.3475e+05 48062 25261 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.188 0.12165 0.0031875 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.291e-07 0.07497 0.00032688 5.6856e-06 INSTANT 0.876675000E-01 TIME STEP NUMBER 56873 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283181271E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.855301687E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13781E-01 0.22258E+01 Friction velocity uk : 0.13781E-01 0.22258E+01 Dimensionless distance yplus : 0.13264E-01 0.21886E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 5.051036700e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29567E+08 1 0.19795E-09 0.41568E+02 0.24074E+04 c Velocity[X] 0.23765E+02 c Velocity[Y] 0.17804E+02 c Velocity[Z] 0.11309E-05 c Pressure 0.18677E-03 102 0.96342E-04 0.12133E-02 0.93645E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -33.178 46.979 5.6092 8.0016 v Velocity[Y] -34.299 36.92 -0.18623 -0.12499 v Velocity[Z] -3.1565 3.1698 2.1603e-06 -5.3926e-08 v ǁVelocityǁ 0.0010759 47.265 9.0053 8.2447 v Pressure -4.3274e+05 2.3217e+05 -54733 -76982 v TurbVisc 3.8832e-19 0.028912 0.00022132 8.4038e-05 v CourantNb 2.9742e-08 0.01162 0.00017175 4.9796e-06 v FourierNb 1.2463e-07 0.074314 0.00015517 7.068e-07 v total_pressure -3.3142e+05 3.335e+05 46592 24343 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1886 0.12169 0.0031885 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.297e-07 0.075358 0.00032692 5.6864e-06 INSTANT 0.876676000E-01 TIME STEP NUMBER 56874 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283186258E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.855681529E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13209E-01 0.22265E+01 Friction velocity uk : 0.13209E-01 0.22265E+01 Dimensionless distance yplus : 0.12823E-01 0.21893E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 5.119699079e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29568E+08 1 0.19802E-09 0.41599E+02 0.24081E+04 c Velocity[X] 0.23795E+02 c Velocity[Y] 0.17804E+02 c Velocity[Z] 0.11268E-05 c Pressure 0.19069E-03 195 0.82005E-04 0.12379E-02 0.72672E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -33.194 46.993 5.6092 8.0017 v Velocity[Y] -34.311 36.934 -0.18634 -0.12534 v Velocity[Z] -3.1568 3.17 2.1599e-06 -5.3926e-08 v ǁVelocityǁ 0.0010658 47.279 9.0069 8.245 v Pressure -4.3416e+05 2.3081e+05 -56233 -77806 v TurbVisc 4.0488e-19 0.028926 0.00022139 8.414e-05 v CourantNb 2.8142e-08 0.011621 0.00017176 4.9797e-06 v FourierNb 1.2463e-07 0.0747 0.00015519 7.0749e-07 v total_pressure -3.3283e+05 3.3214e+05 45092 23519 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1893 0.12174 0.0031896 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.303e-07 0.075745 0.00032695 5.6872e-06 INSTANT 0.876677000E-01 TIME STEP NUMBER 56875 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283190974E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.856051527E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.87361E-02 0.22271E+01 Friction velocity uk : 0.87361E-02 0.22271E+01 Dimensionless distance yplus : 0.84809E-02 0.21899E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 5.132010408e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29569E+08 1 0.19808E-09 0.41657E+02 0.24096E+04 c Velocity[X] 0.23817E+02 c Velocity[Y] 0.17840E+02 c Velocity[Z] 0.11368E-05 c Pressure 0.18973E-03 9 0.60472E-04 0.12309E-02 0.68157E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -33.209 47.006 5.6093 8.0018 v Velocity[Y] -34.323 36.948 -0.18646 -0.12568 v Velocity[Z] -3.1572 3.1701 2.1595e-06 -5.3926e-08 v ǁVelocityǁ 0.0010535 47.293 9.0085 8.2453 v Pressure -4.3555e+05 2.2957e+05 -57780 -78674 v TurbVisc 4.0384e-19 0.02894 0.00022147 8.4242e-05 v CourantNb 2.5403e-08 0.011622 0.00017177 4.9798e-06 v FourierNb 1.2463e-07 0.075085 0.00015521 7.0819e-07 v total_pressure -3.3423e+05 3.309e+05 43545 22651 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1899 0.12179 0.0031906 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.309e-07 0.076131 0.00032698 5.688e-06 INSTANT 0.876678000E-01 TIME STEP NUMBER 56876 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283195420E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.856413229E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.63013E-02 0.22277E+01 Friction velocity uk : 0.63013E-02 0.22277E+01 Dimensionless distance yplus : 0.61172E-02 0.21905E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 5.111233629e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29569E+08 1 0.19813E-09 0.41712E+02 0.24110E+04 c Velocity[X] 0.23848E+02 c Velocity[Y] 0.17864E+02 c Velocity[Z] 0.11342E-05 c Pressure 0.19444E-03 64 0.77971E-04 0.12606E-02 0.10850E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -33.225 47.02 5.6094 8.0019 v Velocity[Y] -34.336 36.963 -0.18657 -0.12603 v Velocity[Z] -3.1575 3.1702 2.159e-06 -5.3927e-08 v ǁVelocityǁ 0.001042 47.307 9.01 8.2457 v Pressure -4.3549e+05 2.2798e+05 -59379 -79912 v TurbVisc 4.0042e-19 0.028954 0.00022154 8.4344e-05 v CourantNb 2.2879e-08 0.011624 0.00017178 4.9799e-06 v FourierNb 1.2463e-07 0.075467 0.00015523 7.0889e-07 v total_pressure -3.3416e+05 3.2931e+05 41946 21413 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1905 0.12184 0.0031917 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.3151e-07 0.076514 0.00032701 5.6888e-06 INSTANT 0.876679000E-01 TIME STEP NUMBER 56877 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283200068E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.856767938E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11734E-01 0.22284E+01 Friction velocity uk : 0.11734E-01 0.22284E+01 Dimensionless distance yplus : 0.11392E-01 0.21911E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 5.133625261e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29570E+08 1 0.19822E-09 0.41762E+02 0.24123E+04 c Velocity[X] 0.23877E+02 c Velocity[Y] 0.17885E+02 c Velocity[Z] 0.11343E-05 c Pressure 0.19754E-03 523 0.83822E-04 0.12798E-02 0.84953E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -33.24 47.033 5.6094 8.002 v Velocity[Y] -34.348 36.977 -0.18669 -0.12637 v Velocity[Z] -3.1578 3.1703 2.1586e-06 -5.3927e-08 v ǁVelocityǁ 0.0010354 47.32 9.0116 8.246 v Pressure -4.373e+05 2.2653e+05 -61004 -80825 v TurbVisc 4.9783e-19 0.028968 0.00022162 8.4446e-05 v CourantNb 1.9984e-08 0.011625 0.00017179 4.98e-06 v FourierNb 1.2463e-07 0.075848 0.00015525 7.0958e-07 v total_pressure -3.3598e+05 3.2786e+05 40321 20500 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1911 0.12188 0.0031927 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.3211e-07 0.076896 0.00032704 5.6896e-06 INSTANT 0.876680000E-01 TIME STEP NUMBER 56878 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283204272E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.857118043E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.14591E-01 0.22290E+01 Friction velocity uk : 0.14591E-01 0.22290E+01 Dimensionless distance yplus : 0.14044E-01 0.21917E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 5.123690656e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29571E+08 1 0.19827E-09 0.41817E+02 0.24137E+04 c Velocity[X] 0.23894E+02 c Velocity[Y] 0.17922E+02 c Velocity[Z] 0.11342E-05 c Pressure 0.20117E-03 34 0.97445E-04 0.13024E-02 0.10194E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -33.256 47.047 5.6095 8.002 v Velocity[Y] -34.36 36.991 -0.18681 -0.12672 v Velocity[Z] -3.1582 3.1704 2.1581e-06 -5.3927e-08 v ǁVelocityǁ 0.0010307 47.334 9.0132 8.2463 v Pressure -4.3725e+05 2.2518e+05 -62633 -81888 v TurbVisc 3.9968e-19 0.028982 0.0002217 8.4549e-05 v CourantNb 1.7057e-08 0.011626 0.0001718 4.9801e-06 v FourierNb 1.2463e-07 0.076228 0.00015527 7.1028e-07 v total_pressure -3.3592e+05 3.265e+05 38692 19437 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1917 0.12193 0.0031937 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.3272e-07 0.077277 0.00032707 5.6904e-06 INSTANT 0.876681000E-01 TIME STEP NUMBER 56879 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283208613E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.857464020E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.14879E-01 0.22296E+01 Friction velocity uk : 0.14879E-01 0.22296E+01 Dimensionless distance yplus : 0.14321E-01 0.21924E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 5.141682154e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29572E+08 1 0.19834E-09 0.41847E+02 0.24144E+04 c Velocity[X] 0.23928E+02 c Velocity[Y] 0.17919E+02 c Velocity[Z] 0.11309E-05 c Pressure 0.20469E-03 273 0.83074E-04 0.13243E-02 0.75854E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -33.271 47.06 5.6095 8.0021 v Velocity[Y] -34.372 37.005 -0.18692 -0.12707 v Velocity[Z] -3.1585 3.1706 2.1577e-06 -5.3927e-08 v ǁVelocityǁ 0.0010271 47.348 9.0147 8.2467 v Pressure -4.3864e+05 2.2365e+05 -64278 -82769 v TurbVisc 3.9327e-19 0.028996 0.00022177 8.4651e-05 v CourantNb 1.4793e-08 0.011627 0.0001718 4.9802e-06 v FourierNb 1.2463e-07 0.076605 0.00015529 7.1098e-07 v total_pressure -3.3731e+05 3.2498e+05 37047 18556 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1924 0.12198 0.0031947 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.3333e-07 0.077655 0.0003271 5.6911e-06 INSTANT 0.876682000E-01 TIME STEP NUMBER 56880 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283212701E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.857798822E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15219E-01 0.22303E+01 Friction velocity uk : 0.15219E-01 0.22303E+01 Dimensionless distance yplus : 0.14648E-01 0.21930E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 5.105723616e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29573E+08 1 0.19840E-09 0.41905E+02 0.24159E+04 c Velocity[X] 0.23949E+02 c Velocity[Y] 0.17956E+02 c Velocity[Z] 0.11435E-05 c Pressure 0.20351E-03 9 0.61682E-04 0.13158E-02 0.71122E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -33.286 47.074 5.6096 8.0022 v Velocity[Y] -34.385 37.02 -0.18704 -0.12741 v Velocity[Z] -3.1589 3.1707 2.1572e-06 -5.3927e-08 v ǁVelocityǁ 0.001019 47.361 9.0163 8.247 v Pressure -4.4007e+05 2.2229e+05 -65963 -83701 v TurbVisc 4.0704e-19 0.02901 0.00022185 8.4753e-05 v CourantNb 1.4603e-08 0.011628 0.00017181 4.9803e-06 v FourierNb 1.2463e-07 0.076981 0.00015531 7.1168e-07 v total_pressure -3.3875e+05 3.2361e+05 35362 17624 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.193 0.12202 0.0031958 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.3393e-07 0.078032 0.00032713 5.6919e-06 INSTANT 0.876683000E-01 TIME STEP NUMBER 56881 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283216491E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.858125224E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15611E-01 0.22309E+01 Friction velocity uk : 0.15611E-01 0.22309E+01 Dimensionless distance yplus : 0.15026E-01 0.21936E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 5.040989332e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29574E+08 1 0.19845E-09 0.41961E+02 0.24173E+04 c Velocity[X] 0.23980E+02 c Velocity[Y] 0.17981E+02 c Velocity[Z] 0.11398E-05 c Pressure 0.20773E-03 63 0.78921E-04 0.13422E-02 0.11786E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -33.302 47.087 5.6097 8.0023 v Velocity[Y] -34.397 37.034 -0.18716 -0.12777 v Velocity[Z] -3.1592 3.1708 2.1568e-06 -5.3927e-08 v ǁVelocityǁ 0.0010094 47.375 9.0179 8.2473 v Pressure -4.4003e+05 2.2052e+05 -67720 -85109 v TurbVisc 4.1703e-19 0.029024 0.00022193 8.4856e-05 v CourantNb 1.4684e-08 0.011629 0.00017182 4.9803e-06 v FourierNb 1.2463e-07 0.077352 0.00015534 7.1238e-07 v total_pressure -3.387e+05 3.2185e+05 33605 16216 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1936 0.12207 0.0031968 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.3455e-07 0.078404 0.00032716 5.6927e-06 INSTANT 0.876684000E-01 TIME STEP NUMBER 56882 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283220441E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.858443336E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15483E-01 0.22315E+01 Friction velocity uk : 0.15483E-01 0.22315E+01 Dimensionless distance yplus : 0.14954E-01 0.21942E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 4.989912491e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29575E+08 1 0.19853E-09 0.42012E+02 0.24186E+04 c Velocity[X] 0.24013E+02 c Velocity[Y] 0.17999E+02 c Velocity[Z] 0.11356E-05 c Pressure 0.21047E-03 532 0.84931E-04 0.13590E-02 0.81164E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -33.317 47.1 5.6097 8.0023 v Velocity[Y] -34.409 37.048 -0.18728 -0.12811 v Velocity[Z] -3.1596 3.1709 2.1564e-06 -5.3927e-08 v ǁVelocityǁ 0.0010011 47.389 9.0194 8.2476 v Pressure -4.418e+05 2.1899e+05 -69449 -85954 v TurbVisc 4.1915e-19 0.029038 0.000222 8.4958e-05 v CourantNb 1.4805e-08 0.011631 0.00017183 4.9804e-06 v FourierNb 1.2463e-07 0.077724 0.00015536 7.1307e-07 v total_pressure -3.4047e+05 3.2032e+05 31876 15371 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1942 0.12212 0.0031978 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.3516e-07 0.078777 0.00032719 5.6935e-06 INSTANT 0.876685000E-01 TIME STEP NUMBER 56883 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283224023E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.858757486E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10093E-01 0.22321E+01 Friction velocity uk : 0.10093E-01 0.22321E+01 Dimensionless distance yplus : 0.97603E-02 0.21948E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 4.922345871e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29576E+08 1 0.19859E-09 0.42068E+02 0.24201E+04 c Velocity[X] 0.24029E+02 c Velocity[Y] 0.18038E+02 c Velocity[Z] 0.11340E-05 c Pressure 0.21360E-03 35 0.98800E-04 0.13783E-02 0.10871E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -33.332 47.114 5.6098 8.0024 v Velocity[Y] -34.421 37.062 -0.1874 -0.12847 v Velocity[Z] -3.1599 3.1711 2.1559e-06 -5.3927e-08 v ǁVelocityǁ 0.00099282 47.402 9.021 8.248 v Pressure -4.4178e+05 2.175e+05 -71221 -87156 v TurbVisc 4.337e-19 0.029052 0.00022208 8.5061e-05 v CourantNb 1.4945e-08 0.011632 0.00017184 4.9805e-06 v FourierNb 1.2463e-07 0.078092 0.00015538 7.1378e-07 v total_pressure -3.4046e+05 3.1882e+05 30104 14169 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1948 0.12216 0.0031988 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.3577e-07 0.079146 0.00032722 5.6943e-06 INSTANT 0.876686000E-01 TIME STEP NUMBER 56884 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283227680E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.859065299E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.91971E-02 0.22327E+01 Friction velocity uk : 0.91971E-02 0.22327E+01 Dimensionless distance yplus : 0.88826E-02 0.21954E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 4.870301459e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29576E+08 1 0.19866E-09 0.42098E+02 0.24208E+04 c Velocity[X] 0.24063E+02 c Velocity[Y] 0.18035E+02 c Velocity[Z] 0.11306E-05 c Pressure 0.21667E-03 595 0.83911E-04 0.13971E-02 0.80398E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -33.348 47.127 5.6098 8.0024 v Velocity[Y] -34.433 37.076 -0.18752 -0.12882 v Velocity[Z] -3.1602 3.1712 2.1555e-06 -5.3927e-08 v ǁVelocityǁ 0.00098209 47.416 9.0226 8.2483 v Pressure -4.4319e+05 2.1583e+05 -72999 -88130 v TurbVisc 4.196e-19 0.029066 0.00022216 8.5164e-05 v CourantNb 1.2721e-08 0.011633 0.00017185 4.9806e-06 v FourierNb 1.2463e-07 0.078458 0.0001554 7.1448e-07 v total_pressure -3.4186e+05 3.1716e+05 28326 13195 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1954 0.12221 0.0031998 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.3638e-07 0.079513 0.00032725 5.6951e-06 INSTANT 0.876687000E-01 TIME STEP NUMBER 56885 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283231071E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.859360888E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.92917E-02 0.22333E+01 Friction velocity uk : 0.92917E-02 0.22333E+01 Dimensionless distance yplus : 0.89740E-02 0.21960E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 4.760385081e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29577E+08 1 0.19872E-09 0.42157E+02 0.24223E+04 c Velocity[X] 0.24085E+02 c Velocity[Y] 0.18072E+02 c Velocity[Z] 0.11454E-05 c Pressure 0.21514E-03 9 0.62408E-04 0.13863E-02 0.71357E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -33.363 47.14 5.6099 8.0025 v Velocity[Y] -34.445 37.09 -0.18764 -0.12917 v Velocity[Z] -3.1606 3.1713 2.155e-06 -5.3927e-08 v ǁVelocityǁ 0.00096244 47.429 9.0241 8.2486 v Pressure -4.4465e+05 2.1439e+05 -74794 -89090 v TurbVisc 4.3622e-19 0.02908 0.00022223 8.5266e-05 v CourantNb 1.2578e-08 0.011634 0.00017186 4.9807e-06 v FourierNb 1.2463e-07 0.078821 0.00015542 7.1518e-07 v total_pressure -3.4332e+05 3.1571e+05 26531 12235 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.196 0.12225 0.0032008 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.37e-07 0.079876 0.00032728 5.6959e-06 INSTANT 0.876688000E-01 TIME STEP NUMBER 56886 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283234155E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.859647999E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12511E-01 0.22339E+01 Friction velocity uk : 0.12511E-01 0.22339E+01 Dimensionless distance yplus : 0.12083E-01 0.21966E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 4.586419922e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29578E+08 1 0.19877E-09 0.42214E+02 0.24238E+04 c Velocity[X] 0.24117E+02 c Velocity[Y] 0.18097E+02 c Velocity[Z] 0.11401E-05 c Pressure 0.21884E-03 60 0.79639E-04 0.14092E-02 0.12174E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -33.378 47.154 5.6099 8.0025 v Velocity[Y] -34.457 37.104 -0.18776 -0.12952 v Velocity[Z] -3.1609 3.1714 2.1546e-06 -5.3927e-08 v ǁVelocityǁ 0.00093821 47.443 9.0257 8.2489 v Pressure -4.446e+05 2.1249e+05 -76672 -90593 v TurbVisc 4.3824e-19 0.029094 0.00022231 8.5369e-05 v CourantNb 1.276e-08 0.011635 0.00017187 4.9808e-06 v FourierNb 1.2463e-07 0.079179 0.00015544 7.1588e-07 v total_pressure -3.4328e+05 3.1381e+05 24653 10732 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1966 0.1223 0.0032017 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.3761e-07 0.080235 0.00032731 5.6967e-06 INSTANT 0.876689000E-01 TIME STEP NUMBER 56887 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283237394E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.859925332E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15757E-01 0.22345E+01 Friction velocity uk : 0.15757E-01 0.22345E+01 Dimensionless distance yplus : 0.15219E-01 0.21972E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 4.471378268e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29579E+08 1 0.19885E-09 0.42265E+02 0.24251E+04 c Velocity[X] 0.24150E+02 c Velocity[Y] 0.18114E+02 c Velocity[Z] 0.11332E-05 c Pressure 0.22111E-03 710 0.85740E-04 0.14229E-02 0.82480E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -33.394 47.167 5.61 8.0026 v Velocity[Y] -34.47 37.118 -0.18788 -0.12987 v Velocity[Z] -3.1613 3.1715 2.1542e-06 -5.3927e-08 v ǁVelocityǁ 0.00090907 47.456 9.0273 8.2492 v Pressure -4.4639e+05 2.1085e+05 -78512 -91489 v TurbVisc 4.3441e-19 0.029108 0.00022238 8.5472e-05 v CourantNb 1.2989e-08 0.011636 0.00017188 4.9809e-06 v FourierNb 1.2463e-07 0.079536 0.00015546 7.1658e-07 v total_pressure -3.4506e+05 3.1218e+05 22813 9836.4 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1972 0.12234 0.0032027 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.3823e-07 0.080593 0.00032734 5.6975e-06 INSTANT 0.876690000E-01 TIME STEP NUMBER 56888 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283240254E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.860198585E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.18569E-01 0.22351E+01 Friction velocity uk : 0.18569E-01 0.22351E+01 Dimensionless distance yplus : 0.17934E-01 0.21978E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 4.313127820e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29580E+08 1 0.19891E-09 0.42322E+02 0.24265E+04 c Velocity[X] 0.24167E+02 c Velocity[Y] 0.18154E+02 c Velocity[Z] 0.11287E-05 c Pressure 0.22376E-03 86 0.99649E-04 0.14389E-02 0.11100E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -33.409 47.18 5.61 8.0026 v Velocity[Y] -34.482 37.132 -0.188 -0.13023 v Velocity[Z] -3.1616 3.1717 2.1537e-06 -5.3927e-08 v ǁVelocityǁ 0.00088106 47.47 9.0288 8.2495 v Pressure -4.4638e+05 2.0925e+05 -80392 -92765 v TurbVisc 4.6575e-19 0.029122 0.00022246 8.5575e-05 v CourantNb 1.338e-08 0.011638 0.00017189 4.981e-06 v FourierNb 1.2463e-07 0.079889 0.00015548 7.1728e-07 v total_pressure -3.4506e+05 3.1058e+05 20933 8560.2 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1978 0.12238 0.0032036 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.3885e-07 0.080947 0.00032737 5.6982e-06 INSTANT 0.876691000E-01 TIME STEP NUMBER 56889 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283243177E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.860465091E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.20304E-01 0.22357E+01 Friction velocity uk : 0.20304E-01 0.22357E+01 Dimensionless distance yplus : 0.19543E-01 0.21983E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 4.155375233e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29580E+08 1 0.19898E-09 0.42352E+02 0.24273E+04 c Velocity[X] 0.24203E+02 c Velocity[Y] 0.18150E+02 c Velocity[Z] 0.11283E-05 c Pressure 0.22632E-03 593 0.84567E-04 0.14544E-02 0.82130E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -33.424 47.193 5.6101 8.0027 v Velocity[Y] -34.494 37.146 -0.18812 -0.13058 v Velocity[Z] -3.1619 3.1718 2.1533e-06 -5.3927e-08 v ǁVelocityǁ 0.00084492 47.483 9.0304 8.2498 v Pressure -4.478e+05 2.0749e+05 -82274 -93792 v TurbVisc 4.4685e-19 0.029136 0.00022254 8.5678e-05 v CourantNb 1.3695e-08 0.011639 0.0001719 4.981e-06 v FourierNb 1.2463e-07 0.080239 0.0001555 7.1799e-07 v total_pressure -3.4647e+05 3.0881e+05 19051 7532.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1983 0.12243 0.0032046 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.3947e-07 0.081298 0.0003274 5.699e-06 INSTANT 0.876692000E-01 TIME STEP NUMBER 56890 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283245830E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.860718569E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.21081E-01 0.22363E+01 Friction velocity uk : 0.21081E-01 0.22363E+01 Dimensionless distance yplus : 0.20291E-01 0.21989E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 3.968959084e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29581E+08 1 0.19904E-09 0.42412E+02 0.24288E+04 c Velocity[X] 0.24224E+02 c Velocity[Y] 0.18188E+02 c Velocity[Z] 0.11444E-05 c Pressure 0.22438E-03 9 0.63166E-04 0.14410E-02 0.73041E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -33.439 47.206 5.6101 8.0027 v Velocity[Y] -34.506 37.16 -0.18824 -0.13093 v Velocity[Z] -3.1623 3.1719 2.1528e-06 -5.3928e-08 v ǁVelocityǁ 0.00079811 47.497 9.0319 8.2501 v Pressure -4.493e+05 2.0595e+05 -84165 -94805 v TurbVisc 4.54e-19 0.02915 0.00022261 8.5781e-05 v CourantNb 1.4801e-08 0.01164 0.00017191 4.9811e-06 v FourierNb 1.2463e-07 0.080585 0.00015552 7.1869e-07 v total_pressure -3.4797e+05 3.0728e+05 17160 6520.2 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1989 0.12247 0.0032055 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.4009e-07 0.081644 0.00032743 5.6998e-06 INSTANT 0.876693000E-01 TIME STEP NUMBER 56891 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283248157E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.860963172E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.21537E-01 0.22368E+01 Friction velocity uk : 0.21537E-01 0.22368E+01 Dimensionless distance yplus : 0.20788E-01 0.21994E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 3.683941376e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29582E+08 1 0.19909E-09 0.42470E+02 0.24303E+04 c Velocity[X] 0.24259E+02 c Velocity[Y] 0.18212E+02 c Velocity[Z] 0.11357E-05 c Pressure 0.22756E-03 190 0.80442E-04 0.14604E-02 0.12323E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -33.455 47.219 5.6101 8.0028 v Velocity[Y] -34.517 37.174 -0.18836 -0.13129 v Velocity[Z] -3.1626 3.172 2.1524e-06 -5.3928e-08 v ǁVelocityǁ 0.00074471 47.51 9.0335 8.2504 v Pressure -4.4923e+05 2.0394e+05 -86139 -96374 v TurbVisc 4.7255e-19 0.029164 0.00022269 8.5884e-05 v CourantNb 1.7001e-08 0.011641 0.00017191 4.9812e-06 v FourierNb 1.2463e-07 0.080924 0.00015554 7.194e-07 v total_pressure -3.479e+05 3.0527e+05 15186 4950.5 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.1994 0.12251 0.0032064 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.4071e-07 0.081985 0.00032745 5.7006e-06 INSTANT 0.876694000E-01 TIME STEP NUMBER 56892 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283250645E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.861197437E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19274E-01 0.22374E+01 Friction velocity uk : 0.19274E-01 0.22374E+01 Dimensionless distance yplus : 0.18604E-01 0.22000E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 3.487027956e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29583E+08 1 0.19917E-09 0.42522E+02 0.24316E+04 c Velocity[X] 0.24293E+02 c Velocity[Y] 0.18230E+02 c Velocity[Z] 0.11291E-05 c Pressure 0.22933E-03 654 0.86375E-04 0.14707E-02 0.82854E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -33.47 47.232 5.6102 8.0028 v Velocity[Y] -34.529 37.188 -0.18848 -0.13164 v Velocity[Z] -3.163 3.1722 2.152e-06 -5.3928e-08 v ǁVelocityǁ 0.0006872 47.523 9.0351 8.2507 v Pressure -4.5104e+05 2.0224e+05 -88065 -97313 v TurbVisc 2.2604e-19 0.029178 0.00022276 8.5988e-05 v CourantNb 2.012e-08 0.011642 0.00017192 4.9813e-06 v FourierNb 1.2463e-07 0.081263 0.00015556 7.201e-07 v total_pressure -3.4972e+05 3.0357e+05 13260 4012 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2 0.12255 0.0032072 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.4134e-07 0.082324 0.00032748 5.7014e-06 INSTANT 0.876695000E-01 TIME STEP NUMBER 56893 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283252735E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.861427269E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.17205E-01 0.22380E+01 Friction velocity uk : 0.17205E-01 0.22380E+01 Dimensionless distance yplus : 0.16606E-01 0.22006E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 3.235230398e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29584E+08 1 0.19923E-09 0.42560E+02 0.24325E+04 c Velocity[X] 0.24312E+02 c Velocity[Y] 0.18247E+02 c Velocity[Z] 0.11260E-05 c Pressure 0.23146E-03 53 0.75195E-04 0.14834E-02 0.96375E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -33.485 47.245 5.6102 8.0028 v Velocity[Y] -34.541 37.202 -0.1886 -0.132 v Velocity[Z] -3.1633 3.1723 2.1515e-06 -5.3928e-08 v ǁVelocityǁ 0.00062988 47.537 9.0366 8.251 v Pressure -4.5153e+05 2.0053e+05 -90035 -98612 v TurbVisc 5.8159e-19 0.029192 0.00022284 8.6091e-05 v CourantNb 2.2796e-08 0.011643 0.00017193 4.9814e-06 v FourierNb 1.2463e-07 0.081596 0.00015558 7.2081e-07 v total_pressure -3.5021e+05 3.0186e+05 11290 2712.7 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2006 0.12259 0.0032081 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.4196e-07 0.082658 0.00032751 5.7022e-06 INSTANT 0.876696000E-01 TIME STEP NUMBER 56894 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283254788E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.861649645E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.14958E-01 0.22385E+01 Friction velocity uk : 0.14958E-01 0.22385E+01 Dimensionless distance yplus : 0.14438E-01 0.22011E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 3.000264136e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29584E+08 1 0.19929E-09 0.42619E+02 0.24341E+04 c Velocity[X] 0.24337E+02 c Velocity[Y] 0.18282E+02 c Velocity[Z] 0.11486E-05 c Pressure 0.22994E-03 9 0.57040E-04 0.14726E-02 0.75923E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -33.5 47.258 5.6102 8.0029 v Velocity[Y] -34.553 37.216 -0.18873 -0.13236 v Velocity[Z] -3.1636 3.1724 2.1511e-06 -5.3928e-08 v ǁVelocityǁ 0.00057208 47.55 9.0382 8.2513 v Pressure -4.5215e+05 1.9887e+05 -91987 -99674 v TurbVisc 5.2867e-19 0.029206 0.00022292 8.6195e-05 v CourantNb 2.5324e-08 0.011644 0.00017194 4.9814e-06 v FourierNb 1.2463e-07 0.081925 0.0001556 7.2151e-07 v total_pressure -3.5082e+05 3.002e+05 9337.6 1651.1 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2011 0.12263 0.0032089 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.4259e-07 0.082988 0.00032754 5.7029e-06 INSTANT 0.876697000E-01 TIME STEP NUMBER 56895 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283256677E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.861859754E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12943E-01 0.22391E+01 Friction velocity uk : 0.12943E-01 0.22391E+01 Dimensionless distance yplus : 0.12493E-01 0.22016E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 2.642097782e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29585E+08 1 0.19935E-09 0.42668E+02 0.24353E+04 c Velocity[X] 0.24375E+02 c Velocity[Y] 0.18293E+02 c Velocity[Z] 0.11344E-05 c Pressure 0.23234E-03 45 0.96607E-04 0.14869E-02 0.89733E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -33.515 47.271 5.6103 8.0029 v Velocity[Y] -34.565 37.23 -0.18885 -0.13272 v Velocity[Z] -3.164 3.1725 2.1506e-06 -5.3928e-08 v ǁVelocityǁ 0.00052306 47.563 9.0397 8.2516 v Pressure -4.5325e+05 1.9695e+05 -93932 -1.0093e+05 v TurbVisc 5.2331e-19 0.029219 0.00022299 8.6298e-05 v CourantNb 2.7515e-08 0.011645 0.00017195 4.9815e-06 v FourierNb 1.2463e-07 0.082247 0.00015562 7.2222e-07 v total_pressure -3.5192e+05 2.9827e+05 7393.3 395.52 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2016 0.12267 0.0032098 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.4322e-07 0.083311 0.00032757 5.7037e-06 INSTANT 0.876698000E-01 TIME STEP NUMBER 56896 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283258395E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.862058041E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.98320E-02 0.22396E+01 Friction velocity uk : 0.98320E-02 0.22396E+01 Dimensionless distance yplus : 0.94900E-02 0.22022E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 2.400739998e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29586E+08 1 0.19943E-09 0.42718E+02 0.24366E+04 c Velocity[X] 0.24407E+02 c Velocity[Y] 0.18312E+02 c Velocity[Z] 0.11184E-05 c Pressure 0.23277E-03 46 0.80903E-04 0.14887E-02 0.84982E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -33.53 47.284 5.6103 8.0029 v Velocity[Y] -34.577 37.244 -0.18897 -0.13307 v Velocity[Z] -3.1643 3.1726 2.1502e-06 -5.3928e-08 v ǁVelocityǁ 0.00049787 47.576 9.0413 8.2518 v Pressure -4.5438e+05 1.9513e+05 -95970 -1.0216e+05 v TurbVisc 4.8526e-19 0.029233 0.00022307 8.6401e-05 v CourantNb 3.0685e-08 0.011646 0.00017196 4.9816e-06 v FourierNb 1.2463e-07 0.082567 0.00015564 7.2292e-07 v total_pressure -3.5306e+05 2.9646e+05 5354.7 -833.55 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2022 0.12271 0.0032105 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.4385e-07 0.083631 0.0003276 5.7045e-06 INSTANT 0.876699000E-01 TIME STEP NUMBER 56897 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283259948E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.862245566E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.60290E-02 0.22401E+01 Friction velocity uk : 0.60290E-02 0.22401E+01 Dimensionless distance yplus : 0.58193E-02 0.22027E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 2.061016351e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29586E+08 1 0.19948E-09 0.42778E+02 0.24381E+04 c Velocity[X] 0.24435E+02 c Velocity[Y] 0.18344E+02 c Velocity[Z] 0.11404E-05 c Pressure 0.23286E-03 9 0.56723E-04 0.14883E-02 0.76594E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -33.545 47.297 5.6103 8.0029 v Velocity[Y] -34.588 37.257 -0.18909 -0.13343 v Velocity[Z] -3.1646 3.1728 2.1498e-06 -5.3928e-08 v ǁVelocityǁ 0.00050081 47.589 9.0428 8.2521 v Pressure -4.5572e+05 1.9337e+05 -97991 -1.0327e+05 v TurbVisc 4.1727e-19 0.029247 0.00022314 8.6505e-05 v CourantNb 3.3367e-08 0.011647 0.00017197 4.9817e-06 v FourierNb 1.2463e-07 0.08288 0.00015566 7.2363e-07 v total_pressure -3.544e+05 2.947e+05 3333.6 -1940.2 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2027 0.12275 0.0032113 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.4447e-07 0.083945 0.00032763 5.7053e-06 INSTANT 0.876700000E-01 TIME STEP NUMBER 56898 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283261264E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.862428520E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.22821E-02 0.22406E+01 Friction velocity uk : 0.22821E-02 0.22406E+01 Dimensionless distance yplus : 0.22027E-02 0.22032E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.657976339e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29587E+08 1 0.19953E-09 0.42829E+02 0.24394E+04 c Velocity[X] 0.24469E+02 c Velocity[Y] 0.18360E+02 c Velocity[Z] 0.11291E-05 c Pressure 0.23514E-03 28 0.97576E-04 0.15018E-02 0.98414E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -33.56 47.31 5.6103 8.0029 v Velocity[Y] -34.6 37.271 -0.18922 -0.13379 v Velocity[Z] -3.165 3.1729 2.1493e-06 -5.3928e-08 v ǁVelocityǁ 0.00046474 47.602 9.0444 8.2524 v Pressure -4.5631e+05 1.9146e+05 -99991 -1.0467e+05 v TurbVisc 5.1547e-19 0.029261 0.00022322 8.6609e-05 v CourantNb 3.5231e-08 0.011648 0.00017198 4.9817e-06 v FourierNb 1.2464e-07 0.083187 0.00015568 7.2434e-07 v total_pressure -3.5498e+05 2.9278e+05 1334.2 -3340 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2032 0.12278 0.003212 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.4511e-07 0.084253 0.00032766 5.7061e-06 INSTANT 0.876701000E-01 TIME STEP NUMBER 56899 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283262508E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.862602168E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.23132E-02 0.22412E+01 Friction velocity uk : 0.23132E-02 0.22412E+01 Dimensionless distance yplus : 0.22327E-02 0.22037E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.442538067e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29588E+08 1 0.19961E-09 0.42878E+02 0.24407E+04 c Velocity[X] 0.24496E+02 c Velocity[Y] 0.18382E+02 c Velocity[Z] 0.11158E-05 c Pressure 0.23531E-03 222 0.82820E-04 0.15018E-02 0.85327E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -33.575 47.323 5.6103 8.0029 v Velocity[Y] -34.612 37.285 -0.18934 -0.13415 v Velocity[Z] -3.1653 3.173 2.1489e-06 -5.3928e-08 v ǁVelocityǁ 0.00046364 47.615 9.0459 8.2527 v Pressure -4.571e+05 1.8958e+05 -1.0203e+05 -1.0593e+05 v TurbVisc 4.8192e-19 0.029275 0.00022329 8.6713e-05 v CourantNb 3.7983e-08 0.01165 0.00017199 4.9818e-06 v FourierNb 1.2464e-07 0.083489 0.0001557 7.2505e-07 v total_pressure -3.5577e+05 2.909e+05 -703.37 -4601.1 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2037 0.12282 0.0032127 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.4574e-07 0.084556 0.00032769 5.7068e-06 INSTANT 0.876702000E-01 TIME STEP NUMBER 56900 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283263599E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.862763910E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.24300E-02 0.22417E+01 Friction velocity uk : 0.24300E-02 0.22417E+01 Dimensionless distance yplus : 0.23455E-02 0.22042E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 9.689467186e-03 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29588E+08 1 0.19967E-09 0.42940E+02 0.24422E+04 c Velocity[X] 0.24517E+02 c Velocity[Y] 0.18423E+02 c Velocity[Z] 0.11412E-05 c Pressure 0.23503E-03 9 0.57784E-04 0.14990E-02 0.80710E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -33.59 47.335 5.6104 8.0029 v Velocity[Y] -34.623 37.299 -0.18946 -0.13451 v Velocity[Z] -3.1657 3.1731 2.1484e-06 -5.3928e-08 v ǁVelocityǁ 0.00045559 47.628 9.0475 8.2529 v Pressure -4.5783e+05 1.8789e+05 -1.0408e+05 -1.071e+05 v TurbVisc 6.1514e-19 0.029289 0.00022337 8.6817e-05 v CourantNb 3.8352e-08 0.011651 0.000172 4.9819e-06 v FourierNb 1.2464e-07 0.083784 0.00015572 7.2576e-07 v total_pressure -3.565e+05 2.8921e+05 -2758.2 -5772.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2042 0.12286 0.0032135 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.4637e-07 0.084852 0.00032772 5.7076e-06 INSTANT 0.876703000E-01 TIME STEP NUMBER 56901 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283264544E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.862918922E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.24877E-02 0.22421E+01 Friction velocity uk : 0.24877E-02 0.22421E+01 Dimensionless distance yplus : 0.24011E-02 0.22046E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 6.455462127e-03 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29589E+08 1 0.19972E-09 0.42996E+02 0.24437E+04 c Velocity[X] 0.24566E+02 c Velocity[Y] 0.18430E+02 c Velocity[Z] 0.11262E-05 c Pressure 0.23701E-03 151 0.75738E-04 0.15106E-02 0.92606E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -33.605 47.348 5.6104 8.003 v Velocity[Y] -34.635 37.312 -0.18958 -0.13487 v Velocity[Z] -3.166 3.1732 2.148e-06 -5.3928e-08 v ǁVelocityǁ 0.00050367 47.641 9.049 8.2532 v Pressure -4.5933e+05 1.8589e+05 -1.0607e+05 -1.0831e+05 v TurbVisc 5.0686e-19 0.029303 0.00022344 8.692e-05 v CourantNb 3.8301e-08 0.011652 0.000172 4.9819e-06 v FourierNb 1.2464e-07 0.084073 0.00015574 7.2646e-07 v total_pressure -3.5801e+05 2.8722e+05 -4742.6 -6984.4 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2046 0.12289 0.0032142 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.4701e-07 0.085142 0.00032774 5.7084e-06 INSTANT 0.876704000E-01 TIME STEP NUMBER 56902 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283265264E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.863062965E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.82735E-02 0.22426E+01 Friction velocity uk : 0.82735E-02 0.22426E+01 Dimensionless distance yplus : 0.79857E-02 0.22051E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 3.005792558e-03 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29590E+08 1 0.19980E-09 0.43055E+02 0.24452E+04 c Velocity[X] 0.24591E+02 c Velocity[Y] 0.18464E+02 c Velocity[Z] 0.11078E-05 c Pressure 0.23754E-03 62 0.80096E-04 0.15130E-02 0.96225E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -33.62 47.361 5.6104 8.003 v Velocity[Y] -34.647 37.326 -0.18971 -0.13523 v Velocity[Z] -3.1663 3.1734 2.1476e-06 -5.3928e-08 v ǁVelocityǁ 0.00044859 47.654 9.0506 8.2535 v Pressure -4.5948e+05 1.8407e+05 -1.0814e+05 -1.096e+05 v TurbVisc 5.0173e-19 0.029317 0.00022352 8.7024e-05 v CourantNb 3.8487e-08 0.011653 0.00017201 4.982e-06 v FourierNb 1.2464e-07 0.084357 0.00015576 7.2717e-07 v total_pressure -3.5816e+05 2.8539e+05 -6819.5 -8271.7 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2051 0.12293 0.003215 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.4764e-07 0.085426 0.00032777 5.7092e-06 INSTANT 0.876705000E-01 TIME STEP NUMBER 56903 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283266007E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.863196874E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.96870E-02 0.22431E+01 Friction velocity uk : 0.96870E-02 0.22431E+01 Dimensionless distance yplus : 0.93500E-02 0.22056E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -6.325807263e-04 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29590E+08 1 0.19986E-09 0.43111E+02 0.24466E+04 c Velocity[X] 0.24624E+02 c Velocity[Y] 0.18487E+02 c Velocity[Z] 0.11091E-05 c Pressure 0.23847E-03 281 0.93347E-04 0.15178E-02 0.91764E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -33.634 47.373 5.6104 8.003 v Velocity[Y] -34.658 37.339 -0.18983 -0.1356 v Velocity[Z] -3.1667 3.1735 2.1471e-06 -5.3928e-08 v ǁVelocityǁ 0.00047748 47.667 9.0521 8.2537 v Pressure -4.6147e+05 1.8224e+05 -1.1019e+05 -1.108e+05 v TurbVisc 4.748e-19 0.02933 0.00022359 8.7128e-05 v CourantNb 3.8629e-08 0.011654 0.00017202 4.9821e-06 v FourierNb 1.2464e-07 0.084632 0.00015578 7.2788e-07 v total_pressure -3.6015e+05 2.8357e+05 -8865.1 -9475 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2056 0.12296 0.0032156 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.4828e-07 0.085702 0.0003278 5.7099e-06 INSTANT 0.876706000E-01 TIME STEP NUMBER 56904 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283266234E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.863322229E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10608E-01 0.22435E+01 Friction velocity uk : 0.10608E-01 0.22435E+01 Dimensionless distance yplus : 0.10239E-01 0.22060E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -4.416098462e-03 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29591E+08 1 0.19991E-09 0.43151E+02 0.24476E+04 c Velocity[X] 0.24654E+02 c Velocity[Y] 0.18498E+02 c Velocity[Z] 0.11062E-05 c Pressure 0.23932E-03 99 0.79069E-04 0.15222E-02 0.89257E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -33.649 47.386 5.6104 8.0029 v Velocity[Y] -34.67 37.353 -0.18995 -0.13596 v Velocity[Z] -3.167 3.1736 2.1467e-06 -5.3929e-08 v ǁVelocityǁ 0.00071533 47.679 9.0536 8.254 v Pressure -4.6184e+05 1.8052e+05 -1.1224e+05 -1.1208e+05 v TurbVisc 4.7384e-19 0.029344 0.00022367 8.7233e-05 v CourantNb 3.8719e-08 0.011654 0.00017203 4.9821e-06 v FourierNb 1.2464e-07 0.0849 0.0001558 7.2859e-07 v total_pressure -3.6051e+05 2.8185e+05 -10917 -10755 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.206 0.12299 0.0032163 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.4892e-07 0.08597 0.00032783 5.7107e-06 INSTANT 0.876707000E-01 TIME STEP NUMBER 56905 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283266532E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.863436106E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11219E-01 0.22440E+01 Friction velocity uk : 0.11219E-01 0.22440E+01 Dimensionless distance yplus : 0.10829E-01 0.22065E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -8.002251746e-03 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29591E+08 1 0.19998E-09 0.43214E+02 0.24493E+04 c Velocity[X] 0.24678E+02 c Velocity[Y] 0.18536E+02 c Velocity[Z] 0.11332E-05 c Pressure 0.23632E-03 9 0.58323E-04 0.15021E-02 0.75773E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -33.664 47.398 5.6104 8.0029 v Velocity[Y] -34.681 37.367 -0.19007 -0.13632 v Velocity[Z] -3.1673 3.1737 2.1462e-06 -5.3929e-08 v ǁVelocityǁ 0.0010452 47.692 9.0552 8.2543 v Pressure -4.6251e+05 1.8072e+05 -1.1428e+05 -1.1321e+05 v TurbVisc 5.455e-19 0.029358 0.00022374 8.7337e-05 v CourantNb 3.882e-08 0.011655 0.00017204 4.9822e-06 v FourierNb 1.2464e-07 0.085159 0.00015582 7.2931e-07 v total_pressure -3.6119e+05 2.8204e+05 -12954 -11884 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2065 0.12303 0.0032169 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.4956e-07 0.08623 0.00032786 5.7115e-06 INSTANT 0.876708000E-01 TIME STEP NUMBER 56906 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283266631E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.863539477E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.97380E-02 0.22444E+01 Friction velocity uk : 0.97380E-02 0.22444E+01 Dimensionless distance yplus : 0.93993E-02 0.22069E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.273649233e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29592E+08 1 0.20003E-09 0.43267E+02 0.24506E+04 c Velocity[X] 0.24721E+02 c Velocity[Y] 0.18545E+02 c Velocity[Z] 0.11152E-05 c Pressure 0.23760E-03 135 0.99809E-04 0.15092E-02 0.88539E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -33.678 47.41 5.6103 8.0029 v Velocity[Y] -34.693 37.38 -0.1902 -0.13669 v Velocity[Z] -3.1677 3.1738 2.1458e-06 -5.3929e-08 v ǁVelocityǁ 0.0014428 47.705 9.0567 8.2545 v Pressure -4.6362e+05 1.81e+05 -1.163e+05 -1.1452e+05 v TurbVisc 5.457e-19 0.029372 0.00022382 8.7441e-05 v CourantNb 3.8752e-08 0.011656 0.00017205 4.9822e-06 v FourierNb 1.2464e-07 0.085411 0.00015584 7.3002e-07 v total_pressure -3.623e+05 2.8232e+05 -14978 -13198 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2069 0.12306 0.0032174 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.502e-07 0.086482 0.00032789 5.7123e-06 INSTANT 0.876709000E-01 TIME STEP NUMBER 56907 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283266561E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.863631608E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11414E-01 0.22448E+01 Friction velocity uk : 0.11414E-01 0.22448E+01 Dimensionless distance yplus : 0.11017E-01 0.22073E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.592007729e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29593E+08 1 0.20011E-09 0.43320E+02 0.24520E+04 c Velocity[X] 0.24756E+02 c Velocity[Y] 0.18564E+02 c Velocity[Z] 0.10972E-05 c Pressure 0.23686E-03 53 0.83719E-04 0.15034E-02 0.79273E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -33.693 47.423 5.6103 8.0029 v Velocity[Y] -34.704 37.394 -0.19032 -0.13705 v Velocity[Z] -3.168 3.174 2.1454e-06 -5.3929e-08 v ǁVelocityǁ 0.0018306 47.717 9.0582 8.2548 v Pressure -4.6476e+05 1.8127e+05 -1.1838e+05 -1.1575e+05 v TurbVisc 5.8191e-19 0.029386 0.00022389 8.7545e-05 v CourantNb 3.8971e-08 0.011657 0.00017206 4.9823e-06 v FourierNb 1.2464e-07 0.085654 0.00015586 7.3073e-07 v total_pressure -3.6343e+05 2.826e+05 -17055 -14422 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2073 0.12309 0.003218 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.5085e-07 0.086726 0.00032792 5.713e-06 INSTANT 0.876710000E-01 TIME STEP NUMBER 56908 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283266331E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.863714837E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11459E-01 0.22453E+01 Friction velocity uk : 0.11459E-01 0.22453E+01 Dimensionless distance yplus : 0.11061E-01 0.22077E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.951585711e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29593E+08 1 0.20017E-09 0.43385E+02 0.24536E+04 c Velocity[X] 0.24787E+02 c Velocity[Y] 0.18597E+02 c Velocity[Z] 0.11155E-05 c Pressure 0.23562E-03 9 0.58876E-04 0.14945E-02 0.74996E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -33.707 47.435 5.6103 8.0029 v Velocity[Y] -34.715 37.407 -0.19044 -0.13742 v Velocity[Z] -3.1684 3.1741 2.1449e-06 -5.3929e-08 v ǁVelocityǁ 0.0022103 47.73 9.0597 8.255 v Pressure -4.6613e+05 1.8154e+05 -1.2046e+05 -1.169e+05 v TurbVisc 5.2805e-19 0.029399 0.00022397 8.765e-05 v CourantNb 3.9142e-08 0.011658 0.00017206 4.9824e-06 v FourierNb 1.2464e-07 0.085888 0.00015588 7.3144e-07 v total_pressure -3.6481e+05 2.8286e+05 -19131 -15577 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2077 0.12312 0.0032185 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.5149e-07 0.08696 0.00032795 5.7138e-06 INSTANT 0.876711000E-01 TIME STEP NUMBER 56909 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283265840E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.863791705E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.89832E-02 0.22456E+01 Friction velocity uk : 0.89832E-02 0.22456E+01 Dimensionless distance yplus : 0.86707E-02 0.22081E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -2.419341093e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29594E+08 1 0.20021E-09 0.43447E+02 0.24552E+04 c Velocity[X] 0.24823E+02 c Velocity[Y] 0.18623E+02 c Velocity[Z] 0.11050E-05 c Pressure 0.23682E-03 33 0.76530E-04 0.15011E-02 0.11116E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -33.722 47.447 5.6103 8.0029 v Velocity[Y] -34.727 37.42 -0.19056 -0.13779 v Velocity[Z] -3.1687 3.1742 2.1445e-06 -5.3929e-08 v ǁVelocityǁ 0.0022639 47.743 9.0613 8.2552 v Pressure -4.6623e+05 1.8183e+05 -1.2252e+05 -1.1848e+05 v TurbVisc 5.3284e-19 0.029413 0.00022404 8.7754e-05 v CourantNb 3.9283e-08 0.011659 0.00017207 4.9824e-06 v FourierNb 1.2464e-07 0.086114 0.0001559 7.3215e-07 v total_pressure -3.649e+05 2.8315e+05 -21194 -17159 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2081 0.12315 0.003219 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.5214e-07 0.087187 0.00032797 5.7146e-06 INSTANT 0.876712000E-01 TIME STEP NUMBER 56910 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283265424E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.863858974E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10095E-01 0.22460E+01 Friction velocity uk : 0.10095E-01 0.22460E+01 Dimensionless distance yplus : 0.97442E-02 0.22085E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -2.702036410e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29594E+08 1 0.20029E-09 0.43504E+02 0.24567E+04 c Velocity[X] 0.24861E+02 c Velocity[Y] 0.18643E+02 c Velocity[Z] 0.10914E-05 c Pressure 0.23652E-03 370 0.81224E-04 0.14981E-02 0.75162E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -33.736 47.46 5.6103 8.0028 v Velocity[Y] -34.738 37.434 -0.19068 -0.13815 v Velocity[Z] -3.169 3.1743 2.144e-06 -5.3929e-08 v ǁVelocityǁ 0.0022613 47.755 9.0628 8.2555 v Pressure -4.68e+05 1.821e+05 -1.2454e+05 -1.1947e+05 v TurbVisc 5.4604e-19 0.029427 0.00022412 8.7859e-05 v CourantNb 4.1166e-08 0.01166 0.00017208 4.9825e-06 v FourierNb 1.2464e-07 0.086329 0.00015592 7.3287e-07 v total_pressure -3.6667e+05 2.8343e+05 -23215 -18142 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2085 0.12317 0.0032194 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.5278e-07 0.087403 0.000328 5.7153e-06 INSTANT 0.876713000E-01 TIME STEP NUMBER 56911 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283264610E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.863915852E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.91293E-02 0.22464E+01 Friction velocity uk : 0.91293E-02 0.22464E+01 Dimensionless distance yplus : 0.88118E-02 0.22089E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -3.079789679e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29595E+08 1 0.20034E-09 0.43567E+02 0.24583E+04 c Velocity[X] 0.24887E+02 c Velocity[Y] 0.18680E+02 c Velocity[Z] 0.10867E-05 c Pressure 0.23655E-03 37 0.94627E-04 0.14973E-02 0.10101E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -33.751 47.472 5.6102 8.0028 v Velocity[Y] -34.749 37.447 -0.19081 -0.13852 v Velocity[Z] -3.1694 3.1744 2.1436e-06 -5.3929e-08 v ǁVelocityǁ 0.0022593 47.768 9.0643 8.2557 v Pressure -4.6806e+05 1.8238e+05 -1.266e+05 -1.2085e+05 v TurbVisc 5.6619e-19 0.029441 0.00022419 8.7963e-05 v CourantNb 4.2727e-08 0.011661 0.00017209 4.9825e-06 v FourierNb 1.2464e-07 0.086533 0.00015594 7.3358e-07 v total_pressure -3.6674e+05 2.8371e+05 -25277 -19528 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2089 0.1232 0.0032199 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.5343e-07 0.087608 0.00032803 5.7161e-06 INSTANT 0.876714000E-01 TIME STEP NUMBER 56912 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283263820E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.863962077E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.75837E-02 0.22468E+01 Friction velocity uk : 0.75837E-02 0.22468E+01 Dimensionless distance yplus : 0.73200E-02 0.22092E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -3.443089072e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29595E+08 1 0.20041E-09 0.43606E+02 0.24593E+04 c Velocity[X] 0.24927E+02 c Velocity[Y] 0.18679E+02 c Velocity[Z] 0.10818E-05 c Pressure 0.23655E-03 191 0.80193E-04 0.14962E-02 0.74024E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -33.765 47.484 5.6102 8.0028 v Velocity[Y] -34.76 37.46 -0.19093 -0.13889 v Velocity[Z] -3.1697 3.1745 2.1432e-06 -5.3929e-08 v ǁVelocityǁ 0.002258 47.78 9.0658 8.2559 v Pressure -4.6949e+05 1.8266e+05 -1.2861e+05 -1.2193e+05 v TurbVisc 5.5457e-19 0.029455 0.00022426 8.8068e-05 v CourantNb 4.4002e-08 0.011662 0.0001721 4.9826e-06 v FourierNb 1.2464e-07 0.086728 0.00015596 7.3429e-07 v total_pressure -3.6817e+05 2.8399e+05 -27286 -20604 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2092 0.12323 0.0032203 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.5408e-07 0.087803 0.00032806 5.7169e-06 INSTANT 0.876715000E-01 TIME STEP NUMBER 56913 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283262765E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.863994881E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.51941E-02 0.22471E+01 Friction velocity uk : 0.51941E-02 0.22471E+01 Dimensionless distance yplus : 0.50134E-02 0.22096E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -3.791469739e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29596E+08 1 0.20047E-09 0.43671E+02 0.24610E+04 c Velocity[X] 0.24954E+02 c Velocity[Y] 0.18717E+02 c Velocity[Z] 0.11060E-05 c Pressure 0.23246E-03 9 0.60469E-04 0.14694E-02 0.70317E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -33.779 47.496 5.6102 8.0027 v Velocity[Y] -34.771 37.474 -0.19105 -0.13925 v Velocity[Z] -3.17 3.1747 2.1427e-06 -5.3929e-08 v ǁVelocityǁ 0.0022575 47.792 9.0673 8.2562 v Pressure -4.7097e+05 1.8292e+05 -1.3063e+05 -1.2305e+05 v TurbVisc 5.7925e-19 0.029468 0.00022434 8.8173e-05 v CourantNb 4.5274e-08 0.011662 0.00017211 4.9826e-06 v FourierNb 1.2464e-07 0.08691 0.00015598 7.3501e-07 v total_pressure -3.6964e+05 2.8425e+05 -29309 -21728 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2096 0.12325 0.0032206 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.5473e-07 0.087986 0.00032809 5.7176e-06 INSTANT 0.876716000E-01 TIME STEP NUMBER 56914 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283261374E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.864016914E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.23179E-02 0.22475E+01 Friction velocity uk : 0.23179E-02 0.22475E+01 Dimensionless distance yplus : 0.22372E-02 0.22099E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -4.222164394e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29596E+08 1 0.20051E-09 0.43736E+02 0.24627E+04 c Velocity[X] 0.24997E+02 c Velocity[Y] 0.18739E+02 c Velocity[Z] 0.10909E-05 c Pressure 0.23298E-03 317 0.76013E-04 0.14716E-02 0.11022E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -33.794 47.508 5.6101 8.0027 v Velocity[Y] -34.782 37.487 -0.19117 -0.13963 v Velocity[Z] -3.1704 3.1748 2.1423e-06 -5.3929e-08 v ǁVelocityǁ 0.0022567 47.805 9.0688 8.2564 v Pressure -4.7097e+05 1.8321e+05 -1.3271e+05 -1.2467e+05 v TurbVisc 6.1185e-19 0.029482 0.00022441 8.8277e-05 v CourantNb 4.5973e-08 0.011663 0.00017211 4.9827e-06 v FourierNb 1.2464e-07 0.087083 0.000156 7.3572e-07 v total_pressure -3.6965e+05 2.8454e+05 -31382 -23346 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2099 0.12328 0.003221 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.5538e-07 0.088159 0.00032812 5.7184e-06 INSTANT 0.876717000E-01 TIME STEP NUMBER 56915 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283260141E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.864029226E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.22463E-02 0.22478E+01 Friction velocity uk : 0.22463E-02 0.22478E+01 Dimensionless distance yplus : 0.21682E-02 0.22102E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -4.500022089e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29597E+08 1 0.20059E-09 0.43794E+02 0.24641E+04 c Velocity[X] 0.25034E+02 c Velocity[Y] 0.18760E+02 c Velocity[Z] 0.10803E-05 c Pressure 0.23225E-03 182 0.81473E-04 0.14660E-02 0.69915E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -33.808 47.52 5.6101 8.0027 v Velocity[Y] -34.793 37.5 -0.19129 -0.13999 v Velocity[Z] -3.1707 3.1749 2.1418e-06 -5.3929e-08 v ǁVelocityǁ 0.0022566 47.817 9.0704 8.2566 v Pressure -4.7276e+05 1.8349e+05 -1.3467e+05 -1.256e+05 v TurbVisc 5.9197e-19 0.029496 0.00022448 8.8382e-05 v CourantNb 4.7554e-08 0.011664 0.00017212 4.9827e-06 v FourierNb 1.2464e-07 0.087243 0.00015602 7.3644e-07 v total_pressure -3.7143e+05 2.8482e+05 -33348 -24276 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2102 0.1233 0.0032213 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.5604e-07 0.08832 0.00032815 5.7192e-06 INSTANT 0.876718000E-01 TIME STEP NUMBER 56916 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283258512E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.864037418E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10905E-02 0.22481E+01 Friction velocity uk : 0.10905E-02 0.22481E+01 Dimensionless distance yplus : 0.10526E-02 0.22106E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -4.836116691e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29597E+08 1 0.20064E-09 0.43859E+02 0.24658E+04 c Velocity[X] 0.25065E+02 c Velocity[Y] 0.18794E+02 c Velocity[Z] 0.10795E-05 c Pressure 0.23173E-03 37 0.94660E-04 0.14617E-02 0.98771E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -33.822 47.532 5.61 8.0026 v Velocity[Y] -34.804 37.513 -0.19141 -0.14037 v Velocity[Z] -3.1711 3.175 2.1414e-06 -5.3929e-08 v ǁVelocityǁ 0.002257 47.829 9.0719 8.2569 v Pressure -4.7277e+05 1.8377e+05 -1.3671e+05 -1.2699e+05 v TurbVisc 6.0334e-19 0.02951 0.00022456 8.8487e-05 v CourantNb 4.8821e-08 0.011665 0.00017213 4.9828e-06 v FourierNb 1.2464e-07 0.087391 0.00015604 7.3715e-07 v total_pressure -3.7145e+05 2.851e+05 -35389 -25669 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2106 0.12332 0.0032217 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.5669e-07 0.088468 0.00032817 5.7199e-06 INSTANT 0.876719000E-01 TIME STEP NUMBER 56917 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283256935E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.864034829E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.71561E-02 0.22485E+01 Friction velocity uk : 0.71561E-02 0.22485E+01 Dimensionless distance yplus : 0.69072E-02 0.22109E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -5.104624381e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29598E+08 1 0.20070E-09 0.43899E+02 0.24668E+04 c Velocity[X] 0.25105E+02 c Velocity[Y] 0.18794E+02 c Velocity[Z] 0.10692E-05 c Pressure 0.23126E-03 194 0.80371E-04 0.14577E-02 0.70743E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -33.836 47.544 5.61 8.0026 v Velocity[Y] -34.815 37.526 -0.19153 -0.14074 v Velocity[Z] -3.1714 3.1751 2.141e-06 -5.3929e-08 v ǁVelocityǁ 0.0022579 47.841 9.0734 8.2571 v Pressure -4.7422e+05 1.8406e+05 -1.3868e+05 -1.2805e+05 v TurbVisc 6.0437e-19 0.029523 0.00022463 8.8592e-05 v CourantNb 4.8091e-08 0.011666 0.00017214 4.9828e-06 v FourierNb 1.2464e-07 0.087526 0.00015606 7.3787e-07 v total_pressure -3.729e+05 2.8538e+05 -37355 -26725 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2109 0.12335 0.003222 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.5735e-07 0.088603 0.0003282 5.7207e-06 INSTANT 0.876720000E-01 TIME STEP NUMBER 56918 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283255082E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.864020206E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10222E-01 0.22488E+01 Friction velocity uk : 0.10222E-01 0.22488E+01 Dimensionless distance yplus : 0.98664E-02 0.22112E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -5.403182400e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29598E+08 1 0.20076E-09 0.43965E+02 0.24685E+04 c Velocity[X] 0.25133E+02 c Velocity[Y] 0.18833E+02 c Velocity[Z] 0.10933E-05 c Pressure 0.22653E-03 9 0.60639E-04 0.14269E-02 0.66932E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -33.85 47.556 5.6099 8.0025 v Velocity[Y] -34.826 37.539 -0.19165 -0.14111 v Velocity[Z] -3.1717 3.1753 2.1405e-06 -5.393e-08 v ǁVelocityǁ 0.0022594 47.853 9.0749 8.2573 v Pressure -4.7572e+05 1.8432e+05 -1.4065e+05 -1.2915e+05 v TurbVisc 6.2457e-19 0.029537 0.0002247 8.8697e-05 v CourantNb 4.7168e-08 0.011666 0.00017215 4.9828e-06 v FourierNb 1.2464e-07 0.087647 0.00015608 7.3859e-07 v total_pressure -3.7439e+05 2.8565e+05 -39329 -27823 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2112 0.12337 0.0032223 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.58e-07 0.088725 0.00032823 5.7214e-06 INSTANT 0.876721000E-01 TIME STEP NUMBER 56919 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283252894E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.863993647E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13205E-01 0.22490E+01 Friction velocity uk : 0.13205E-01 0.22490E+01 Dimensionless distance yplus : 0.12746E-01 0.22114E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -5.760233857e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29599E+08 1 0.20080E-09 0.44032E+02 0.24702E+04 c Velocity[X] 0.25179E+02 c Velocity[Y] 0.18853E+02 c Velocity[Z] 0.10746E-05 c Pressure 0.22657E-03 57 0.76239E-04 0.14262E-02 0.99518E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -33.864 47.568 5.6099 8.0025 v Velocity[Y] -34.837 37.552 -0.19178 -0.14148 v Velocity[Z] -3.1721 3.1754 2.1401e-06 -5.393e-08 v ǁVelocityǁ 0.0022609 47.865 9.0764 8.2575 v Pressure -4.7565e+05 1.8462e+05 -1.4264e+05 -1.3063e+05 v TurbVisc 6.5205e-19 0.029551 0.00022478 8.8802e-05 v CourantNb 4.5259e-08 0.011667 0.00017215 4.9829e-06 v FourierNb 1.2465e-07 0.087757 0.0001561 7.393e-07 v total_pressure -3.7432e+05 2.8594e+05 -41317 -29302 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2114 0.1234 0.0032226 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.5866e-07 0.088836 0.00032826 5.7222e-06 INSTANT 0.876722000E-01 TIME STEP NUMBER 56920 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283250913E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.863956085E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15060E-01 0.22493E+01 Friction velocity uk : 0.15060E-01 0.22493E+01 Dimensionless distance yplus : 0.14536E-01 0.22117E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -6.003858732e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29599E+08 1 0.20088E-09 0.44092E+02 0.24718E+04 c Velocity[X] 0.25214E+02 c Velocity[Y] 0.18878E+02 c Velocity[Z] 0.10626E-05 c Pressure 0.22524E-03 293 0.81502E-04 0.14168E-02 0.77960E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -33.878 47.579 5.6098 8.0024 v Velocity[Y] -34.848 37.565 -0.1919 -0.14185 v Velocity[Z] -3.1724 3.1755 2.1396e-06 -5.393e-08 v ǁVelocityǁ 0.0022626 47.877 9.0779 8.2577 v Pressure -4.7757e+05 1.8489e+05 -1.4462e+05 -1.3177e+05 v TurbVisc 6.679e-19 0.029565 0.00022485 8.8908e-05 v CourantNb 4.3001e-08 0.011668 0.00017216 4.9829e-06 v FourierNb 1.2465e-07 0.087852 0.00015612 7.4002e-07 v total_pressure -3.7625e+05 2.8621e+05 -43297 -30447 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2117 0.12342 0.0032229 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.5932e-07 0.088931 0.00032828 5.7229e-06 INSTANT 0.876723000E-01 TIME STEP NUMBER 56921 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283248429E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.863911589E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.17082E-01 0.22496E+01 Friction velocity uk : 0.17082E-01 0.22496E+01 Dimensionless distance yplus : 0.16488E-01 0.22120E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -6.273693130e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29599E+08 1 0.20093E-09 0.44157E+02 0.24735E+04 c Velocity[X] 0.25248E+02 c Velocity[Y] 0.18910E+02 c Velocity[Z] 0.10572E-05 c Pressure 0.22435E-03 34 0.94772E-04 0.14102E-02 0.84814E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -33.891 47.591 5.6098 8.0023 v Velocity[Y] -34.859 37.578 -0.19202 -0.14223 v Velocity[Z] -3.1727 3.1756 2.1392e-06 -5.393e-08 v ǁVelocityǁ 0.0022658 47.889 9.0794 8.2579 v Pressure -4.7748e+05 1.8518e+05 -1.4654e+05 -1.3294e+05 v TurbVisc 5.4932e-19 0.029578 0.00022492 8.9013e-05 v CourantNb 4.084e-08 0.011669 0.00017217 4.983e-06 v FourierNb 1.2465e-07 0.087933 0.00015614 7.4074e-07 v total_pressure -3.7616e+05 2.8651e+05 -45217 -31617 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.212 0.12343 0.003223 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.5998e-07 0.089012 0.00032831 5.7237e-06 INSTANT 0.876724000E-01 TIME STEP NUMBER 56922 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283246090E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.863860572E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.17159E-01 0.22499E+01 Friction velocity uk : 0.17159E-01 0.22499E+01 Dimensionless distance yplus : 0.16512E-01 0.22123E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -6.478993120e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29600E+08 1 0.20099E-09 0.44199E+02 0.24745E+04 c Velocity[X] 0.25288E+02 c Velocity[Y] 0.18910E+02 c Velocity[Z] 0.10522E-05 c Pressure 0.22334E-03 208 0.80388E-04 0.14029E-02 0.68910E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -33.905 47.603 5.6097 8.0023 v Velocity[Y] -34.869 37.591 -0.19214 -0.1426 v Velocity[Z] -3.1731 3.1757 2.1388e-06 -5.393e-08 v ǁVelocityǁ 0.0019618 47.901 9.0808 8.2581 v Pressure -4.7896e+05 1.8547e+05 -1.4845e+05 -1.34e+05 v TurbVisc 6.7e-19 0.029592 0.00022499 8.9118e-05 v CourantNb 3.8579e-08 0.011669 0.00017218 4.983e-06 v FourierNb 1.2465e-07 0.087999 0.00015616 7.4146e-07 v total_pressure -3.7763e+05 2.8679e+05 -47127 -32676 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2123 0.12345 0.0032232 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.6065e-07 0.089079 0.00032834 5.7245e-06 INSTANT 0.876725000E-01 TIME STEP NUMBER 56923 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283243461E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.863795474E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11346E-01 0.22502E+01 Friction velocity uk : 0.11346E-01 0.22502E+01 Dimensionless distance yplus : 0.10918E-01 0.22125E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -6.723541256e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29600E+08 1 0.20105E-09 0.44267E+02 0.24762E+04 c Velocity[X] 0.25318E+02 c Velocity[Y] 0.18949E+02 c Velocity[Z] 0.10649E-05 c Pressure 0.21797E-03 9 0.60240E-04 0.13682E-02 0.62345E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -33.919 47.614 5.6096 8.0022 v Velocity[Y] -34.88 37.604 -0.19226 -0.14298 v Velocity[Z] -3.1734 3.1758 2.1383e-06 -5.393e-08 v ǁVelocityǁ 0.0015385 47.913 9.0823 8.2583 v Pressure -4.8044e+05 1.8574e+05 -1.5035e+05 -1.3505e+05 v TurbVisc 6.8457e-19 0.029606 0.00022507 8.9224e-05 v CourantNb 3.6229e-08 0.01167 0.00017219 4.983e-06 v FourierNb 1.2465e-07 0.088051 0.00015618 7.4218e-07 v total_pressure -3.7912e+05 2.8706e+05 -49025 -33724 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2125 0.12347 0.0032233 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.6131e-07 0.089131 0.00032837 5.7252e-06 INSTANT 0.876726000E-01 TIME STEP NUMBER 56924 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283240507E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.863719155E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.66001E-02 0.22504E+01 Friction velocity uk : 0.66001E-02 0.22504E+01 Dimensionless distance yplus : 0.63513E-02 0.22128E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -6.997572622e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29601E+08 1 0.20109E-09 0.44334E+02 0.24780E+04 c Velocity[X] 0.25364E+02 c Velocity[Y] 0.18970E+02 c Velocity[Z] 0.10563E-05 c Pressure 0.21759E-03 77 0.76140E-04 0.13649E-02 0.99185E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -33.932 47.626 5.6096 8.0021 v Velocity[Y] -34.891 37.616 -0.19238 -0.14335 v Velocity[Z] -3.1737 3.176 2.1379e-06 -5.393e-08 v ǁVelocityǁ 0.0011321 47.925 9.0838 8.2585 v Pressure -4.8041e+05 1.8603e+05 -1.5228e+05 -1.3657e+05 v TurbVisc 7.146e-19 0.029619 0.00022514 8.9329e-05 v CourantNb 3.3845e-08 0.011671 0.00017219 4.9831e-06 v FourierNb 1.2465e-07 0.08809 0.0001562 7.429e-07 v total_pressure -3.7908e+05 2.8736e+05 -50955 -35248 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2128 0.12349 0.0032233 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.6198e-07 0.08917 0.00032839 5.726e-06 INSTANT 0.876727000E-01 TIME STEP NUMBER 56925 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283237720E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.863632340E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.14743E-01 0.22507E+01 Friction velocity uk : 0.14743E-01 0.22507E+01 Dimensionless distance yplus : 0.14188E-01 0.22131E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -7.177953809e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29601E+08 1 0.20117E-09 0.44395E+02 0.24795E+04 c Velocity[X] 0.25403E+02 c Velocity[Y] 0.18992E+02 c Velocity[Z] 0.10449E-05 c Pressure 0.21583E-03 271 0.81609E-04 0.13529E-02 0.67678E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -33.946 47.637 5.6095 8.0021 v Velocity[Y] -34.901 37.629 -0.1925 -0.14373 v Velocity[Z] -3.1741 3.1761 2.1374e-06 -5.393e-08 v ǁVelocityǁ 0.00077555 47.937 9.0853 8.2587 v Pressure -4.8224e+05 1.8631e+05 -1.5414e+05 -1.3752e+05 v TurbVisc 7.5904e-19 0.029633 0.00022521 8.9435e-05 v CourantNb 3.1371e-08 0.011672 0.0001722 4.9831e-06 v FourierNb 1.2465e-07 0.088113 0.00015622 7.4362e-07 v total_pressure -3.8091e+05 2.8764e+05 -52818 -36194 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2131 0.1235 0.0032233 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.6264e-07 0.089193 0.00032842 5.7267e-06 INSTANT 0.876728000E-01 TIME STEP NUMBER 56926 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283234535E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.863540167E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10911E-01 0.22509E+01 Friction velocity uk : 0.10911E-01 0.22509E+01 Dimensionless distance yplus : 0.10495E-01 0.22133E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -7.358317464e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29601E+08 1 0.20121E-09 0.44462E+02 0.24813E+04 c Velocity[X] 0.25436E+02 c Velocity[Y] 0.19026E+02 c Velocity[Z] 0.10378E-05 c Pressure 0.21448E-03 109 0.94901E-04 0.13435E-02 0.83691E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -33.959 47.649 5.6094 8.002 v Velocity[Y] -34.912 37.642 -0.19262 -0.14411 v Velocity[Z] -3.1744 3.1762 2.137e-06 -5.393e-08 v ǁVelocityǁ 0.00056621 47.948 9.0868 8.2589 v Pressure -4.8219e+05 1.8661e+05 -1.5599e+05 -1.3871e+05 v TurbVisc 6.3188e-19 0.029647 0.00022528 8.954e-05 v CourantNb 2.8839e-08 0.011672 0.00017221 4.9831e-06 v FourierNb 1.2465e-07 0.088121 0.00015624 7.4434e-07 v total_pressure -3.8086e+05 2.8793e+05 -54663 -37383 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2133 0.12351 0.0032232 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.6331e-07 0.089201 0.00032845 5.7275e-06 INSTANT 0.876729000E-01 TIME STEP NUMBER 56927 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283231452E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.863440383E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.62982E-02 0.22512E+01 Friction velocity uk : 0.62982E-02 0.22512E+01 Dimensionless distance yplus : 0.60592E-02 0.22136E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -7.490700454e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29602E+08 1 0.20128E-09 0.44504E+02 0.24823E+04 c Velocity[X] 0.25477E+02 c Velocity[Y] 0.19026E+02 c Velocity[Z] 0.10354E-05 c Pressure 0.21307E-03 198 0.80718E-04 0.13338E-02 0.64247E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -33.973 47.66 5.6093 8.0019 v Velocity[Y] -34.922 37.655 -0.19275 -0.14448 v Velocity[Z] -3.1747 3.1763 2.1366e-06 -5.393e-08 v ǁVelocityǁ 0.00056431 47.96 9.0883 8.2591 v Pressure -4.8366e+05 1.8689e+05 -1.578e+05 -1.3971e+05 v TurbVisc 7.154e-19 0.02966 0.00022535 8.9646e-05 v CourantNb 2.6276e-08 0.011673 0.00017222 4.9832e-06 v FourierNb 1.2465e-07 0.088112 0.00015626 7.4506e-07 v total_pressure -3.8233e+05 2.8822e+05 -56476 -38386 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2136 0.12353 0.0032232 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.6398e-07 0.089193 0.00032847 5.7282e-06 INSTANT 0.876730000E-01 TIME STEP NUMBER 56928 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283228079E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.863327085E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.27559E-02 0.22514E+01 Friction velocity uk : 0.27559E-02 0.22514E+01 Dimensionless distance yplus : 0.26513E-02 0.22138E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -7.660376539e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29602E+08 1 0.20133E-09 0.44573E+02 0.24841E+04 c Velocity[X] 0.25508E+02 c Velocity[Y] 0.19065E+02 c Velocity[Z] 0.10434E-05 c Pressure 0.20702E-03 9 0.60155E-04 0.12950E-02 0.58052E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -33.986 47.671 5.6093 8.0018 v Velocity[Y] -34.933 37.667 -0.19287 -0.14486 v Velocity[Z] -3.1751 3.1764 2.1361e-06 -5.393e-08 v ǁVelocityǁ 0.00079298 47.972 9.0898 8.2593 v Pressure -4.8514e+05 1.8717e+05 -1.596e+05 -1.4071e+05 v TurbVisc 7.1854e-19 0.029674 0.00022542 8.9751e-05 v CourantNb 2.3677e-08 0.011674 0.00017222 4.9832e-06 v FourierNb 1.2465e-07 0.088088 0.00015628 7.4578e-07 v total_pressure -3.8381e+05 2.8849e+05 -58280 -39383 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2138 0.12355 0.0032236 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.6465e-07 0.089169 0.0003285 5.729e-06 INSTANT 0.876731000E-01 TIME STEP NUMBER 56929 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283224399E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.863202369E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11722E-01 0.22516E+01 Friction velocity uk : 0.11722E-01 0.22516E+01 Dimensionless distance yplus : 0.11280E-01 0.22140E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -7.852150158e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29602E+08 1 0.20137E-09 0.44641E+02 0.24859E+04 c Velocity[X] 0.25555E+02 c Velocity[Y] 0.19086E+02 c Velocity[Z] 0.10389E-05 c Pressure 0.20630E-03 81 0.76533E-04 0.12896E-02 0.93566E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -34 47.682 5.6092 8.0017 v Velocity[Y] -34.943 37.68 -0.19299 -0.14524 v Velocity[Z] -3.1754 3.1765 2.1357e-06 -5.393e-08 v ǁVelocityǁ 0.0011726 47.983 9.0912 8.2595 v Pressure -4.851e+05 1.8746e+05 -1.6143e+05 -1.4217e+05 v TurbVisc 7.2292e-19 0.029688 0.00022549 8.9857e-05 v CourantNb 2.1016e-08 0.011674 0.00017223 4.9832e-06 v FourierNb 1.2465e-07 0.08805 0.0001563 7.465e-07 v total_pressure -3.8377e+05 2.8879e+05 -60104 -40848 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.214 0.12357 0.0032241 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.6532e-07 0.089131 0.00032853 5.7297e-06 INSTANT 0.876732000E-01 TIME STEP NUMBER 56930 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283220891E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.863067872E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.14608E-01 0.22519E+01 Friction velocity uk : 0.14608E-01 0.22519E+01 Dimensionless distance yplus : 0.14057E-01 0.22143E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -7.952882544e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29603E+08 1 0.20144E-09 0.44703E+02 0.24874E+04 c Velocity[X] 0.25594E+02 c Velocity[Y] 0.19109E+02 c Velocity[Z] 0.10315E-05 c Pressure 0.20412E-03 791 0.81933E-04 0.12751E-02 0.61825E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -34.013 47.694 5.6091 8.0017 v Velocity[Y] -34.953 37.692 -0.19311 -0.14562 v Velocity[Z] -3.1757 3.1767 2.1352e-06 -5.393e-08 v ǁVelocityǁ 0.0015875 47.994 9.0927 8.2597 v Pressure -4.8692e+05 1.8775e+05 -1.6317e+05 -1.4302e+05 v TurbVisc 6.9185e-19 0.029701 0.00022557 8.9963e-05 v CourantNb 1.8346e-08 0.011675 0.00017224 4.9833e-06 v FourierNb 1.2465e-07 0.087996 0.00015631 7.4722e-07 v total_pressure -3.856e+05 2.8908e+05 -61848 -41696 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2143 0.12359 0.0032245 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.66e-07 0.089078 0.00032855 5.7305e-06 INSTANT 0.876733000E-01 TIME STEP NUMBER 56931 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283216999E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.862928242E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.87331E-02 0.22521E+01 Friction velocity uk : 0.87331E-02 0.22521E+01 Dimensionless distance yplus : 0.84040E-02 0.22145E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -8.070629890e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29603E+08 1 0.20149E-09 0.44771E+02 0.24892E+04 c Velocity[X] 0.25628E+02 c Velocity[Y] 0.19143E+02 c Velocity[Z] 0.10202E-05 c Pressure 0.20237E-03 34 0.95354E-04 0.12633E-02 0.81814E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -34.026 47.705 5.609 8.0016 v Velocity[Y] -34.964 37.705 -0.19324 -0.146 v Velocity[Z] -3.1761 3.1768 2.1348e-06 -5.3931e-08 v ǁVelocityǁ 0.0020147 48.006 9.0942 8.2598 v Pressure -4.8686e+05 1.8804e+05 -1.6492e+05 -1.4421e+05 v TurbVisc 6.8961e-19 0.029715 0.00022564 9.0069e-05 v CourantNb 1.5666e-08 0.011676 0.00017225 4.9833e-06 v FourierNb 1.2465e-07 0.087925 0.00015633 7.4794e-07 v total_pressure -3.8554e+05 2.8937e+05 -63599 -42884 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2145 0.12361 0.0032248 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.6667e-07 0.089007 0.00032858 5.7312e-06 INSTANT 0.876734000E-01 TIME STEP NUMBER 56932 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283213209E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.862780847E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10375E-01 0.22524E+01 Friction velocity uk : 0.10375E-01 0.22524E+01 Dimensionless distance yplus : 0.99840E-02 0.22147E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -8.122936501e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29603E+08 1 0.20155E-09 0.44813E+02 0.24902E+04 c Velocity[X] 0.25671E+02 c Velocity[Y] 0.19142E+02 c Velocity[Z] 0.10149E-05 c Pressure 0.20065E-03 260 0.81086E-04 0.12516E-02 0.58207E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -34.039 47.716 5.609 8.0015 v Velocity[Y] -34.974 37.717 -0.19336 -0.14638 v Velocity[Z] -3.1764 3.1769 2.1344e-06 -5.3931e-08 v ǁVelocityǁ 0.0023575 48.017 9.0957 8.26 v Pressure -4.8832e+05 1.8834e+05 -1.6661e+05 -1.4512e+05 v TurbVisc 7.6236e-19 0.029729 0.00022571 9.0175e-05 v CourantNb 1.2949e-08 0.011676 0.00017226 4.9833e-06 v FourierNb 1.2465e-07 0.087838 0.00015635 7.4867e-07 v total_pressure -3.87e+05 2.8966e+05 -65290 -43796 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2147 0.12362 0.0032252 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.6735e-07 0.08892 0.00032861 5.732e-06 INSTANT 0.876735000E-01 TIME STEP NUMBER 56933 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283209154E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.862621457E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.95407E-02 0.22526E+01 Friction velocity uk : 0.95407E-02 0.22526E+01 Dimensionless distance yplus : 0.91810E-02 0.22150E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -8.222877486e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29603E+08 1 0.20160E-09 0.44883E+02 0.24920E+04 c Velocity[X] 0.25701E+02 c Velocity[Y] 0.19182E+02 c Velocity[Z] 0.10259E-05 c Pressure 0.19390E-03 9 0.60197E-04 0.12087E-02 0.53386E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -34.052 47.727 5.6089 8.0014 v Velocity[Y] -34.984 37.729 -0.19348 -0.14676 v Velocity[Z] -3.1767 3.177 2.1339e-06 -5.3931e-08 v ǁVelocityǁ 0.0023736 48.028 9.0971 8.2602 v Pressure -4.898e+05 1.8861e+05 -1.683e+05 -1.4606e+05 v TurbVisc 7.7131e-19 0.029742 0.00022578 9.0281e-05 v CourantNb 1.1497e-08 0.011677 0.00017226 4.9833e-06 v FourierNb 1.2465e-07 0.087733 0.00015637 7.4939e-07 v total_pressure -3.8847e+05 2.8994e+05 -66971 -44730 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.215 0.12364 0.0032255 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.6803e-07 0.088816 0.00032863 5.7327e-06 INSTANT 0.876736000E-01 TIME STEP NUMBER 56934 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283204801E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.862451591E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12616E-01 0.22528E+01 Friction velocity uk : 0.12616E-01 0.22528E+01 Dimensionless distance yplus : 0.12141E-01 0.22152E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -8.336438695e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29604E+08 1 0.20164E-09 0.44952E+02 0.24938E+04 c Velocity[X] 0.25750E+02 c Velocity[Y] 0.19202E+02 c Velocity[Z] 0.10161E-05 c Pressure 0.19295E-03 46 0.76955E-04 0.12019E-02 0.83218E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -34.065 47.738 5.6088 8.0013 v Velocity[Y] -34.994 37.742 -0.1936 -0.14714 v Velocity[Z] -3.1771 3.1771 2.1335e-06 -5.3931e-08 v ǁVelocityǁ 0.0023876 48.04 9.0986 8.2604 v Pressure -4.897e+05 1.8892e+05 -1.6998e+05 -1.4736e+05 v TurbVisc 7.6352e-19 0.029756 0.00022585 9.0387e-05 v CourantNb 1.1207e-08 0.011677 0.00017227 4.9833e-06 v FourierNb 1.2465e-07 0.087614 0.00015639 7.5011e-07 v total_pressure -3.8837e+05 2.9024e+05 -68651 -46033 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2152 0.12366 0.0032258 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.6871e-07 0.088697 0.00032866 5.7335e-06 INSTANT 0.876737000E-01 TIME STEP NUMBER 56935 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283200666E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.862272289E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12807E-01 0.22531E+01 Friction velocity uk : 0.12807E-01 0.22531E+01 Dimensionless distance yplus : 0.12324E-01 0.22154E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -8.352894284e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29604E+08 1 0.20172E-09 0.45014E+02 0.24954E+04 c Velocity[X] 0.25789E+02 c Velocity[Y] 0.19225E+02 c Velocity[Z] 0.10136E-05 c Pressure 0.19036E-03 664 0.82756E-04 0.11850E-02 0.63081E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -34.078 47.748 5.6087 8.0012 v Velocity[Y] -35.004 37.754 -0.19373 -0.14752 v Velocity[Z] -3.1774 3.1772 2.133e-06 -5.3931e-08 v ǁVelocityǁ 0.0024038 48.051 9.1001 8.2605 v Pressure -4.9159e+05 1.892e+05 -1.7162e+05 -1.4828e+05 v TurbVisc 7.5909e-19 0.029769 0.00022592 9.0493e-05 v CourantNb 9.7327e-09 0.011678 0.00017228 4.9834e-06 v FourierNb 1.2465e-07 0.08748 0.00015641 7.5084e-07 v total_pressure -3.9027e+05 2.9052e+05 -70299 -46954 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2154 0.12367 0.0032261 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.6939e-07 0.088563 0.00032868 5.7342e-06 INSTANT 0.876738000E-01 TIME STEP NUMBER 56936 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283196074E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.862086952E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.16849E-01 0.22533E+01 Friction velocity uk : 0.16849E-01 0.22533E+01 Dimensionless distance yplus : 0.16214E-01 0.22156E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -8.418145828e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29604E+08 1 0.20176E-09 0.45082E+02 0.24972E+04 c Velocity[X] 0.25820E+02 c Velocity[Y] 0.19262E+02 c Velocity[Z] 0.10027E-05 c Pressure 0.18840E-03 39 0.96041E-04 0.11719E-02 0.74951E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -34.091 47.759 5.6086 8.0011 v Velocity[Y] -35.014 37.766 -0.19385 -0.14791 v Velocity[Z] -3.1777 3.1774 2.1326e-06 -5.3931e-08 v ǁVelocityǁ 0.0024215 48.062 9.1015 8.2607 v Pressure -4.9152e+05 1.8951e+05 -1.7322e+05 -1.4933e+05 v TurbVisc 8.105e-19 0.029783 0.00022599 9.0599e-05 v CourantNb 7.0408e-09 0.011679 0.00017229 4.9834e-06 v FourierNb 1.2466e-07 0.087327 0.00015642 7.5156e-07 v total_pressure -3.9019e+05 2.9083e+05 -71893 -48006 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2156 0.12369 0.0032264 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.7007e-07 0.088411 0.00032871 5.735e-06 INSTANT 0.876739000E-01 TIME STEP NUMBER 56937 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283191640E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.861896247E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.18321E-01 0.22535E+01 Friction velocity uk : 0.18321E-01 0.22535E+01 Dimensionless distance yplus : 0.17630E-01 0.22159E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -8.419541289e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29605E+08 1 0.20182E-09 0.45124E+02 0.24982E+04 c Velocity[X] 0.25862E+02 c Velocity[Y] 0.19262E+02 c Velocity[Z] 0.99392E-06 c Pressure 0.18640E-03 534 0.81946E-04 0.11587E-02 0.55502E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -34.104 47.77 5.6085 8.001 v Velocity[Y] -35.024 37.778 -0.19398 -0.14829 v Velocity[Z] -3.1781 3.1775 2.1321e-06 -5.3931e-08 v ǁVelocityǁ 0.00244 48.073 9.103 8.2609 v Pressure -4.93e+05 1.898e+05 -1.7479e+05 -1.5022e+05 v TurbVisc 8.0398e-19 0.029797 0.00022606 9.0706e-05 v CourantNb 4.2739e-09 0.011679 0.00017229 4.9834e-06 v FourierNb 1.2466e-07 0.087157 0.00015644 7.5229e-07 v total_pressure -3.9167e+05 2.9112e+05 -73467 -48894 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2159 0.1237 0.0032266 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.7075e-07 0.088241 0.00032874 5.7357e-06 INSTANT 0.876740000E-01 TIME STEP NUMBER 56938 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283186925E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.861692816E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.18037E-01 0.22538E+01 Friction velocity uk : 0.18037E-01 0.22538E+01 Dimensionless distance yplus : 0.17510E-01 0.22161E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -8.444770985e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29605E+08 1 0.20187E-09 0.45195E+02 0.25000E+04 c Velocity[X] 0.25900E+02 c Velocity[Y] 0.19295E+02 c Velocity[Z] 0.99873E-06 c Pressure 0.17895E-03 9 0.59794E-04 0.11116E-02 0.41843E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -34.117 47.781 5.6084 8.0009 v Velocity[Y] -35.034 37.79 -0.1941 -0.14868 v Velocity[Z] -3.1784 3.1776 2.1317e-06 -5.3931e-08 v ǁVelocityǁ 0.0024599 48.084 9.1045 8.261 v Pressure -4.9431e+05 1.9009e+05 -1.7629e+05 -1.5093e+05 v TurbVisc 8.0888e-19 0.02981 0.00022613 9.0812e-05 v CourantNb 3.3341e-09 0.01168 0.0001723 4.9834e-06 v FourierNb 1.2466e-07 0.086969 0.00015646 7.5301e-07 v total_pressure -3.9298e+05 2.9141e+05 -74960 -49610 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2161 0.12372 0.0032269 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.7144e-07 0.088053 0.00032876 5.7364e-06 INSTANT 0.876741000E-01 TIME STEP NUMBER 56939 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283182019E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.861481311E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15336E-01 0.22540E+01 Friction velocity uk : 0.15336E-01 0.22540E+01 Dimensionless distance yplus : 0.14888E-01 0.22163E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -8.493082484e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29605E+08 1 0.20191E-09 0.45263E+02 0.25018E+04 c Velocity[X] 0.25943E+02 c Velocity[Y] 0.19320E+02 c Velocity[Z] 0.99263E-06 c Pressure 0.17784E-03 536 0.78179E-04 0.11039E-02 0.82287E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -34.13 47.791 5.6084 8.0007 v Velocity[Y] -35.044 37.802 -0.19423 -0.14906 v Velocity[Z] -3.1787 3.1777 2.1313e-06 -5.3931e-08 v ǁVelocityǁ 0.0024579 48.095 9.1059 8.2612 v Pressure -4.9436e+05 1.9039e+05 -1.7785e+05 -1.5226e+05 v TurbVisc 8.4731e-19 0.029824 0.00022619 9.0918e-05 v CourantNb 4.582e-09 0.011681 0.00017231 4.9834e-06 v FourierNb 1.2466e-07 0.086767 0.00015648 7.5374e-07 v total_pressure -3.9304e+05 2.9171e+05 -76528 -50933 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2163 0.12373 0.0032271 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.7213e-07 0.087851 0.00032879 5.7372e-06 INSTANT 0.876742000E-01 TIME STEP NUMBER 56940 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283177233E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.861258755E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12529E-01 0.22542E+01 Friction velocity uk : 0.12529E-01 0.22542E+01 Dimensionless distance yplus : 0.12163E-01 0.22165E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -8.510644527e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29605E+08 1 0.20198E-09 0.45326E+02 0.25034E+04 c Velocity[X] 0.25983E+02 c Velocity[Y] 0.19342E+02 c Velocity[Z] 0.98949E-06 c Pressure 0.17501E-03 471 0.84038E-04 0.10856E-02 0.55575E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -34.142 47.802 5.6083 8.0006 v Velocity[Y] -35.054 37.814 -0.19436 -0.14945 v Velocity[Z] -3.1791 3.1778 2.1308e-06 -5.3931e-08 v ǁVelocityǁ 0.0021887 48.105 9.1074 8.2613 v Pressure -4.9617e+05 1.9068e+05 -1.7933e+05 -1.5302e+05 v TurbVisc 1.1808e-18 0.029837 0.00022626 9.1025e-05 v CourantNb 4.6688e-09 0.011681 0.00017232 4.9835e-06 v FourierNb 1.2466e-07 0.086547 0.00015649 7.5446e-07 v total_pressure -3.9485e+05 2.92e+05 -78005 -51694 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2165 0.12374 0.0032273 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.7281e-07 0.087632 0.00032881 5.7379e-06 INSTANT 0.876743000E-01 TIME STEP NUMBER 56941 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283172070E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.861031766E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.84444E-02 0.22545E+01 Friction velocity uk : 0.84444E-02 0.22545E+01 Dimensionless distance yplus : 0.81978E-02 0.22168E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -8.478519050e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29605E+08 1 0.20202E-09 0.45395E+02 0.25051E+04 c Velocity[X] 0.26015E+02 c Velocity[Y] 0.19380E+02 c Velocity[Z] 0.98256E-06 c Pressure 0.17284E-03 35 0.97657E-04 0.10714E-02 0.72764E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -34.155 47.812 5.6082 8.0005 v Velocity[Y] -35.064 37.826 -0.19448 -0.14984 v Velocity[Z] -3.1794 3.1779 2.1304e-06 -5.3931e-08 v ǁVelocityǁ 0.001944 48.116 9.1088 8.2615 v Pressure -4.9611e+05 1.9099e+05 -1.8079e+05 -1.5405e+05 v TurbVisc 7.3086e-19 0.029851 0.00022633 9.1131e-05 v CourantNb 7.264e-09 0.011682 0.00017233 4.9835e-06 v FourierNb 1.2466e-07 0.08631 0.00015651 7.5519e-07 v total_pressure -3.9478e+05 2.9231e+05 -79463 -52727 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2168 0.12376 0.0032275 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.735e-07 0.087394 0.00032884 5.7387e-06 INSTANT 0.876744000E-01 TIME STEP NUMBER 56942 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283167048E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.860798946E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.51352E-02 0.22547E+01 Friction velocity uk : 0.51352E-02 0.22547E+01 Dimensionless distance yplus : 0.49852E-02 0.22170E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -8.472151980e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29606E+08 1 0.20209E-09 0.45436E+02 0.25061E+04 c Velocity[X] 0.26060E+02 c Velocity[Y] 0.19377E+02 c Velocity[Z] 0.97449E-06 c Pressure 0.17074E-03 352 0.82954E-04 0.10576E-02 0.47740E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -34.168 47.822 5.6081 8.0004 v Velocity[Y] -35.073 37.838 -0.19461 -0.15022 v Velocity[Z] -3.1797 3.1781 2.1299e-06 -5.3931e-08 v ǁVelocityǁ 0.0017327 48.127 9.1103 8.2617 v Pressure -4.9752e+05 1.9129e+05 -1.8218e+05 -1.5478e+05 v TurbVisc 6.8793e-19 0.029865 0.0002264 9.1238e-05 v CourantNb 9.9463e-09 0.011683 0.00017233 4.9835e-06 v FourierNb 1.2466e-07 0.086052 0.00015653 7.5592e-07 v total_pressure -3.9619e+05 2.9261e+05 -80856 -53451 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.217 0.12377 0.0032277 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.7401e-07 0.087137 0.00032886 5.7394e-06 INSTANT 0.876745000E-01 TIME STEP NUMBER 56943 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283161800E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.860555244E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10238E-01 0.22549E+01 Friction velocity uk : 0.10238E-01 0.22549E+01 Dimensionless distance yplus : 0.99392E-02 0.22172E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -8.459719388e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29606E+08 1 0.20213E-09 0.45507E+02 0.25080E+04 c Velocity[X] 0.26091E+02 c Velocity[Y] 0.19416E+02 c Velocity[Z] 0.97831E-06 c Pressure 0.16238E-03 9 0.60427E-04 0.10051E-02 0.41510E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -34.18 47.833 5.608 8.0003 v Velocity[Y] -35.083 37.85 -0.19474 -0.15061 v Velocity[Z] -3.18 3.1782 2.1295e-06 -5.3931e-08 v ǁVelocityǁ 0.0015706 48.137 9.1118 8.2618 v Pressure -4.9893e+05 1.9158e+05 -1.8354e+05 -1.5551e+05 v TurbVisc 7.5073e-19 0.029878 0.00022647 9.1345e-05 v CourantNb 1.2616e-08 0.011683 0.00017234 4.9835e-06 v FourierNb 1.2466e-07 0.085777 0.00015654 7.5664e-07 v total_pressure -3.9761e+05 2.929e+05 -82220 -54183 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2172 0.12378 0.0032278 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.7452e-07 0.086862 0.00032889 5.7402e-06 INSTANT 0.876746000E-01 TIME STEP NUMBER 56944 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283156320E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.860303117E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13808E-01 0.22551E+01 Friction velocity uk : 0.13808E-01 0.22551E+01 Dimensionless distance yplus : 0.13404E-01 0.22174E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -8.473256798e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29606E+08 1 0.20217E-09 0.45575E+02 0.25097E+04 c Velocity[X] 0.26138E+02 c Velocity[Y] 0.19437E+02 c Velocity[Z] 0.97554E-06 c Pressure 0.16137E-03 53 0.78812E-04 0.99816E-03 0.72341E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -34.193 47.843 5.6079 8.0002 v Velocity[Y] -35.092 37.862 -0.19487 -0.151 v Velocity[Z] -3.1804 3.1783 2.1291e-06 -5.3931e-08 v ǁVelocityǁ 0.0014757 48.148 9.1132 8.262 v Pressure -4.9888e+05 1.9189e+05 -1.8492e+05 -1.5666e+05 v TurbVisc 8.078e-19 0.029892 0.00022654 9.1451e-05 v CourantNb 1.526e-08 0.011684 0.00017235 4.9835e-06 v FourierNb 1.2466e-07 0.085485 0.00015656 7.5737e-07 v total_pressure -3.9755e+05 2.9321e+05 -83599 -55338 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2174 0.12379 0.0032278 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.7504e-07 0.08657 0.00032891 5.7409e-06 INSTANT 0.876747000E-01 TIME STEP NUMBER 56945 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283151012E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.860042690E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.74902E-02 0.22554E+01 Friction velocity uk : 0.74902E-02 0.22554E+01 Dimensionless distance yplus : 0.72428E-02 0.22177E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -8.466188019e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29606E+08 1 0.20225E-09 0.45638E+02 0.25113E+04 c Velocity[X] 0.26174E+02 c Velocity[Y] 0.19463E+02 c Velocity[Z] 0.98659E-06 c Pressure 0.15831E-03 65 0.84638E-04 0.97858E-03 0.51933E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -34.205 47.853 5.6078 8 v Velocity[Y] -35.102 37.874 -0.19499 -0.15138 v Velocity[Z] -3.1807 3.1784 2.1286e-06 -5.3932e-08 v ǁVelocityǁ 0.0014548 48.158 9.1147 8.2621 v Pressure -5.0076e+05 1.9218e+05 -1.8624e+05 -1.5736e+05 v TurbVisc 8.0166e-19 0.029905 0.0002266 9.1558e-05 v CourantNb 1.7692e-08 0.011685 0.00017236 4.9835e-06 v FourierNb 1.2466e-07 0.085176 0.00015658 7.581e-07 v total_pressure -3.9944e+05 2.9351e+05 -84910 -56035 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2177 0.1238 0.0032279 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.7555e-07 0.086261 0.00032893 5.7416e-06 INSTANT 0.876748000E-01 TIME STEP NUMBER 56946 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283145303E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.859777065E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.59917E-02 0.22556E+01 Friction velocity uk : 0.59917E-02 0.22556E+01 Dimensionless distance yplus : 0.57644E-02 0.22179E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -8.446794457e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29606E+08 1 0.20229E-09 0.45707E+02 0.25130E+04 c Velocity[X] 0.26212E+02 c Velocity[Y] 0.19495E+02 c Velocity[Z] 0.96593E-06 c Pressure 0.15610E-03 103 0.98300E-04 0.96424E-03 0.65968E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -34.218 47.863 5.6077 7.9999 v Velocity[Y] -35.111 37.885 -0.19512 -0.15178 v Velocity[Z] -3.181 3.1785 2.1282e-06 -5.3932e-08 v ǁVelocityǁ 0.0014755 48.169 9.1161 8.2623 v Pressure -5.0058e+05 1.925e+05 -1.8752e+05 -1.5827e+05 v TurbVisc 8.2874e-19 0.029919 0.00022667 9.1665e-05 v CourantNb 1.7554e-08 0.011685 0.00017236 4.9836e-06 v FourierNb 1.2466e-07 0.084847 0.00015659 7.5883e-07 v total_pressure -3.9925e+05 2.9382e+05 -86198 -56941 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2179 0.12381 0.003228 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.7607e-07 0.085932 0.00032896 5.7424e-06 INSTANT 0.876749000E-01 TIME STEP NUMBER 56947 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283139807E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.859506476E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.73655E-02 0.22558E+01 Friction velocity uk : 0.73655E-02 0.22558E+01 Dimensionless distance yplus : 0.70862E-02 0.22181E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -8.406623990e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29607E+08 1 0.20235E-09 0.45746E+02 0.25140E+04 c Velocity[X] 0.26252E+02 c Velocity[Y] 0.19494E+02 c Velocity[Z] 0.95919E-06 c Pressure 0.15400E-03 324 0.83605E-04 0.95061E-03 0.42327E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -34.23 47.873 5.6077 7.9998 v Velocity[Y] -35.121 37.897 -0.19525 -0.15217 v Velocity[Z] -3.1814 3.1786 2.1277e-06 -5.3932e-08 v ǁVelocityǁ 0.0015749 48.179 9.1176 8.2624 v Pressure -5.0203e+05 1.928e+05 -1.8873e+05 -1.5889e+05 v TurbVisc 8.6577e-19 0.029932 0.00022674 9.1772e-05 v CourantNb 1.8025e-08 0.011686 0.00017237 4.9836e-06 v FourierNb 1.2466e-07 0.084498 0.00015661 7.5956e-07 v total_pressure -4.0071e+05 2.9413e+05 -87409 -57567 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2181 0.12382 0.0032282 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.7659e-07 0.085583 0.00032898 5.7431e-06 INSTANT 0.876750000E-01 TIME STEP NUMBER 56948 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283134067E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.859227185E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.83542E-02 0.22561E+01 Friction velocity uk : 0.83542E-02 0.22561E+01 Dimensionless distance yplus : 0.80374E-02 0.22184E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -8.405453428e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29607E+08 1 0.20240E-09 0.45817E+02 0.25158E+04 c Velocity[X] 0.26284E+02 c Velocity[Y] 0.19534E+02 c Velocity[Z] 0.97821E-06 c Pressure 0.14478E-03 18 0.61352E-04 0.89304E-03 0.36389E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -34.242 47.883 5.6076 7.9996 v Velocity[Y] -35.13 37.908 -0.19538 -0.15256 v Velocity[Z] -3.1817 3.1787 2.1273e-06 -5.3932e-08 v ǁVelocityǁ 0.0017362 48.189 9.119 8.2626 v Pressure -5.0341e+05 1.931e+05 -1.8992e+05 -1.5953e+05 v TurbVisc 8.6882e-19 0.029946 0.00022681 9.1879e-05 v CourantNb 1.846e-08 0.011686 0.00017238 4.9836e-06 v FourierNb 1.2466e-07 0.084129 0.00015662 7.6029e-07 v total_pressure -4.0209e+05 2.9442e+05 -88593 -58202 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2184 0.12383 0.0032284 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.7711e-07 0.085215 0.00032901 5.7439e-06 INSTANT 0.876751000E-01 TIME STEP NUMBER 56949 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283128134E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.858939344E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15950E-01 0.22563E+01 Friction velocity uk : 0.15950E-01 0.22563E+01 Dimensionless distance yplus : 0.15345E-01 0.22186E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -8.437730858e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29607E+08 1 0.20243E-09 0.45885E+02 0.25176E+04 c Velocity[X] 0.26327E+02 c Velocity[Y] 0.19558E+02 c Velocity[Z] 0.96420E-06 c Pressure 0.14404E-03 441 0.80097E-04 0.88786E-03 0.71847E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -34.254 47.893 5.6075 7.9995 v Velocity[Y] -35.14 37.92 -0.19551 -0.15295 v Velocity[Z] -3.182 3.1789 2.1269e-06 -5.3932e-08 v ǁVelocityǁ 0.0019597 48.2 9.1205 8.2627 v Pressure -5.0344e+05 1.9341e+05 -1.9116e+05 -1.607e+05 v TurbVisc 8.0908e-19 0.029959 0.00022687 9.1986e-05 v CourantNb 2.0347e-08 0.011687 0.00017239 4.9836e-06 v FourierNb 1.2466e-07 0.083741 0.00015664 7.6102e-07 v total_pressure -4.0211e+05 2.9473e+05 -89830 -59372 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2186 0.12384 0.0032286 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.7763e-07 0.084827 0.00032903 5.7446e-06 INSTANT 0.876752000E-01 TIME STEP NUMBER 56950 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283122316E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.858643433E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11121E-01 0.22565E+01 Friction velocity uk : 0.11121E-01 0.22565E+01 Dimensionless distance yplus : 0.10921E-01 0.22188E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -8.407477928e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29607E+08 1 0.20251E-09 0.45947E+02 0.25191E+04 c Velocity[X] 0.26371E+02 c Velocity[Y] 0.19576E+02 c Velocity[Z] 0.94823E-06 c Pressure 0.14104E-03 693 0.86132E-04 0.86876E-03 0.44098E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -34.267 47.903 5.6074 7.9994 v Velocity[Y] -35.149 37.932 -0.19564 -0.15334 v Velocity[Z] -3.1824 3.179 2.1264e-06 -5.3932e-08 v ǁVelocityǁ 0.0022121 48.21 9.1219 8.2628 v Pressure -5.0514e+05 1.9371e+05 -1.9222e+05 -1.6107e+05 v TurbVisc 9.0263e-19 0.029973 0.00022694 9.2093e-05 v CourantNb 2.1202e-08 0.011688 0.0001724 4.9836e-06 v FourierNb 1.2466e-07 0.083336 0.00015666 7.6175e-07 v total_pressure -4.0382e+05 2.9504e+05 -90890 -59740 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2188 0.12384 0.0032287 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.7815e-07 0.084422 0.00032905 5.7453e-06 INSTANT 0.876753000E-01 TIME STEP NUMBER 56951 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283116225E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.858347152E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.38378E-02 0.22568E+01 Friction velocity uk : 0.38378E-02 0.22568E+01 Dimensionless distance yplus : 0.37689E-02 0.22190E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -8.423874918e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29607E+08 1 0.20255E-09 0.45992E+02 0.25202E+04 c Velocity[X] 0.26398E+02 c Velocity[Y] 0.19595E+02 c Velocity[Z] 0.94280E-06 c Pressure 0.13889E-03 55 0.75028E-04 0.85490E-03 0.52633E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -34.279 47.913 5.6073 7.9992 v Velocity[Y] -35.158 37.943 -0.19578 -0.15373 v Velocity[Z] -3.1827 3.1791 2.126e-06 -5.3932e-08 v ǁVelocityǁ 0.0022663 48.22 9.1234 8.263 v Pressure -5.0561e+05 1.9403e+05 -1.9334e+05 -1.6194e+05 v TurbVisc 8.9225e-19 0.029986 0.00022701 9.22e-05 v CourantNb 2.6228e-08 0.011688 0.0001724 4.9836e-06 v FourierNb 1.2467e-07 0.08291 0.00015667 7.6248e-07 v total_pressure -4.0428e+05 2.9536e+05 -92019 -60620 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.219 0.12385 0.0032288 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.7867e-07 0.083996 0.00032907 5.7461e-06 INSTANT 0.876754000E-01 TIME STEP NUMBER 56952 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283110176E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.858042330E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.92197E-02 0.22570E+01 Friction velocity uk : 0.92197E-02 0.22570E+01 Dimensionless distance yplus : 0.89192E-02 0.22193E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -8.414536131e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29608E+08 1 0.20260E-09 0.46062E+02 0.25220E+04 c Velocity[X] 0.26433E+02 c Velocity[Y] 0.19629E+02 c Velocity[Z] 0.95678E-06 c Pressure 0.13033E-03 16 0.55058E-04 0.80164E-03 0.31753E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -34.291 47.923 5.6072 7.9991 v Velocity[Y] -35.167 37.954 -0.19591 -0.15413 v Velocity[Z] -3.183 3.1792 2.1255e-06 -5.3932e-08 v ǁVelocityǁ 0.0021172 48.23 9.1248 8.2631 v Pressure -5.0605e+05 1.9434e+05 -1.9436e+05 -1.6248e+05 v TurbVisc 9.3675e-19 0.03 0.00022707 9.2307e-05 v CourantNb 3.1001e-08 0.011689 0.00017241 4.9836e-06 v FourierNb 1.2467e-07 0.08246 0.00015669 7.6321e-07 v total_pressure -4.0473e+05 2.9566e+05 -93032 -61155 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2193 0.12386 0.0032289 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.7919e-07 0.083546 0.0003291 5.7468e-06 INSTANT 0.876755000E-01 TIME STEP NUMBER 56953 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283104110E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.857730825E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10306E-01 0.22572E+01 Friction velocity uk : 0.10306E-01 0.22572E+01 Dimensionless distance yplus : 0.99748E-02 0.22194E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -8.470848690e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29608E+08 1 0.20265E-09 0.46116E+02 0.25234E+04 c Velocity[X] 0.26475E+02 c Velocity[Y] 0.19641E+02 c Velocity[Z] 0.95123E-06 c Pressure 0.12928E-03 136 0.97002E-04 0.79462E-03 0.39450E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -34.303 47.932 5.6071 7.999 v Velocity[Y] -35.176 37.966 -0.19604 -0.15452 v Velocity[Z] -3.1833 3.1793 2.1251e-06 -5.3932e-08 v ǁVelocityǁ 0.00196 48.24 9.1262 8.2633 v Pressure -5.0723e+05 1.9465e+05 -1.9537e+05 -1.632e+05 v TurbVisc 1.3088e-18 0.030013 0.00022714 9.2414e-05 v CourantNb 3.2406e-08 0.011689 0.00017242 4.9836e-06 v FourierNb 1.2467e-07 0.081989 0.0001567 7.6394e-07 v total_pressure -4.059e+05 2.9598e+05 -94042 -61872 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2194 0.12387 0.0032289 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.7971e-07 0.083075 0.00032912 5.7476e-06 INSTANT 0.876756000E-01 TIME STEP NUMBER 56954 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283097890E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.857410207E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.27034E-02 0.22574E+01 Friction velocity uk : 0.27034E-02 0.22574E+01 Dimensionless distance yplus : 0.26166E-02 0.22197E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -8.458481890e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29608E+08 1 0.20271E-09 0.46175E+02 0.25249E+04 c Velocity[X] 0.26516E+02 c Velocity[Y] 0.19660E+02 c Velocity[Z] 0.93341E-06 c Pressure 0.12478E-03 35 0.81162E-04 0.76641E-03 0.31425E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -34.315 47.942 5.607 7.9988 v Velocity[Y] -35.185 37.977 -0.19617 -0.15492 v Velocity[Z] -3.1837 3.1794 2.1246e-06 -5.3932e-08 v ǁVelocityǁ 0.0018101 48.25 9.1277 8.2634 v Pressure -5.0825e+05 1.9496e+05 -1.9633e+05 -1.6379e+05 v TurbVisc 9.0862e-19 0.030027 0.0002272 9.2522e-05 v CourantNb 3.2212e-08 0.01169 0.00017243 4.9836e-06 v FourierNb 1.2467e-07 0.0815 0.00015671 7.6467e-07 v total_pressure -4.0692e+05 2.9629e+05 -95010 -62463 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2197 0.12388 0.003229 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.8024e-07 0.082586 0.00032914 5.7483e-06 INSTANT 0.876757000E-01 TIME STEP NUMBER 56955 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283091622E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.857086253E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.76118E-02 0.22577E+01 Friction velocity uk : 0.76118E-02 0.22577E+01 Dimensionless distance yplus : 0.73675E-02 0.22199E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -8.513985936e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29608E+08 1 0.20276E-09 0.46244E+02 0.25266E+04 c Velocity[X] 0.26551E+02 c Velocity[Y] 0.19693E+02 c Velocity[Z] 0.96278E-06 c Pressure 0.11945E-03 15 0.55052E-04 0.73318E-03 0.30298E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -34.327 47.951 5.6069 7.9987 v Velocity[Y] -35.194 37.988 -0.19631 -0.15531 v Velocity[Z] -3.184 3.1795 2.1242e-06 -5.3932e-08 v ǁVelocityǁ 0.0016643 48.26 9.1291 8.2635 v Pressure -5.0947e+05 1.9527e+05 -1.9727e+05 -1.6431e+05 v TurbVisc 9.7954e-19 0.03004 0.00022727 9.2629e-05 v CourantNb 3.1742e-08 0.011691 0.00017244 4.9836e-06 v FourierNb 1.2467e-07 0.080984 0.00015673 7.654e-07 v total_pressure -4.0815e+05 2.966e+05 -95946 -62983 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2199 0.12391 0.0032295 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.8076e-07 0.08207 0.00032916 5.749e-06 INSTANT 0.876758000E-01 TIME STEP NUMBER 56956 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283085246E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.856756862E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.69469E-02 0.22579E+01 Friction velocity uk : 0.69469E-02 0.22579E+01 Dimensionless distance yplus : 0.66835E-02 0.22201E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -8.620951582e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29608E+08 1 0.20280E-09 0.46299E+02 0.25280E+04 c Velocity[X] 0.26590E+02 c Velocity[Y] 0.19709E+02 c Velocity[Z] 0.94293E-06 c Pressure 0.11907E-03 21 0.99195E-04 0.73032E-03 0.44372E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -34.339 47.961 5.6068 7.9986 v Velocity[Y] -35.203 38 -0.19644 -0.1557 v Velocity[Z] -3.1843 3.1797 2.1238e-06 -5.3932e-08 v ǁVelocityǁ 0.0013603 48.269 9.1306 8.2637 v Pressure -5.1013e+05 1.9558e+05 -1.9819e+05 -1.6514e+05 v TurbVisc 1.2743e-18 0.030054 0.00022734 9.2736e-05 v CourantNb 3.0873e-08 0.011691 0.00017244 4.9836e-06 v FourierNb 1.2467e-07 0.08045 0.00015674 7.6614e-07 v total_pressure -4.088e+05 2.9691e+05 -96864 -63813 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2201 0.12392 0.0032299 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.8129e-07 0.081537 0.00032919 5.7498e-06 INSTANT 0.876759000E-01 TIME STEP NUMBER 56957 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283078798E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.856422355E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.86968E-02 0.22581E+01 Friction velocity uk : 0.86968E-02 0.22581E+01 Dimensionless distance yplus : 0.83969E-02 0.22204E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -8.590354181e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29608E+08 1 0.20287E-09 0.46355E+02 0.25294E+04 c Velocity[X] 0.26621E+02 c Velocity[Y] 0.19734E+02 c Velocity[Z] 0.92188E-06 c Pressure 0.11465E-03 49 0.83955E-04 0.70273E-03 0.27249E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -34.351 47.97 5.6067 7.9984 v Velocity[Y] -35.212 38.011 -0.19657 -0.1561 v Velocity[Z] -3.1847 3.1798 2.1233e-06 -5.3932e-08 v ǁVelocityǁ 0.00096065 48.279 9.132 8.2638 v Pressure -5.108e+05 1.9591e+05 -1.9901e+05 -1.6564e+05 v TurbVisc 8.5209e-19 0.030067 0.0002274 9.2844e-05 v CourantNb 3.0777e-08 0.011692 0.00017245 4.9836e-06 v FourierNb 1.2467e-07 0.079892 0.00015675 7.6687e-07 v total_pressure -4.0947e+05 2.9723e+05 -97687 -64311 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2204 0.12394 0.0032304 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.8182e-07 0.080978 0.00032921 5.7505e-06 INSTANT 0.876760000E-01 TIME STEP NUMBER 56958 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283072367E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.856085325E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10326E-01 0.22583E+01 Friction velocity uk : 0.10326E-01 0.22583E+01 Dimensionless distance yplus : 0.99728E-02 0.22206E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -8.677080185e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29608E+08 1 0.20292E-09 0.46425E+02 0.25312E+04 c Velocity[X] 0.26653E+02 c Velocity[Y] 0.19772E+02 c Velocity[Z] 0.94827E-06 c Pressure 0.10919E-03 15 0.55633E-04 0.66876E-03 0.28893E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -34.363 47.98 5.6066 7.9983 v Velocity[Y] -35.221 38.022 -0.19671 -0.1565 v Velocity[Z] -3.185 3.1799 2.1229e-06 -5.3933e-08 v ǁVelocityǁ 0.00057365 48.289 9.1334 8.2639 v Pressure -5.1128e+05 1.9623e+05 -1.9981e+05 -1.6611e+05 v TurbVisc 1.0885e-18 0.030081 0.00022747 9.2952e-05 v CourantNb 3.0223e-08 0.011692 0.00017246 4.9837e-06 v FourierNb 1.2467e-07 0.079306 0.00015677 7.676e-07 v total_pressure -4.0995e+05 2.9755e+05 -98487 -64780 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2206 0.12398 0.0032314 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.8234e-07 0.080393 0.00032923 5.7513e-06 INSTANT 0.876761000E-01 TIME STEP NUMBER 56959 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283065957E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.855742336E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10467E-01 0.22585E+01 Friction velocity uk : 0.10467E-01 0.22585E+01 Dimensionless distance yplus : 0.10100E-01 0.22208E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -8.851045996e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29609E+08 1 0.20297E-09 0.46483E+02 0.25326E+04 c Velocity[X] 0.26700E+02 c Velocity[Y] 0.19783E+02 c Velocity[Z] 0.94044E-06 c Pressure 0.10943E-03 256 0.77228E-04 0.66977E-03 0.42651E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -34.374 47.989 5.6065 7.9981 v Velocity[Y] -35.23 38.033 -0.19684 -0.1569 v Velocity[Z] -3.1853 3.18 2.1224e-06 -5.3933e-08 v ǁVelocityǁ 0.00032967 48.299 9.1348 8.2641 v Pressure -5.1294e+05 1.9655e+05 -2.0057e+05 -1.6663e+05 v TurbVisc 1.1966e-18 0.030094 0.00022753 9.3059e-05 v CourantNb 2.944e-08 0.011693 0.00017247 4.9837e-06 v FourierNb 1.2467e-07 0.078698 0.00015678 7.6834e-07 v total_pressure -4.1162e+05 2.9787e+05 -99243 -65300 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2208 0.12401 0.0032322 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.8287e-07 0.079784 0.00032925 5.752e-06 INSTANT 0.876762000E-01 TIME STEP NUMBER 56960 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283059301E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.855393576E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.33671E-02 0.22588E+01 Friction velocity uk : 0.33671E-02 0.22588E+01 Dimensionless distance yplus : 0.32489E-02 0.22210E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -8.862075211e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29609E+08 1 0.20302E-09 0.46549E+02 0.25343E+04 c Velocity[X] 0.26731E+02 c Velocity[Y] 0.19818E+02 c Velocity[Z] 0.93163E-06 c Pressure 0.10679E-03 55 0.81576E-04 0.65317E-03 0.43329E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -34.386 47.998 5.6064 7.998 v Velocity[Y] -35.239 38.044 -0.19698 -0.1573 v Velocity[Z] -3.1856 3.1801 2.122e-06 -5.3933e-08 v ǁVelocityǁ 0.00035725 48.308 9.1363 8.2642 v Pressure -5.1289e+05 1.9688e+05 -2.0128e+05 -1.671e+05 v TurbVisc 8.6971e-19 0.030108 0.0002276 9.3167e-05 v CourantNb 2.9149e-08 0.011694 0.00017248 4.9837e-06 v FourierNb 1.2467e-07 0.078064 0.00015679 7.6907e-07 v total_pressure -4.1156e+05 2.982e+05 -99954 -65777 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.221 0.12404 0.0032329 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.834e-07 0.07915 0.00032927 5.7527e-06 INSTANT 0.876763000E-01 TIME STEP NUMBER 56961 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283052880E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.855042133E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10425E-01 0.22590E+01 Friction velocity uk : 0.10425E-01 0.22590E+01 Dimensionless distance yplus : 0.10059E-01 0.22212E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -8.967431791e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29609E+08 1 0.20308E-09 0.46609E+02 0.25358E+04 c Velocity[X] 0.26767E+02 c Velocity[Y] 0.19842E+02 c Velocity[Z] 0.91629E-06 c Pressure 0.10551E-03 102 0.95504E-04 0.64490E-03 0.45612E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -34.398 48.008 5.6063 7.9978 v Velocity[Y] -35.247 38.055 -0.19711 -0.15769 v Velocity[Z] -3.186 3.1802 2.1215e-06 -5.3933e-08 v ǁVelocityǁ 0.00064637 48.318 9.1377 8.2643 v Pressure -5.1482e+05 1.9718e+05 -2.0196e+05 -1.6752e+05 v TurbVisc 9.1323e-19 0.030122 0.00022766 9.3274e-05 v CourantNb 2.872e-08 0.011694 0.00017248 4.9837e-06 v FourierNb 1.2467e-07 0.077401 0.00015681 7.6981e-07 v total_pressure -4.1349e+05 2.9851e+05 -1.0063e+05 -66198 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2212 0.12407 0.0032336 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.8393e-07 0.078487 0.00032929 5.7535e-06 INSTANT 0.876764000E-01 TIME STEP NUMBER 56962 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283046065E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.854685484E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.14835E-01 0.22592E+01 Friction velocity uk : 0.14835E-01 0.22592E+01 Dimensionless distance yplus : 0.14315E-01 0.22214E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -9.071462402e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29609E+08 1 0.20312E-09 0.46651E+02 0.25368E+04 c Velocity[X] 0.26800E+02 c Velocity[Y] 0.19851E+02 c Velocity[Z] 0.91217E-06 c Pressure 0.10454E-03 83 0.81033E-04 0.63850E-03 0.37190E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -34.409 48.017 5.6062 7.9977 v Velocity[Y] -35.256 38.066 -0.19725 -0.15809 v Velocity[Z] -3.1863 3.1803 2.1211e-06 -5.3933e-08 v ǁVelocityǁ 0.00072143 48.327 9.1391 8.2645 v Pressure -5.1507e+05 1.9751e+05 -2.0261e+05 -1.6808e+05 v TurbVisc 9.5086e-19 0.030136 0.00022772 9.3382e-05 v CourantNb 2.8238e-08 0.011695 0.00017249 4.9837e-06 v FourierNb 1.2467e-07 0.076707 0.00015682 7.7054e-07 v total_pressure -4.1375e+05 2.9884e+05 -1.0129e+05 -66756 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2214 0.12409 0.0032342 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.8447e-07 0.077794 0.00032931 5.7542e-06 INSTANT 0.876765000E-01 TIME STEP NUMBER 56963 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283039433E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.854324907E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.14578E-01 0.22594E+01 Friction velocity uk : 0.14578E-01 0.22594E+01 Dimensionless distance yplus : 0.14134E-01 0.22216E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -9.182127448e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29609E+08 1 0.20318E-09 0.46720E+02 0.25385E+04 c Velocity[X] 0.26829E+02 c Velocity[Y] 0.19891E+02 c Velocity[Z] 0.92563E-06 c Pressure 0.93618E-04 13 0.56369E-04 0.57138E-03 0.22549E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -34.421 48.026 5.6061 7.9975 v Velocity[Y] -35.265 38.077 -0.19738 -0.1585 v Velocity[Z] -3.1866 3.1804 2.1207e-06 -5.3933e-08 v ǁVelocityǁ 0.00064472 48.337 9.1405 8.2646 v Pressure -5.155e+05 1.9785e+05 -2.0314e+05 -1.6837e+05 v TurbVisc 1.0156e-18 0.03015 0.00022779 9.349e-05 v CourantNb 2.7789e-08 0.011695 0.0001725 4.9837e-06 v FourierNb 1.2467e-07 0.075984 0.00015683 7.7128e-07 v total_pressure -4.1417e+05 2.9917e+05 -1.0182e+05 -67042 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2216 0.12412 0.0032348 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.85e-07 0.07707 0.00032933 5.755e-06 INSTANT 0.876766000E-01 TIME STEP NUMBER 56964 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283032850E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.853961890E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12949E-01 0.22596E+01 Friction velocity uk : 0.12949E-01 0.22596E+01 Dimensionless distance yplus : 0.12555E-01 0.22218E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -9.365620578e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29609E+08 1 0.20323E-09 0.46776E+02 0.25400E+04 c Velocity[X] 0.26874E+02 c Velocity[Y] 0.19902E+02 c Velocity[Z] 0.91874E-06 c Pressure 0.94911E-04 82 0.77044E-04 0.57886E-03 0.39897E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -34.433 48.035 5.606 7.9974 v Velocity[Y] -35.273 38.088 -0.19752 -0.1589 v Velocity[Z] -3.187 3.1806 2.1202e-06 -5.3933e-08 v ǁVelocityǁ 0.0006108 48.346 9.142 8.2647 v Pressure -5.1719e+05 1.9816e+05 -2.0374e+05 -1.6879e+05 v TurbVisc 9.1314e-19 0.030164 0.00022785 9.3598e-05 v CourantNb 9.2711e-09 0.011696 0.00017251 4.9837e-06 v FourierNb 1.2468e-07 0.075224 0.00015684 7.7201e-07 v total_pressure -4.1586e+05 2.9949e+05 -1.0242e+05 -67468 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2218 0.12414 0.0032353 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.8553e-07 0.076311 0.00032935 5.7557e-06 INSTANT 0.876767000E-01 TIME STEP NUMBER 56965 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283025983E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.853594457E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12365E-01 0.22598E+01 Friction velocity uk : 0.12365E-01 0.22598E+01 Dimensionless distance yplus : 0.11989E-01 0.22221E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -9.415894385e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29609E+08 1 0.20329E-09 0.46842E+02 0.25416E+04 c Velocity[X] 0.26905E+02 c Velocity[Y] 0.19937E+02 c Velocity[Z] 0.90540E-06 c Pressure 0.93114E-04 67 0.82292E-04 0.56750E-03 0.42379E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -34.444 48.044 5.6059 7.9972 v Velocity[Y] -35.282 38.099 -0.19765 -0.1593 v Velocity[Z] -3.1873 3.1807 2.1198e-06 -5.3933e-08 v ǁVelocityǁ 0.00062574 48.355 9.1434 8.2648 v Pressure -5.1713e+05 1.985e+05 -2.0424e+05 -1.6922e+05 v TurbVisc 1.0293e-18 0.030178 0.00022792 9.3706e-05 v CourantNb 2.6757e-08 0.011697 0.00017252 4.9837e-06 v FourierNb 1.2468e-07 0.07444 0.00015685 7.7275e-07 v total_pressure -4.1581e+05 2.9983e+05 -1.0291e+05 -67895 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2221 0.12416 0.0032358 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.8607e-07 0.075526 0.00032937 5.7564e-06 INSTANT 0.876768000E-01 TIME STEP NUMBER 56966 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283019389E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.853224913E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13842E-01 0.22600E+01 Friction velocity uk : 0.13842E-01 0.22600E+01 Dimensionless distance yplus : 0.13420E-01 0.22223E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -9.574802979e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29610E+08 1 0.20335E-09 0.46900E+02 0.25431E+04 c Velocity[X] 0.26940E+02 c Velocity[Y] 0.19961E+02 c Velocity[Z] 0.89538E-06 c Pressure 0.92922E-04 116 0.95982E-04 0.56593E-03 0.43434E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -34.456 48.053 5.6058 7.9971 v Velocity[Y] -35.291 38.11 -0.19779 -0.1597 v Velocity[Z] -3.1876 3.1808 2.1193e-06 -5.3933e-08 v ǁVelocityǁ 0.00062319 48.365 9.1448 8.265 v Pressure -5.1904e+05 1.9882e+05 -2.0468e+05 -1.6947e+05 v TurbVisc 1.0937e-18 0.030192 0.00022798 9.3814e-05 v CourantNb 2.6559e-08 0.011698 0.00017253 4.9837e-06 v FourierNb 1.2468e-07 0.073613 0.00015687 7.7348e-07 v total_pressure -4.1772e+05 3.0015e+05 -1.0336e+05 -68145 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2223 0.12418 0.0032363 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.866e-07 0.074699 0.00032939 5.7572e-06 INSTANT 0.876769000E-01 TIME STEP NUMBER 56967 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283012440E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.852853978E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.16129E-01 0.22602E+01 Friction velocity uk : 0.16129E-01 0.22602E+01 Dimensionless distance yplus : 0.15638E-01 0.22225E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -9.717464123e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29610E+08 1 0.20339E-09 0.46940E+02 0.25440E+04 c Velocity[X] 0.26971E+02 c Velocity[Y] 0.19970E+02 c Velocity[Z] 0.89269E-06 c Pressure 0.93098E-04 86 0.81525E-04 0.56660E-03 0.32723E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -34.467 48.062 5.6057 7.9969 v Velocity[Y] -35.299 38.12 -0.19792 -0.1601 v Velocity[Z] -3.1879 3.1809 2.1189e-06 -5.3933e-08 v ǁVelocityǁ 0.00048076 48.374 9.1462 8.2651 v Pressure -5.1928e+05 1.9916e+05 -2.0512e+05 -1.699e+05 v TurbVisc 1.1104e-18 0.030206 0.00022804 9.3922e-05 v CourantNb 2.615e-08 0.011699 0.00017253 4.9837e-06 v FourierNb 1.2468e-07 0.072745 0.00015688 7.7422e-07 v total_pressure -4.1795e+05 3.0048e+05 -1.0379e+05 -68574 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2225 0.1242 0.0032366 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.8714e-07 0.073831 0.00032941 5.7579e-06 INSTANT 0.876770000E-01 TIME STEP NUMBER 56968 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283005684E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.852480131E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10980E-01 0.22604E+01 Friction velocity uk : 0.10980E-01 0.22604E+01 Dimensionless distance yplus : 0.10660E-01 0.22227E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -9.868211981e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29610E+08 1 0.20345E-09 0.47008E+02 0.25457E+04 c Velocity[X] 0.26999E+02 c Velocity[Y] 0.20009E+02 c Velocity[Z] 0.89432E-06 c Pressure 0.81814E-04 7 0.56488E-04 0.49757E-03 0.19458E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -34.478 48.071 5.6056 7.9968 v Velocity[Y] -35.308 38.131 -0.19806 -0.16051 v Velocity[Z] -3.1883 3.181 2.1184e-06 -5.3933e-08 v ǁVelocityǁ 0.00039798 48.383 9.1476 8.2652 v Pressure -5.1964e+05 1.995e+05 -2.0541e+05 -1.7007e+05 v TurbVisc 1.1122e-18 0.03022 0.00022811 9.403e-05 v CourantNb 2.5753e-08 0.011701 0.00017254 4.9837e-06 v FourierNb 1.2468e-07 0.071837 0.00015689 7.7496e-07 v total_pressure -4.1832e+05 3.0082e+05 -1.0409e+05 -68742 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2227 0.12421 0.0032369 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.8768e-07 0.072923 0.00032943 5.7587e-06 INSTANT 0.876771000E-01 TIME STEP NUMBER 56969 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282999020E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.852103825E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.46373E-02 0.22606E+01 Friction velocity uk : 0.46373E-02 0.22606E+01 Dimensionless distance yplus : 0.45096E-02 0.22228E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.009949188e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29610E+08 1 0.20350E-09 0.47063E+02 0.25471E+04 c Velocity[X] 0.27040E+02 c Velocity[Y] 0.20022E+02 c Velocity[Z] 0.89365E-06 c Pressure 0.84736E-04 125 0.77894E-04 0.51497E-03 0.37355E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -34.49 48.08 5.6055 7.9966 v Velocity[Y] -35.316 38.142 -0.19819 -0.16091 v Velocity[Z] -3.1886 3.1811 2.118e-06 -5.3933e-08 v ǁVelocityǁ 0.0005667 48.392 9.149 8.2654 v Pressure -5.214e+05 1.9982e+05 -2.0583e+05 -1.7037e+05 v TurbVisc 1.0384e-18 0.030234 0.00022817 9.4139e-05 v CourantNb 2.468e-08 0.011702 0.00017255 4.9837e-06 v FourierNb 1.2468e-07 0.070877 0.0001569 7.757e-07 v total_pressure -4.2008e+05 3.0114e+05 -1.045e+05 -69047 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2228 0.12422 0.0032371 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.8822e-07 0.071963 0.00032945 5.7594e-06 INSTANT 0.876772000E-01 TIME STEP NUMBER 56970 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282992048E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.851719672E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.32608E-02 0.22608E+01 Friction velocity uk : 0.32608E-02 0.22608E+01 Dimensionless distance yplus : 0.31607E-02 0.22230E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.011467034e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29610E+08 1 0.20355E-09 0.47128E+02 0.25487E+04 c Velocity[X] 0.27071E+02 c Velocity[Y] 0.20057E+02 c Velocity[Z] 0.89003E-06 c Pressure 0.84243E-04 62 0.82971E-04 0.51162E-03 0.39341E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -34.501 48.089 5.6054 7.9965 v Velocity[Y] -35.324 38.153 -0.19833 -0.16132 v Velocity[Z] -3.1889 3.1812 2.1176e-06 -5.3933e-08 v ǁVelocityǁ 0.00059612 48.401 9.1504 8.2655 v Pressure -5.2128e+05 2.0016e+05 -2.0607e+05 -1.7065e+05 v TurbVisc 1.0897e-18 0.030248 0.00022823 9.4247e-05 v CourantNb 2.4929e-08 0.011703 0.00017256 4.9837e-06 v FourierNb 1.2468e-07 0.069878 0.00015691 7.7644e-07 v total_pressure -4.1995e+05 3.0149e+05 -1.0475e+05 -69324 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.223 0.12424 0.0032375 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.8876e-07 0.070964 0.00032947 5.7601e-06 INSTANT 0.876773000E-01 TIME STEP NUMBER 56971 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282985396E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.851342991E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.26336E-02 0.22610E+01 Friction velocity uk : 0.26336E-02 0.22610E+01 Dimensionless distance yplus : 0.25660E-02 0.22232E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.031878001e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29610E+08 1 0.20361E-09 0.47185E+02 0.25501E+04 c Velocity[X] 0.27104E+02 c Velocity[Y] 0.20080E+02 c Velocity[Z] 0.88380E-06 c Pressure 0.85423E-04 120 0.96878E-04 0.51841E-03 0.42980E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -34.512 48.098 5.6053 7.9963 v Velocity[Y] -35.333 38.163 -0.19846 -0.16172 v Velocity[Z] -3.1892 3.1814 2.1171e-06 -5.3934e-08 v ǁVelocityǁ 0.00060637 48.411 9.1518 8.2656 v Pressure -5.2319e+05 2.0049e+05 -2.0631e+05 -1.7081e+05 v TurbVisc 1.1595e-18 0.030262 0.0002283 9.4355e-05 v CourantNb 2.482e-08 0.011704 0.00017257 4.9837e-06 v FourierNb 1.2468e-07 0.068821 0.00015692 7.7717e-07 v total_pressure -4.2187e+05 3.0181e+05 -1.0499e+05 -69481 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2232 0.12426 0.0032379 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.893e-07 0.069906 0.00032948 5.7609e-06 INSTANT 0.876774000E-01 TIME STEP NUMBER 56972 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282978401E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.850961371E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.31052E-02 0.22612E+01 Friction velocity uk : 0.31052E-02 0.22612E+01 Dimensionless distance yplus : 0.30255E-02 0.22234E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.048191919e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29611E+08 1 0.20366E-09 0.47222E+02 0.25510E+04 c Velocity[X] 0.27134E+02 c Velocity[Y] 0.20089E+02 c Velocity[Z] 0.87890E-06 c Pressure 0.87059E-04 440 0.82210E-04 0.52796E-03 0.28838E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -34.524 48.106 5.6052 7.9962 v Velocity[Y] -35.341 38.174 -0.1986 -0.16213 v Velocity[Z] -3.1896 3.1815 2.1167e-06 -5.3934e-08 v ǁVelocityǁ 0.00061175 48.42 9.1532 8.2657 v Pressure -5.2339e+05 2.0083e+05 -2.0652e+05 -1.7109e+05 v TurbVisc 1.1896e-18 0.030276 0.00022836 9.4464e-05 v CourantNb 2.4519e-08 0.011705 0.00017257 4.9837e-06 v FourierNb 1.2468e-07 0.067704 0.00015693 7.7791e-07 v total_pressure -4.2207e+05 3.0216e+05 -1.0519e+05 -69768 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2234 0.12429 0.0032382 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.8984e-07 0.06879 0.0003295 5.7616e-06 INSTANT 0.876775000E-01 TIME STEP NUMBER 56973 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282971626E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.850579032E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.36184E-02 0.22614E+01 Friction velocity uk : 0.36184E-02 0.22614E+01 Dimensionless distance yplus : 0.35029E-02 0.22236E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.063135804e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29611E+08 1 0.20372E-09 0.47289E+02 0.25527E+04 c Velocity[X] 0.27162E+02 c Velocity[Y] 0.20127E+02 c Velocity[Z] 0.88198E-06 c Pressure 0.76121E-04 6 0.57156E-04 0.46130E-03 0.17839E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -34.535 48.115 5.6051 7.996 v Velocity[Y] -35.349 38.185 -0.19874 -0.16254 v Velocity[Z] -3.1899 3.1816 2.1162e-06 -5.3934e-08 v ǁVelocityǁ 0.00061833 48.429 9.1546 8.2659 v Pressure -5.2373e+05 2.0118e+05 -2.0659e+05 -1.7116e+05 v TurbVisc 1.1708e-18 0.03029 0.00022842 9.4572e-05 v CourantNb 2.4244e-08 0.011707 0.00017258 4.9837e-06 v FourierNb 1.2468e-07 0.066525 0.00015694 7.7865e-07 v total_pressure -4.224e+05 3.025e+05 -1.0527e+05 -69831 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2236 0.12431 0.0032385 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.9039e-07 0.06761 0.00032952 5.7624e-06 INSTANT 0.876776000E-01 TIME STEP NUMBER 56974 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282964971E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.850195514E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.39372E-02 0.22616E+01 Friction velocity uk : 0.39372E-02 0.22616E+01 Dimensionless distance yplus : 0.37875E-02 0.22238E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.084201245e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29611E+08 1 0.20377E-09 0.47342E+02 0.25540E+04 c Velocity[X] 0.27199E+02 c Velocity[Y] 0.20143E+02 c Velocity[Z] 0.87757E-06 c Pressure 0.80957E-04 46 0.78307E-04 0.49026E-03 0.35197E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -34.546 48.124 5.6049 7.9959 v Velocity[Y] -35.358 38.195 -0.19887 -0.16294 v Velocity[Z] -3.1902 3.1817 2.1158e-06 -5.3934e-08 v ǁVelocityǁ 0.00056124 48.438 9.156 8.266 v Pressure -5.2552e+05 2.015e+05 -2.0678e+05 -1.713e+05 v TurbVisc 1.0731e-18 0.030304 0.00022848 9.4681e-05 v CourantNb 2.3581e-08 0.011708 0.00017259 4.9837e-06 v FourierNb 1.2468e-07 0.065267 0.00015695 7.7939e-07 v total_pressure -4.2419e+05 3.0283e+05 -1.0546e+05 -69978 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2238 0.12433 0.0032389 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.9093e-07 0.066352 0.00032954 5.7631e-06 INSTANT 0.876777000E-01 TIME STEP NUMBER 56975 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282957998E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.849804635E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.92320E-02 0.22618E+01 Friction velocity uk : 0.92320E-02 0.22618E+01 Dimensionless distance yplus : 0.88811E-02 0.22240E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.088232933e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29611E+08 1 0.20383E-09 0.47406E+02 0.25556E+04 c Velocity[X] 0.27226E+02 c Velocity[Y] 0.20179E+02 c Velocity[Z] 0.87457E-06 c Pressure 0.81789E-04 455 0.83713E-04 0.49494E-03 0.38869E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -34.557 48.132 5.6048 7.9957 v Velocity[Y] -35.366 38.206 -0.19901 -0.16335 v Velocity[Z] -3.1905 3.1818 2.1153e-06 -5.3934e-08 v ǁVelocityǁ 0.00061007 48.447 9.1574 8.2661 v Pressure -5.2539e+05 2.0186e+05 -2.0682e+05 -1.7151e+05 v TurbVisc 1.2295e-18 0.030318 0.00022855 9.4789e-05 v CourantNb 2.3655e-08 0.011709 0.0001726 4.9837e-06 v FourierNb 1.2468e-07 0.063951 0.00015696 7.8013e-07 v total_pressure -4.2406e+05 3.0318e+05 -1.055e+05 -70184 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.224 0.12436 0.0032395 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.9148e-07 0.065036 0.00032955 5.7638e-06 INSTANT 0.876778000E-01 TIME STEP NUMBER 56976 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282951361E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.849423407E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.70591E-02 0.22620E+01 Friction velocity uk : 0.70591E-02 0.22620E+01 Dimensionless distance yplus : 0.67912E-02 0.22242E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.104799111e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29611E+08 1 0.20389E-09 0.47461E+02 0.25569E+04 c Velocity[X] 0.27266E+02 c Velocity[Y] 0.20196E+02 c Velocity[Z] 0.86682E-06 c Pressure 0.84487E-04 101 0.97740E-04 0.51090E-03 0.44634E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -34.568 48.141 5.6047 7.9956 v Velocity[Y] -35.374 38.216 -0.19914 -0.16376 v Velocity[Z] -3.1909 3.1819 2.1149e-06 -5.3934e-08 v ǁVelocityǁ 0.00082494 48.456 9.1588 8.2663 v Pressure -5.2717e+05 2.0219e+05 -2.0681e+05 -1.7143e+05 v TurbVisc 1.2248e-18 0.030332 0.00022861 9.4898e-05 v CourantNb 2.3641e-08 0.01171 0.0001726 4.9837e-06 v FourierNb 1.2468e-07 0.062546 0.00015697 7.8087e-07 v total_pressure -4.2585e+05 3.0351e+05 -1.0548e+05 -70107 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2242 0.12438 0.0032399 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.9202e-07 0.063631 0.00032957 5.7646e-06 INSTANT 0.876779000E-01 TIME STEP NUMBER 56977 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282944473E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.849038548E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.68975E-02 0.22622E+01 Friction velocity uk : 0.68975E-02 0.22622E+01 Dimensionless distance yplus : 0.66357E-02 0.22243E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.119629434e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29611E+08 1 0.20393E-09 0.47497E+02 0.25578E+04 c Velocity[X] 0.27287E+02 c Velocity[Y] 0.20211E+02 c Velocity[Z] 0.86361E-06 c Pressure 0.87555E-04 103 0.82766E-04 0.52908E-03 0.29583E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -34.579 48.15 5.6046 7.9954 v Velocity[Y] -35.382 38.227 -0.19928 -0.16417 v Velocity[Z] -3.1912 3.182 2.1144e-06 -5.3934e-08 v ǁVelocityǁ 0.001045 48.464 9.1602 8.2664 v Pressure -5.2746e+05 2.0254e+05 -2.068e+05 -1.7165e+05 v TurbVisc 1.2317e-18 0.030346 0.00022867 9.5007e-05 v CourantNb 2.3465e-08 0.011711 0.00017261 4.9837e-06 v FourierNb 1.2469e-07 0.061051 0.00015698 7.8161e-07 v total_pressure -4.2614e+05 3.0386e+05 -1.0548e+05 -70322 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2243 0.1244 0.0032405 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.9257e-07 0.062136 0.00032959 5.7653e-06 INSTANT 0.876780000E-01 TIME STEP NUMBER 56978 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282937744E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.848652832E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.44233E-02 0.22623E+01 Friction velocity uk : 0.44233E-02 0.22623E+01 Dimensionless distance yplus : 0.43197E-02 0.22245E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.131612288e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29612E+08 1 0.20399E-09 0.47563E+02 0.25594E+04 c Velocity[X] 0.27317E+02 c Velocity[Y] 0.20246E+02 c Velocity[Z] 0.86646E-06 c Pressure 0.77916E-04 6 0.57283E-04 0.47050E-03 0.17158E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -34.59 48.158 5.6045 7.9953 v Velocity[Y] -35.391 38.237 -0.19941 -0.16458 v Velocity[Z] -3.1915 3.1821 2.114e-06 -5.3934e-08 v ǁVelocityǁ 0.00097678 48.473 9.1616 8.2665 v Pressure -5.2773e+05 2.0288e+05 -2.0676e+05 -1.7168e+05 v TurbVisc 1.2459e-18 0.03036 0.00022873 9.5115e-05 v CourantNb 2.331e-08 0.011712 0.00017262 4.9837e-06 v FourierNb 1.2469e-07 0.059461 0.00015698 7.8236e-07 v total_pressure -4.264e+05 3.0421e+05 -1.0543e+05 -70354 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2245 0.12442 0.0032411 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.9312e-07 0.060545 0.0003296 5.7661e-06 INSTANT 0.876781000E-01 TIME STEP NUMBER 56979 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282931172E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.848267330E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10391E-01 0.22625E+01 Friction velocity uk : 0.10391E-01 0.22625E+01 Dimensionless distance yplus : 0.10148E-01 0.22247E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.134627040e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29612E+08 1 0.20405E-09 0.47614E+02 0.25607E+04 c Velocity[X] 0.27350E+02 c Velocity[Y] 0.20264E+02 c Velocity[Z] 0.86221E-06 c Pressure 0.84112E-04 46 0.79030E-04 0.50755E-03 0.35696E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -34.601 48.167 5.6044 7.9951 v Velocity[Y] -35.399 38.248 -0.19955 -0.16499 v Velocity[Z] -3.1918 3.1822 2.1136e-06 -5.3934e-08 v ǁVelocityǁ 0.00092016 48.482 9.163 8.2667 v Pressure -5.2954e+05 2.0322e+05 -2.0657e+05 -1.716e+05 v TurbVisc 1.3586e-18 0.030374 0.00022879 9.5224e-05 v CourantNb 2.3362e-08 0.011714 0.00017263 4.9837e-06 v FourierNb 1.2469e-07 0.057777 0.00015699 7.831e-07 v total_pressure -4.2822e+05 3.0455e+05 -1.0525e+05 -70275 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2247 0.12446 0.003242 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.9367e-07 0.058862 0.00032962 5.7668e-06 INSTANT 0.876782000E-01 TIME STEP NUMBER 56980 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282924329E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.847885856E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.14456E-01 0.22627E+01 Friction velocity uk : 0.14456E-01 0.22627E+01 Dimensionless distance yplus : 0.13979E-01 0.22249E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.159977844e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29612E+08 1 0.20410E-09 0.47677E+02 0.25622E+04 c Velocity[X] 0.27380E+02 c Velocity[Y] 0.20297E+02 c Velocity[Z] 0.86487E-06 c Pressure 0.86286E-04 69 0.84070E-04 0.52029E-03 0.36907E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -34.612 48.175 5.6042 7.995 v Velocity[Y] -35.407 38.258 -0.19968 -0.1654 v Velocity[Z] -3.1922 3.1824 2.1131e-06 -5.3934e-08 v ǁVelocityǁ 0.00087338 48.491 9.1644 8.2668 v Pressure -5.2931e+05 2.0358e+05 -2.0642e+05 -1.7161e+05 v TurbVisc 1.2251e-18 0.030388 0.00022885 9.5333e-05 v CourantNb 2.3199e-08 0.011715 0.00017264 4.9837e-06 v FourierNb 1.2469e-07 0.055965 0.000157 7.8384e-07 v total_pressure -4.2798e+05 3.0491e+05 -1.051e+05 -70290 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2249 0.12448 0.003243 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.9422e-07 0.05705 0.00032964 5.7676e-06 INSTANT 0.876783000E-01 TIME STEP NUMBER 56981 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282917856E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.847498059E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.71327E-02 0.22629E+01 Friction velocity uk : 0.71327E-02 0.22629E+01 Dimensionless distance yplus : 0.68971E-02 0.22251E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.163833054e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29612E+08 1 0.20417E-09 0.47731E+02 0.25636E+04 c Velocity[X] 0.27412E+02 c Velocity[Y] 0.20320E+02 c Velocity[Z] 0.85402E-06 c Pressure 0.90130E-04 192 0.98249E-04 0.54308E-03 0.44015E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -34.623 48.184 5.6041 7.9948 v Velocity[Y] -35.415 38.269 -0.19982 -0.16581 v Velocity[Z] -3.1925 3.1825 2.1127e-06 -5.3934e-08 v ǁVelocityǁ 0.00083998 48.5 9.1657 8.2669 v Pressure -5.312e+05 2.0392e+05 -2.0623e+05 -1.7153e+05 v TurbVisc 1.2851e-18 0.030402 0.00022892 9.5442e-05 v CourantNb 2.3005e-08 0.011716 0.00017264 4.9837e-06 v FourierNb 1.2469e-07 0.054047 0.00015701 7.8458e-07 v total_pressure -4.2988e+05 3.0525e+05 -1.049e+05 -70202 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2251 0.12451 0.0032437 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.9477e-07 0.05513 0.00032965 5.7683e-06 INSTANT 0.876784000E-01 TIME STEP NUMBER 56982 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282911094E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.847112903E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15851E-02 0.22631E+01 Friction velocity uk : 0.15851E-02 0.22631E+01 Dimensionless distance yplus : 0.15327E-02 0.22252E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.170353507e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29612E+08 1 0.20422E-09 0.47765E+02 0.25643E+04 c Velocity[X] 0.27434E+02 c Velocity[Y] 0.20331E+02 c Velocity[Z] 0.85265E-06 c Pressure 0.94190E-04 122 0.83397E-04 0.56714E-03 0.27291E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -34.634 48.192 5.604 7.9947 v Velocity[Y] -35.423 38.279 -0.19995 -0.16622 v Velocity[Z] -3.1928 3.1826 2.1122e-06 -5.3934e-08 v ǁVelocityǁ 0.000823 48.509 9.1671 8.2671 v Pressure -5.3142e+05 2.0427e+05 -2.06e+05 -1.7159e+05 v TurbVisc 1.2733e-18 0.030416 0.00022898 9.5551e-05 v CourantNb 2.2897e-08 0.011717 0.00017265 4.9837e-06 v FourierNb 1.2469e-07 0.052009 0.00015702 7.8533e-07 v total_pressure -4.3009e+05 3.056e+05 -1.0468e+05 -70267 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2252 0.12453 0.0032444 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.9533e-07 0.053092 0.00032967 5.7691e-06 INSTANT 0.876785000E-01 TIME STEP NUMBER 56983 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282904537E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.846730327E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11669E-01 0.22632E+01 Friction velocity uk : 0.11669E-01 0.22632E+01 Dimensionless distance yplus : 0.11424E-01 0.22254E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.176343633e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29613E+08 1 0.20428E-09 0.47831E+02 0.25660E+04 c Velocity[X] 0.27463E+02 c Velocity[Y] 0.20368E+02 c Velocity[Z] 0.85986E-06 c Pressure 0.86376E-04 6 0.57661E-04 0.51972E-03 0.17764E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -34.645 48.201 5.6039 7.9945 v Velocity[Y] -35.431 38.289 -0.20009 -0.16664 v Velocity[Z] -3.1931 3.1827 2.1118e-06 -5.3934e-08 v ǁVelocityǁ 0.0008227 48.517 9.1685 8.2672 v Pressure -5.317e+05 2.0462e+05 -2.0579e+05 -1.716e+05 v TurbVisc 1.3054e-18 0.03043 0.00022904 9.566e-05 v CourantNb 2.2867e-08 0.011718 0.00017266 4.9837e-06 v FourierNb 1.2469e-07 0.049849 0.00015703 7.8607e-07 v total_pressure -4.3038e+05 3.0595e+05 -1.0446e+05 -70272 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2254 0.12456 0.0032452 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.9586e-07 0.050932 0.00032969 5.7698e-06 INSTANT 0.876786000E-01 TIME STEP NUMBER 56984 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282898125E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.846349867E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.55660E-02 0.22634E+01 Friction velocity uk : 0.55660E-02 0.22634E+01 Dimensionless distance yplus : 0.54492E-02 0.22256E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.169928569e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29613E+08 1 0.20434E-09 0.47880E+02 0.25671E+04 c Velocity[X] 0.27496E+02 c Velocity[Y] 0.20384E+02 c Velocity[Z] 0.85592E-06 c Pressure 0.93094E-04 44 0.79631E-04 0.55974E-03 0.42817E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -34.655 48.209 5.6038 7.9944 v Velocity[Y] -35.439 38.3 -0.20022 -0.16705 v Velocity[Z] -3.1934 3.1828 2.1113e-06 -5.3934e-08 v ǁVelocityǁ 0.00082171 48.526 9.1699 8.2673 v Pressure -5.3343e+05 2.0498e+05 -2.0528e+05 -1.712e+05 v TurbVisc 1.4493e-18 0.030444 0.0002291 9.5769e-05 v CourantNb 2.3596e-08 0.011719 0.00017267 4.9837e-06 v FourierNb 1.2469e-07 0.049607 0.00015703 7.8681e-07 v total_pressure -4.321e+05 3.0631e+05 -1.0395e+05 -69871 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2256 0.12457 0.0032458 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.9599e-07 0.050278 0.0003297 5.7706e-06 INSTANT 0.876787000E-01 TIME STEP NUMBER 56985 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282891533E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.845978170E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10434E-01 0.22636E+01 Friction velocity uk : 0.10434E-01 0.22636E+01 Dimensionless distance yplus : 0.10218E-01 0.22258E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.195761674e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29613E+08 1 0.20439E-09 0.47942E+02 0.25687E+04 c Velocity[X] 0.27523E+02 c Velocity[Y] 0.20419E+02 c Velocity[Z] 0.86430E-06 c Pressure 0.96328E-04 52 0.84916E-04 0.57877E-03 0.38090E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -34.666 48.218 5.6037 7.9942 v Velocity[Y] -35.447 38.31 -0.20036 -0.16747 v Velocity[Z] -3.1938 3.1829 2.1109e-06 -5.3935e-08 v ǁVelocityǁ 0.00071595 48.535 9.1713 8.2675 v Pressure -5.3322e+05 2.0534e+05 -2.0498e+05 -1.7119e+05 v TurbVisc 1.363e-18 0.030458 0.00022916 9.5878e-05 v CourantNb 2.2932e-08 0.011721 0.00017267 4.9838e-06 v FourierNb 1.2469e-07 0.049678 0.00015704 7.8756e-07 v total_pressure -4.319e+05 3.0667e+05 -1.0366e+05 -69864 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2258 0.1246 0.0032465 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.9611e-07 0.050349 0.00032972 5.7713e-06 INSTANT 0.876788000E-01 TIME STEP NUMBER 56986 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282885284E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.845593129E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.48598E-02 0.22638E+01 Friction velocity uk : 0.48598E-02 0.22638E+01 Dimensionless distance yplus : 0.46950E-02 0.22260E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.186906876e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29613E+08 1 0.20446E-09 0.47996E+02 0.25700E+04 c Velocity[X] 0.27555E+02 c Velocity[Y] 0.20441E+02 c Velocity[Z] 0.84893E-06 c Pressure 0.10083E-03 127 0.99312E-04 0.60538E-03 0.46375E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -34.677 48.226 5.6035 7.9941 v Velocity[Y] -35.455 38.32 -0.20049 -0.16788 v Velocity[Z] -3.1941 3.183 2.1104e-06 -5.3935e-08 v ǁVelocityǁ 0.00061006 48.544 9.1726 8.2676 v Pressure -5.3509e+05 2.0568e+05 -2.0456e+05 -1.7097e+05 v TurbVisc 1.34e-18 0.030471 0.00022922 9.5988e-05 v CourantNb 2.2708e-08 0.011722 0.00017268 4.9838e-06 v FourierNb 1.2469e-07 0.049749 0.00015705 7.883e-07 v total_pressure -4.3377e+05 3.0701e+05 -1.0324e+05 -69648 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.226 0.12463 0.0032471 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.9623e-07 0.05042 0.00032973 5.7721e-06 INSTANT 0.876789000E-01 TIME STEP NUMBER 56987 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282878769E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.845216138E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.37105E-02 0.22640E+01 Friction velocity uk : 0.37105E-02 0.22640E+01 Dimensionless distance yplus : 0.35952E-02 0.22261E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.187035981e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29614E+08 1 0.20451E-09 0.48028E+02 0.25707E+04 c Velocity[X] 0.27578E+02 c Velocity[Y] 0.20451E+02 c Velocity[Z] 0.84449E-06 c Pressure 0.10547E-03 889 0.84386E-04 0.63277E-03 0.27993E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -34.688 48.234 5.6034 7.994 v Velocity[Y] -35.463 38.331 -0.20063 -0.1683 v Velocity[Z] -3.1944 3.1831 2.11e-06 -5.3935e-08 v ǁVelocityǁ 0.00064037 48.552 9.174 8.2678 v Pressure -5.3525e+05 2.0604e+05 -2.0411e+05 -1.7086e+05 v TurbVisc 1.3618e-18 0.030485 0.00022928 9.6097e-05 v CourantNb 2.2702e-08 0.011723 0.00017269 4.9838e-06 v FourierNb 1.2469e-07 0.049819 0.00015706 7.8905e-07 v total_pressure -4.3393e+05 3.0737e+05 -1.0278e+05 -69535 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2261 0.12466 0.0032479 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.9636e-07 0.05049 0.00032975 5.7728e-06 INSTANT 0.876790000E-01 TIME STEP NUMBER 56988 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282872498E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.844842792E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.40808E-02 0.22642E+01 Friction velocity uk : 0.40808E-02 0.22642E+01 Dimensionless distance yplus : 0.39540E-02 0.22263E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.185298082e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29614E+08 1 0.20457E-09 0.48094E+02 0.25723E+04 c Velocity[X] 0.27600E+02 c Velocity[Y] 0.20494E+02 c Velocity[Z] 0.84916E-06 c Pressure 0.99267E-04 7 0.58403E-04 0.59514E-03 0.19905E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -34.698 48.243 5.6033 7.9938 v Velocity[Y] -35.471 38.341 -0.20076 -0.16872 v Velocity[Z] -3.1947 3.1832 2.1095e-06 -5.3935e-08 v ǁVelocityǁ 0.00054573 48.561 9.1754 8.2679 v Pressure -5.356e+05 2.064e+05 -2.0372e+05 -1.7086e+05 v TurbVisc 1.3875e-18 0.030499 0.00022934 9.6206e-05 v CourantNb 2.2686e-08 0.011724 0.0001727 4.9838e-06 v FourierNb 1.2469e-07 0.049888 0.00015707 7.8979e-07 v total_pressure -4.3428e+05 3.0773e+05 -1.0239e+05 -69536 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2263 0.12471 0.003249 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.9648e-07 0.050559 0.00032976 5.7736e-06 INSTANT 0.876791000E-01 TIME STEP NUMBER 56989 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282866357E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.844471484E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13152E-01 0.22644E+01 Friction velocity uk : 0.13152E-01 0.22644E+01 Dimensionless distance yplus : 0.12706E-01 0.22265E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.170872587e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29614E+08 1 0.20463E-09 0.48142E+02 0.25735E+04 c Velocity[X] 0.27637E+02 c Velocity[Y] 0.20505E+02 c Velocity[Z] 0.84035E-06 c Pressure 0.10607E-03 57 0.80810E-04 0.63548E-03 0.48120E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -34.709 48.251 5.6032 7.9937 v Velocity[Y] -35.479 38.351 -0.2009 -0.16913 v Velocity[Z] -3.1951 3.1834 2.1091e-06 -5.3935e-08 v ǁVelocityǁ 0.0007003 48.57 9.1768 8.268 v Pressure -5.3725e+05 2.0676e+05 -2.03e+05 -1.7031e+05 v TurbVisc 1.5923e-18 0.030513 0.0002294 9.6316e-05 v CourantNb 2.373e-08 0.011725 0.00017271 4.9838e-06 v FourierNb 1.2469e-07 0.049956 0.00015708 7.9054e-07 v total_pressure -4.3593e+05 3.0809e+05 -1.0168e+05 -68989 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2265 0.12475 0.0032499 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.9661e-07 0.050627 0.00032978 5.7743e-06 INSTANT 0.876792000E-01 TIME STEP NUMBER 56990 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282860064E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.844111336E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.17778E-01 0.22645E+01 Friction velocity uk : 0.17778E-01 0.22645E+01 Dimensionless distance yplus : 0.17237E-01 0.22267E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.187511146e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29614E+08 1 0.20469E-09 0.48204E+02 0.25750E+04 c Velocity[X] 0.27661E+02 c Velocity[Y] 0.20543E+02 c Velocity[Z] 0.83920E-06 c Pressure 0.10978E-03 128 0.85964E-04 0.65720E-03 0.39626E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -34.72 48.26 5.6031 7.9935 v Velocity[Y] -35.487 38.362 -0.20103 -0.16955 v Velocity[Z] -3.1954 3.1835 2.1086e-06 -5.3935e-08 v ǁVelocityǁ 0.00094952 48.578 9.1781 8.2682 v Pressure -5.3705e+05 2.0713e+05 -2.0248e+05 -1.7018e+05 v TurbVisc 1.3955e-18 0.030527 0.00022946 9.6425e-05 v CourantNb 2.2837e-08 0.011726 0.00017271 4.9838e-06 v FourierNb 1.247e-07 0.050024 0.00015709 7.9129e-07 v total_pressure -4.3572e+05 3.0846e+05 -1.0116e+05 -68851 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2267 0.1248 0.0032509 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.9673e-07 0.050694 0.0003298 5.7751e-06 INSTANT 0.876793000E-01 TIME STEP NUMBER 56991 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282854139E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.843740509E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19425E-01 0.22647E+01 Friction velocity uk : 0.19425E-01 0.22647E+01 Dimensionless distance yplus : 0.18833E-01 0.22269E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.171082409e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29615E+08 1 0.20476E-09 0.48237E+02 0.25757E+04 c Velocity[X] 0.27689E+02 c Velocity[Y] 0.20548E+02 c Velocity[Z] 0.83144E-06 c Pressure 0.11452E-03 48 0.75479E-04 0.68510E-03 0.30735E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -34.73 48.268 5.6029 7.9934 v Velocity[Y] -35.495 38.372 -0.20117 -0.16997 v Velocity[Z] -3.1957 3.1836 2.1082e-06 -5.3935e-08 v ǁVelocityǁ 0.0011572 48.587 9.1795 8.2683 v Pressure -5.3837e+05 2.0749e+05 -2.0186e+05 -1.6984e+05 v TurbVisc 1.4367e-18 0.030541 0.00022952 9.6535e-05 v CourantNb 2.2456e-08 0.011727 0.00017272 4.9838e-06 v FourierNb 1.247e-07 0.05009 0.00015709 7.9203e-07 v total_pressure -4.3704e+05 3.0881e+05 -1.0053e+05 -68514 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2269 0.12484 0.0032517 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.9686e-07 0.050761 0.00032982 5.7758e-06 INSTANT 0.876794000E-01 TIME STEP NUMBER 56992 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282848084E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.843377439E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19690E-01 0.22649E+01 Friction velocity uk : 0.19690E-01 0.22649E+01 Dimensionless distance yplus : 0.19031E-01 0.22271E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.162601989e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29615E+08 1 0.20481E-09 0.48299E+02 0.25773E+04 c Velocity[X] 0.27717E+02 c Velocity[Y] 0.20582E+02 c Velocity[Z] 0.84063E-06 c Pressure 0.11107E-03 7 0.56017E-04 0.66399E-03 0.19842E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -34.741 48.276 5.6028 7.9933 v Velocity[Y] -35.503 38.382 -0.2013 -0.17039 v Velocity[Z] -3.196 3.1837 2.1077e-06 -5.3935e-08 v ǁVelocityǁ 0.0012267 48.596 9.1809 8.2685 v Pressure -5.3949e+05 2.0784e+05 -2.0127e+05 -1.6969e+05 v TurbVisc 1.4433e-18 0.030555 0.00022958 9.6645e-05 v CourantNb 2.2496e-08 0.011729 0.00017273 4.9838e-06 v FourierNb 1.247e-07 0.050156 0.0001571 7.9278e-07 v total_pressure -4.3816e+05 3.0916e+05 -99940 -68370 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2271 0.12488 0.0032525 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.9735e-07 0.050827 0.00032983 5.7766e-06 INSTANT 0.876795000E-01 TIME STEP NUMBER 56993 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282842063E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.843018358E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15646E-01 0.22652E+01 Friction velocity uk : 0.15646E-01 0.22652E+01 Dimensionless distance yplus : 0.15122E-01 0.22273E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.147405253e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29615E+08 1 0.20486E-09 0.48341E+02 0.25783E+04 c Velocity[X] 0.27744E+02 c Velocity[Y] 0.20597E+02 c Velocity[Z] 0.83455E-06 c Pressure 0.11717E-03 239 0.98031E-04 0.69992E-03 0.29835E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -34.751 48.285 5.6027 7.9931 v Velocity[Y] -35.511 38.392 -0.20144 -0.17081 v Velocity[Z] -3.1963 3.1838 2.1073e-06 -5.3935e-08 v ǁVelocityǁ 0.0013427 48.604 9.1822 8.2686 v Pressure -5.3993e+05 2.0821e+05 -2.0047e+05 -1.6922e+05 v TurbVisc 1.4164e-18 0.030569 0.00022964 9.6754e-05 v CourantNb 2.3155e-08 0.01173 0.00017274 4.9838e-06 v FourierNb 1.247e-07 0.050221 0.00015711 7.9353e-07 v total_pressure -4.3861e+05 3.0954e+05 -99149 -67891 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2273 0.12492 0.0032532 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.9802e-07 0.050892 0.00032985 5.7773e-06 INSTANT 0.876796000E-01 TIME STEP NUMBER 56994 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282836221E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.842668680E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10356E-01 0.22653E+01 Friction velocity uk : 0.10356E-01 0.22653E+01 Dimensionless distance yplus : 0.10009E-01 0.22275E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.143943200e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29616E+08 1 0.20493E-09 0.48391E+02 0.25794E+04 c Velocity[X] 0.27766E+02 c Velocity[Y] 0.20624E+02 c Velocity[Z] 0.82633E-06 c Pressure 0.11916E-03 37 0.81485E-04 0.71129E-03 0.17462E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -34.762 48.293 5.6026 7.993 v Velocity[Y] -35.519 38.402 -0.20157 -0.17123 v Velocity[Z] -3.1967 3.1839 2.1069e-06 -5.3935e-08 v ǁVelocityǁ 0.0014414 48.613 9.1836 8.2688 v Pressure -5.4053e+05 2.0858e+05 -1.998e+05 -1.6902e+05 v TurbVisc 1.4553e-18 0.030582 0.0002297 9.6864e-05 v CourantNb 2.2447e-08 0.011731 0.00017275 4.9838e-06 v FourierNb 1.247e-07 0.050285 0.00015712 7.9428e-07 v total_pressure -4.3921e+05 3.099e+05 -98471 -67697 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2275 0.12495 0.003254 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.987e-07 0.050956 0.00032987 5.7781e-06 INSTANT 0.876797000E-01 TIME STEP NUMBER 56995 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282830450E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.842315359E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.75502E-02 0.22656E+01 Friction velocity uk : 0.75502E-02 0.22656E+01 Dimensionless distance yplus : 0.72975E-02 0.22277E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.124122886e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29616E+08 1 0.20499E-09 0.48453E+02 0.25810E+04 c Velocity[X] 0.27786E+02 c Velocity[Y] 0.20667E+02 c Velocity[Z] 0.83579E-06 c Pressure 0.12023E-03 9 0.52529E-04 0.71719E-03 0.24745E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -34.773 48.301 5.6025 7.9929 v Velocity[Y] -35.527 38.413 -0.20171 -0.17165 v Velocity[Z] -3.197 3.184 2.1064e-06 -5.3935e-08 v ǁVelocityǁ 0.0015296 48.622 9.185 8.2689 v Pressure -5.4094e+05 2.0894e+05 -1.9902e+05 -1.6874e+05 v TurbVisc 1.3647e-18 0.030596 0.00022976 9.6974e-05 v CourantNb 2.2154e-08 0.011732 0.00017275 4.9838e-06 v FourierNb 1.247e-07 0.050348 0.00015713 7.9503e-07 v total_pressure -4.3962e+05 3.1027e+05 -97693 -67411 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2277 0.12499 0.0032547 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 7.9937e-07 0.051019 0.00032989 5.7789e-06 INSTANT 0.876798000E-01 TIME STEP NUMBER 56996 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282824845E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.841969870E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12861E-01 0.22658E+01 Friction velocity uk : 0.12861E-01 0.22658E+01 Dimensionless distance yplus : 0.12627E-01 0.22279E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.109716303e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29616E+08 1 0.20505E-09 0.48495E+02 0.25819E+04 c Velocity[X] 0.27821E+02 c Velocity[Y] 0.20674E+02 c Velocity[Z] 0.82630E-06 c Pressure 0.12635E-03 86 0.98961E-04 0.75316E-03 0.36896E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -34.783 48.31 5.6024 7.9927 v Velocity[Y] -35.535 38.423 -0.20184 -0.17207 v Velocity[Z] -3.1973 3.1841 2.106e-06 -5.3935e-08 v ǁVelocityǁ 0.0016476 48.63 9.1863 8.2691 v Pressure -5.4191e+05 2.0932e+05 -1.9817e+05 -1.6811e+05 v TurbVisc 1.2476e-18 0.03061 0.00022982 9.7084e-05 v CourantNb 2.2112e-08 0.011733 0.00017276 4.9839e-06 v FourierNb 1.247e-07 0.05041 0.00015714 7.9577e-07 v total_pressure -4.4059e+05 3.1065e+05 -96848 -66789 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2279 0.12502 0.0032554 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 8.0005e-07 0.051081 0.00032991 5.7796e-06 INSTANT 0.876799000E-01 TIME STEP NUMBER 56997 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282819272E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.841626828E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.49547E-02 0.22660E+01 Friction velocity uk : 0.49547E-02 0.22660E+01 Dimensionless distance yplus : 0.48645E-02 0.22281E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.098120446e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29617E+08 1 0.20512E-09 0.48546E+02 0.25832E+04 c Velocity[X] 0.27850E+02 c Velocity[Y] 0.20696E+02 c Velocity[Z] 0.82597E-06 c Pressure 0.12852E-03 84 0.84760E-04 0.76552E-03 0.24697E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -34.794 48.318 5.6023 7.9926 v Velocity[Y] -35.543 38.433 -0.20198 -0.17249 v Velocity[Z] -3.1976 3.1842 2.1055e-06 -5.3935e-08 v ǁVelocityǁ 0.001755 48.639 9.1877 8.2693 v Pressure -5.4285e+05 2.0969e+05 -1.9732e+05 -1.6773e+05 v TurbVisc 1.7572e-18 0.030624 0.00022988 9.7194e-05 v CourantNb 2.1896e-08 0.011734 0.00017277 4.9839e-06 v FourierNb 1.247e-07 0.050471 0.00015715 7.9652e-07 v total_pressure -4.4152e+05 3.1101e+05 -95998 -66407 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2281 0.12505 0.003256 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 8.0073e-07 0.051142 0.00032992 5.7804e-06 INSTANT 0.876800000E-01 TIME STEP NUMBER 56998 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282813759E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.841289559E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10034E-01 0.22662E+01 Friction velocity uk : 0.10034E-01 0.22662E+01 Dimensionless distance yplus : 0.98512E-02 0.22284E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.081321741e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29617E+08 1 0.20518E-09 0.48610E+02 0.25847E+04 c Velocity[X] 0.27876E+02 c Velocity[Y] 0.20734E+02 c Velocity[Z] 0.84195E-06 c Pressure 0.12973E-03 15 0.57659E-04 0.77213E-03 0.26416E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -34.804 48.326 5.6022 7.9925 v Velocity[Y] -35.551 38.443 -0.20212 -0.17291 v Velocity[Z] -3.198 3.1843 2.1051e-06 -5.3936e-08 v ǁVelocityǁ 0.0018472 48.648 9.1891 8.2694 v Pressure -5.4398e+05 2.1005e+05 -1.9645e+05 -1.6739e+05 v TurbVisc 1.3835e-18 0.030638 0.00022994 9.7304e-05 v CourantNb 2.1582e-08 0.011736 0.00017278 4.9839e-06 v FourierNb 1.247e-07 0.050532 0.00015717 7.9727e-07 v total_pressure -4.4265e+05 3.1137e+05 -95123 -66065 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2284 0.12509 0.0032566 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 8.0141e-07 0.051202 0.00032994 5.7812e-06 INSTANT 0.876801000E-01 TIME STEP NUMBER 56999 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282808297E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.840955159E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.76274E-02 0.22665E+01 Friction velocity uk : 0.76274E-02 0.22665E+01 Dimensionless distance yplus : 0.73624E-02 0.22286E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.046419634e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29617E+08 1 0.20523E-09 0.48662E+02 0.25860E+04 c Velocity[X] 0.27899E+02 c Velocity[Y] 0.20763E+02 c Velocity[Z] 0.84206E-06 c Pressure 0.13598E-03 252 0.78565E-04 0.80875E-03 0.43327E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -34.815 48.335 5.6021 7.9924 v Velocity[Y] -35.559 38.454 -0.20225 -0.17334 v Velocity[Z] -3.1983 3.1844 2.1046e-06 -5.3936e-08 v ǁVelocityǁ 0.0019698 48.656 9.1905 8.2696 v Pressure -5.4393e+05 2.1043e+05 -1.9552e+05 -1.669e+05 v TurbVisc 1.1329e-18 0.030652 0.00023 9.7414e-05 v CourantNb 2.1365e-08 0.011737 0.00017279 4.9839e-06 v FourierNb 1.247e-07 0.05059 0.00015718 7.9803e-07 v total_pressure -4.4261e+05 3.1175e+05 -94194 -65576 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2286 0.12512 0.0032573 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 8.021e-07 0.051261 0.00032996 5.7819e-06 INSTANT 0.876802000E-01 TIME STEP NUMBER 57000 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282803076E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.840626961E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12350E-02 0.22667E+01 Friction velocity uk : 0.12350E-02 0.22667E+01 Dimensionless distance yplus : 0.11921E-02 0.22288E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.039548175e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29618E+08 1 0.20531E-09 0.48716E+02 0.25873E+04 c Velocity[X] 0.27926E+02 c Velocity[Y] 0.20790E+02 c Velocity[Z] 0.82838E-06 c Pressure 0.13942E-03 57 0.83951E-04 0.82859E-03 0.43811E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -34.825 48.343 5.602 7.9923 v Velocity[Y] -35.567 38.464 -0.20239 -0.17376 v Velocity[Z] -3.1986 3.1846 2.1042e-06 -5.3936e-08 v ǁVelocityǁ 0.0020041 48.665 9.1918 8.2698 v Pressure -5.4563e+05 2.1079e+05 -1.9458e+05 -1.6648e+05 v TurbVisc 1.3585e-18 0.030666 0.00023006 9.7524e-05 v CourantNb 2.1048e-08 0.011738 0.00017279 4.9839e-06 v FourierNb 1.247e-07 0.050649 0.00015719 7.9878e-07 v total_pressure -4.4431e+05 3.1211e+05 -93256 -65150 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2288 0.12516 0.0032579 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 8.0278e-07 0.05132 0.00032998 5.7827e-06 INSTANT 0.876803000E-01 TIME STEP NUMBER 57001 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282797693E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.840301759E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.87709E-02 0.22670E+01 Friction velocity uk : 0.87709E-02 0.22670E+01 Dimensionless distance yplus : 0.84662E-02 0.22291E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.015116849e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29618E+08 1 0.20536E-09 0.48776E+02 0.25887E+04 c Velocity[X] 0.27953E+02 c Velocity[Y] 0.20823E+02 c Velocity[Z] 0.81796E-06 c Pressure 0.14374E-03 228 0.97588E-04 0.85365E-03 0.49742E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -34.836 48.351 5.6019 7.9921 v Velocity[Y] -35.575 38.474 -0.20253 -0.17419 v Velocity[Z] -3.1989 3.1847 2.1037e-06 -5.3936e-08 v ǁVelocityǁ 0.0018467 48.673 9.1932 8.2699 v Pressure -5.4515e+05 2.1119e+05 -1.9357e+05 -1.6597e+05 v TurbVisc 1.4085e-18 0.030679 0.00023012 9.7634e-05 v CourantNb 2.0738e-08 0.011739 0.0001728 4.9839e-06 v FourierNb 1.247e-07 0.050706 0.0001572 7.9953e-07 v total_pressure -4.4382e+05 3.1251e+05 -92244 -64646 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2291 0.1252 0.0032587 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 8.0347e-07 0.051377 0.00033 5.7835e-06 INSTANT 0.876804000E-01 TIME STEP NUMBER 57002 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282792815E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.839983405E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12751E-01 0.22673E+01 Friction velocity uk : 0.12751E-01 0.22673E+01 Dimensionless distance yplus : 0.12308E-01 0.22294E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -9.900279940e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29619E+08 1 0.20544E-09 0.48804E+02 0.25893E+04 c Velocity[X] 0.27980E+02 c Velocity[Y] 0.20825E+02 c Velocity[Z] 0.81351E-06 c Pressure 0.14816E-03 132 0.82923E-04 0.87930E-03 0.38756E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -34.846 48.36 5.6018 7.992 v Velocity[Y] -35.583 38.484 -0.20266 -0.17461 v Velocity[Z] -3.1992 3.1848 2.1033e-06 -5.3936e-08 v ǁVelocityǁ 0.0017492 48.682 9.1946 8.2701 v Pressure -5.4654e+05 2.1155e+05 -1.9255e+05 -1.6545e+05 v TurbVisc 1.4494e-18 0.030693 0.00023018 9.7745e-05 v CourantNb 2.0305e-08 0.01174 0.00017281 4.984e-06 v FourierNb 1.247e-07 0.050762 0.00015721 8.0028e-07 v total_pressure -4.4521e+05 3.1288e+05 -91230 -64125 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2294 0.12524 0.0032594 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 8.0416e-07 0.051433 0.00033002 5.7842e-06 INSTANT 0.876805000E-01 TIME STEP NUMBER 57003 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282787790E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.839669651E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15434E-01 0.22675E+01 Friction velocity uk : 0.15434E-01 0.22675E+01 Dimensionless distance yplus : 0.14898E-01 0.22296E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -9.676511656e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29619E+08 1 0.20549E-09 0.48869E+02 0.25909E+04 c Velocity[X] 0.28009E+02 c Velocity[Y] 0.20860E+02 c Velocity[Z] 0.83633E-06 c Pressure 0.14485E-03 16 0.59178E-04 0.85901E-03 0.28625E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -34.857 48.368 5.6017 7.9919 v Velocity[Y] -35.591 38.494 -0.2028 -0.17504 v Velocity[Z] -3.1996 3.1849 2.1028e-06 -5.3936e-08 v ǁVelocityǁ 0.0017204 48.691 9.1959 8.2703 v Pressure -5.476e+05 2.1193e+05 -1.9153e+05 -1.6506e+05 v TurbVisc 1.4551e-18 0.030707 0.00023024 9.7855e-05 v CourantNb 1.9827e-08 0.011741 0.00017282 4.984e-06 v FourierNb 1.2471e-07 0.050817 0.00015722 8.0103e-07 v total_pressure -4.4627e+05 3.1325e+05 -90207 -63731 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2296 0.12528 0.0032601 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 8.0485e-07 0.051488 0.00033004 5.785e-06 INSTANT 0.876806000E-01 TIME STEP NUMBER 57004 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282782879E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.839362713E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.16019E-01 0.22679E+01 Friction velocity uk : 0.16019E-01 0.22679E+01 Dimensionless distance yplus : 0.15462E-01 0.22299E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -9.330852060e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29619E+08 1 0.20555E-09 0.48921E+02 0.25921E+04 c Velocity[X] 0.28029E+02 c Velocity[Y] 0.20891E+02 c Velocity[Z] 0.82153E-06 c Pressure 0.15058E-03 251 0.79457E-04 0.89235E-03 0.50334E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -34.867 48.376 5.6016 7.9918 v Velocity[Y] -35.599 38.504 -0.20294 -0.17547 v Velocity[Z] -3.1999 3.185 2.1024e-06 -5.3936e-08 v ǁVelocityǁ 0.0015324 48.699 9.1973 8.2704 v Pressure -5.4753e+05 2.1231e+05 -1.9041e+05 -1.644e+05 v TurbVisc 1.2239e-18 0.030721 0.0002303 9.7966e-05 v CourantNb 1.929e-08 0.011743 0.00017283 4.984e-06 v FourierNb 1.2471e-07 0.05087 0.00015724 8.0178e-07 v total_pressure -4.4621e+05 3.1364e+05 -89084 -63077 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2299 0.12532 0.0032607 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 8.0554e-07 0.051542 0.00033006 5.7858e-06 INSTANT 0.876807000E-01 TIME STEP NUMBER 57005 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282778214E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.839063944E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19302E-01 0.22681E+01 Friction velocity uk : 0.19302E-01 0.22681E+01 Dimensionless distance yplus : 0.18631E-01 0.22302E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -9.182504572e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29620E+08 1 0.20562E-09 0.48976E+02 0.25934E+04 c Velocity[X] 0.28057E+02 c Velocity[Y] 0.20919E+02 c Velocity[Z] 0.82678E-06 c Pressure 0.15387E-03 44 0.85584E-04 0.91114E-03 0.48498E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -34.878 48.385 5.6015 7.9917 v Velocity[Y] -35.607 38.515 -0.20308 -0.17589 v Velocity[Z] -3.2002 3.1851 2.1019e-06 -5.3936e-08 v ǁVelocityǁ 0.0012462 48.708 9.1987 8.2706 v Pressure -5.4926e+05 2.1268e+05 -1.893e+05 -1.6387e+05 v TurbVisc 1.3178e-18 0.030735 0.00023036 9.8076e-05 v CourantNb 1.873e-08 0.011744 0.00017284 4.984e-06 v FourierNb 1.2471e-07 0.050923 0.00015725 8.0254e-07 v total_pressure -4.4793e+05 3.1401e+05 -87978 -62544 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2302 0.12536 0.0032614 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 8.0623e-07 0.051596 0.00033008 5.7866e-06 INSTANT 0.876808000E-01 TIME STEP NUMBER 57006 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282773393E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.838766049E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15286E-01 0.22684E+01 Friction velocity uk : 0.15286E-01 0.22684E+01 Dimensionless distance yplus : 0.14934E-01 0.22305E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -8.888043607e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29620E+08 1 0.20568E-09 0.49037E+02 0.25949E+04 c Velocity[X] 0.28083E+02 c Velocity[Y] 0.20954E+02 c Velocity[Z] 0.81360E-06 c Pressure 0.15789E-03 336 0.99263E-04 0.93429E-03 0.53657E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -34.888 48.393 5.6014 7.9916 v Velocity[Y] -35.615 38.525 -0.20322 -0.17632 v Velocity[Z] -3.2005 3.1852 2.1015e-06 -5.3936e-08 v ǁVelocityǁ 0.001115 48.717 9.2 8.2708 v Pressure -5.4876e+05 2.1308e+05 -1.8814e+05 -1.633e+05 v TurbVisc 1.4006e-18 0.030748 0.00023042 9.8187e-05 v CourantNb 1.9112e-08 0.011745 0.00017284 4.9841e-06 v FourierNb 1.2471e-07 0.050975 0.00015726 8.0329e-07 v total_pressure -4.4743e+05 3.1441e+05 -86810 -61977 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2305 0.1254 0.0032621 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 8.0693e-07 0.051648 0.0003301 5.7873e-06 INSTANT 0.876809000E-01 TIME STEP NUMBER 57007 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282769078E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.838475468E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.26932E-02 0.22687E+01 Friction velocity uk : 0.26932E-02 0.22687E+01 Dimensionless distance yplus : 0.25928E-02 0.22308E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -8.595126301e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29621E+08 1 0.20576E-09 0.49065E+02 0.25955E+04 c Velocity[X] 0.28112E+02 c Velocity[Y] 0.20953E+02 c Velocity[Z] 0.80751E-06 c Pressure 0.16201E-03 117 0.84737E-04 0.95798E-03 0.45235E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -34.899 48.401 5.6013 7.9915 v Velocity[Y] -35.623 38.535 -0.20336 -0.17675 v Velocity[Z] -3.2008 3.1853 2.101e-06 -5.3936e-08 v ǁVelocityǁ 0.0011303 48.725 9.2014 8.271 v Pressure -5.501e+05 2.1346e+05 -1.8696e+05 -1.6264e+05 v TurbVisc 1.4354e-18 0.030762 0.00023048 9.8297e-05 v CourantNb 1.9097e-08 0.011746 0.00017285 4.9841e-06 v FourierNb 1.2471e-07 0.051026 0.00015727 8.0405e-07 v total_pressure -4.4878e+05 3.1478e+05 -85631 -61314 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2308 0.12543 0.0032627 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 8.0763e-07 0.0517 0.00033013 5.7881e-06 INSTANT 0.876810000E-01 TIME STEP NUMBER 57008 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282764663E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.838190651E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.35016E-02 0.22691E+01 Friction velocity uk : 0.35016E-02 0.22691E+01 Dimensionless distance yplus : 0.34209E-02 0.22311E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -8.325248565e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29621E+08 1 0.20582E-09 0.49131E+02 0.25971E+04 c Velocity[X] 0.28140E+02 c Velocity[Y] 0.20991E+02 c Velocity[Z] 0.84269E-06 c Pressure 0.15871E-03 16 0.60850E-04 0.93772E-03 0.31303E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -34.91 48.41 5.6013 7.9914 v Velocity[Y] -35.631 38.545 -0.2035 -0.17718 v Velocity[Z] -3.2012 3.1854 2.1006e-06 -5.3936e-08 v ǁVelocityǁ 0.0012599 48.734 9.2028 8.2712 v Pressure -5.512e+05 2.1383e+05 -1.8579e+05 -1.622e+05 v TurbVisc 1.4531e-18 0.030776 0.00023053 9.8408e-05 v CourantNb 1.9341e-08 0.011747 0.00017286 4.9841e-06 v FourierNb 1.2471e-07 0.051076 0.00015728 8.048e-07 v total_pressure -4.4987e+05 3.1516e+05 -84463 -60872 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2311 0.12548 0.0032637 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 8.0833e-07 0.05175 0.00033015 5.7889e-06 INSTANT 0.876811000E-01 TIME STEP NUMBER 57009 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282760354E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.837913880E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.67029E-02 0.22694E+01 Friction velocity uk : 0.67029E-02 0.22694E+01 Dimensionless distance yplus : 0.65486E-02 0.22315E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -7.930059523e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29622E+08 1 0.20587E-09 0.49184E+02 0.25983E+04 c Velocity[X] 0.28159E+02 c Velocity[Y] 0.21025E+02 c Velocity[Z] 0.81091E-06 c Pressure 0.16402E-03 562 0.81448E-04 0.96841E-03 0.54949E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -34.92 48.418 5.6012 7.9913 v Velocity[Y] -35.639 38.555 -0.20364 -0.17761 v Velocity[Z] -3.2015 3.1855 2.1001e-06 -5.3936e-08 v ǁVelocityǁ 0.0015562 48.743 9.2042 8.2714 v Pressure -5.5112e+05 2.1423e+05 -1.8452e+05 -1.6147e+05 v TurbVisc 1.2168e-18 0.03079 0.00023059 9.8519e-05 v CourantNb 1.9248e-08 0.011749 0.00017287 4.9841e-06 v FourierNb 1.2471e-07 0.051125 0.0001573 8.0556e-07 v total_pressure -4.498e+05 3.1555e+05 -83196 -60141 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2315 0.12553 0.0032646 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 8.0903e-07 0.0518 0.00033017 5.7897e-06 INSTANT 0.876812000E-01 TIME STEP NUMBER 57010 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282756289E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.837646861E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.99022E-02 0.22698E+01 Friction velocity uk : 0.99022E-02 0.22698E+01 Dimensionless distance yplus : 0.96742E-02 0.22318E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -7.767828932e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29622E+08 1 0.20595E-09 0.49241E+02 0.25997E+04 c Velocity[X] 0.28196E+02 c Velocity[Y] 0.21045E+02 c Velocity[Z] 0.80349E-06 c Pressure 0.16698E-03 400 0.87909E-04 0.98513E-03 0.58337E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -34.931 48.426 5.6011 7.9912 v Velocity[Y] -35.647 38.566 -0.20378 -0.17804 v Velocity[Z] -3.2018 3.1856 2.0997e-06 -5.3936e-08 v ǁVelocityǁ 0.001667 48.751 9.2055 8.2715 v Pressure -5.5272e+05 2.146e+05 -1.8323e+05 -1.607e+05 v TurbVisc 1.2866e-18 0.030804 0.00023065 9.863e-05 v CourantNb 1.9712e-08 0.01175 0.00017288 4.9842e-06 v FourierNb 1.2471e-07 0.051173 0.00015731 8.0631e-07 v total_pressure -4.514e+05 3.1593e+05 -81901 -59375 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2318 0.12558 0.0032656 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 8.0973e-07 0.051848 0.00033019 5.7905e-06 INSTANT 0.876813000E-01 TIME STEP NUMBER 57011 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282752149E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.837381044E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15061E-01 0.22701E+01 Friction velocity uk : 0.15061E-01 0.22701E+01 Dimensionless distance yplus : 0.14714E-01 0.22322E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -7.426940027e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29623E+08 1 0.20601E-09 0.49277E+02 0.26005E+04 c Velocity[X] 0.28212E+02 c Velocity[Y] 0.21065E+02 c Velocity[Z] 0.80069E-06 c Pressure 0.17074E-03 154 0.76650E-04 0.10066E-02 0.36786E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -34.941 48.435 5.601 7.9911 v Velocity[Y] -35.655 38.576 -0.20392 -0.17847 v Velocity[Z] -3.2021 3.1857 2.0992e-06 -5.3937e-08 v ǁVelocityǁ 0.0015148 48.76 9.2069 8.2717 v Pressure -5.5295e+05 2.1499e+05 -1.8199e+05 -1.6027e+05 v TurbVisc 1.3817e-18 0.030817 0.00023071 9.8741e-05 v CourantNb 2.008e-08 0.011751 0.00017289 4.9842e-06 v FourierNb 1.2471e-07 0.05122 0.00015732 8.0707e-07 v total_pressure -4.5163e+05 3.1632e+05 -80669 -58948 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2322 0.12562 0.0032666 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 8.1043e-07 0.051896 0.00033021 5.7913e-06 INSTANT 0.876814000E-01 TIME STEP NUMBER 57012 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282748286E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.837121444E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.18718E-01 0.22705E+01 Friction velocity uk : 0.18718E-01 0.22705E+01 Dimensionless distance yplus : 0.18287E-01 0.22325E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -7.127948430e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29624E+08 1 0.20607E-09 0.49343E+02 0.26021E+04 c Velocity[X] 0.28244E+02 c Velocity[Y] 0.21099E+02 c Velocity[Z] 0.82613E-06 c Pressure 0.16842E-03 18 0.55276E-04 0.99220E-03 0.34221E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -34.952 48.443 5.601 7.991 v Velocity[Y] -35.663 38.586 -0.20407 -0.17891 v Velocity[Z] -3.2024 3.1859 2.0988e-06 -5.3937e-08 v ǁVelocityǁ 0.0014499 48.769 9.2083 8.2719 v Pressure -5.5306e+05 2.1539e+05 -1.8069e+05 -1.5971e+05 v TurbVisc 1.4242e-18 0.030831 0.00023077 9.8852e-05 v CourantNb 2.033e-08 0.011752 0.0001729 4.9842e-06 v FourierNb 1.2471e-07 0.051267 0.00015733 8.0782e-07 v total_pressure -4.5173e+05 3.1671e+05 -79364 -58385 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2325 0.12567 0.0032675 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 8.1114e-07 0.051943 0.00033023 5.7921e-06 INSTANT 0.876815000E-01 TIME STEP NUMBER 57013 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282744712E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.836873317E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.20998E-01 0.22709E+01 Friction velocity uk : 0.20998E-01 0.22709E+01 Dimensionless distance yplus : 0.20197E-01 0.22329E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -6.725107356e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29624E+08 1 0.20614E-09 0.49384E+02 0.26030E+04 c Velocity[X] 0.28271E+02 c Velocity[Y] 0.21113E+02 c Velocity[Z] 0.81257E-06 c Pressure 0.17284E-03 163 0.99141E-04 0.10175E-02 0.55642E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -34.963 48.452 5.6009 7.9909 v Velocity[Y] -35.671 38.596 -0.20421 -0.17934 v Velocity[Z] -3.2027 3.186 2.0983e-06 -5.3937e-08 v ǁVelocityǁ 0.0013723 48.777 9.2097 8.2721 v Pressure -5.5413e+05 2.1579e+05 -1.7931e+05 -1.5874e+05 v TurbVisc 1.5296e-18 0.030845 0.00023083 9.8963e-05 v CourantNb 2.0325e-08 0.011753 0.00017291 4.9843e-06 v FourierNb 1.2471e-07 0.051311 0.00015735 8.0858e-07 v total_pressure -4.528e+05 3.1711e+05 -77990 -57417 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2329 0.12572 0.0032684 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 8.1185e-07 0.051989 0.00033025 5.7929e-06 INSTANT 0.876816000E-01 TIME STEP NUMBER 57014 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282741147E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.836634739E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.16885E-01 0.22713E+01 Friction velocity uk : 0.16885E-01 0.22713E+01 Dimensionless distance yplus : 0.16240E-01 0.22333E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -6.578742218e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29625E+08 1 0.20621E-09 0.49439E+02 0.26043E+04 c Velocity[X] 0.28300E+02 c Velocity[Y] 0.21139E+02 c Velocity[Z] 0.79720E-06 c Pressure 0.17421E-03 75 0.83188E-04 0.10248E-02 0.40092E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -34.973 48.46 5.6008 7.9908 v Velocity[Y] -35.679 38.606 -0.20435 -0.17977 v Velocity[Z] -3.2031 3.1861 2.0979e-06 -5.3937e-08 v ǁVelocityǁ 0.00093146 48.786 9.211 8.2723 v Pressure -5.5505e+05 2.1617e+05 -1.7793e+05 -1.5806e+05 v TurbVisc 1.4299e-18 0.030859 0.00023089 9.9074e-05 v CourantNb 2.075e-08 0.011755 0.00017291 4.9843e-06 v FourierNb 1.2471e-07 0.051356 0.00015736 8.0934e-07 v total_pressure -4.5373e+05 3.1749e+05 -76606 -56730 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2333 0.12576 0.0032693 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 8.1256e-07 0.052035 0.00033027 5.7936e-06 INSTANT 0.876817000E-01 TIME STEP NUMBER 57015 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282737667E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.836400497E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11822E-01 0.22717E+01 Friction velocity uk : 0.11822E-01 0.22717E+01 Dimensionless distance yplus : 0.11371E-01 0.22337E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -6.296280640e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29625E+08 1 0.20628E-09 0.49507E+02 0.26059E+04 c Velocity[X] 0.28329E+02 c Velocity[Y] 0.21178E+02 c Velocity[Z] 0.80069E-06 c Pressure 0.17494E-03 9 0.54658E-04 0.10283E-02 0.38385E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -34.984 48.469 5.6008 7.9907 v Velocity[Y] -35.687 38.617 -0.2045 -0.18021 v Velocity[Z] -3.2034 3.1862 2.0974e-06 -5.3937e-08 v ǁVelocityǁ 0.00050852 48.795 9.2124 8.2725 v Pressure -5.5611e+05 2.1654e+05 -1.7655e+05 -1.5745e+05 v TurbVisc 9.5587e-19 0.030872 0.00023095 9.9185e-05 v CourantNb 2.1075e-08 0.011756 0.00017292 4.9843e-06 v FourierNb 1.2471e-07 0.0514 0.00015737 8.101e-07 v total_pressure -4.5479e+05 3.1787e+05 -75226 -56123 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2337 0.1258 0.0032701 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 8.1327e-07 0.05208 0.0003303 5.7944e-06 INSTANT 0.876818000E-01 TIME STEP NUMBER 57016 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282734296E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.836171448E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.33393E-02 0.22721E+01 Friction velocity uk : 0.33393E-02 0.22721E+01 Dimensionless distance yplus : 0.32119E-02 0.22341E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -5.717941080e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29626E+08 1 0.20633E-09 0.49562E+02 0.26072E+04 c Velocity[X] 0.28354E+02 c Velocity[Y] 0.21208E+02 c Velocity[Z] 0.79946E-06 c Pressure 0.17925E-03 154 0.75801E-04 0.10529E-02 0.54977E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -34.995 48.477 5.6007 7.9906 v Velocity[Y] -35.695 38.627 -0.20464 -0.18064 v Velocity[Z] -3.2037 3.1863 2.097e-06 -5.3937e-08 v ǁVelocityǁ 0.00024709 48.804 9.2138 8.2728 v Pressure -5.5608e+05 2.1693e+05 -1.7516e+05 -1.5668e+05 v TurbVisc 1.3202e-18 0.030886 0.00023101 9.9296e-05 v CourantNb 2.1122e-08 0.011757 0.00017293 4.9844e-06 v FourierNb 1.2471e-07 0.051443 0.00015738 8.1085e-07 v total_pressure -4.5475e+05 3.1825e+05 -73832 -55352 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2341 0.12585 0.0032709 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 8.1398e-07 0.052123 0.00033032 5.7952e-06 INSTANT 0.876819000E-01 TIME STEP NUMBER 57017 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282731181E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.835951686E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.41375E-02 0.22725E+01 Friction velocity uk : 0.41375E-02 0.22725E+01 Dimensionless distance yplus : 0.39795E-02 0.22345E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -5.623268892e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29627E+08 1 0.20641E-09 0.49620E+02 0.26086E+04 c Velocity[X] 0.28381E+02 c Velocity[Y] 0.21238E+02 c Velocity[Z] 0.79493E-06 c Pressure 0.18143E-03 64 0.80735E-04 0.10649E-02 0.55754E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -35.005 48.485 5.6007 7.9906 v Velocity[Y] -35.703 38.637 -0.20479 -0.18108 v Velocity[Z] -3.204 3.1864 2.0966e-06 -5.3937e-08 v ǁVelocityǁ 0.00041023 48.812 9.2152 8.273 v Pressure -5.5772e+05 2.1731e+05 -1.7371e+05 -1.5593e+05 v TurbVisc 1.3014e-18 0.0309 0.00023107 9.9407e-05 v CourantNb 2.1549e-08 0.011758 0.00017294 4.9844e-06 v FourierNb 1.2472e-07 0.051485 0.0001574 8.1161e-07 v total_pressure -4.5639e+05 3.1864e+05 -72387 -54600 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2345 0.12589 0.0032719 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 8.147e-07 0.052167 0.00033034 5.796e-06 INSTANT 0.876820000E-01 TIME STEP NUMBER 57018 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282727969E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.835740443E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11457E-01 0.22729E+01 Friction velocity uk : 0.11457E-01 0.22729E+01 Dimensionless distance yplus : 0.11115E-01 0.22349E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -5.313623743e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29627E+08 1 0.20647E-09 0.49684E+02 0.26101E+04 c Velocity[X] 0.28413E+02 c Velocity[Y] 0.21271E+02 c Velocity[Z] 0.79439E-06 c Pressure 0.18430E-03 311 0.93703E-04 0.10809E-02 0.56758E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -35.016 48.494 5.6006 7.9905 v Velocity[Y] -35.711 38.647 -0.20493 -0.18151 v Velocity[Z] -3.2043 3.1865 2.0961e-06 -5.3937e-08 v ǁVelocityǁ 0.00082477 48.821 9.2166 8.2732 v Pressure -5.572e+05 2.1772e+05 -1.7226e+05 -1.5521e+05 v TurbVisc 1.3456e-18 0.030914 0.00023113 9.9519e-05 v CourantNb 2.1833e-08 0.011759 0.00017295 4.9845e-06 v FourierNb 1.2472e-07 0.051527 0.00015741 8.1237e-07 v total_pressure -4.5588e+05 3.1905e+05 -70937 -53884 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2349 0.12594 0.003273 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 8.1542e-07 0.05221 0.00033036 5.7968e-06 INSTANT 0.876821000E-01 TIME STEP NUMBER 57019 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282725305E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.835536456E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.88542E-02 0.22734E+01 Friction velocity uk : 0.88542E-02 0.22734E+01 Dimensionless distance yplus : 0.85899E-02 0.22354E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -5.005178212e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29628E+08 1 0.20655E-09 0.49718E+02 0.26108E+04 c Velocity[X] 0.28442E+02 c Velocity[Y] 0.21276E+02 c Velocity[Z] 0.79929E-06 c Pressure 0.18713E-03 102 0.79678E-04 0.10967E-02 0.50750E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -35.027 48.502 5.6006 7.9904 v Velocity[Y] -35.719 38.658 -0.20508 -0.18195 v Velocity[Z] -3.2046 3.1866 2.0957e-06 -5.3937e-08 v ǁVelocityǁ 0.0012714 48.83 9.2179 8.2734 v Pressure -5.5853e+05 2.181e+05 -1.708e+05 -1.5443e+05 v TurbVisc 1.4189e-18 0.030927 0.00023119 9.963e-05 v CourantNb 2.2125e-08 0.011761 0.00017296 4.9845e-06 v FourierNb 1.2472e-07 0.051568 0.00015742 8.1313e-07 v total_pressure -4.5721e+05 3.1943e+05 -69476 -53102 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2354 0.12599 0.003274 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 8.1613e-07 0.052252 0.00033038 5.7976e-06 INSTANT 0.876822000E-01 TIME STEP NUMBER 57020 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282722537E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.835341681E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.57679E-02 0.22738E+01 Friction velocity uk : 0.57679E-02 0.22738E+01 Dimensionless distance yplus : 0.55957E-02 0.22358E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -4.719062238e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29629E+08 1 0.20662E-09 0.49787E+02 0.26125E+04 c Velocity[X] 0.28473E+02 c Velocity[Y] 0.21314E+02 c Velocity[Z] 0.80267E-06 c Pressure 0.18412E-03 9 0.56225E-04 0.10782E-02 0.39186E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -35.038 48.511 5.6005 7.9904 v Velocity[Y] -35.727 38.668 -0.20522 -0.18239 v Velocity[Z] -3.205 3.1867 2.0952e-06 -5.3937e-08 v ǁVelocityǁ 0.0017272 48.839 9.2193 8.2736 v Pressure -5.5955e+05 2.185e+05 -1.6934e+05 -1.5381e+05 v TurbVisc 1.4387e-18 0.030941 0.00023125 9.9742e-05 v CourantNb 2.239e-08 0.011762 0.00017297 4.9846e-06 v FourierNb 1.2472e-07 0.051608 0.00015743 8.1389e-07 v total_pressure -4.5823e+05 3.1982e+05 -68016 -52485 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2358 0.12603 0.0032751 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 8.1685e-07 0.052293 0.0003304 5.7984e-06 INSTANT 0.876823000E-01 TIME STEP NUMBER 57021 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282719930E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.835156929E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.33163E-02 0.22743E+01 Friction velocity uk : 0.33163E-02 0.22743E+01 Dimensionless distance yplus : 0.32173E-02 0.22363E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -4.352536204e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29629E+08 1 0.20667E-09 0.49843E+02 0.26138E+04 c Velocity[X] 0.28497E+02 c Velocity[Y] 0.21346E+02 c Velocity[Z] 0.79575E-06 c Pressure 0.18777E-03 159 0.75757E-04 0.10988E-02 0.61148E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -35.048 48.519 5.6005 7.9903 v Velocity[Y] -35.735 38.678 -0.20537 -0.18283 v Velocity[Z] -3.2053 3.1868 2.0948e-06 -5.3937e-08 v ǁVelocityǁ 0.0021871 48.848 9.2207 8.2739 v Pressure -5.595e+05 2.1889e+05 -1.6782e+05 -1.5292e+05 v TurbVisc 1.5245e-18 0.030955 0.00023131 9.9853e-05 v CourantNb 2.2411e-08 0.011763 0.00017298 4.9846e-06 v FourierNb 1.2472e-07 0.051648 0.00015745 8.1465e-07 v total_pressure -4.5818e+05 3.2021e+05 -66500 -51596 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2363 0.12608 0.0032761 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 8.1758e-07 0.052334 0.00033043 5.7993e-06 INSTANT 0.876824000E-01 TIME STEP NUMBER 57022 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282717570E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.834981651E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.44039E-02 0.22747E+01 Friction velocity uk : 0.44039E-02 0.22747E+01 Dimensionless distance yplus : 0.42724E-02 0.22367E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -4.179862742e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29630E+08 1 0.20675E-09 0.49904E+02 0.26152E+04 c Velocity[X] 0.28527E+02 c Velocity[Y] 0.21376E+02 c Velocity[Z] 0.79676E-06 c Pressure 0.18955E-03 52 0.81522E-04 0.11084E-02 0.59786E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -35.059 48.528 5.6005 7.9902 v Velocity[Y] -35.743 38.689 -0.20552 -0.18326 v Velocity[Z] -3.2056 3.1869 2.0943e-06 -5.3937e-08 v ǁVelocityǁ 0.0026532 48.857 9.2221 8.2741 v Pressure -5.6116e+05 2.1927e+05 -1.6629e+05 -1.521e+05 v TurbVisc 1.4284e-18 0.030969 0.00023137 9.9965e-05 v CourantNb 2.2416e-08 0.011764 0.00017299 4.9846e-06 v FourierNb 1.2472e-07 0.051687 0.00015746 8.1541e-07 v total_pressure -4.5984e+05 3.206e+05 -64961 -50778 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2367 0.12612 0.0032771 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 8.183e-07 0.052374 0.00033045 5.8001e-06 INSTANT 0.876825000E-01 TIME STEP NUMBER 57023 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282715115E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.834812669E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.37814E-02 0.22752E+01 Friction velocity uk : 0.37814E-02 0.22752E+01 Dimensionless distance yplus : 0.36685E-02 0.22372E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -3.915481623e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29631E+08 1 0.20681E-09 0.49970E+02 0.26168E+04 c Velocity[X] 0.28559E+02 c Velocity[Y] 0.21411E+02 c Velocity[Z] 0.79495E-06 c Pressure 0.19193E-03 308 0.94431E-04 0.11214E-02 0.60115E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -35.07 48.537 5.6004 7.9902 v Velocity[Y] -35.751 38.699 -0.20566 -0.1837 v Velocity[Z] -3.2059 3.187 2.0939e-06 -5.3938e-08 v ǁVelocityǁ 0.0031182 48.865 9.2235 8.2743 v Pressure -5.6065e+05 2.1968e+05 -1.6475e+05 -1.5134e+05 v TurbVisc 1.454e-18 0.030982 0.00023143 0.00010008 v CourantNb 2.2619e-08 0.011766 0.000173 4.9847e-06 v FourierNb 1.2472e-07 0.051725 0.00015747 8.1618e-07 v total_pressure -4.5933e+05 3.2101e+05 -63421 -50011 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2372 0.12617 0.0032781 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 8.1903e-07 0.052414 0.00033047 5.8009e-06 INSTANT 0.876826000E-01 TIME STEP NUMBER 57024 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282713206E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.834650428E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.36189E-02 0.22757E+01 Friction velocity uk : 0.36189E-02 0.22757E+01 Dimensionless distance yplus : 0.35108E-02 0.22377E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -3.649572133e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29632E+08 1 0.20689E-09 0.50006E+02 0.26175E+04 c Velocity[X] 0.28590E+02 c Velocity[Y] 0.21416E+02 c Velocity[Z] 0.79709E-06 c Pressure 0.19429E-03 79 0.80350E-04 0.11344E-02 0.53914E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -35.081 48.545 5.6004 7.9901 v Velocity[Y] -35.76 38.709 -0.20581 -0.18414 v Velocity[Z] -3.2062 3.1871 2.0934e-06 -5.3938e-08 v ǁVelocityǁ 0.0033067 48.874 9.2249 8.2745 v Pressure -5.6199e+05 2.2007e+05 -1.632e+05 -1.505e+05 v TurbVisc 1.4695e-18 0.030996 0.00023148 0.00010019 v CourantNb 2.2804e-08 0.011767 0.00017301 4.9848e-06 v FourierNb 1.2472e-07 0.051764 0.00015748 8.1694e-07 v total_pressure -4.6066e+05 3.2139e+05 -61879 -49178 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2377 0.12622 0.0032791 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 8.1974e-07 0.052454 0.00033049 5.8017e-06 INSTANT 0.876827000E-01 TIME STEP NUMBER 57025 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282711202E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.834498217E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.52881E-02 0.22762E+01 Friction velocity uk : 0.52881E-02 0.22762E+01 Dimensionless distance yplus : 0.51303E-02 0.22382E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -3.404276285e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29632E+08 1 0.20696E-09 0.50078E+02 0.26193E+04 c Velocity[X] 0.28624E+02 c Velocity[Y] 0.21455E+02 c Velocity[Z] 0.80095E-06 c Pressure 0.19084E-03 9 0.56815E-04 0.11134E-02 0.41387E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -35.092 48.554 5.6004 7.9901 v Velocity[Y] -35.768 38.72 -0.20596 -0.18458 v Velocity[Z] -3.2065 3.1872 2.093e-06 -5.3938e-08 v ǁVelocityǁ 0.0032816 48.883 9.2263 8.2748 v Pressure -5.63e+05 2.2046e+05 -1.6167e+05 -1.4985e+05 v TurbVisc 1.4856e-18 0.03101 0.00023154 0.0001003 v CourantNb 2.2969e-08 0.011768 0.00017302 4.9848e-06 v FourierNb 1.2472e-07 0.051802 0.0001575 8.177e-07 v total_pressure -4.6168e+05 3.2179e+05 -60345 -48524 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2382 0.12626 0.0032801 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 8.2035e-07 0.052493 0.00033051 5.8025e-06 INSTANT 0.876828000E-01 TIME STEP NUMBER 57026 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282709370E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.834357275E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.54508E-02 0.22767E+01 Friction velocity uk : 0.54508E-02 0.22767E+01 Dimensionless distance yplus : 0.52881E-02 0.22387E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -3.094329614e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29633E+08 1 0.20701E-09 0.50137E+02 0.26206E+04 c Velocity[X] 0.28650E+02 c Velocity[Y] 0.21487E+02 c Velocity[Z] 0.79472E-06 c Pressure 0.19398E-03 158 0.76478E-04 0.11308E-02 0.64060E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -35.103 48.563 5.6003 7.99 v Velocity[Y] -35.776 38.73 -0.20611 -0.18503 v Velocity[Z] -3.2069 3.1873 2.0925e-06 -5.3938e-08 v ǁVelocityǁ 0.0032352 48.892 9.2276 8.275 v Pressure -5.6293e+05 2.2086e+05 -1.6009e+05 -1.4892e+05 v TurbVisc 1.5413e-18 0.031023 0.0002316 0.00010041 v CourantNb 2.2835e-08 0.011769 0.00017303 4.9849e-06 v FourierNb 1.2472e-07 0.051838 0.00015751 8.1846e-07 v total_pressure -4.6161e+05 3.2218e+05 -58760 -47592 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2387 0.12631 0.003281 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 8.2096e-07 0.052532 0.00033054 5.8033e-06 INSTANT 0.876829000E-01 TIME STEP NUMBER 57027 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282707791E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.834226970E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.50205E-02 0.22772E+01 Friction velocity uk : 0.50205E-02 0.22772E+01 Dimensionless distance yplus : 0.48706E-02 0.22391E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -2.943633906e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29634E+08 1 0.20710E-09 0.50200E+02 0.26221E+04 c Velocity[X] 0.28681E+02 c Velocity[Y] 0.21519E+02 c Velocity[Z] 0.78885E-06 c Pressure 0.19525E-03 91 0.82189E-04 0.11374E-02 0.62756E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -35.114 48.571 5.6003 7.99 v Velocity[Y] -35.784 38.741 -0.20626 -0.18547 v Velocity[Z] -3.2072 3.1875 2.0921e-06 -5.3938e-08 v ǁVelocityǁ 0.0032045 48.901 9.229 8.2753 v Pressure -5.6461e+05 2.2124e+05 -1.5848e+05 -1.4805e+05 v TurbVisc 1.4654e-18 0.031037 0.00023166 0.00010052 v CourantNb 2.3236e-08 0.011771 0.00017304 4.9849e-06 v FourierNb 1.2472e-07 0.051876 0.00015752 8.1923e-07 v total_pressure -4.6328e+05 3.2257e+05 -57153 -46728 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2391 0.12635 0.003282 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 8.2157e-07 0.05257 0.00033056 5.8041e-06 INSTANT 0.876830000E-01 TIME STEP NUMBER 57028 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282706120E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.834103666E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.45423E-02 0.22777E+01 Friction velocity uk : 0.45423E-02 0.22777E+01 Dimensionless distance yplus : 0.44067E-02 0.22396E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -2.724988149e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29635E+08 1 0.20715E-09 0.50270E+02 0.26238E+04 c Velocity[X] 0.28715E+02 c Velocity[Y] 0.21555E+02 c Velocity[Z] 0.79143E-06 c Pressure 0.19711E-03 252 0.95081E-04 0.11474E-02 0.60951E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -35.125 48.58 5.6003 7.9899 v Velocity[Y] -35.793 38.751 -0.20641 -0.18591 v Velocity[Z] -3.2075 3.1876 2.0916e-06 -5.3938e-08 v ǁVelocityǁ 0.0031759 48.91 9.2304 8.2755 v Pressure -5.6408e+05 2.2166e+05 -1.5689e+05 -1.4729e+05 v TurbVisc 1.4853e-18 0.031051 0.00023172 0.00010064 v CourantNb 2.3433e-08 0.011772 0.00017305 4.985e-06 v FourierNb 1.2472e-07 0.051912 0.00015753 8.1999e-07 v total_pressure -4.6275e+05 3.2298e+05 -55562 -45968 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2396 0.1264 0.003283 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 8.2219e-07 0.052608 0.00033058 5.805e-06 INSTANT 0.876831000E-01 TIME STEP NUMBER 57029 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282705003E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.833987387E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.41297E-02 0.22782E+01 Friction velocity uk : 0.41297E-02 0.22782E+01 Dimensionless distance yplus : 0.40064E-02 0.22401E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -2.529232962e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29636E+08 1 0.20724E-09 0.50308E+02 0.26246E+04 c Velocity[X] 0.28748E+02 c Velocity[Y] 0.21560E+02 c Velocity[Z] 0.79249E-06 c Pressure 0.19894E-03 84 0.80880E-04 0.11571E-02 0.58693E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -35.136 48.589 5.6003 7.9899 v Velocity[Y] -35.801 38.762 -0.20656 -0.18635 v Velocity[Z] -3.2078 3.1877 2.0912e-06 -5.3938e-08 v ǁVelocityǁ 0.0031482 48.919 9.2318 8.2758 v Pressure -5.6541e+05 2.2205e+05 -1.5528e+05 -1.4638e+05 v TurbVisc 1.4948e-18 0.031065 0.00023178 0.00010075 v CourantNb 2.3627e-08 0.011773 0.00017306 4.985e-06 v FourierNb 1.2472e-07 0.051949 0.00015755 8.2076e-07 v total_pressure -4.6409e+05 3.2337e+05 -53951 -45052 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2401 0.12644 0.0032839 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 8.2281e-07 0.052646 0.0003306 5.8058e-06 INSTANT 0.876832000E-01 TIME STEP NUMBER 57030 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282703797E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.833882100E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.42479E-02 0.22788E+01 Friction velocity uk : 0.42479E-02 0.22788E+01 Dimensionless distance yplus : 0.41211E-02 0.22407E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -2.328681837e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29636E+08 1 0.20730E-09 0.50383E+02 0.26264E+04 c Velocity[X] 0.28783E+02 c Velocity[Y] 0.21600E+02 c Velocity[Z] 0.79970E-06 c Pressure 0.19501E-03 9 0.57302E-04 0.11334E-02 0.42439E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -35.147 48.598 5.6002 7.9898 v Velocity[Y] -35.809 38.772 -0.20671 -0.1868 v Velocity[Z] -3.2081 3.1878 2.0907e-06 -5.3938e-08 v ǁVelocityǁ 0.0031338 48.928 9.2332 8.276 v Pressure -5.6644e+05 2.2244e+05 -1.537e+05 -1.4571e+05 v TurbVisc 1.514e-18 0.031078 0.00023184 0.00010086 v CourantNb 2.3794e-08 0.011775 0.00017307 4.9851e-06 v FourierNb 1.2472e-07 0.051985 0.00015756 8.2152e-07 v total_pressure -4.6511e+05 3.2377e+05 -52372 -44387 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2407 0.12648 0.0032849 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 8.2342e-07 0.052684 0.00033063 5.8066e-06 INSTANT 0.876833000E-01 TIME STEP NUMBER 57031 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282702765E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.833787658E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.41258E-02 0.22793E+01 Friction velocity uk : 0.41258E-02 0.22793E+01 Dimensionless distance yplus : 0.39825E-02 0.22412E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -2.073338782e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29637E+08 1 0.20736E-09 0.50444E+02 0.26278E+04 c Velocity[X] 0.28811E+02 c Velocity[Y] 0.21633E+02 c Velocity[Z] 0.79503E-06 c Pressure 0.19762E-03 159 0.77048E-04 0.11477E-02 0.66045E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -35.158 48.606 5.6002 7.9898 v Velocity[Y] -35.818 38.783 -0.20686 -0.18724 v Velocity[Z] -3.2084 3.1879 2.0903e-06 -5.3938e-08 v ǁVelocityǁ 0.0030981 48.937 9.2346 8.2763 v Pressure -5.6635e+05 2.2284e+05 -1.5207e+05 -1.4476e+05 v TurbVisc 1.5604e-18 0.031092 0.0002319 0.00010097 v CourantNb 2.3677e-08 0.011776 0.00017308 4.9852e-06 v FourierNb 1.2472e-07 0.05202 0.00015757 8.2229e-07 v total_pressure -4.6503e+05 3.2416e+05 -50744 -43436 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2412 0.12653 0.0032858 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 8.2405e-07 0.052721 0.00033065 5.8075e-06 INSTANT 0.876834000E-01 TIME STEP NUMBER 57032 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282701992E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.833704593E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.44165E-02 0.22798E+01 Friction velocity uk : 0.44165E-02 0.22798E+01 Dimensionless distance yplus : 0.42631E-02 0.22417E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.984694752e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29638E+08 1 0.20744E-09 0.50510E+02 0.26293E+04 c Velocity[X] 0.28845E+02 c Velocity[Y] 0.21666E+02 c Velocity[Z] 0.78982E-06 c Pressure 0.19838E-03 65 0.82640E-04 0.11512E-02 0.64784E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -35.169 48.615 5.6002 7.9898 v Velocity[Y] -35.826 38.793 -0.20701 -0.18769 v Velocity[Z] -3.2087 3.188 2.0898e-06 -5.3938e-08 v ǁVelocityǁ 0.0030772 48.947 9.236 8.2766 v Pressure -5.6804e+05 2.2322e+05 -1.5042e+05 -1.4387e+05 v TurbVisc 1.4935e-18 0.031106 0.00023196 0.00010109 v CourantNb 2.4065e-08 0.011777 0.00017309 4.9852e-06 v FourierNb 1.2472e-07 0.052056 0.00015758 8.2305e-07 v total_pressure -4.6671e+05 3.2455e+05 -49096 -42548 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2417 0.12657 0.0032867 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 8.2467e-07 0.052758 0.00033067 5.8083e-06 INSTANT 0.876835000E-01 TIME STEP NUMBER 57033 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282701125E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.833628582E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.55137E-02 0.22803E+01 Friction velocity uk : 0.55137E-02 0.22803E+01 Dimensionless distance yplus : 0.53491E-02 0.22422E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.830285310e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29639E+08 1 0.20750E-09 0.50583E+02 0.26310E+04 c Velocity[X] 0.28881E+02 c Velocity[Y] 0.21702E+02 c Velocity[Z] 0.79290E-06 c Pressure 0.19972E-03 240 0.95680E-04 0.11582E-02 0.62903E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -35.18 48.624 5.6002 7.9898 v Velocity[Y] -35.834 38.804 -0.20716 -0.18814 v Velocity[Z] -3.2091 3.1881 2.0894e-06 -5.3938e-08 v ǁVelocityǁ 0.003057 48.956 9.2374 8.2768 v Pressure -5.6749e+05 2.2364e+05 -1.488e+05 -1.4309e+05 v TurbVisc 1.476e-18 0.031119 0.00023202 0.0001012 v CourantNb 2.4259e-08 0.011778 0.0001731 4.9853e-06 v FourierNb 1.2473e-07 0.052092 0.00015759 8.2382e-07 v total_pressure -4.6616e+05 3.2497e+05 -47472 -41766 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2422 0.12662 0.0032877 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 8.2529e-07 0.052796 0.00033069 5.8091e-06 INSTANT 0.876836000E-01 TIME STEP NUMBER 57034 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282700824E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.833560062E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.47664E-02 0.22809E+01 Friction velocity uk : 0.47664E-02 0.22809E+01 Dimensionless distance yplus : 0.46241E-02 0.22428E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.680954088e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29640E+08 1 0.20759E-09 0.50623E+02 0.26319E+04 c Velocity[X] 0.28916E+02 c Velocity[Y] 0.21708E+02 c Velocity[Z] 0.79202E-06 c Pressure 0.20104E-03 92 0.81310E-04 0.11649E-02 0.60385E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -35.192 48.633 5.6002 7.9897 v Velocity[Y] -35.843 38.814 -0.20731 -0.18858 v Velocity[Z] -3.2094 3.1882 2.0889e-06 -5.3938e-08 v ǁVelocityǁ 0.0030374 48.965 9.2388 8.2771 v Pressure -5.6883e+05 2.2403e+05 -1.4716e+05 -1.4216e+05 v TurbVisc 1.5276e-18 0.031133 0.00023209 0.00010131 v CourantNb 2.4555e-08 0.01178 0.00017311 4.9854e-06 v FourierNb 1.2473e-07 0.052127 0.00015761 8.2459e-07 v total_pressure -4.6751e+05 3.2536e+05 -45831 -40832 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2428 0.12666 0.0032887 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 8.2591e-07 0.052833 0.00033072 5.81e-06 INSTANT 0.876837000E-01 TIME STEP NUMBER 57035 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282700430E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.833503187E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.33748E-02 0.22814E+01 Friction velocity uk : 0.33748E-02 0.22814E+01 Dimensionless distance yplus : 0.32741E-02 0.22433E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.543441010e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29641E+08 1 0.20765E-09 0.50702E+02 0.26338E+04 c Velocity[X] 0.28953E+02 c Velocity[Y] 0.21749E+02 c Velocity[Z] 0.79866E-06 c Pressure 0.19652E-03 9 0.57643E-04 0.11379E-02 0.43962E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -35.203 48.642 5.6002 7.9897 v Velocity[Y] -35.851 38.825 -0.20746 -0.18903 v Velocity[Z] -3.2097 3.1883 2.0884e-06 -5.3938e-08 v ǁVelocityǁ 0.0030295 48.974 9.2402 8.2774 v Pressure -5.6986e+05 2.2443e+05 -1.4555e+05 -1.4147e+05 v TurbVisc 1.5399e-18 0.031147 0.00023215 0.00010142 v CourantNb 2.672e-08 0.011781 0.00017312 4.9854e-06 v FourierNb 1.2473e-07 0.052163 0.00015762 8.2536e-07 v total_pressure -4.6854e+05 3.2575e+05 -44225 -40148 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2433 0.12671 0.0032897 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 8.2654e-07 0.05287 0.00033074 5.8108e-06 INSTANT 0.876838000E-01 TIME STEP NUMBER 57036 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282700215E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.833457507E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.25098E-02 0.22820E+01 Friction velocity uk : 0.25098E-02 0.22820E+01 Dimensionless distance yplus : 0.24349E-02 0.22439E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.339793819e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29642E+08 1 0.20771E-09 0.50766E+02 0.26353E+04 c Velocity[X] 0.28983E+02 c Velocity[Y] 0.21783E+02 c Velocity[Z] 0.80125E-06 c Pressure 0.19863E-03 171 0.77396E-04 0.11492E-02 0.66880E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -35.214 48.651 5.6002 7.9897 v Velocity[Y] -35.86 38.836 -0.20761 -0.18948 v Velocity[Z] -3.21 3.1884 2.088e-06 -5.3939e-08 v ǁVelocityǁ 0.0029001 48.984 9.2416 8.2776 v Pressure -5.6977e+05 2.2482e+05 -1.4391e+05 -1.4053e+05 v TurbVisc 1.5971e-18 0.03116 0.00023221 0.00010154 v CourantNb 2.8799e-08 0.011782 0.00017313 4.9855e-06 v FourierNb 1.2473e-07 0.052197 0.00015763 8.2612e-07 v total_pressure -4.6844e+05 3.2615e+05 -42584 -39202 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2439 0.12675 0.0032907 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 8.2716e-07 0.052907 0.00033076 5.8116e-06 INSTANT 0.876839000E-01 TIME STEP NUMBER 57037 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282700258E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.833423638E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.52593E-02 0.22825E+01 Friction velocity uk : 0.52593E-02 0.22825E+01 Dimensionless distance yplus : 0.51023E-02 0.22444E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.317046219e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29643E+08 1 0.20779E-09 0.50835E+02 0.26369E+04 c Velocity[X] 0.29022E+02 c Velocity[Y] 0.21813E+02 c Velocity[Z] 0.79536E-06 c Pressure 0.19887E-03 409 0.83363E-04 0.11497E-02 0.71215E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -35.226 48.66 5.6002 7.9897 v Velocity[Y] -35.869 38.847 -0.20776 -0.18992 v Velocity[Z] -3.2103 3.1885 2.0875e-06 -5.3939e-08 v ǁVelocityǁ 0.0025947 48.993 9.243 8.2779 v Pressure -5.714e+05 2.2522e+05 -1.4222e+05 -1.3952e+05 v TurbVisc 1.5171e-18 0.031174 0.00023227 0.00010165 v CourantNb 3.108e-08 0.011784 0.00017314 4.9856e-06 v FourierNb 1.2473e-07 0.052233 0.00015764 8.2689e-07 v total_pressure -4.7008e+05 3.2654e+05 -40892 -38194 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2444 0.12679 0.0032916 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 8.2779e-07 0.052944 0.00033078 5.8125e-06 INSTANT 0.876840000E-01 TIME STEP NUMBER 57038 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282700247E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.833396981E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.40315E-02 0.22831E+01 Friction velocity uk : 0.40315E-02 0.22831E+01 Dimensionless distance yplus : 0.39111E-02 0.22449E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.203894902e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29644E+08 1 0.20785E-09 0.50911E+02 0.26387E+04 c Velocity[X] 0.29054E+02 c Velocity[Y] 0.21857E+02 c Velocity[Z] 0.79402E-06 c Pressure 0.19979E-03 119 0.96582E-04 0.11541E-02 0.58983E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -35.237 48.669 5.6002 7.9897 v Velocity[Y] -35.877 38.857 -0.20791 -0.19037 v Velocity[Z] -3.2106 3.1886 2.0871e-06 -5.3939e-08 v ǁVelocityǁ 0.0023772 49.003 9.2444 8.2782 v Pressure -5.7095e+05 2.2563e+05 -1.4064e+05 -1.3894e+05 v TurbVisc 1.528e-18 0.031188 0.00023233 0.00010176 v CourantNb 3.3291e-08 0.011785 0.00017315 4.9857e-06 v FourierNb 1.2473e-07 0.052268 0.00015766 8.2766e-07 v total_pressure -4.6963e+05 3.2695e+05 -39319 -37616 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2449 0.12684 0.0032926 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 8.2842e-07 0.052981 0.00033081 5.8133e-06 INSTANT 0.876841000E-01 TIME STEP NUMBER 57039 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282700723E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.833376346E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.32931E-02 0.22836E+01 Friction velocity uk : 0.32931E-02 0.22836E+01 Dimensionless distance yplus : 0.31948E-02 0.22455E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.105358507e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29645E+08 1 0.20794E-09 0.50954E+02 0.26396E+04 c Velocity[X] 0.29094E+02 c Velocity[Y] 0.21860E+02 c Velocity[Z] 0.79586E-06 c Pressure 0.20052E-03 91 0.82020E-04 0.11575E-02 0.66167E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -35.248 48.679 5.6002 7.9897 v Velocity[Y] -35.886 38.868 -0.20806 -0.19082 v Velocity[Z] -3.2109 3.1887 2.0866e-06 -5.3939e-08 v ǁVelocityǁ 0.0022689 49.012 9.2458 8.2785 v Pressure -5.7226e+05 2.2602e+05 -1.3897e+05 -1.3791e+05 v TurbVisc 1.562e-18 0.031201 0.00023239 0.00010188 v CourantNb 3.5498e-08 0.011786 0.00017316 4.9857e-06 v FourierNb 1.2473e-07 0.052303 0.00015767 8.2843e-07 v total_pressure -4.7094e+05 3.2734e+05 -37643 -36582 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2455 0.12688 0.0032935 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 8.2905e-07 0.053018 0.00033083 5.8142e-06 INSTANT 0.876842000E-01 TIME STEP NUMBER 57040 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282701150E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.833371059E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.32680E-02 0.22842E+01 Friction velocity uk : 0.32680E-02 0.22842E+01 Dimensionless distance yplus : 0.31704E-02 0.22460E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.030790947e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29646E+08 1 0.20800E-09 0.51035E+02 0.26415E+04 c Velocity[X] 0.29134E+02 c Velocity[Y] 0.21902E+02 c Velocity[Z] 0.80352E-06 c Pressure 0.19536E-03 9 0.58167E-04 0.11268E-02 0.45104E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -35.26 48.688 5.6002 7.9897 v Velocity[Y] -35.895 38.879 -0.20821 -0.19127 v Velocity[Z] -3.2113 3.1888 2.0862e-06 -5.3939e-08 v ǁVelocityǁ 0.0022679 49.022 9.2472 8.2788 v Pressure -5.7329e+05 2.2642e+05 -1.3736e+05 -1.3721e+05 v TurbVisc 1.5484e-18 0.031215 0.00023245 0.00010199 v CourantNb 3.7755e-08 0.011787 0.00017317 4.9858e-06 v FourierNb 1.2473e-07 0.052339 0.00015768 8.292e-07 v total_pressure -4.7196e+05 3.2774e+05 -36039 -35886 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.246 0.12692 0.0032944 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 8.2969e-07 0.053055 0.00033085 5.815e-06 INSTANT 0.876843000E-01 TIME STEP NUMBER 57041 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282701757E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.833375533E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.50906E-02 0.22848E+01 Friction velocity uk : 0.50906E-02 0.22848E+01 Dimensionless distance yplus : 0.49386E-02 0.22466E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -8.852191398e-03 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29647E+08 1 0.20806E-09 0.51103E+02 0.26431E+04 c Velocity[X] 0.29166E+02 c Velocity[Y] 0.21937E+02 c Velocity[Z] 0.80512E-06 c Pressure 0.19702E-03 259 0.78107E-04 0.11355E-02 0.68429E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -35.271 48.697 5.6001 7.9897 v Velocity[Y] -35.903 38.89 -0.20836 -0.19173 v Velocity[Z] -3.2116 3.1889 2.0857e-06 -5.3939e-08 v ǁVelocityǁ 0.002331 49.031 9.2486 8.2791 v Pressure -5.7319e+05 2.2682e+05 -1.3573e+05 -1.3626e+05 v TurbVisc 1.6268e-18 0.031228 0.00023251 0.0001021 v CourantNb 4.0038e-08 0.011789 0.00017318 4.9859e-06 v FourierNb 1.2473e-07 0.052374 0.0001577 8.2997e-07 v total_pressure -4.7187e+05 3.2814e+05 -34402 -34934 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2466 0.12697 0.0032952 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 8.3032e-07 0.053092 0.00033088 5.8159e-06 INSTANT 0.876844000E-01 TIME STEP NUMBER 57042 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282702620E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.833392278E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.73259E-02 0.22853E+01 Friction velocity uk : 0.73259E-02 0.22853E+01 Dimensionless distance yplus : 0.71072E-02 0.22471E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -8.562548096e-03 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29648E+08 1 0.20815E-09 0.51175E+02 0.26447E+04 c Velocity[X] 0.29208E+02 c Velocity[Y] 0.21967E+02 c Velocity[Z] 0.79982E-06 c Pressure 0.19676E-03 410 0.84250E-04 0.11331E-02 0.69697E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -35.283 48.706 5.6001 7.9897 v Velocity[Y] -35.912 38.901 -0.20851 -0.19218 v Velocity[Z] -3.2119 3.189 2.0853e-06 -5.3939e-08 v ǁVelocityǁ 0.002495 49.041 9.25 8.2794 v Pressure -5.7483e+05 2.272e+05 -1.3406e+05 -1.3531e+05 v TurbVisc 1.538e-18 0.031242 0.00023257 0.00010221 v CourantNb 4.2205e-08 0.01179 0.00017319 4.986e-06 v FourierNb 1.2473e-07 0.052409 0.00015771 8.3074e-07 v total_pressure -4.7351e+05 3.2853e+05 -32739 -33987 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2471 0.12701 0.0032961 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 8.3096e-07 0.053129 0.0003309 5.8167e-06 INSTANT 0.876845000E-01 TIME STEP NUMBER 57043 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282703414E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.833415655E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.24641E-02 0.22859E+01 Friction velocity uk : 0.24641E-02 0.22859E+01 Dimensionless distance yplus : 0.23715E-02 0.22477E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -7.960131159e-03 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29649E+08 1 0.20821E-09 0.51255E+02 0.26466E+04 c Velocity[X] 0.29241E+02 c Velocity[Y] 0.22014E+02 c Velocity[Z] 0.79891E-06 c Pressure 0.19717E-03 162 0.97610E-04 0.11346E-02 0.61399E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -35.294 48.716 5.6002 7.9897 v Velocity[Y] -35.921 38.912 -0.20866 -0.19263 v Velocity[Z] -3.2122 3.1891 2.0848e-06 -5.3939e-08 v ǁVelocityǁ 0.0027581 49.05 9.2514 8.2797 v Pressure -5.7438e+05 2.2762e+05 -1.325e+05 -1.347e+05 v TurbVisc 1.5692e-18 0.031256 0.00023263 0.00010233 v CourantNb 4.4412e-08 0.011791 0.0001732 4.9861e-06 v FourierNb 1.2473e-07 0.052445 0.00015772 8.3152e-07 v total_pressure -4.7305e+05 3.2895e+05 -31172 -33378 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2477 0.12705 0.0032969 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 8.3159e-07 0.053166 0.00033092 5.8176e-06 INSTANT 0.876846000E-01 TIME STEP NUMBER 57044 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282704715E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.833446319E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.99766E-02 0.22865E+01 Friction velocity uk : 0.99766E-02 0.22865E+01 Dimensionless distance yplus : 0.96788E-02 0.22483E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -7.275199440e-03 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29650E+08 1 0.20829E-09 0.51299E+02 0.26476E+04 c Velocity[X] 0.29284E+02 c Velocity[Y] 0.22016E+02 c Velocity[Z] 0.79922E-06 c Pressure 0.19746E-03 92 0.83020E-04 0.11354E-02 0.65880E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -35.306 48.725 5.6002 7.9897 v Velocity[Y] -35.93 38.923 -0.20882 -0.19308 v Velocity[Z] -3.2125 3.1892 2.0844e-06 -5.3939e-08 v ǁVelocityǁ 0.0028977 49.06 9.2528 8.28 v Pressure -5.757e+05 2.2801e+05 -1.3085e+05 -1.337e+05 v TurbVisc 1.576e-18 0.031269 0.0002327 0.00010244 v CourantNb 4.6654e-08 0.011793 0.00017321 4.9861e-06 v FourierNb 1.2473e-07 0.05248 0.00015773 8.3229e-07 v total_pressure -4.7437e+05 3.2934e+05 -29525 -32370 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2483 0.1271 0.003298 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 8.3223e-07 0.053204 0.00033095 5.8184e-06 INSTANT 0.876847000E-01 TIME STEP NUMBER 57045 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282705952E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.833491505E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11016E-01 0.22871E+01 Friction velocity uk : 0.11016E-01 0.22871E+01 Dimensionless distance yplus : 0.10687E-01 0.22488E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -6.789949884e-03 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29652E+08 1 0.20836E-09 0.51385E+02 0.26496E+04 c Velocity[X] 0.29325E+02 c Velocity[Y] 0.22060E+02 c Velocity[Z] 0.80734E-06 c Pressure 0.19154E-03 9 0.58725E-04 0.11005E-02 0.44496E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -35.318 48.735 5.6002 7.9897 v Velocity[Y] -35.939 38.934 -0.20897 -0.19354 v Velocity[Z] -3.2128 3.1893 2.0839e-06 -5.3939e-08 v ǁVelocityǁ 0.0028978 49.07 9.2542 8.2803 v Pressure -5.7674e+05 2.2841e+05 -1.2928e+05 -1.3302e+05 v TurbVisc 1.5695e-18 0.031283 0.00023276 0.00010255 v CourantNb 4.8934e-08 0.011794 0.00017322 4.9862e-06 v FourierNb 1.2473e-07 0.052516 0.00015775 8.3306e-07 v total_pressure -4.7542e+05 3.2974e+05 -27953 -31700 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2488 0.12714 0.003299 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 8.3287e-07 0.053241 0.00033097 5.8193e-06 INSTANT 0.876848000E-01 TIME STEP NUMBER 57046 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282707362E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.833546718E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11933E-01 0.22877E+01 Friction velocity uk : 0.11933E-01 0.22877E+01 Dimensionless distance yplus : 0.11577E-01 0.22494E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -5.521094086e-03 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29653E+08 1 0.20842E-09 0.51455E+02 0.26512E+04 c Velocity[X] 0.29360E+02 c Velocity[Y] 0.22095E+02 c Velocity[Z] 0.80714E-06 c Pressure 0.19279E-03 273 0.79023E-04 0.11068E-02 0.69465E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -35.329 48.744 5.6002 7.9897 v Velocity[Y] -35.948 38.945 -0.20912 -0.19399 v Velocity[Z] -3.2131 3.1895 2.0835e-06 -5.3939e-08 v ǁVelocityǁ 0.0028773 49.08 9.2556 8.2806 v Pressure -5.7662e+05 2.2881e+05 -1.2767e+05 -1.3207e+05 v TurbVisc 1.623e-18 0.031296 0.00023282 0.00010267 v CourantNb 5.0973e-08 0.011795 0.00017323 4.9863e-06 v FourierNb 1.2473e-07 0.052551 0.00015776 8.3384e-07 v total_pressure -4.753e+05 3.3013e+05 -26341 -30746 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2494 0.12718 0.0033 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 8.3351e-07 0.053278 0.00033099 5.8202e-06 INSTANT 0.876849000E-01 TIME STEP NUMBER 57047 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282709038E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.833614194E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13189E-01 0.22882E+01 Friction velocity uk : 0.13189E-01 0.22882E+01 Dimensionless distance yplus : 0.12795E-01 0.22500E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -5.324306940e-03 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29654E+08 1 0.20850E-09 0.51531E+02 0.26529E+04 c Velocity[X] 0.29403E+02 c Velocity[Y] 0.22128E+02 c Velocity[Z] 0.80365E-06 c Pressure 0.19205E-03 108 0.85072E-04 0.11017E-02 0.67096E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -35.341 48.754 5.6002 7.9897 v Velocity[Y] -35.957 38.956 -0.20927 -0.19445 v Velocity[Z] -3.2134 3.1896 2.083e-06 -5.3939e-08 v ǁVelocityǁ 0.0028202 49.09 9.257 8.2809 v Pressure -5.7831e+05 2.292e+05 -1.2606e+05 -1.312e+05 v TurbVisc 1.5795e-18 0.03131 0.00023288 0.00010278 v CourantNb 5.3381e-08 0.011797 0.00017324 4.9864e-06 v FourierNb 1.2473e-07 0.052587 0.00015777 8.3461e-07 v total_pressure -4.7699e+05 3.3052e+05 -24738 -29877 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.25 0.12723 0.003301 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 8.3416e-07 0.053316 0.00033102 5.821e-06 INSTANT 0.876850000E-01 TIME STEP NUMBER 57048 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282710634E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.833687975E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13316E-01 0.22888E+01 Friction velocity uk : 0.13316E-01 0.22888E+01 Dimensionless distance yplus : 0.12817E-01 0.22505E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -4.789301234e-03 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29655E+08 1 0.20856E-09 0.51613E+02 0.26549E+04 c Velocity[X] 0.29441E+02 c Velocity[Y] 0.22173E+02 c Velocity[Z] 0.80325E-06 c Pressure 0.19197E-03 236 0.98637E-04 0.11003E-02 0.64009E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -35.353 48.764 5.6002 7.9897 v Velocity[Y] -35.966 38.967 -0.20942 -0.1949 v Velocity[Z] -3.2138 3.1897 2.0826e-06 -5.3939e-08 v ǁVelocityǁ 0.0019614 49.1 9.2584 8.2812 v Pressure -5.7782e+05 2.2961e+05 -1.2451e+05 -1.3054e+05 v TurbVisc 1.568e-18 0.031324 0.00023294 0.0001029 v CourantNb 5.451e-08 0.011798 0.00017325 4.9865e-06 v FourierNb 1.2473e-07 0.052623 0.00015779 8.3538e-07 v total_pressure -4.7649e+05 3.3094e+05 -23184 -29211 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2505 0.12727 0.0033019 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 8.348e-07 0.053353 0.00033104 5.8219e-06 INSTANT 0.876851000E-01 TIME STEP NUMBER 57049 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282712729E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.833770264E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.78562E-02 0.22894E+01 Friction velocity uk : 0.78562E-02 0.22894E+01 Dimensionless distance yplus : 0.75617E-02 0.22511E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -4.222857321e-03 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29656E+08 1 0.20865E-09 0.51660E+02 0.26559E+04 c Velocity[X] 0.29485E+02 c Velocity[Y] 0.22176E+02 c Velocity[Z] 0.81412E-06 c Pressure 0.19187E-03 78 0.83793E-04 0.10989E-02 0.63359E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -35.365 48.773 5.6002 7.9898 v Velocity[Y] -35.975 38.978 -0.20957 -0.19536 v Velocity[Z] -3.2141 3.1898 2.0821e-06 -5.394e-08 v ǁVelocityǁ 0.0016342 49.11 9.2598 8.2816 v Pressure -5.7915e+05 2.3e+05 -1.2293e+05 -1.2959e+05 v TurbVisc 1.5942e-18 0.031337 0.00023301 0.00010301 v CourantNb 5.4505e-08 0.011799 0.00017326 4.9866e-06 v FourierNb 1.2473e-07 0.052659 0.0001578 8.3616e-07 v total_pressure -4.7783e+05 3.3133e+05 -21604 -28265 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2511 0.12731 0.0033027 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 8.3545e-07 0.053391 0.00033106 5.8228e-06 INSTANT 0.876852000E-01 TIME STEP NUMBER 57050 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282714763E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.833864718E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.57887E-02 0.22900E+01 Friction velocity uk : 0.57887E-02 0.22900E+01 Dimensionless distance yplus : 0.55716E-02 0.22517E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -3.436946942e-03 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29658E+08 1 0.20872E-09 0.51749E+02 0.26580E+04 c Velocity[X] 0.29528E+02 c Velocity[Y] 0.22221E+02 c Velocity[Z] 0.81873E-06 c Pressure 0.18514E-03 9 0.59143E-04 0.10596E-02 0.43207E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -35.377 48.783 5.6002 7.9898 v Velocity[Y] -35.984 38.989 -0.20972 -0.19582 v Velocity[Z] -3.2144 3.1899 2.0817e-06 -5.394e-08 v ǁVelocityǁ 0.0021212 49.12 9.2612 8.2819 v Pressure -5.8022e+05 2.304e+05 -1.2141e+05 -1.2896e+05 v TurbVisc 1.6157e-18 0.031351 0.00023307 0.00010312 v CourantNb 5.4485e-08 0.011801 0.00017327 4.9867e-06 v FourierNb 1.2473e-07 0.052695 0.00015781 8.3693e-07 v total_pressure -4.789e+05 3.3172e+05 -20088 -27632 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2517 0.12735 0.0033036 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 8.3609e-07 0.053429 0.00033109 5.8236e-06 INSTANT 0.876853000E-01 TIME STEP NUMBER 57051 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282716955E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.833970277E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.89073E-02 0.22906E+01 Friction velocity uk : 0.89073E-02 0.22906E+01 Dimensionless distance yplus : 0.85734E-02 0.22523E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -2.211895674e-03 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29659E+08 1 0.20878E-09 0.51823E+02 0.26597E+04 c Velocity[X] 0.29565E+02 c Velocity[Y] 0.22258E+02 c Velocity[Z] 0.81381E-06 c Pressure 0.18605E-03 265 0.79697E-04 0.10639E-02 0.68633E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -35.389 48.793 5.6002 7.9898 v Velocity[Y] -35.993 39.001 -0.20987 -0.19628 v Velocity[Z] -3.2147 3.19 2.0812e-06 -5.394e-08 v ǁVelocityǁ 0.0028397 49.13 9.2626 8.2822 v Pressure -5.8009e+05 2.308e+05 -1.1986e+05 -1.2804e+05 v TurbVisc 1.6595e-18 0.031364 0.00023313 0.00010324 v CourantNb 5.3987e-08 0.011802 0.00017328 4.9868e-06 v FourierNb 1.2474e-07 0.05273 0.00015783 8.3771e-07 v total_pressure -4.7877e+05 3.3212e+05 -18535 -26712 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2523 0.12739 0.0033046 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 8.3674e-07 0.053466 0.00033111 5.8245e-06 INSTANT 0.876854000E-01 TIME STEP NUMBER 57052 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282719420E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.834087368E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.66903E-02 0.22912E+01 Friction velocity uk : 0.66903E-02 0.22912E+01 Dimensionless distance yplus : 0.64395E-02 0.22529E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.714356887e-03 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29660E+08 1 0.20886E-09 0.51901E+02 0.26615E+04 c Velocity[X] 0.29610E+02 c Velocity[Y] 0.22291E+02 c Velocity[Z] 0.81110E-06 c Pressure 0.18483E-03 109 0.85812E-04 0.10561E-02 0.66372E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -35.4 48.803 5.6002 7.9899 v Velocity[Y] -36.002 39.012 -0.21002 -0.19673 v Velocity[Z] -3.215 3.1901 2.0808e-06 -5.394e-08 v ǁVelocityǁ 0.0028343 49.14 9.2641 8.2825 v Pressure -5.818e+05 2.3118e+05 -1.1832e+05 -1.272e+05 v TurbVisc 1.61e-18 0.031378 0.00023319 0.00010335 v CourantNb 5.1905e-08 0.011803 0.0001733 4.9869e-06 v FourierNb 1.2474e-07 0.052766 0.00015784 8.3849e-07 v total_pressure -4.8048e+05 3.3251e+05 -16999 -25880 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2529 0.12743 0.0033057 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 8.3739e-07 0.053504 0.00033114 5.8254e-06 INSTANT 0.876855000E-01 TIME STEP NUMBER 57053 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282721792E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.834211006E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11205E-01 0.22918E+01 Friction velocity uk : 0.11205E-01 0.22918E+01 Dimensionless distance yplus : 0.10785E-01 0.22535E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -9.818558251e-04 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29661E+08 1 0.20892E-09 0.51986E+02 0.26634E+04 c Velocity[X] 0.29648E+02 c Velocity[Y] 0.22338E+02 c Velocity[Z] 0.81322E-06 c Pressure 0.18435E-03 231 0.99500E-04 0.10526E-02 0.64165E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -35.412 48.813 5.6002 7.9899 v Velocity[Y] -36.012 39.023 -0.21017 -0.19719 v Velocity[Z] -3.2153 3.1902 2.0803e-06 -5.394e-08 v ǁVelocityǁ 0.0028297 49.15 9.2655 8.2829 v Pressure -5.8132e+05 2.316e+05 -1.1684e+05 -1.2659e+05 v TurbVisc 1.5951e-18 0.031392 0.00023326 0.00010346 v CourantNb 4.9706e-08 0.011804 0.00017331 4.987e-06 v FourierNb 1.2474e-07 0.052802 0.00015785 8.3926e-07 v total_pressure -4.7999e+05 3.3292e+05 -15515 -25261 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2535 0.12748 0.0033067 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 8.3805e-07 0.053542 0.00033116 5.8262e-06 INSTANT 0.876856000E-01 TIME STEP NUMBER 57054 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282724644E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.834342880E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.48296E-02 0.22924E+01 Friction velocity uk : 0.48296E-02 0.22924E+01 Dimensionless distance yplus : 0.46659E-02 0.22541E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -5.479139520e-06 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29663E+08 1 0.20901E-09 0.52036E+02 0.26645E+04 c Velocity[X] 0.29693E+02 c Velocity[Y] 0.22342E+02 c Velocity[Z] 0.81981E-06 c Pressure 0.18390E-03 338 0.84628E-04 0.10491E-02 0.60181E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -35.425 48.823 5.6003 7.9899 v Velocity[Y] -36.021 39.035 -0.21032 -0.19765 v Velocity[Z] -3.2156 3.1903 2.0799e-06 -5.394e-08 v ǁVelocityǁ 0.0028265 49.16 9.2669 8.2832 v Pressure -5.8268e+05 2.3199e+05 -1.1535e+05 -1.2571e+05 v TurbVisc 1.6362e-18 0.031405 0.00023332 0.00010358 v CourantNb 4.7516e-08 0.011806 0.00017332 4.9871e-06 v FourierNb 1.2474e-07 0.052838 0.00015787 8.4004e-07 v total_pressure -4.8135e+05 3.3331e+05 -14023 -24388 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2541 0.12752 0.0033076 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 8.387e-07 0.05358 0.00033118 5.8271e-06 INSTANT 0.876857000E-01 TIME STEP NUMBER 57055 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282727437E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.834486453E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.16828E-02 0.22930E+01 Friction velocity uk : 0.16828E-02 0.22930E+01 Dimensionless distance yplus : 0.16257E-02 0.22547E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 9.731501123e-04 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29664E+08 1 0.20908E-09 0.52127E+02 0.26666E+04 c Velocity[X] 0.29745E+02 c Velocity[Y] 0.22382E+02 c Velocity[Z] 0.82616E-06 c Pressure 0.17628E-03 9 0.59515E-04 0.10049E-02 0.44865E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -35.437 48.833 5.6003 7.99 v Velocity[Y] -36.03 39.046 -0.21047 -0.19811 v Velocity[Z] -3.2159 3.1904 2.0794e-06 -5.394e-08 v ǁVelocityǁ 0.0028336 49.171 9.2683 8.2836 v Pressure -5.8367e+05 2.3238e+05 -1.1389e+05 -1.2505e+05 v TurbVisc 1.638e-18 0.031419 0.00023338 0.00010369 v CourantNb 4.5287e-08 0.011807 0.00017333 4.9872e-06 v FourierNb 1.2474e-07 0.052874 0.00015788 8.4082e-07 v total_pressure -4.8235e+05 3.3371e+05 -12562 -23727 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2547 0.12756 0.0033086 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 8.3935e-07 0.053617 0.00033121 5.828e-06 INSTANT 0.876858000E-01 TIME STEP NUMBER 57056 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282730407E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.834641491E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.50547E-02 0.22937E+01 Friction velocity uk : 0.50547E-02 0.22937E+01 Dimensionless distance yplus : 0.49627E-02 0.22553E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 2.701406323e-03 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29665E+08 1 0.20914E-09 0.52203E+02 0.26684E+04 c Velocity[X] 0.29778E+02 c Velocity[Y] 0.22425E+02 c Velocity[Z] 0.82461E-06 c Pressure 0.17698E-03 306 0.80686E-04 0.10081E-02 0.66332E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -35.449 48.843 5.6003 7.99 v Velocity[Y] -36.04 39.058 -0.21062 -0.19857 v Velocity[Z] -3.2162 3.1905 2.079e-06 -5.394e-08 v ǁVelocityǁ 0.002816 49.181 9.2697 8.2839 v Pressure -5.8362e+05 2.3278e+05 -1.1243e+05 -1.2422e+05 v TurbVisc 1.6869e-18 0.031432 0.00023345 0.00010381 v CourantNb 4.2934e-08 0.011808 0.00017334 4.9873e-06 v FourierNb 1.2474e-07 0.052909 0.0001579 8.416e-07 v total_pressure -4.823e+05 3.3411e+05 -11109 -22894 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2553 0.1276 0.0033097 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 8.4001e-07 0.053655 0.00033123 5.8289e-06 INSTANT 0.876859000E-01 TIME STEP NUMBER 57057 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282733616E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.834806593E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.28978E-02 0.22943E+01 Friction velocity uk : 0.28978E-02 0.22943E+01 Dimensionless distance yplus : 0.28450E-02 0.22559E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 3.589199977e-03 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29667E+08 1 0.20922E-09 0.52284E+02 0.26702E+04 c Velocity[X] 0.29828E+02 c Velocity[Y] 0.22456E+02 c Velocity[Z] 0.82177E-06 c Pressure 0.17535E-03 429 0.86941E-04 0.99800E-03 0.66968E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -35.461 48.853 5.6003 7.9901 v Velocity[Y] -36.049 39.069 -0.21077 -0.19903 v Velocity[Z] -3.2166 3.1906 2.0785e-06 -5.394e-08 v ǁVelocityǁ 0.0026878 49.192 9.2711 8.2842 v Pressure -5.8531e+05 2.3316e+05 -1.1097e+05 -1.234e+05 v TurbVisc 1.6331e-18 0.031446 0.00023351 0.00010392 v CourantNb 4.0783e-08 0.01181 0.00017335 4.9874e-06 v FourierNb 1.2474e-07 0.052945 0.00015791 8.4238e-07 v total_pressure -4.8398e+05 3.3449e+05 -9649 -22073 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2559 0.12765 0.0033108 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 8.4067e-07 0.053692 0.00033126 5.8298e-06 INSTANT 0.876860000E-01 TIME STEP NUMBER 57058 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282736722E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.834978534E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12381E-01 0.22949E+01 Friction velocity uk : 0.12381E-01 0.22949E+01 Dimensionless distance yplus : 0.12156E-01 0.22566E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 4.833556631e-03 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29668E+08 1 0.20928E-09 0.52345E+02 0.26716E+04 c Velocity[X] 0.29863E+02 c Velocity[Y] 0.22482E+02 c Velocity[Z] 0.82112E-06 c Pressure 0.17460E-03 287 0.75534E-04 0.99294E-03 0.43727E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -35.473 48.863 5.6003 7.9901 v Velocity[Y] -36.059 39.081 -0.21092 -0.1995 v Velocity[Z] -3.2169 3.1907 2.0781e-06 -5.394e-08 v ǁVelocityǁ 0.0022372 49.202 9.2726 8.2846 v Pressure -5.8549e+05 2.3357e+05 -1.0962e+05 -1.2289e+05 v TurbVisc 1.6552e-18 0.031459 0.00023357 0.00010404 v CourantNb 3.8493e-08 0.011811 0.00017336 4.9875e-06 v FourierNb 1.2474e-07 0.05298 0.00015792 8.4316e-07 v total_pressure -4.8417e+05 3.3489e+05 -8292.7 -21560 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2566 0.1277 0.0033118 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 8.4133e-07 0.053729 0.00033128 5.8307e-06 INSTANT 0.876861000E-01 TIME STEP NUMBER 57059 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282740148E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.835157291E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10970E-01 0.22956E+01 Friction velocity uk : 0.10970E-01 0.22956E+01 Dimensionless distance yplus : 0.10717E-01 0.22572E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 6.387533498e-03 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29669E+08 1 0.20936E-09 0.52437E+02 0.26737E+04 c Velocity[X] 0.29912E+02 c Velocity[Y] 0.22525E+02 c Velocity[Z] 0.85220E-06 c Pressure 0.16752E-03 18 0.54213E-04 0.95189E-03 0.38232E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -35.485 48.874 5.6004 7.9902 v Velocity[Y] -36.068 39.092 -0.21107 -0.19996 v Velocity[Z] -3.2172 3.1908 2.0776e-06 -5.394e-08 v ǁVelocityǁ 0.0024063 49.213 9.274 8.2849 v Pressure -5.8559e+05 2.3396e+05 -1.0825e+05 -1.2232e+05 v TurbVisc 1.6533e-18 0.031473 0.00023364 0.00010415 v CourantNb 3.6187e-08 0.011813 0.00017337 4.9876e-06 v FourierNb 1.2474e-07 0.053015 0.00015794 8.4394e-07 v total_pressure -4.8426e+05 3.3529e+05 -6927.1 -20992 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2572 0.12774 0.0033128 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 8.4199e-07 0.053767 0.00033131 5.8315e-06 INSTANT 0.876862000E-01 TIME STEP NUMBER 57060 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282743869E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.835349821E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.83670E-02 0.22962E+01 Friction velocity uk : 0.83670E-02 0.22962E+01 Dimensionless distance yplus : 0.81743E-02 0.22578E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 8.695433850e-03 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29671E+08 1 0.20944E-09 0.52502E+02 0.26752E+04 c Velocity[X] 0.29959E+02 c Velocity[Y] 0.22543E+02 c Velocity[Z] 0.84203E-06 c Pressure 0.16744E-03 163 0.97324E-04 0.95069E-03 0.63926E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -35.498 48.884 5.6004 7.9902 v Velocity[Y] -36.078 39.104 -0.21122 -0.20043 v Velocity[Z] -3.2175 3.1909 2.0771e-06 -5.394e-08 v ǁVelocityǁ 0.002324 49.223 9.2754 8.2853 v Pressure -5.8667e+05 2.3437e+05 -1.0685e+05 -1.2131e+05 v TurbVisc 1.7429e-18 0.031486 0.0002337 0.00010426 v CourantNb 3.5496e-08 0.011814 0.00017338 4.9877e-06 v FourierNb 1.2474e-07 0.05305 0.00015795 8.4472e-07 v total_pressure -4.8534e+05 3.357e+05 -5521.7 -19980 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2578 0.12779 0.0033138 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 8.4265e-07 0.053803 0.00033133 5.8324e-06 INSTANT 0.876863000E-01 TIME STEP NUMBER 57061 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282747603E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.835554647E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.56043E-02 0.22968E+01 Friction velocity uk : 0.56043E-02 0.22968E+01 Dimensionless distance yplus : 0.54753E-02 0.22584E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 9.192259067e-03 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29672E+08 1 0.20951E-09 0.52582E+02 0.26770E+04 c Velocity[X] 0.30003E+02 c Velocity[Y] 0.22578E+02 c Velocity[Z] 0.83083E-06 c Pressure 0.16417E-03 304 0.81480E-04 0.93139E-03 0.43410E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -35.51 48.894 5.6004 7.9903 v Velocity[Y] -36.088 39.116 -0.21138 -0.20089 v Velocity[Z] -3.2178 3.191 2.0767e-06 -5.3941e-08 v ǁVelocityǁ 0.0022103 49.234 9.2768 8.2857 v Pressure -5.8766e+05 2.3476e+05 -1.0549e+05 -1.2065e+05 v TurbVisc 1.7346e-18 0.0315 0.00023377 0.00010438 v CourantNb 3.5573e-08 0.011815 0.00017339 4.9878e-06 v FourierNb 1.2474e-07 0.053085 0.00015796 8.455e-07 v total_pressure -4.8634e+05 3.3608e+05 -4168.9 -19322 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2584 0.12783 0.0033148 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 8.4331e-07 0.05384 0.00033136 5.8333e-06 INSTANT 0.876864000E-01 TIME STEP NUMBER 57062 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282751392E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.835764329E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.44713E-02 0.22975E+01 Friction velocity uk : 0.44713E-02 0.22975E+01 Dimensionless distance yplus : 0.43683E-02 0.22591E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.211410010e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29674E+08 1 0.20958E-09 0.52675E+02 0.26791E+04 c Velocity[X] 0.30054E+02 c Velocity[Y] 0.22621E+02 c Velocity[Z] 0.85740E-06 c Pressure 0.16012E-03 18 0.54422E-04 0.90770E-03 0.40245E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -35.522 48.905 5.6005 7.9904 v Velocity[Y] -36.097 39.128 -0.21153 -0.20135 v Velocity[Z] -3.2181 3.1911 2.0762e-06 -5.3941e-08 v ǁVelocityǁ 0.0021037 49.245 9.2782 8.286 v Pressure -5.8868e+05 2.3514e+05 -1.0418e+05 -1.2007e+05 v TurbVisc 1.1551e-18 0.031513 0.00023383 0.00010449 v CourantNb 3.5565e-08 0.011817 0.0001734 4.9879e-06 v FourierNb 1.2474e-07 0.05312 0.00015798 8.4628e-07 v total_pressure -4.8736e+05 3.3646e+05 -2851.5 -18742 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2591 0.12787 0.0033158 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 8.4398e-07 0.053877 0.00033138 5.8342e-06 INSTANT 0.876865000E-01 TIME STEP NUMBER 57063 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282755311E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.835981163E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.25269E-02 0.22982E+01 Friction velocity uk : 0.25269E-02 0.22982E+01 Dimensionless distance yplus : 0.24687E-02 0.22598E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.425772581e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29675E+08 1 0.20965E-09 0.52744E+02 0.26807E+04 c Velocity[X] 0.30097E+02 c Velocity[Y] 0.22646E+02 c Velocity[Z] 0.85064E-06 c Pressure 0.16028E-03 229 0.99685E-04 0.90784E-03 0.50113E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -35.535 48.915 5.6005 7.9904 v Velocity[Y] -36.107 39.139 -0.21168 -0.20182 v Velocity[Z] -3.2184 3.1912 2.0758e-06 -5.3941e-08 v ǁVelocityǁ 0.001919 49.256 9.2797 8.2864 v Pressure -5.8921e+05 2.3553e+05 -1.029e+05 -1.1932e+05 v TurbVisc 1.8699e-18 0.031527 0.0002339 0.00010461 v CourantNb 3.5503e-08 0.011818 0.00017341 4.9881e-06 v FourierNb 1.2474e-07 0.053153 0.00015799 8.4707e-07 v total_pressure -4.8789e+05 3.3686e+05 -1579.7 -17995 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2598 0.12792 0.0033167 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 8.4465e-07 0.053912 0.00033141 5.8351e-06 INSTANT 0.876866000E-01 TIME STEP NUMBER 57064 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282759387E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.836208550E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.40894E-02 0.22988E+01 Friction velocity uk : 0.40894E-02 0.22988E+01 Dimensionless distance yplus : 0.39952E-02 0.22604E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.503223025e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29676E+08 1 0.20972E-09 0.52823E+02 0.26825E+04 c Velocity[X] 0.30139E+02 c Velocity[Y] 0.22684E+02 c Velocity[Z] 0.83938E-06 c Pressure 0.15668E-03 46 0.84036E-04 0.88673E-03 0.33641E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -35.547 48.926 5.6005 7.9905 v Velocity[Y] -36.117 39.151 -0.21183 -0.20229 v Velocity[Z] -3.2187 3.1913 2.0753e-06 -5.3941e-08 v ǁVelocityǁ 0.0014354 49.266 9.2811 8.2868 v Pressure -5.8972e+05 2.3592e+05 -1.0166e+05 -1.1883e+05 v TurbVisc 9.8104e-19 0.03154 0.00023396 0.00010472 v CourantNb 3.5469e-08 0.011819 0.00017342 4.9882e-06 v FourierNb 1.2474e-07 0.053187 0.00015801 8.4785e-07 v total_pressure -4.8839e+05 3.3725e+05 -339.97 -17508 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2604 0.12796 0.0033176 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 8.4532e-07 0.053949 0.00033143 5.836e-06 INSTANT 0.876867000E-01 TIME STEP NUMBER 57065 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282763607E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.836444795E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.33625E-02 0.22995E+01 Friction velocity uk : 0.33625E-02 0.22995E+01 Dimensionless distance yplus : 0.32515E-02 0.22610E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.793448469e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29678E+08 1 0.20980E-09 0.52918E+02 0.26847E+04 c Velocity[X] 0.30177E+02 c Velocity[Y] 0.22741E+02 c Velocity[Z] 0.87706E-06 c Pressure 0.15216E-03 16 0.55306E-04 0.86049E-03 0.38871E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -35.56 48.937 5.6006 7.9906 v Velocity[Y] -36.127 39.163 -0.21198 -0.20276 v Velocity[Z] -3.219 3.1914 2.0749e-06 -5.3941e-08 v ǁVelocityǁ 0.00098808 49.277 9.2825 8.2871 v Pressure -5.9005e+05 2.3632e+05 -1.0042e+05 -1.1832e+05 v TurbVisc 1.1969e-18 0.031554 0.00023402 0.00010484 v CourantNb 3.5481e-08 0.011821 0.00017344 4.9883e-06 v FourierNb 1.2474e-07 0.053221 0.00015802 8.4863e-07 v total_pressure -4.8872e+05 3.3764e+05 904.55 -16998 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.261 0.128 0.0033186 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 8.4598e-07 0.053985 0.00033146 5.8369e-06 INSTANT 0.876868000E-01 TIME STEP NUMBER 57066 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282768047E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.836690006E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10897E-01 0.23002E+01 Friction velocity uk : 0.10897E-01 0.23002E+01 Dimensionless distance yplus : 0.10646E-01 0.22617E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 2.129492139e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29679E+08 1 0.20987E-09 0.52993E+02 0.26863E+04 c Velocity[X] 0.30238E+02 c Velocity[Y] 0.22754E+02 c Velocity[Z] 0.85960E-06 c Pressure 0.15239E-03 49 0.77477E-04 0.86106E-03 0.74832E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -35.573 48.947 5.6006 7.9906 v Velocity[Y] -36.137 39.175 -0.21213 -0.20322 v Velocity[Z] -3.2193 3.1915 2.0744e-06 -5.3941e-08 v ǁVelocityǁ 0.00056391 49.288 9.284 8.2875 v Pressure -5.9167e+05 2.367e+05 -99167 -1.1734e+05 v TurbVisc 1.3958e-18 0.031567 0.00023409 0.00010495 v CourantNb 3.5217e-08 0.011822 0.00017345 4.9884e-06 v FourierNb 1.2474e-07 0.053254 0.00015803 8.4942e-07 v total_pressure -4.9034e+05 3.3803e+05 2157.8 -16012 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2617 0.12805 0.0033197 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 8.4666e-07 0.054019 0.00033148 5.8378e-06 INSTANT 0.876869000E-01 TIME STEP NUMBER 57067 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282772372E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.836944502E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.14727E-01 0.23008E+01 Friction velocity uk : 0.14727E-01 0.23008E+01 Dimensionless distance yplus : 0.14388E-01 0.22624E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 2.209252925e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29681E+08 1 0.20994E-09 0.53085E+02 0.26885E+04 c Velocity[X] 0.30279E+02 c Velocity[Y] 0.22807E+02 c Velocity[Z] 0.86936E-06 c Pressure 0.15009E-03 804 0.81563E-04 0.84740E-03 0.51570E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -35.585 48.958 5.6006 7.9907 v Velocity[Y] -36.147 39.187 -0.21229 -0.20369 v Velocity[Z] -3.2197 3.1916 2.074e-06 -5.3941e-08 v ǁVelocityǁ 0.00043555 49.299 9.2854 8.2879 v Pressure -5.9141e+05 2.371e+05 -98006 -1.1691e+05 v TurbVisc 1.3841e-18 0.031581 0.00023416 0.00010507 v CourantNb 3.5358e-08 0.011823 0.00017346 4.9885e-06 v FourierNb 1.2474e-07 0.053287 0.00015805 8.502e-07 v total_pressure -4.9009e+05 3.3843e+05 3319.1 -15588 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2624 0.1281 0.0033207 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 8.4733e-07 0.054054 0.00033151 5.8387e-06 INSTANT 0.876870000E-01 TIME STEP NUMBER 57068 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282777146E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.837203798E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.97769E-02 0.23015E+01 Friction velocity uk : 0.97769E-02 0.23015E+01 Dimensionless distance yplus : 0.94141E-02 0.22631E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 2.531196644e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29682E+08 1 0.21003E-09 0.53168E+02 0.26904E+04 c Velocity[X] 0.30333E+02 c Velocity[Y] 0.22835E+02 c Velocity[Z] 0.85355E-06 c Pressure 0.14876E-03 107 0.95486E-04 0.83921E-03 0.64700E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -35.598 48.969 5.6007 7.9908 v Velocity[Y] -36.157 39.199 -0.21244 -0.20416 v Velocity[Z] -3.22 3.1917 2.0735e-06 -5.3941e-08 v ǁVelocityǁ 0.00070258 49.31 9.2869 8.2883 v Pressure -5.9324e+05 2.3748e+05 -96859 -1.1628e+05 v TurbVisc 1.5748e-18 0.031594 0.00023422 0.00010518 v CourantNb 3.5368e-08 0.011825 0.00017347 4.9886e-06 v FourierNb 1.2474e-07 0.053319 0.00015806 8.5099e-07 v total_pressure -4.9191e+05 3.3881e+05 4465.9 -14959 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2631 0.12814 0.0033217 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 8.48e-07 0.054089 0.00033153 5.8396e-06 INSTANT 0.876871000E-01 TIME STEP NUMBER 57069 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282781709E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.837471549E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.46293E-02 0.23022E+01 Friction velocity uk : 0.46293E-02 0.23022E+01 Dimensionless distance yplus : 0.44575E-02 0.22637E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 2.761034148e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29684E+08 1 0.21009E-09 0.53231E+02 0.26917E+04 c Velocity[X] 0.30370E+02 c Velocity[Y] 0.22861E+02 c Velocity[Z] 0.85810E-06 c Pressure 0.14746E-03 178 0.80808E-04 0.83118E-03 0.41131E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -35.611 48.98 5.6007 7.9909 v Velocity[Y] -36.167 39.211 -0.21259 -0.20463 v Velocity[Z] -3.2203 3.1918 2.0731e-06 -5.3941e-08 v ǁVelocityǁ 0.0011137 49.322 9.2883 8.2887 v Pressure -5.9342e+05 2.3787e+05 -95769 -1.1589e+05 v TurbVisc 1.5814e-18 0.031608 0.00023429 0.0001053 v CourantNb 3.5332e-08 0.011826 0.00017348 4.9888e-06 v FourierNb 1.2474e-07 0.053351 0.00015808 8.5178e-07 v total_pressure -4.9209e+05 3.392e+05 5556.5 -14568 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2637 0.12819 0.0033227 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 8.4868e-07 0.054124 0.00033156 5.8405e-06 INSTANT 0.876872000E-01 TIME STEP NUMBER 57070 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282786550E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.837749620E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.79330E-02 0.23029E+01 Friction velocity uk : 0.79330E-02 0.23029E+01 Dimensionless distance yplus : 0.76386E-02 0.22644E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 3.019821915e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29685E+08 1 0.21017E-09 0.53329E+02 0.26940E+04 c Velocity[X] 0.30419E+02 c Velocity[Y] 0.22910E+02 c Velocity[Z] 0.88775E-06 c Pressure 0.13785E-03 12 0.55994E-04 0.77640E-03 0.31721E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -35.623 48.991 5.6008 7.991 v Velocity[Y] -36.177 39.223 -0.21275 -0.2051 v Velocity[Z] -3.2206 3.1919 2.0726e-06 -5.3941e-08 v ǁVelocityǁ 0.0011115 49.333 9.2897 8.289 v Pressure -5.9358e+05 2.3827e+05 -94708 -1.1549e+05 v TurbVisc 1.6618e-18 0.031621 0.00023435 0.00010542 v CourantNb 3.5281e-08 0.011828 0.00017349 4.9889e-06 v FourierNb 1.2474e-07 0.053383 0.00015809 8.5256e-07 v total_pressure -4.9225e+05 3.3959e+05 6616.6 -14165 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2644 0.12823 0.0033237 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 8.4935e-07 0.054158 0.00033158 5.8415e-06 INSTANT 0.876873000E-01 TIME STEP NUMBER 57071 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282791647E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.838036688E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.76399E-02 0.23037E+01 Friction velocity uk : 0.76399E-02 0.23037E+01 Dimensionless distance yplus : 0.73563E-02 0.22652E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 3.377612195e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29687E+08 1 0.21025E-09 0.53404E+02 0.26957E+04 c Velocity[X] 0.30472E+02 c Velocity[Y] 0.22933E+02 c Velocity[Z] 0.86468E-06 c Pressure 0.13801E-03 36 0.77129E-04 0.77666E-03 0.70632E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -35.636 49.002 5.6008 7.991 v Velocity[Y] -36.187 39.235 -0.2129 -0.20557 v Velocity[Z] -3.2209 3.192 2.0722e-06 -5.3941e-08 v ǁVelocityǁ 0.001077 49.344 9.2912 8.2894 v Pressure -5.9538e+05 2.3866e+05 -93581 -1.146e+05 v TurbVisc 1.1691e-18 0.031635 0.00023442 0.00010553 v CourantNb 3.4843e-08 0.011829 0.0001735 4.989e-06 v FourierNb 1.2474e-07 0.053414 0.00015811 8.5335e-07 v total_pressure -4.9405e+05 3.3998e+05 7744.4 -13277 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2652 0.12828 0.0033247 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 8.5003e-07 0.054191 0.00033161 5.8424e-06 INSTANT 0.876874000E-01 TIME STEP NUMBER 57072 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282796549E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.838333378E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.71660E-02 0.23043E+01 Friction velocity uk : 0.71660E-02 0.23043E+01 Dimensionless distance yplus : 0.69001E-02 0.22658E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 3.498159761e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29689E+08 1 0.21031E-09 0.53499E+02 0.26978E+04 c Velocity[X] 0.30512E+02 c Velocity[Y] 0.22987E+02 c Velocity[Z] 0.86621E-06 c Pressure 0.13570E-03 353 0.81956E-04 0.76304E-03 0.50026E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -35.649 49.013 5.6009 7.9911 v Velocity[Y] -36.197 39.247 -0.21306 -0.20604 v Velocity[Z] -3.2212 3.1921 2.0717e-06 -5.3941e-08 v ǁVelocityǁ 0.001756 49.355 9.2926 8.2898 v Pressure -5.9515e+05 2.3905e+05 -92586 -1.1428e+05 v TurbVisc 1.5887e-18 0.031648 0.00023449 0.00010565 v CourantNb 3.2109e-08 0.01183 0.00017351 4.9891e-06 v FourierNb 1.2474e-07 0.053445 0.00015812 8.5414e-07 v total_pressure -4.9383e+05 3.4037e+05 8739 -12953 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2658 0.12832 0.0033258 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 8.5071e-07 0.054224 0.00033163 5.8433e-06 INSTANT 0.876875000E-01 TIME STEP NUMBER 57073 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282801868E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.838631407E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15349E-01 0.23051E+01 Friction velocity uk : 0.15349E-01 0.23051E+01 Dimensionless distance yplus : 0.14779E-01 0.22665E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 3.844774351e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29690E+08 1 0.21040E-09 0.53584E+02 0.26997E+04 c Velocity[X] 0.30573E+02 c Velocity[Y] 0.23011E+02 c Velocity[Z] 0.86769E-06 c Pressure 0.13436E-03 42 0.95966E-04 0.75491E-03 0.65282E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -35.662 49.024 5.601 7.9912 v Velocity[Y] -36.207 39.26 -0.21321 -0.20651 v Velocity[Z] -3.2215 3.1922 2.0713e-06 -5.3941e-08 v ǁVelocityǁ 0.0018401 49.367 9.2941 8.2902 v Pressure -5.9694e+05 2.3942e+05 -91584 -1.1367e+05 v TurbVisc 1.6804e-18 0.031662 0.00023455 0.00010576 v CourantNb 2.9719e-08 0.011832 0.00017353 4.9893e-06 v FourierNb 1.2474e-07 0.053475 0.00015813 8.5492e-07 v total_pressure -4.9561e+05 3.4075e+05 9740.5 -12346 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2665 0.12837 0.0033268 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 8.5139e-07 0.054257 0.00033166 5.8442e-06 INSTANT 0.876876000E-01 TIME STEP NUMBER 57074 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282807003E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.838936437E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.75038E-02 0.23058E+01 Friction velocity uk : 0.75038E-02 0.23058E+01 Dimensionless distance yplus : 0.73464E-02 0.22672E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 4.091392812e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29692E+08 1 0.21046E-09 0.53648E+02 0.27011E+04 c Velocity[X] 0.30608E+02 c Velocity[Y] 0.23040E+02 c Velocity[Z] 0.86935E-06 c Pressure 0.13321E-03 259 0.81262E-04 0.74783E-03 0.40001E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -35.675 49.035 5.601 7.9913 v Velocity[Y] -36.217 39.272 -0.21337 -0.20699 v Velocity[Z] -3.2218 3.1923 2.0708e-06 -5.3942e-08 v ǁVelocityǁ 0.0020344 49.378 9.2955 8.2906 v Pressure -5.9716e+05 2.3981e+05 -90649 -1.1337e+05 v TurbVisc 1.7212e-18 0.031675 0.00023462 0.00010588 v CourantNb 2.9746e-08 0.011833 0.00017354 4.9894e-06 v FourierNb 1.2475e-07 0.053505 0.00015815 8.5571e-07 v total_pressure -4.9583e+05 3.4113e+05 10676 -12045 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2672 0.12841 0.0033278 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 8.5208e-07 0.05429 0.00033169 5.8451e-06 INSTANT 0.876877000E-01 TIME STEP NUMBER 57075 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282812377E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.839251555E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.59265E-02 0.23065E+01 Friction velocity uk : 0.59265E-02 0.23065E+01 Dimensionless distance yplus : 0.58022E-02 0.22680E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 4.366805204e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29693E+08 1 0.21054E-09 0.53746E+02 0.27034E+04 c Velocity[X] 0.30656E+02 c Velocity[Y] 0.23090E+02 c Velocity[Z] 0.89206E-06 c Pressure 0.12262E-03 9 0.56056E-04 0.68781E-03 0.27567E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -35.688 49.046 5.6011 7.9914 v Velocity[Y] -36.228 39.284 -0.21352 -0.20746 v Velocity[Z] -3.2221 3.1924 2.0704e-06 -5.3942e-08 v ǁVelocityǁ 0.0022811 49.39 9.297 8.291 v Pressure -5.9734e+05 2.402e+05 -89770 -1.1308e+05 v TurbVisc 1.7546e-18 0.031688 0.00023469 0.00010599 v CourantNb 2.9924e-08 0.011835 0.00017355 4.9895e-06 v FourierNb 1.2475e-07 0.053535 0.00015816 8.565e-07 v total_pressure -4.9601e+05 3.4152e+05 11555 -11754 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.268 0.12845 0.0033287 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 8.5276e-07 0.054322 0.00033171 5.846e-06 INSTANT 0.876878000E-01 TIME STEP NUMBER 57076 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282817989E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.839574067E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.41191E-02 0.23073E+01 Friction velocity uk : 0.41191E-02 0.23073E+01 Dimensionless distance yplus : 0.39876E-02 0.22687E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 4.729794683e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29695E+08 1 0.21062E-09 0.53824E+02 0.27051E+04 c Velocity[X] 0.30716E+02 c Velocity[Y] 0.23107E+02 c Velocity[Z] 0.88154E-06 c Pressure 0.12317E-03 621 0.77718E-04 0.69032E-03 0.71366E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -35.701 49.057 5.6011 7.9915 v Velocity[Y] -36.238 39.296 -0.21368 -0.20793 v Velocity[Z] -3.2224 3.1925 2.0699e-06 -5.3942e-08 v ǁVelocityǁ 0.0024312 49.401 9.2985 8.2914 v Pressure -5.9908e+05 2.4059e+05 -88776 -1.122e+05 v TurbVisc 1.7246e-18 0.031702 0.00023475 0.00010611 v CourantNb 3.0029e-08 0.011836 0.00017356 4.9897e-06 v FourierNb 1.2475e-07 0.053564 0.00015818 8.5729e-07 v total_pressure -4.9775e+05 3.4191e+05 12549 -10870 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2687 0.12849 0.0033297 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 8.5344e-07 0.054354 0.00033174 5.847e-06 INSTANT 0.876879000E-01 TIME STEP NUMBER 57077 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282823451E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.839906039E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.77417E-02 0.23080E+01 Friction velocity uk : 0.77417E-02 0.23080E+01 Dimensionless distance yplus : 0.74946E-02 0.22694E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 4.858496185e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29697E+08 1 0.21069E-09 0.53920E+02 0.27073E+04 c Velocity[X] 0.30750E+02 c Velocity[Y] 0.23170E+02 c Velocity[Z] 0.88493E-06 c Pressure 0.12097E-03 82 0.82825E-04 0.67746E-03 0.49177E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -35.715 49.069 5.6012 7.9916 v Velocity[Y] -36.249 39.309 -0.21383 -0.20841 v Velocity[Z] -3.2227 3.1926 2.0695e-06 -5.3942e-08 v ǁVelocityǁ 0.0023788 49.413 9.2999 8.2918 v Pressure -5.9896e+05 2.4097e+05 -88016 -1.1216e+05 v TurbVisc 1.7715e-18 0.031715 0.00023482 0.00010623 v CourantNb 2.8884e-08 0.011838 0.00017357 4.9898e-06 v FourierNb 1.2475e-07 0.053593 0.00015819 8.5808e-07 v total_pressure -4.9763e+05 3.423e+05 13309 -10838 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2694 0.12854 0.0033308 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 8.5413e-07 0.054386 0.00033176 5.8479e-06 INSTANT 0.876880000E-01 TIME STEP NUMBER 57078 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282829226E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.840238350E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11683E-01 0.23087E+01 Friction velocity uk : 0.11683E-01 0.23087E+01 Dimensionless distance yplus : 0.11327E-01 0.22702E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 5.182677377e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29698E+08 1 0.21078E-09 0.54005E+02 0.27092E+04 c Velocity[X] 0.30811E+02 c Velocity[Y] 0.23194E+02 c Velocity[Z] 0.88510E-06 c Pressure 0.11984E-03 33 0.97148E-04 0.67054E-03 0.64970E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -35.728 49.08 5.6013 7.9917 v Velocity[Y] -36.259 39.321 -0.21399 -0.20889 v Velocity[Z] -3.223 3.1927 2.069e-06 -5.3942e-08 v ǁVelocityǁ 0.0023348 49.424 9.3014 8.2922 v Pressure -6.0079e+05 2.4135e+05 -87168 -1.116e+05 v TurbVisc 1.8862e-18 0.031729 0.00023489 0.00010634 v CourantNb 2.5834e-08 0.011839 0.00017359 4.9899e-06 v FourierNb 1.2475e-07 0.053622 0.00015821 8.5887e-07 v total_pressure -4.9947e+05 3.4267e+05 14157 -10279 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2702 0.12859 0.0033319 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 8.5482e-07 0.054417 0.00033179 5.8488e-06 INSTANT 0.876881000E-01 TIME STEP NUMBER 57079 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282834820E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.840580116E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.98114E-02 0.23095E+01 Friction velocity uk : 0.98114E-02 0.23095E+01 Dimensionless distance yplus : 0.94508E-02 0.22709E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 5.433941928e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29700E+08 1 0.21084E-09 0.54069E+02 0.27105E+04 c Velocity[X] 0.30849E+02 c Velocity[Y] 0.23220E+02 c Velocity[Z] 0.89183E-06 c Pressure 0.11908E-03 185 0.82245E-04 0.66576E-03 0.37299E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -35.741 49.091 5.6014 7.9918 v Velocity[Y] -36.269 39.334 -0.21415 -0.20936 v Velocity[Z] -3.2233 3.1928 2.0685e-06 -5.3942e-08 v ǁVelocityǁ 0.0023006 49.436 9.3029 8.2926 v Pressure -6.0097e+05 2.4173e+05 -86413 -1.1139e+05 v TurbVisc 1.8353e-18 0.031742 0.00023496 0.00010646 v CourantNb 2.2697e-08 0.01184 0.0001736 4.9901e-06 v FourierNb 1.2475e-07 0.05365 0.00015822 8.5967e-07 v total_pressure -4.9965e+05 3.4305e+05 14912 -10061 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2709 0.12863 0.0033328 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 8.5551e-07 0.054448 0.00033182 5.8497e-06 INSTANT 0.876882000E-01 TIME STEP NUMBER 57080 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282840658E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.840929397E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.24006E-02 0.23103E+01 Friction velocity uk : 0.24006E-02 0.23103E+01 Dimensionless distance yplus : 0.23124E-02 0.22717E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 5.692098689e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29702E+08 1 0.21092E-09 0.54168E+02 0.27128E+04 c Velocity[X] 0.30894E+02 c Velocity[Y] 0.23274E+02 c Velocity[Z] 0.92191E-06 c Pressure 0.10734E-03 13 0.56249E-04 0.59962E-03 0.24765E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -35.754 49.103 5.6014 7.9919 v Velocity[Y] -36.28 39.346 -0.21431 -0.20984 v Velocity[Z] -3.2236 3.1929 2.0681e-06 -5.3942e-08 v ǁVelocityǁ 0.0022278 49.448 9.3043 8.293 v Pressure -6.0121e+05 2.4211e+05 -85744 -1.112e+05 v TurbVisc 1.8487e-18 0.031756 0.00023502 0.00010657 v CourantNb 1.9515e-08 0.011842 0.00017361 4.9902e-06 v FourierNb 1.2475e-07 0.053678 0.00015823 8.6046e-07 v total_pressure -4.9988e+05 3.4344e+05 15581 -9872.5 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2717 0.12867 0.0033337 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 8.562e-07 0.054479 0.00033184 5.8507e-06 INSTANT 0.876883000E-01 TIME STEP NUMBER 57081 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282846710E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.841285050E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.61897E-02 0.23111E+01 Friction velocity uk : 0.61897E-02 0.23111E+01 Dimensionless distance yplus : 0.59997E-02 0.22724E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 6.026273518e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29703E+08 1 0.21100E-09 0.54247E+02 0.27145E+04 c Velocity[X] 0.30955E+02 c Velocity[Y] 0.23292E+02 c Velocity[Z] 0.91005E-06 c Pressure 0.10866E-03 44 0.78276E-04 0.60647E-03 0.63492E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -35.768 49.114 5.6015 7.992 v Velocity[Y] -36.29 39.359 -0.21447 -0.21032 v Velocity[Z] -3.224 3.193 2.0676e-06 -5.3942e-08 v ǁVelocityǁ 0.0020031 49.459 9.3058 8.2934 v Pressure -6.0299e+05 2.4249e+05 -84902 -1.105e+05 v TurbVisc 1.8562e-18 0.031769 0.00023509 0.00010669 v CourantNb 1.645e-08 0.011843 0.00017362 4.9903e-06 v FourierNb 1.2475e-07 0.053706 0.00015825 8.6125e-07 v total_pressure -5.0166e+05 3.4382e+05 16423 -9178.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2724 0.12873 0.003335 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 8.5689e-07 0.05451 0.00033187 5.8516e-06 INSTANT 0.876884000E-01 TIME STEP NUMBER 57082 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282852553E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.841648860E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.59599E-02 0.23118E+01 Friction velocity uk : 0.59599E-02 0.23118E+01 Dimensionless distance yplus : 0.57479E-02 0.22732E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 6.106449921e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29705E+08 1 0.21107E-09 0.54344E+02 0.27167E+04 c Velocity[X] 0.30996E+02 c Velocity[Y] 0.23348E+02 c Velocity[Z] 0.90495E-06 c Pressure 0.10668E-03 79 0.83319E-04 0.59494E-03 0.47908E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -35.781 49.126 5.6016 7.9921 v Velocity[Y] -36.301 39.371 -0.21462 -0.2108 v Velocity[Z] -3.2243 3.1931 2.0672e-06 -5.3942e-08 v ǁVelocityǁ 0.0022686 49.471 9.3073 8.2938 v Pressure -6.0276e+05 2.4288e+05 -84299 -1.1037e+05 v TurbVisc 1.7028e-18 0.031782 0.00023516 0.00010681 v CourantNb 1.2981e-08 0.011845 0.00017363 4.9905e-06 v FourierNb 1.2475e-07 0.053733 0.00015826 8.6205e-07 v total_pressure -5.0143e+05 3.442e+05 17026 -9040.8 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2732 0.12877 0.0033361 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 8.5759e-07 0.05454 0.0003319 5.8525e-06 INSTANT 0.876885000E-01 TIME STEP NUMBER 57083 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282858796E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.842013703E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.14678E-01 0.23126E+01 Friction velocity uk : 0.14678E-01 0.23126E+01 Dimensionless distance yplus : 0.14249E-01 0.22739E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 6.405357948e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29707E+08 1 0.21116E-09 0.54430E+02 0.27186E+04 c Velocity[X] 0.31052E+02 c Velocity[Y] 0.23378E+02 c Velocity[Z] 0.90149E-06 c Pressure 0.10620E-03 33 0.97534E-04 0.59179E-03 0.59300E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -35.795 49.137 5.6017 7.9922 v Velocity[Y] -36.312 39.384 -0.21478 -0.21127 v Velocity[Z] -3.2246 3.1932 2.0667e-06 -5.3942e-08 v ǁVelocityǁ 0.0022844 49.483 9.3087 8.2943 v Pressure -6.047e+05 2.4325e+05 -83673 -1.1001e+05 v TurbVisc 1.7522e-18 0.031796 0.00023523 0.00010692 v CourantNb 1.1323e-08 0.011846 0.00017365 4.9906e-06 v FourierNb 1.2475e-07 0.05376 0.00015828 8.6284e-07 v total_pressure -5.0337e+05 3.4457e+05 17652 -8690 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2739 0.12883 0.0033375 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 8.5828e-07 0.05457 0.00033192 5.8535e-06 INSTANT 0.876886000E-01 TIME STEP NUMBER 57084 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282864772E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.842383838E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.41549E-02 0.23134E+01 Friction velocity uk : 0.41549E-02 0.23134E+01 Dimensionless distance yplus : 0.40336E-02 0.22747E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 6.615277097e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29708E+08 1 0.21123E-09 0.54493E+02 0.27200E+04 c Velocity[X] 0.31093E+02 c Velocity[Y] 0.23400E+02 c Velocity[Z] 0.91000E-06 c Pressure 0.10606E-03 520 0.82695E-04 0.59052E-03 0.34960E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -35.808 49.149 5.6018 7.9923 v Velocity[Y] -36.322 39.397 -0.21494 -0.21175 v Velocity[Z] -3.2249 3.1933 2.0663e-06 -5.3942e-08 v ǁVelocityǁ 0.0021496 49.495 9.3102 8.2947 v Pressure -6.0484e+05 2.4362e+05 -83096 -1.0986e+05 v TurbVisc 1.7986e-18 0.031809 0.0002353 0.00010704 v CourantNb 1.1364e-08 0.011848 0.00017366 4.9908e-06 v FourierNb 1.2475e-07 0.053787 0.00015829 8.6363e-07 v total_pressure -5.0351e+05 3.4495e+05 18229 -8539.8 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2747 0.12889 0.003339 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 8.5898e-07 0.0546 0.00033195 5.8544e-06 INSTANT 0.876887000E-01 TIME STEP NUMBER 57085 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282871008E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.842761236E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.40507E-02 0.23142E+01 Friction velocity uk : 0.40507E-02 0.23142E+01 Dimensionless distance yplus : 0.39468E-02 0.22755E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 6.818433539e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29710E+08 1 0.21131E-09 0.54593E+02 0.27222E+04 c Velocity[X] 0.31131E+02 c Velocity[Y] 0.23462E+02 c Velocity[Z] 0.92330E-06 c Pressure 0.93370E-04 7 0.57058E-04 0.51942E-03 0.24143E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -35.822 49.161 5.6018 7.9924 v Velocity[Y] -36.333 39.409 -0.21511 -0.21224 v Velocity[Z] -3.2252 3.1934 2.0658e-06 -5.3942e-08 v ǁVelocityǁ 0.001676 49.507 9.3117 8.2951 v Pressure -6.052e+05 2.44e+05 -82673 -1.0985e+05 v TurbVisc 1.8553e-18 0.031822 0.00023537 0.00010716 v CourantNb 1.1406e-08 0.011849 0.00017367 4.9909e-06 v FourierNb 1.2475e-07 0.053814 0.00015831 8.6443e-07 v total_pressure -5.0387e+05 3.4532e+05 18652 -8528.9 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2755 0.12896 0.0033406 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 8.5968e-07 0.05463 0.00033198 5.8553e-06 INSTANT 0.876888000E-01 TIME STEP NUMBER 57086 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282877378E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.843143199E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.72349E-02 0.23150E+01 Friction velocity uk : 0.72349E-02 0.23150E+01 Dimensionless distance yplus : 0.70235E-02 0.22763E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 7.156676492e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29712E+08 1 0.21139E-09 0.54673E+02 0.27240E+04 c Velocity[X] 0.31195E+02 c Velocity[Y] 0.23478E+02 c Velocity[Z] 0.92015E-06 c Pressure 0.95801E-04 44 0.79092E-04 0.53250E-03 0.57411E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -35.835 49.172 5.6019 7.9926 v Velocity[Y] -36.344 39.422 -0.21527 -0.21272 v Velocity[Z] -3.2255 3.1935 2.0654e-06 -5.3943e-08 v ǁVelocityǁ 0.002158 49.519 9.3132 8.2955 v Pressure -6.0694e+05 2.4438e+05 -81987 -1.0931e+05 v TurbVisc 1.9277e-18 0.031836 0.00023544 0.00010727 v CourantNb 1.1213e-08 0.011851 0.00017368 4.9911e-06 v FourierNb 1.2475e-07 0.05384 0.00015832 8.6522e-07 v total_pressure -5.0561e+05 3.457e+05 19338 -7984.6 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2763 0.12904 0.0033424 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 8.6038e-07 0.054659 0.000332 5.8563e-06 INSTANT 0.876889000E-01 TIME STEP NUMBER 57087 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282883575E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.843539323E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12493E-01 0.23157E+01 Friction velocity uk : 0.12493E-01 0.23157E+01 Dimensionless distance yplus : 0.12128E-01 0.22770E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 7.060332015e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29714E+08 1 0.21146E-09 0.54769E+02 0.27262E+04 c Velocity[X] 0.31237E+02 c Velocity[Y] 0.23532E+02 c Velocity[Z] 0.92601E-06 c Pressure 0.94613E-04 70 0.84145E-04 0.52546E-03 0.47396E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -35.849 49.184 5.602 7.9927 v Velocity[Y] -36.355 39.435 -0.21543 -0.2132 v Velocity[Z] -3.2258 3.1936 2.0649e-06 -5.3943e-08 v ǁVelocityǁ 0.0024901 49.531 9.3147 8.2959 v Pressure -6.067e+05 2.4476e+05 -81601 -1.0925e+05 v TurbVisc 1.8949e-18 0.031849 0.0002355 0.00010739 v CourantNb 1.4872e-08 0.011852 0.0001737 4.9912e-06 v FourierNb 1.2475e-07 0.053867 0.00015834 8.6602e-07 v total_pressure -5.0537e+05 3.4608e+05 19724 -7924.9 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.277 0.12911 0.003344 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 8.6108e-07 0.054689 0.00033203 5.8572e-06 INSTANT 0.876890000E-01 TIME STEP NUMBER 57088 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282890149E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.843925525E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12733E-01 0.23166E+01 Friction velocity uk : 0.12733E-01 0.23166E+01 Dimensionless distance yplus : 0.12281E-01 0.22778E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 7.344586748e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29715E+08 1 0.21156E-09 0.54855E+02 0.27281E+04 c Velocity[X] 0.31293E+02 c Velocity[Y] 0.23563E+02 c Velocity[Z] 0.92054E-06 c Pressure 0.95051E-04 133 0.98316E-04 0.52745E-03 0.57367E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -35.863 49.196 5.6021 7.9928 v Velocity[Y] -36.365 39.447 -0.21559 -0.21368 v Velocity[Z] -3.2261 3.1937 2.0645e-06 -5.3943e-08 v ǁVelocityǁ 0.0025753 49.543 9.3161 8.2964 v Pressure -6.0869e+05 2.4512e+05 -81176 -1.0902e+05 v TurbVisc 1.9565e-18 0.031862 0.00023557 0.00010751 v CourantNb 1.8555e-08 0.011854 0.00017371 4.9913e-06 v FourierNb 1.2475e-07 0.053893 0.00015835 8.6682e-07 v total_pressure -5.0736e+05 3.4645e+05 20149 -7692.8 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2778 0.12919 0.0033457 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 8.6178e-07 0.054718 0.00033206 5.8582e-06 INSTANT 0.876891000E-01 TIME STEP NUMBER 57089 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282896425E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.844321112E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15125E-01 0.23174E+01 Friction velocity uk : 0.15125E-01 0.23174E+01 Dimensionless distance yplus : 0.14588E-01 0.22786E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 7.496027231e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29717E+08 1 0.21162E-09 0.54918E+02 0.27294E+04 c Velocity[X] 0.31329E+02 c Velocity[Y] 0.23589E+02 c Velocity[Z] 0.92430E-06 c Pressure 0.95914E-04 144 0.83223E-04 0.53179E-03 0.34389E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -35.877 49.208 5.6022 7.9929 v Velocity[Y] -36.376 39.46 -0.21575 -0.21416 v Velocity[Z] -3.2264 3.1938 2.064e-06 -5.3943e-08 v ǁVelocityǁ 0.0026727 49.555 9.3176 8.2968 v Pressure -6.0888e+05 2.455e+05 -80829 -1.0905e+05 v TurbVisc 1.9238e-18 0.031876 0.00023564 0.00010762 v CourantNb 2.2182e-08 0.011855 0.00017372 4.9915e-06 v FourierNb 1.2475e-07 0.053919 0.00015837 8.6762e-07 v total_pressure -5.0756e+05 3.4682e+05 20496 -7720.9 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2786 0.12926 0.0033473 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 8.6248e-07 0.054748 0.00033209 5.8591e-06 INSTANT 0.876892000E-01 TIME STEP NUMBER 57090 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282902929E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.844722598E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15094E-01 0.23182E+01 Friction velocity uk : 0.15094E-01 0.23182E+01 Dimensionless distance yplus : 0.14551E-01 0.22794E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 7.617978212e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29719E+08 1 0.21170E-09 0.55018E+02 0.27316E+04 c Velocity[X] 0.31375E+02 c Velocity[Y] 0.23643E+02 c Velocity[Z] 0.93825E-06 c Pressure 0.82474E-04 6 0.57142E-04 0.45689E-03 0.22010E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -35.891 49.22 5.6023 7.993 v Velocity[Y] -36.387 39.473 -0.21591 -0.21465 v Velocity[Z] -3.2267 3.1939 2.0636e-06 -5.3943e-08 v ǁVelocityǁ 0.0027783 49.567 9.3191 8.2972 v Pressure -6.0914e+05 2.4587e+05 -80565 -1.0903e+05 v TurbVisc 1.9751e-18 0.031889 0.00023571 0.00010774 v CourantNb 2.584e-08 0.011856 0.00017373 4.9916e-06 v FourierNb 1.2475e-07 0.053946 0.00015838 8.6841e-07 v total_pressure -5.0782e+05 3.4719e+05 20760 -7703.7 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2794 0.12933 0.0033488 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 8.6319e-07 0.054777 0.00033211 5.86e-06 INSTANT 0.876893000E-01 TIME STEP NUMBER 57091 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282909590E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.845129417E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.35751E-02 0.23190E+01 Friction velocity uk : 0.35751E-02 0.23190E+01 Dimensionless distance yplus : 0.34466E-02 0.22802E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 7.821469076e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29721E+08 1 0.21179E-09 0.55097E+02 0.27334E+04 c Velocity[X] 0.31433E+02 c Velocity[Y] 0.23664E+02 c Velocity[Z] 0.93947E-06 c Pressure 0.86571E-04 43 0.79217E-04 0.47918E-03 0.52424E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -35.904 49.231 5.6024 7.9931 v Velocity[Y] -36.398 39.486 -0.21608 -0.21513 v Velocity[Z] -3.227 3.194 2.0631e-06 -5.3943e-08 v ǁVelocityǁ 0.0029002 49.579 9.3206 8.2976 v Pressure -6.1101e+05 2.4624e+05 -80113 -1.0863e+05 v TurbVisc 2.0018e-18 0.031902 0.00023578 0.00010786 v CourantNb 2.9096e-08 0.011858 0.00017375 4.9918e-06 v FourierNb 1.2475e-07 0.053972 0.0001584 8.6921e-07 v total_pressure -5.0968e+05 3.4757e+05 21212 -7306.1 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2802 0.12939 0.0033503 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 8.6389e-07 0.054807 0.00033214 5.861e-06 INSTANT 0.876894000E-01 TIME STEP NUMBER 57092 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282916037E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.845546605E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.18186E-01 0.23198E+01 Friction velocity uk : 0.18186E-01 0.23198E+01 Dimensionless distance yplus : 0.17532E-01 0.22810E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 7.765695308e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29723E+08 1 0.21186E-09 0.55194E+02 0.27355E+04 c Velocity[X] 0.31475E+02 c Velocity[Y] 0.23719E+02 c Velocity[Z] 0.94629E-06 c Pressure 0.86374E-04 120 0.84354E-04 0.47769E-03 0.47781E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -35.918 49.243 5.6025 7.9932 v Velocity[Y] -36.409 39.499 -0.21624 -0.21562 v Velocity[Z] -3.2273 3.1941 2.0627e-06 -5.3943e-08 v ǁVelocityǁ 0.0030277 49.591 9.3221 8.2981 v Pressure -6.1077e+05 2.4662e+05 -79930 -1.0871e+05 v TurbVisc 1.9982e-18 0.031916 0.00023585 0.00010797 v CourantNb 3.3177e-08 0.011859 0.00017376 4.9919e-06 v FourierNb 1.2475e-07 0.053998 0.00015841 8.7001e-07 v total_pressure -5.0944e+05 3.4794e+05 21395 -7387.9 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.281 0.12947 0.0033521 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 8.646e-07 0.054837 0.00033217 5.8619e-06 INSTANT 0.876895000E-01 TIME STEP NUMBER 57093 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282922833E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.845953597E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19128E-01 0.23206E+01 Friction velocity uk : 0.19128E-01 0.23206E+01 Dimensionless distance yplus : 0.18534E-01 0.22818E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 7.920755126e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29724E+08 1 0.21196E-09 0.55280E+02 0.27374E+04 c Velocity[X] 0.31532E+02 c Velocity[Y] 0.23748E+02 c Velocity[Z] 0.94130E-06 c Pressure 0.88124E-04 111 0.98544E-04 0.48696E-03 0.55641E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -35.932 49.255 5.6026 7.9934 v Velocity[Y] -36.42 39.512 -0.2164 -0.2161 v Velocity[Z] -3.2276 3.1942 2.0622e-06 -5.3943e-08 v ǁVelocityǁ 0.003164 49.604 9.3236 8.2985 v Pressure -6.1276e+05 2.4697e+05 -79734 -1.0862e+05 v TurbVisc 2.0227e-18 0.031929 0.00023592 0.00010809 v CourantNb 3.3634e-08 0.011861 0.00017377 4.9921e-06 v FourierNb 1.2475e-07 0.054025 0.00015842 8.7081e-07 v total_pressure -5.1143e+05 3.483e+05 21591 -7299.5 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2818 0.12954 0.0033537 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 8.6531e-07 0.054866 0.0003322 5.8629e-06 INSTANT 0.876896000E-01 TIME STEP NUMBER 57094 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282929327E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.846368169E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.14065E-01 0.23214E+01 Friction velocity uk : 0.14065E-01 0.23214E+01 Dimensionless distance yplus : 0.13628E-01 0.22826E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 7.962523285e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29726E+08 1 0.21202E-09 0.55342E+02 0.27387E+04 c Velocity[X] 0.31567E+02 c Velocity[Y] 0.23775E+02 c Velocity[Z] 0.94756E-06 c Pressure 0.90308E-04 202 0.83540E-04 0.49861E-03 0.34924E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -35.946 49.267 5.6027 7.9935 v Velocity[Y] -36.431 39.525 -0.21657 -0.21659 v Velocity[Z] -3.2279 3.1943 2.0618e-06 -5.3943e-08 v ǁVelocityǁ 0.0033069 49.616 9.3251 8.2989 v Pressure -6.1298e+05 2.4735e+05 -79590 -1.0875e+05 v TurbVisc 1.9994e-18 0.031942 0.000236 0.00010821 v CourantNb 2.9641e-08 0.011862 0.00017378 4.9922e-06 v FourierNb 1.2475e-07 0.054051 0.00015844 8.7161e-07 v total_pressure -5.1165e+05 3.4867e+05 21735 -7428.8 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2826 0.12961 0.0033554 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 8.6602e-07 0.054896 0.00033222 5.8638e-06 INSTANT 0.876897000E-01 TIME STEP NUMBER 57095 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282936026E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.846788737E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.55181E-02 0.23222E+01 Friction velocity uk : 0.55181E-02 0.23222E+01 Dimensionless distance yplus : 0.53466E-02 0.22834E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 8.017441047e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29728E+08 1 0.21211E-09 0.55441E+02 0.27409E+04 c Velocity[X] 0.31613E+02 c Velocity[Y] 0.23828E+02 c Velocity[Z] 0.96800E-06 c Pressure 0.77155E-04 13 0.57517E-04 0.42562E-03 0.21459E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -35.96 49.279 5.6028 7.9936 v Velocity[Y] -36.442 39.538 -0.21673 -0.21708 v Velocity[Z] -3.2282 3.1944 2.0613e-06 -5.3943e-08 v ǁVelocityǁ 0.0027193 49.628 9.3266 8.2993 v Pressure -6.1324e+05 2.4772e+05 -79521 -1.0878e+05 v TurbVisc 2.061e-18 0.031956 0.00023607 0.00010833 v CourantNb 2.5673e-08 0.011864 0.0001738 4.9924e-06 v FourierNb 1.2475e-07 0.054078 0.00015845 8.7241e-07 v total_pressure -5.1191e+05 3.4904e+05 21804 -7457.5 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2834 0.12967 0.0033569 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 8.6673e-07 0.054926 0.00033225 5.8648e-06 INSTANT 0.876898000E-01 TIME STEP NUMBER 57096 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282942885E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.847212502E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.42550E-02 0.23230E+01 Friction velocity uk : 0.42550E-02 0.23230E+01 Dimensionless distance yplus : 0.41228E-02 0.22842E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 8.148018840e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29730E+08 1 0.21219E-09 0.55521E+02 0.27426E+04 c Velocity[X] 0.31668E+02 c Velocity[Y] 0.23854E+02 c Velocity[Z] 0.96222E-06 c Pressure 0.83073E-04 46 0.79531E-04 0.45788E-03 0.45288E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -35.974 49.291 5.6029 7.9937 v Velocity[Y] -36.453 39.551 -0.2169 -0.21757 v Velocity[Z] -3.2285 3.1945 2.0609e-06 -5.3943e-08 v ǁVelocityǁ 0.0019938 49.64 9.3281 8.2998 v Pressure -6.1517e+05 2.4808e+05 -79337 -1.0868e+05 v TurbVisc 2.2776e-18 0.031969 0.00023614 0.00010844 v CourantNb 2.1714e-08 0.011865 0.00017381 4.9925e-06 v FourierNb 1.2475e-07 0.054105 0.00015847 8.7321e-07 v total_pressure -5.1385e+05 3.4941e+05 21988 -7352 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2842 0.12974 0.0033584 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 8.6744e-07 0.054957 0.00033228 5.8657e-06 INSTANT 0.876899000E-01 TIME STEP NUMBER 57097 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282949454E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.847644351E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.43363E-02 0.23238E+01 Friction velocity uk : 0.43363E-02 0.23238E+01 Dimensionless distance yplus : 0.42016E-02 0.22850E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 7.984275323e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29732E+08 1 0.21227E-09 0.55617E+02 0.27447E+04 c Velocity[X] 0.31711E+02 c Velocity[Y] 0.23906E+02 c Velocity[Z] 0.95989E-06 c Pressure 0.84138E-04 93 0.84724E-04 0.46336E-03 0.47044E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -35.989 49.304 5.6029 7.9938 v Velocity[Y] -36.464 39.564 -0.21706 -0.21806 v Velocity[Z] -3.2288 3.1946 2.0604e-06 -5.3943e-08 v ǁVelocityǁ 0.0022451 49.653 9.3296 8.3002 v Pressure -6.149e+05 2.4846e+05 -79333 -1.0878e+05 v TurbVisc 1.7072e-18 0.031982 0.00023621 0.00010856 v CourantNb 1.7752e-08 0.011867 0.00017382 4.9927e-06 v FourierNb 1.2475e-07 0.054132 0.00015849 8.7401e-07 v total_pressure -5.1358e+05 3.4978e+05 21992 -7455.7 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.285 0.1298 0.00336 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 8.6816e-07 0.054987 0.00033231 5.8667e-06 INSTANT 0.876900000E-01 TIME STEP NUMBER 57098 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282956398E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.848068534E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.68927E-02 0.23246E+01 Friction velocity uk : 0.68927E-02 0.23246E+01 Dimensionless distance yplus : 0.67503E-02 0.22858E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 8.035015684e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29733E+08 1 0.21236E-09 0.55702E+02 0.27466E+04 c Velocity[X] 0.31763E+02 c Velocity[Y] 0.23939E+02 c Velocity[Z] 0.95747E-06 c Pressure 0.87288E-04 109 0.98967E-04 0.48030E-03 0.54383E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -36.003 49.316 5.603 7.994 v Velocity[Y] -36.475 39.577 -0.21723 -0.21854 v Velocity[Z] -3.2291 3.1947 2.06e-06 -5.3943e-08 v ǁVelocityǁ 0.0032693 49.665 9.3311 8.3006 v Pressure -6.1698e+05 2.4881e+05 -79368 -1.0886e+05 v TurbVisc 1.8891e-18 0.031996 0.00023628 0.00010868 v CourantNb 1.3742e-08 0.011868 0.00017384 4.9928e-06 v FourierNb 1.2475e-07 0.05416 0.0001585 8.7482e-07 v total_pressure -5.1565e+05 3.5013e+05 21957 -7535.4 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2858 0.12987 0.0033615 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 8.6887e-07 0.055018 0.00033234 5.8677e-06 INSTANT 0.876901000E-01 TIME STEP NUMBER 57099 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282962977E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.848497305E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.17275E-01 0.23254E+01 Friction velocity uk : 0.17275E-01 0.23254E+01 Dimensionless distance yplus : 0.16918E-01 0.22866E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 8.030120170e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29735E+08 1 0.21243E-09 0.55763E+02 0.27479E+04 c Velocity[X] 0.31802E+02 c Velocity[Y] 0.23961E+02 c Velocity[Z] 0.96505E-06 c Pressure 0.90856E-04 125 0.83785E-04 0.49950E-03 0.33973E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -36.017 49.328 5.6031 7.9941 v Velocity[Y] -36.486 39.59 -0.21739 -0.21903 v Velocity[Z] -3.2294 3.1948 2.0595e-06 -5.3944e-08 v ǁVelocityǁ 0.0030089 49.678 9.3326 8.3011 v Pressure -6.1714e+05 2.4918e+05 -79435 -1.0906e+05 v TurbVisc 1.9863e-18 0.032009 0.00023635 0.0001088 v CourantNb 9.7751e-09 0.01187 0.00017385 4.993e-06 v FourierNb 1.2475e-07 0.054188 0.00015852 8.7562e-07 v total_pressure -5.1582e+05 3.505e+05 21890 -7734.1 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2866 0.12995 0.0033633 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 8.6959e-07 0.05505 0.00033236 5.8686e-06 INSTANT 0.876902000E-01 TIME STEP NUMBER 57100 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282969803E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.848930932E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.18546E-01 0.23263E+01 Friction velocity uk : 0.18546E-01 0.23263E+01 Dimensionless distance yplus : 0.17941E-01 0.22874E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 7.994292033e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29737E+08 1 0.21252E-09 0.55861E+02 0.27500E+04 c Velocity[X] 0.31847E+02 c Velocity[Y] 0.24015E+02 c Velocity[Z] 0.97165E-06 c Pressure 0.79058E-04 6 0.57865E-04 0.43427E-03 0.21917E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -36.031 49.34 5.6032 7.9942 v Velocity[Y] -36.498 39.603 -0.21756 -0.21953 v Velocity[Z] -3.2298 3.1949 2.0591e-06 -5.3944e-08 v ǁVelocityǁ 0.0023266 49.69 9.3341 8.3015 v Pressure -6.1742e+05 2.4955e+05 -79481 -1.0912e+05 v TurbVisc 2.049e-18 0.032022 0.00023642 0.00010892 v CourantNb 5.8375e-09 0.011871 0.00017386 4.9931e-06 v FourierNb 1.2475e-07 0.054216 0.00015853 8.7642e-07 v total_pressure -5.161e+05 3.5087e+05 21844 -7792.8 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2874 0.13003 0.0033651 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 8.7031e-07 0.055081 0.00033239 5.8696e-06 INSTANT 0.876903000E-01 TIME STEP NUMBER 57101 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282976771E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.849366249E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.16234E-01 0.23271E+01 Friction velocity uk : 0.16234E-01 0.23271E+01 Dimensionless distance yplus : 0.15658E-01 0.22882E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 7.885296901e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29739E+08 1 0.21260E-09 0.55942E+02 0.27518E+04 c Velocity[X] 0.31899E+02 c Velocity[Y] 0.24042E+02 c Velocity[Z] 0.97491E-06 c Pressure 0.86347E-04 42 0.79873E-04 0.47391E-03 0.44725E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -36.045 49.352 5.6033 7.9943 v Velocity[Y] -36.509 39.617 -0.21772 -0.22002 v Velocity[Z] -3.2301 3.195 2.0586e-06 -5.3944e-08 v ǁVelocityǁ 0.0024188 49.703 9.3356 8.3019 v Pressure -6.1942e+05 2.499e+05 -79703 -1.0932e+05 v TurbVisc 2.028e-18 0.032035 0.00023649 0.00010903 v CourantNb 4.6884e-09 0.011873 0.00017387 4.9933e-06 v FourierNb 1.2476e-07 0.054245 0.00015855 8.7723e-07 v total_pressure -5.181e+05 3.5122e+05 21622 -7990.2 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2882 0.1301 0.0033669 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 8.7103e-07 0.055113 0.00033242 5.8705e-06 INSTANT 0.876904000E-01 TIME STEP NUMBER 57102 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282983366E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.849798171E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15462E-01 0.23278E+01 Friction velocity uk : 0.15462E-01 0.23278E+01 Dimensionless distance yplus : 0.14914E-01 0.22889E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 7.916018406e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29741E+08 1 0.21269E-09 0.56036E+02 0.27539E+04 c Velocity[X] 0.31942E+02 c Velocity[Y] 0.24094E+02 c Velocity[Z] 0.10019E-05 c Pressure 0.88715E-04 47 0.85113E-04 0.48649E-03 0.48181E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -36.06 49.365 5.6034 7.9944 v Velocity[Y] -36.52 39.63 -0.21789 -0.22051 v Velocity[Z] -3.2304 3.1951 2.0582e-06 -5.3944e-08 v ǁVelocityǁ 0.0032333 49.715 9.3371 8.3024 v Pressure -6.1915e+05 2.5027e+05 -79860 -1.0952e+05 v TurbVisc 2.1153e-18 0.032049 0.00023657 0.00010915 v CourantNb 5.9559e-09 0.011874 0.00017389 4.9934e-06 v FourierNb 1.2476e-07 0.054274 0.00015856 8.7803e-07 v total_pressure -5.1782e+05 3.5159e+05 21465 -8199.4 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2889 0.13018 0.0033686 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 8.7175e-07 0.055145 0.00033245 5.8715e-06 INSTANT 0.876905000E-01 TIME STEP NUMBER 57103 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282990353E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.850239757E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.18359E-01 0.23286E+01 Friction velocity uk : 0.18359E-01 0.23286E+01 Dimensionless distance yplus : 0.17760E-01 0.22897E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 7.797514699e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29743E+08 1 0.21278E-09 0.56121E+02 0.27557E+04 c Velocity[X] 0.31993E+02 c Velocity[Y] 0.24127E+02 c Velocity[Z] 0.98416E-06 c Pressure 0.93032E-04 111 0.99394E-04 0.50972E-03 0.55073E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -36.074 49.377 5.6035 7.9946 v Velocity[Y] -36.531 39.643 -0.21806 -0.221 v Velocity[Z] -3.2307 3.1952 2.0577e-06 -5.3944e-08 v ǁVelocityǁ 0.0031431 49.728 9.3386 8.3028 v Pressure -6.2127e+05 2.5061e+05 -80104 -1.097e+05 v TurbVisc 2.1118e-18 0.032062 0.00023664 0.00010927 v CourantNb 9.7456e-09 0.011876 0.0001739 4.9936e-06 v FourierNb 1.2476e-07 0.054303 0.00015858 8.7884e-07 v total_pressure -5.1994e+05 3.5194e+05 21221 -8376.4 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2897 0.13025 0.0033703 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 8.7247e-07 0.055178 0.00033248 5.8724e-06 INSTANT 0.876906000E-01 TIME STEP NUMBER 57104 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282996947E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.850678587E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19069E-01 0.23294E+01 Friction velocity uk : 0.19069E-01 0.23294E+01 Dimensionless distance yplus : 0.18448E-01 0.22905E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 7.697612096e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29744E+08 1 0.21285E-09 0.56181E+02 0.27569E+04 c Velocity[X] 0.32036E+02 c Velocity[Y] 0.24145E+02 c Velocity[Z] 0.98340E-06 c Pressure 0.97653E-04 514 0.84564E-04 0.53458E-03 0.35331E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -36.089 49.389 5.6036 7.9947 v Velocity[Y] -36.543 39.656 -0.21822 -0.22149 v Velocity[Z] -3.231 3.1953 2.0573e-06 -5.3944e-08 v ǁVelocityǁ 0.0028872 49.74 9.3401 8.3032 v Pressure -6.2138e+05 2.5098e+05 -80379 -1.0999e+05 v TurbVisc 2.1108e-18 0.032075 0.00023671 0.00010939 v CourantNb 1.3497e-08 0.011877 0.00017391 4.9937e-06 v FourierNb 1.2476e-07 0.054333 0.00015859 8.7964e-07 v total_pressure -5.2006e+05 3.5231e+05 20946 -8666 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2905 0.13032 0.0033719 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 8.732e-07 0.055211 0.00033251 5.8734e-06 INSTANT 0.876907000E-01 TIME STEP NUMBER 57105 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283003799E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.851120056E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15304E-01 0.23302E+01 Friction velocity uk : 0.15304E-01 0.23302E+01 Dimensionless distance yplus : 0.14771E-01 0.22913E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 7.587523146e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29746E+08 1 0.21294E-09 0.56278E+02 0.27590E+04 c Velocity[X] 0.32065E+02 c Velocity[Y] 0.24213E+02 c Velocity[Z] 0.99292E-06 c Pressure 0.87917E-04 7 0.59064E-04 0.48087E-03 0.29201E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -36.103 49.402 5.6037 7.9948 v Velocity[Y] -36.554 39.67 -0.21839 -0.22199 v Velocity[Z] -3.2313 3.1954 2.0568e-06 -5.3944e-08 v ǁVelocityǁ 0.0026404 49.753 9.3416 8.3037 v Pressure -6.2186e+05 2.5135e+05 -80679 -1.1025e+05 v TurbVisc 2.1022e-18 0.032088 0.00023678 0.00010951 v CourantNb 1.7239e-08 0.011879 0.00017393 4.9939e-06 v FourierNb 1.2476e-07 0.054363 0.00015861 8.8045e-07 v total_pressure -5.2054e+05 3.5267e+05 20646 -8929.2 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2913 0.13039 0.0033735 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 8.7392e-07 0.055245 0.00033253 5.8744e-06 INSTANT 0.876908000E-01 TIME STEP NUMBER 57106 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283010692E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.851561193E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.88157E-02 0.23310E+01 Friction velocity uk : 0.88157E-02 0.23310E+01 Dimensionless distance yplus : 0.85090E-02 0.22920E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 7.429125437e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29748E+08 1 0.21302E-09 0.56359E+02 0.27608E+04 c Velocity[X] 0.32133E+02 c Velocity[Y] 0.24226E+02 c Velocity[Z] 0.99761E-06 c Pressure 0.95840E-04 70 0.80765E-04 0.52376E-03 0.47220E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -36.117 49.414 5.6038 7.9949 v Velocity[Y] -36.565 39.683 -0.21855 -0.22248 v Velocity[Z] -3.2316 3.1955 2.0564e-06 -5.3944e-08 v ǁVelocityǁ 0.002384 49.766 9.3431 8.3041 v Pressure -6.2368e+05 2.5169e+05 -81078 -1.105e+05 v TurbVisc 2.0671e-18 0.032102 0.00023686 0.00010962 v CourantNb 1.9032e-08 0.01188 0.00017394 4.9941e-06 v FourierNb 1.2476e-07 0.054394 0.00015862 8.8126e-07 v total_pressure -5.2235e+05 3.5301e+05 20247 -9177.8 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.292 0.13046 0.0033751 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 8.7465e-07 0.05528 0.00033256 5.8753e-06 INSTANT 0.876909000E-01 TIME STEP NUMBER 57107 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283017285E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.851999911E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.28446E-02 0.23318E+01 Friction velocity uk : 0.28446E-02 0.23318E+01 Dimensionless distance yplus : 0.27457E-02 0.22928E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 7.355686456e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29750E+08 1 0.21311E-09 0.56453E+02 0.27628E+04 c Velocity[X] 0.32165E+02 c Velocity[Y] 0.24288E+02 c Velocity[Z] 0.99787E-06 c Pressure 0.99254E-04 369 0.86296E-04 0.54195E-03 0.54687E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -36.132 49.426 5.6039 7.995 v Velocity[Y] -36.577 39.696 -0.21872 -0.22298 v Velocity[Z] -3.2319 3.1956 2.0559e-06 -5.3944e-08 v ǁVelocityǁ 0.0021408 49.778 9.3446 8.3046 v Pressure -6.2355e+05 2.5205e+05 -81504 -1.1095e+05 v TurbVisc 2.0864e-18 0.032115 0.00023693 0.00010974 v CourantNb 1.5155e-08 0.011882 0.00017395 4.9942e-06 v FourierNb 1.2476e-07 0.054426 0.00015864 8.8207e-07 v total_pressure -5.2222e+05 3.5338e+05 19821 -9627 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2928 0.13053 0.0033766 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 8.7537e-07 0.055314 0.00033259 5.8763e-06 INSTANT 0.876910000E-01 TIME STEP NUMBER 57108 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283024185E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.852444987E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11990E-01 0.23326E+01 Friction velocity uk : 0.11990E-01 0.23326E+01 Dimensionless distance yplus : 0.11573E-01 0.22936E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 7.196691464e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29752E+08 1 0.21321E-09 0.56513E+02 0.27640E+04 c Velocity[X] 0.32222E+02 c Velocity[Y] 0.24291E+02 c Velocity[Z] 0.99893E-06 c Pressure 0.10435E-03 61 0.75371E-04 0.56930E-03 0.30817E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -36.146 49.439 5.604 7.9952 v Velocity[Y] -36.588 39.71 -0.21889 -0.22348 v Velocity[Z] -3.2322 3.1957 2.0555e-06 -5.3944e-08 v ǁVelocityǁ 0.0019016 49.791 9.3461 8.305 v Pressure -6.2495e+05 2.5241e+05 -81910 -1.1111e+05 v TurbVisc 2.1061e-18 0.032128 0.000237 0.00010986 v CourantNb 1.1436e-08 0.011883 0.00017396 4.9944e-06 v FourierNb 1.2476e-07 0.054458 0.00015866 8.8287e-07 v total_pressure -5.2362e+05 3.5373e+05 19415 -9783.2 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2936 0.1306 0.0033784 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 8.761e-07 0.05535 0.00033262 5.8772e-06 INSTANT 0.876911000E-01 TIME STEP NUMBER 57109 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283030896E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.852889647E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.17236E-01 0.23333E+01 Friction velocity uk : 0.17236E-01 0.23333E+01 Dimensionless distance yplus : 0.16636E-01 0.22943E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 7.038690951e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29754E+08 1 0.21329E-09 0.56605E+02 0.27661E+04 c Velocity[X] 0.32260E+02 c Velocity[Y] 0.24345E+02 c Velocity[Z] 0.10053E-05 c Pressure 0.98465E-04 7 0.56087E-04 0.53671E-03 0.25053E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -36.161 49.451 5.604 7.9953 v Velocity[Y] -36.599 39.723 -0.21905 -0.22397 v Velocity[Z] -3.2325 3.1958 2.055e-06 -5.3944e-08 v ǁVelocityǁ 0.0016546 49.804 9.3477 8.3054 v Pressure -6.2633e+05 2.5276e+05 -82350 -1.1138e+05 v TurbVisc 2.0978e-18 0.032141 0.00023707 0.00010998 v CourantNb 7.7586e-09 0.011885 0.00017398 4.9945e-06 v FourierNb 1.2476e-07 0.05449 0.00015867 8.8368e-07 v total_pressure -5.25e+05 3.5408e+05 18975 -10051 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2943 0.13067 0.00338 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 8.7683e-07 0.055385 0.00033265 5.8782e-06 INSTANT 0.876912000E-01 TIME STEP NUMBER 57110 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283037507E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.853331297E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.21295E-01 0.23341E+01 Friction velocity uk : 0.21295E-01 0.23341E+01 Dimensionless distance yplus : 0.20555E-01 0.22950E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 6.787974909e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29756E+08 1 0.21336E-09 0.56681E+02 0.27677E+04 c Velocity[X] 0.32305E+02 c Velocity[Y] 0.24376E+02 c Velocity[Z] 0.10130E-05 c Pressure 0.10556E-03 91 0.97658E-04 0.57491E-03 0.43308E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -36.175 49.464 5.6041 7.9954 v Velocity[Y] -36.611 39.736 -0.21922 -0.22447 v Velocity[Z] -3.2328 3.1959 2.0546e-06 -5.3944e-08 v ǁVelocityǁ 0.0014438 49.817 9.3492 8.3059 v Pressure -6.2695e+05 2.531e+05 -83046 -1.1211e+05 v TurbVisc 2.0161e-18 0.032154 0.00023715 0.0001101 v CourantNb 6.2782e-09 0.011886 0.00017399 4.9947e-06 v FourierNb 1.2476e-07 0.054524 0.00015869 8.8449e-07 v total_pressure -5.2562e+05 3.5442e+05 18279 -10785 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.295 0.13074 0.0033816 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 8.7756e-07 0.055422 0.00033268 5.8792e-06 INSTANT 0.876913000E-01 TIME STEP NUMBER 57111 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283044079E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.853767074E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.23454E-01 0.23348E+01 Friction velocity uk : 0.23454E-01 0.23348E+01 Dimensionless distance yplus : 0.22671E-01 0.22958E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 6.771398628e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29757E+08 1 0.21346E-09 0.56759E+02 0.27693E+04 c Velocity[X] 0.32347E+02 c Velocity[Y] 0.24412E+02 c Velocity[Z] 0.10109E-05 c Pressure 0.10726E-03 111 0.81281E-04 0.58365E-03 0.20781E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -36.19 49.476 5.6042 7.9955 v Velocity[Y] -36.622 39.75 -0.21939 -0.22497 v Velocity[Z] -3.2331 3.196 2.0541e-06 -5.3945e-08 v ǁVelocityǁ 0.0012364 49.829 9.3507 8.3063 v Pressure -6.2756e+05 2.5346e+05 -83576 -1.1241e+05 v TurbVisc 1.8766e-18 0.032168 0.00023722 0.00011022 v CourantNb 5.9497e-09 0.011888 0.000174 4.9948e-06 v FourierNb 1.2476e-07 0.054557 0.0001587 8.853e-07 v total_pressure -5.2624e+05 3.5478e+05 17749 -11082 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2958 0.13081 0.0033832 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 8.783e-07 0.055458 0.00033271 5.8801e-06 INSTANT 0.876914000E-01 TIME STEP NUMBER 57112 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283050757E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.854214186E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.23085E-01 0.23356E+01 Friction velocity uk : 0.23085E-01 0.23356E+01 Dimensionless distance yplus : 0.22314E-01 0.22966E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 6.498562152e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29759E+08 1 0.21355E-09 0.56852E+02 0.27713E+04 c Velocity[X] 0.32380E+02 c Velocity[Y] 0.24472E+02 c Velocity[Z] 0.10321E-05 c Pressure 0.10786E-03 13 0.52358E-04 0.58640E-03 0.28265E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -36.204 49.489 5.6043 7.9956 v Velocity[Y] -36.634 39.763 -0.21955 -0.22547 v Velocity[Z] -3.2334 3.1961 2.0537e-06 -5.3945e-08 v ǁVelocityǁ 0.001038 49.842 9.3522 8.3067 v Pressure -6.2812e+05 2.5382e+05 -84152 -1.1277e+05 v TurbVisc 2.1339e-18 0.032181 0.0002373 0.00011034 v CourantNb 8.0326e-09 0.011889 0.00017402 4.995e-06 v FourierNb 1.2476e-07 0.054592 0.00015872 8.8611e-07 v total_pressure -5.268e+05 3.5514e+05 17173 -11448 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2966 0.13087 0.0033848 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 8.7903e-07 0.055496 0.00033274 5.8811e-06 INSTANT 0.876915000E-01 TIME STEP NUMBER 57113 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283057448E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.854657052E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.18701E-01 0.23363E+01 Friction velocity uk : 0.18701E-01 0.23363E+01 Dimensionless distance yplus : 0.18010E-01 0.22973E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 6.408534954e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29761E+08 1 0.21363E-09 0.56925E+02 0.27729E+04 c Velocity[X] 0.32436E+02 c Velocity[Y] 0.24490E+02 c Velocity[Z] 0.10313E-05 c Pressure 0.11510E-03 35 0.97943E-04 0.62520E-03 0.32757E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -36.219 49.502 5.6044 7.9957 v Velocity[Y] -36.645 39.777 -0.21972 -0.22597 v Velocity[Z] -3.2337 3.1962 2.0532e-06 -5.3945e-08 v ǁVelocityǁ 0.00086718 49.855 9.3537 8.3072 v Pressure -6.293e+05 2.5416e+05 -84871 -1.133e+05 v TurbVisc 1.3051e-18 0.032194 0.00023737 0.00011045 v CourantNb 6.615e-09 0.011891 0.00017403 4.9951e-06 v FourierNb 1.2476e-07 0.054626 0.00015874 8.8692e-07 v total_pressure -5.2798e+05 3.5548e+05 16454 -11975 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2973 0.13094 0.0033862 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 8.7977e-07 0.055534 0.00033277 5.8821e-06 INSTANT 0.876916000E-01 TIME STEP NUMBER 57114 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283063959E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.855097493E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10582E-01 0.23371E+01 Friction velocity uk : 0.10582E-01 0.23371E+01 Dimensionless distance yplus : 0.10191E-01 0.22980E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 6.222589087e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29763E+08 1 0.21373E-09 0.57006E+02 0.27746E+04 c Velocity[X] 0.32485E+02 c Velocity[Y] 0.24521E+02 c Velocity[Z] 0.10281E-05 c Pressure 0.11709E-03 38 0.83694E-04 0.63545E-03 0.27201E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -36.234 49.514 5.6045 7.9959 v Velocity[Y] -36.657 39.79 -0.21988 -0.22647 v Velocity[Z] -3.234 3.1963 2.0528e-06 -5.3945e-08 v ǁVelocityǁ 0.00073582 49.868 9.3552 8.3076 v Pressure -6.304e+05 2.5451e+05 -85574 -1.1375e+05 v TurbVisc 2.1475e-18 0.032207 0.00023744 0.00011057 v CourantNb 1.4381e-08 0.011892 0.00017404 4.9953e-06 v FourierNb 1.2476e-07 0.054662 0.00015875 8.8773e-07 v total_pressure -5.2908e+05 3.5583e+05 15751 -12422 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.298 0.131 0.0033877 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 8.805e-07 0.055573 0.0003328 5.883e-06 INSTANT 0.876917000E-01 TIME STEP NUMBER 57115 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283070453E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.855533376E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.33895E-02 0.23378E+01 Friction velocity uk : 0.33895E-02 0.23378E+01 Dimensionless distance yplus : 0.32642E-02 0.22987E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 5.984126313e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29765E+08 1 0.21382E-09 0.57100E+02 0.27766E+04 c Velocity[X] 0.32532E+02 c Velocity[Y] 0.24568E+02 c Velocity[Z] 0.10429E-05 c Pressure 0.11807E-03 13 0.56742E-04 0.64025E-03 0.28232E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -36.248 49.527 5.6045 7.996 v Velocity[Y] -36.668 39.804 -0.22005 -0.22696 v Velocity[Z] -3.2343 3.1964 2.0523e-06 -5.3945e-08 v ǁVelocityǁ 0.00065602 49.881 9.3567 8.308 v Pressure -6.3169e+05 2.5485e+05 -86286 -1.1412e+05 v TurbVisc 2.137e-18 0.03222 0.00023752 0.00011069 v CourantNb 1.7521e-08 0.011894 0.00017406 4.9954e-06 v FourierNb 1.2476e-07 0.054698 0.00015877 8.8855e-07 v total_pressure -5.3037e+05 3.5617e+05 15039 -12794 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2987 0.13107 0.0033892 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 8.8124e-07 0.055612 0.00033282 5.884e-06 INSTANT 0.876918000E-01 TIME STEP NUMBER 57116 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283076854E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.855970617E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15333E-01 0.23385E+01 Friction velocity uk : 0.15333E-01 0.23385E+01 Dimensionless distance yplus : 0.14767E-01 0.22994E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 5.770823789e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29767E+08 1 0.21389E-09 0.57186E+02 0.27785E+04 c Velocity[X] 0.32567E+02 c Velocity[Y] 0.24619E+02 c Velocity[Z] 0.10434E-05 c Pressure 0.12563E-03 40 0.77600E-04 0.68060E-03 0.65221E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -36.263 49.539 5.6046 7.9961 v Velocity[Y] -36.68 39.817 -0.22022 -0.22747 v Velocity[Z] -3.2346 3.1965 2.0519e-06 -5.3945e-08 v ǁVelocityǁ 0.00066715 49.894 9.3582 8.3085 v Pressure -6.3178e+05 2.552e+05 -87196 -1.1502e+05 v TurbVisc 1.4032e-18 0.032234 0.00023759 0.00011081 v CourantNb 6.6453e-09 0.011895 0.00017407 4.9956e-06 v FourierNb 1.2476e-07 0.054734 0.00015879 8.8936e-07 v total_pressure -5.3046e+05 3.5652e+05 14129 -13695 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.2994 0.13113 0.0033909 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 8.8198e-07 0.055651 0.00033285 5.8849e-06 INSTANT 0.876919000E-01 TIME STEP NUMBER 57117 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283083366E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.856407403E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.21872E-01 0.23393E+01 Friction velocity uk : 0.21872E-01 0.23393E+01 Dimensionless distance yplus : 0.21063E-01 0.23002E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 5.660646177e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29769E+08 1 0.21400E-09 0.57267E+02 0.27802E+04 c Velocity[X] 0.32615E+02 c Velocity[Y] 0.24652E+02 c Velocity[Z] 0.10295E-05 c Pressure 0.12958E-03 81 0.82437E-04 0.70143E-03 0.47892E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -36.277 49.552 5.6047 7.9962 v Velocity[Y] -36.691 39.831 -0.22038 -0.22797 v Velocity[Z] -3.2349 3.1966 2.0514e-06 -5.3945e-08 v ǁVelocityǁ 0.00065947 49.907 9.3597 8.3089 v Pressure -6.337e+05 2.5554e+05 -87977 -1.1538e+05 v TurbVisc 2.1397e-18 0.032247 0.00023766 0.00011093 v CourantNb 2.3428e-08 0.011897 0.00017408 4.9957e-06 v FourierNb 1.2476e-07 0.054772 0.0001588 8.9017e-07 v total_pressure -5.3238e+05 3.5686e+05 13348 -14059 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3002 0.1312 0.0033925 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 8.8272e-07 0.055692 0.00033288 5.8859e-06 INSTANT 0.876920000E-01 TIME STEP NUMBER 57118 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283089527E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.856841980E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.22900E-01 0.23400E+01 Friction velocity uk : 0.22900E-01 0.23400E+01 Dimensionless distance yplus : 0.22042E-01 0.23009E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 5.445705523e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29771E+08 1 0.21408E-09 0.57357E+02 0.27821E+04 c Velocity[X] 0.32649E+02 c Velocity[Y] 0.24709E+02 c Velocity[Z] 0.10393E-05 c Pressure 0.13479E-03 246 0.96250E-04 0.72896E-03 0.65137E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -36.292 49.565 5.6048 7.9963 v Velocity[Y] -36.703 39.844 -0.22055 -0.22847 v Velocity[Z] -3.2352 3.1967 2.051e-06 -5.3945e-08 v ǁVelocityǁ 0.00063491 49.92 9.3612 8.3093 v Pressure -6.3344e+05 2.5589e+05 -88883 -1.1609e+05 v TurbVisc 2.1052e-18 0.03226 0.00023774 0.00011105 v CourantNb 2.6372e-08 0.011898 0.00017409 4.9959e-06 v FourierNb 1.2476e-07 0.054809 0.00015882 8.9099e-07 v total_pressure -5.3212e+05 3.5722e+05 12442 -14762 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3009 0.13127 0.0033941 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 8.8346e-07 0.055732 0.00033291 5.8869e-06 INSTANT 0.876921000E-01 TIME STEP NUMBER 57119 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283095979E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.857274897E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.21777E-01 0.23407E+01 Friction velocity uk : 0.21777E-01 0.23407E+01 Dimensionless distance yplus : 0.20961E-01 0.23016E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 5.256746097e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29772E+08 1 0.21418E-09 0.57411E+02 0.27832E+04 c Velocity[X] 0.32699E+02 c Velocity[Y] 0.24712E+02 c Velocity[Z] 0.10546E-05 c Pressure 0.14011E-03 706 0.81900E-04 0.75707E-03 0.39534E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -36.307 49.577 5.6048 7.9964 v Velocity[Y] -36.714 39.858 -0.22071 -0.22898 v Velocity[Z] -3.2355 3.1968 2.0505e-06 -5.3945e-08 v ǁVelocityǁ 0.0006311 49.933 9.3628 8.3098 v Pressure -6.3502e+05 2.5624e+05 -89777 -1.1656e+05 v TurbVisc 2.0894e-18 0.032273 0.00023781 0.00011117 v CourantNb 2.92e-08 0.0119 0.00017411 4.996e-06 v FourierNb 1.2476e-07 0.054847 0.00015884 8.918e-07 v total_pressure -5.3369e+05 3.5756e+05 11548 -15239 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3016 0.13133 0.0033957 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 8.842e-07 0.055773 0.00033294 5.8878e-06 INSTANT 0.876922000E-01 TIME STEP NUMBER 57120 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283102147E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.857704983E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.20578E-01 0.23414E+01 Friction velocity uk : 0.20578E-01 0.23414E+01 Dimensionless distance yplus : 0.19807E-01 0.23022E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 5.078990931e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29774E+08 1 0.21427E-09 0.57504E+02 0.27852E+04 c Velocity[X] 0.32746E+02 c Velocity[Y] 0.24758E+02 c Velocity[Z] 0.10600E-05 c Pressure 0.13592E-03 9 0.58709E-04 0.73378E-03 0.30243E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -36.321 49.59 5.6049 7.9965 v Velocity[Y] -36.726 39.872 -0.22088 -0.22948 v Velocity[Z] -3.2358 3.1969 2.0501e-06 -5.3945e-08 v ǁVelocityǁ 0.00064611 49.946 9.3643 8.3102 v Pressure -6.3634e+05 2.5658e+05 -90693 -1.1699e+05 v TurbVisc 2.0893e-18 0.032286 0.00023789 0.00011129 v CourantNb 3.1993e-08 0.011901 0.00017412 4.9962e-06 v FourierNb 1.2476e-07 0.054886 0.00015885 8.9261e-07 v total_pressure -5.3501e+05 3.579e+05 10632 -15664 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3022 0.13139 0.0033972 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 8.8494e-07 0.055815 0.00033297 5.8888e-06 INSTANT 0.876923000E-01 TIME STEP NUMBER 57121 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283108218E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.858130937E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.18714E-01 0.23420E+01 Friction velocity uk : 0.18714E-01 0.23420E+01 Dimensionless distance yplus : 0.18012E-01 0.23029E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 4.825893744e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29776E+08 1 0.21434E-09 0.57591E+02 0.27870E+04 c Velocity[X] 0.32783E+02 c Velocity[Y] 0.24807E+02 c Velocity[Z] 0.10416E-05 c Pressure 0.14301E-03 63 0.78509E-04 0.77141E-03 0.70888E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -36.336 49.603 5.605 7.9966 v Velocity[Y] -36.738 39.885 -0.22105 -0.22999 v Velocity[Z] -3.2361 3.197 2.0496e-06 -5.3945e-08 v ǁVelocityǁ 0.0006467 49.959 9.3658 8.3106 v Pressure -6.3636e+05 2.5692e+05 -91778 -1.1802e+05 v TurbVisc 1.9485e-18 0.032299 0.00023796 0.00011141 v CourantNb 3.4768e-08 0.011903 0.00017413 4.9963e-06 v FourierNb 1.2476e-07 0.054925 0.00015887 8.9343e-07 v total_pressure -5.3503e+05 3.5825e+05 9547.4 -16699 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3029 0.13146 0.0033987 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 8.8569e-07 0.055857 0.000333 5.8898e-06 INSTANT 0.876924000E-01 TIME STEP NUMBER 57122 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283114411E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.858551984E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.17835E-01 0.23428E+01 Friction velocity uk : 0.17835E-01 0.23428E+01 Dimensionless distance yplus : 0.17167E-01 0.23036E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 4.756711972e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29778E+08 1 0.21446E-09 0.57672E+02 0.27887E+04 c Velocity[X] 0.32833E+02 c Velocity[Y] 0.24838E+02 c Velocity[Z] 0.10439E-05 c Pressure 0.14712E-03 535 0.84310E-04 0.79290E-03 0.52022E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -36.351 49.616 5.605 7.9967 v Velocity[Y] -36.749 39.899 -0.22121 -0.23049 v Velocity[Z] -3.2364 3.1971 2.0492e-06 -5.3945e-08 v ǁVelocityǁ 0.00064322 49.972 9.3673 8.311 v Pressure -6.3833e+05 2.5726e+05 -92796 -1.1853e+05 v TurbVisc 2.1135e-18 0.032312 0.00023804 0.00011153 v CourantNb 3.6717e-08 0.011904 0.00017414 4.9965e-06 v FourierNb 1.2476e-07 0.054964 0.00015889 8.9425e-07 v total_pressure -5.3701e+05 3.5858e+05 8529.4 -17208 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3036 0.13152 0.0034002 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 8.8643e-07 0.055899 0.00033303 5.8907e-06 INSTANT 0.876925000E-01 TIME STEP NUMBER 57123 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283120234E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.858973651E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.16308E-01 0.23434E+01 Friction velocity uk : 0.16308E-01 0.23434E+01 Dimensionless distance yplus : 0.15697E-01 0.23043E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 4.554420543e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29780E+08 1 0.21453E-09 0.57762E+02 0.27906E+04 c Velocity[X] 0.32861E+02 c Velocity[Y] 0.24901E+02 c Velocity[Z] 0.10436E-05 c Pressure 0.15224E-03 195 0.98201E-04 0.81974E-03 0.70548E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -36.365 49.628 5.6051 7.9968 v Velocity[Y] -36.761 39.912 -0.22138 -0.231 v Velocity[Z] -3.2367 3.1972 2.0487e-06 -5.3946e-08 v ǁVelocityǁ 0.00066187 49.985 9.3688 8.3115 v Pressure -6.381e+05 2.5762e+05 -93895 -1.1936e+05 v TurbVisc 2.0858e-18 0.032325 0.00023811 0.00011165 v CourantNb 3.4597e-08 0.011905 0.00017416 4.9967e-06 v FourierNb 1.2476e-07 0.055004 0.0001589 8.9506e-07 v total_pressure -5.3677e+05 3.5894e+05 7430.3 -18034 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3043 0.13158 0.0034017 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 8.8718e-07 0.055942 0.00033306 5.8917e-06 INSTANT 0.876926000E-01 TIME STEP NUMBER 57124 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283126315E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.859392858E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13633E-01 0.23441E+01 Friction velocity uk : 0.13633E-01 0.23441E+01 Dimensionless distance yplus : 0.13134E-01 0.23049E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 4.375410244e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29782E+08 1 0.21464E-09 0.57813E+02 0.27916E+04 c Velocity[X] 0.32916E+02 c Velocity[Y] 0.24897E+02 c Velocity[Z] 0.10471E-05 c Pressure 0.15743E-03 275 0.83554E-04 0.84693E-03 0.43449E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -36.38 49.641 5.6051 7.9969 v Velocity[Y] -36.773 39.926 -0.22154 -0.2315 v Velocity[Z] -3.237 3.1973 2.0483e-06 -5.3946e-08 v ǁVelocityǁ 0.00073367 49.998 9.3703 8.3119 v Pressure -6.3963e+05 2.5795e+05 -94985 -1.199e+05 v TurbVisc 2.0444e-18 0.032339 0.00023819 0.00011177 v CourantNb 3.2747e-08 0.011907 0.00017417 4.9968e-06 v FourierNb 1.2476e-07 0.055044 0.00015892 8.9588e-07 v total_pressure -5.383e+05 3.5928e+05 6340.5 -18579 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3049 0.13164 0.0034032 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 8.8793e-07 0.055985 0.00033309 5.8927e-06 INSTANT 0.876927000E-01 TIME STEP NUMBER 57125 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283132146E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.859806265E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12278E-01 0.23448E+01 Friction velocity uk : 0.12278E-01 0.23448E+01 Dimensionless distance yplus : 0.11829E-01 0.23056E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 4.223027200e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29784E+08 1 0.21473E-09 0.57906E+02 0.27936E+04 c Velocity[X] 0.32952E+02 c Velocity[Y] 0.24953E+02 c Velocity[Z] 0.10701E-05 c Pressure 0.15368E-03 16 0.60562E-04 0.82606E-03 0.37698E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -36.395 49.654 5.6052 7.997 v Velocity[Y] -36.784 39.94 -0.22171 -0.23201 v Velocity[Z] -3.2373 3.1974 2.0478e-06 -5.3946e-08 v ǁVelocityǁ 0.00085164 50.011 9.3718 8.3123 v Pressure -6.4112e+05 2.5828e+05 -96126 -1.2052e+05 v TurbVisc 2.0983e-18 0.032352 0.00023826 0.00011189 v CourantNb 3.095e-08 0.011908 0.00017418 4.997e-06 v FourierNb 1.2476e-07 0.055084 0.00015894 8.967e-07 v total_pressure -5.398e+05 3.5961e+05 5199.3 -19196 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3056 0.1317 0.0034046 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 8.8868e-07 0.056028 0.00033312 5.8936e-06 INSTANT 0.876928000E-01 TIME STEP NUMBER 57126 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283137780E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.860214696E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.97118E-02 0.23454E+01 Friction velocity uk : 0.97118E-02 0.23454E+01 Dimensionless distance yplus : 0.93479E-02 0.23062E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 3.988553391e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29786E+08 1 0.21480E-09 0.57994E+02 0.27955E+04 c Velocity[X] 0.32998E+02 c Velocity[Y] 0.24996E+02 c Velocity[Z] 0.10694E-05 c Pressure 0.16053E-03 74 0.79976E-04 0.86208E-03 0.74242E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -36.409 49.667 5.6053 7.9971 v Velocity[Y] -36.796 39.953 -0.22188 -0.23252 v Velocity[Z] -3.2376 3.1975 2.0474e-06 -5.3946e-08 v ǁVelocityǁ 0.0009856 50.024 9.3733 8.3127 v Pressure -6.4104e+05 2.5863e+05 -97378 -1.2165e+05 v TurbVisc 1.8044e-18 0.032365 0.00023834 0.00011201 v CourantNb 1.1597e-08 0.01191 0.00017419 4.9971e-06 v FourierNb 1.2476e-07 0.055125 0.00015896 8.9751e-07 v total_pressure -5.3972e+05 3.5995e+05 3947 -20323 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3062 0.13176 0.003406 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 8.8943e-07 0.056071 0.00033315 5.8946e-06 INSTANT 0.876929000E-01 TIME STEP NUMBER 57127 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283143572E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.860617595E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.72319E-02 0.23461E+01 Friction velocity uk : 0.72319E-02 0.23461E+01 Dimensionless distance yplus : 0.69609E-02 0.23069E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 3.950648245e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29787E+08 1 0.21492E-09 0.58074E+02 0.27972E+04 c Velocity[X] 0.33042E+02 c Velocity[Y] 0.25032E+02 c Velocity[Z] 0.10572E-05 c Pressure 0.16447E-03 74 0.85992E-04 0.88246E-03 0.54246E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -36.424 49.679 5.6053 7.9972 v Velocity[Y] -36.807 39.967 -0.22204 -0.23303 v Velocity[Z] -3.2379 3.1976 2.0469e-06 -5.3946e-08 v ǁVelocityǁ 0.0011402 50.037 9.3748 8.3131 v Pressure -6.431e+05 2.5896e+05 -98591 -1.2225e+05 v TurbVisc 2.1353e-18 0.032378 0.00023841 0.00011213 v CourantNb 2.7906e-08 0.011911 0.00017421 4.9973e-06 v FourierNb 1.2476e-07 0.055166 0.00015897 8.9833e-07 v total_pressure -5.4177e+05 3.6029e+05 2734.1 -20923 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3069 0.13182 0.0034074 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 8.9018e-07 0.056115 0.00033318 5.8956e-06 INSTANT 0.876930000E-01 TIME STEP NUMBER 57128 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283148959E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.861020452E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10082E-02 0.23468E+01 Friction velocity uk : 0.10082E-02 0.23468E+01 Dimensionless distance yplus : 0.97042E-03 0.23075E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 3.755629079e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29789E+08 1 0.21500E-09 0.58134E+02 0.27984E+04 c Velocity[X] 0.33079E+02 c Velocity[Y] 0.25054E+02 c Velocity[Z] 0.10531E-05 c Pressure 0.16935E-03 65 0.75047E-04 0.90788E-03 0.56089E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -36.439 49.692 5.6054 7.9973 v Velocity[Y] -36.819 39.981 -0.22221 -0.23354 v Velocity[Z] -3.2382 3.1977 2.0465e-06 -5.3946e-08 v ǁVelocityǁ 0.0013045 50.05 9.3763 8.3136 v Pressure -6.4341e+05 2.593e+05 -99888 -1.2317e+05 v TurbVisc 2.0871e-18 0.032391 0.00023849 0.00011225 v CourantNb 2.6019e-08 0.011913 0.00017422 4.9974e-06 v FourierNb 1.2477e-07 0.055207 0.00015899 8.9915e-07 v total_pressure -5.4209e+05 3.6063e+05 1437.2 -21840 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3075 0.13188 0.0034088 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 8.9093e-07 0.056159 0.00033321 5.8966e-06 INSTANT 0.876931000E-01 TIME STEP NUMBER 57129 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283154471E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.861418794E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.48581E-02 0.23474E+01 Friction velocity uk : 0.48581E-02 0.23474E+01 Dimensionless distance yplus : 0.46761E-02 0.23082E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 3.640147819e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29791E+08 1 0.21509E-09 0.58224E+02 0.28003E+04 c Velocity[X] 0.33113E+02 c Velocity[Y] 0.25111E+02 c Velocity[Z] 0.10794E-05 c Pressure 0.16742E-03 16 0.55455E-04 0.89673E-03 0.39814E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -36.454 49.705 5.6054 7.9974 v Velocity[Y] -36.831 39.994 -0.22237 -0.23405 v Velocity[Z] -3.2385 3.1977 2.046e-06 -5.3946e-08 v ǁVelocityǁ 0.0014727 50.063 9.3779 8.314 v Pressure -6.4394e+05 2.5964e+05 -1.0115e+05 -1.2382e+05 v TurbVisc 2.1002e-18 0.032404 0.00023856 0.00011237 v CourantNb 2.4444e-08 0.011914 0.00017423 4.9975e-06 v FourierNb 1.2477e-07 0.055248 0.00015901 8.9997e-07 v total_pressure -5.4261e+05 3.6096e+05 172.02 -22498 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3082 0.13194 0.0034102 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 8.9169e-07 0.056203 0.00033324 5.8975e-06 INSTANT 0.876932000E-01 TIME STEP NUMBER 57130 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283159923E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.861811961E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.60018E-02 0.23480E+01 Friction velocity uk : 0.60018E-02 0.23480E+01 Dimensionless distance yplus : 0.57769E-02 0.23088E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 3.441747932e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29793E+08 1 0.21518E-09 0.58297E+02 0.28018E+04 c Velocity[X] 0.33165E+02 c Velocity[Y] 0.25132E+02 c Velocity[Z] 0.10804E-05 c Pressure 0.17325E-03 49 0.97397E-04 0.92714E-03 0.50667E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -36.468 49.718 5.6055 7.9975 v Velocity[Y] -36.842 40.008 -0.22254 -0.23456 v Velocity[Z] -3.2388 3.1978 2.0456e-06 -5.3946e-08 v ǁVelocityǁ 0.0016446 50.076 9.3794 8.3144 v Pressure -6.4519e+05 2.5998e+05 -1.0248e+05 -1.2473e+05 v TurbVisc 1.7874e-18 0.032417 0.00023864 0.00011249 v CourantNb 1.1965e-08 0.011916 0.00017425 4.9977e-06 v FourierNb 1.2477e-07 0.05529 0.00015902 9.0079e-07 v total_pressure -5.4387e+05 3.613e+05 -1154.5 -23408 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3088 0.13199 0.0034117 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 8.9244e-07 0.056247 0.00033327 5.8985e-06 INSTANT 0.876933000E-01 TIME STEP NUMBER 57131 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283165185E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.862195791E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.89361E-02 0.23487E+01 Friction velocity uk : 0.89361E-02 0.23487E+01 Dimensionless distance yplus : 0.86012E-02 0.23094E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 3.424963672e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29795E+08 1 0.21529E-09 0.58375E+02 0.28034E+04 c Velocity[X] 0.33212E+02 c Velocity[Y] 0.25163E+02 c Velocity[Z] 0.10624E-05 c Pressure 0.17548E-03 26 0.81601E-04 0.93820E-03 0.46610E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -36.483 49.73 5.6055 7.9976 v Velocity[Y] -36.854 40.022 -0.22271 -0.23507 v Velocity[Z] -3.2391 3.1979 2.0451e-06 -5.3946e-08 v ǁVelocityǁ 0.0018207 50.089 9.3809 8.3148 v Pressure -6.4637e+05 2.603e+05 -1.0388e+05 -1.256e+05 v TurbVisc 2.0613e-18 0.03243 0.00023871 0.00011261 v CourantNb 2.1731e-08 0.011917 0.00017426 4.9978e-06 v FourierNb 1.2477e-07 0.055331 0.00015904 9.0161e-07 v total_pressure -5.4504e+05 3.6163e+05 -2558.6 -24272 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3094 0.13205 0.0034131 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 8.932e-07 0.056292 0.0003333 5.8995e-06 INSTANT 0.876934000E-01 TIME STEP NUMBER 57132 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283170347E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.862575070E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11475E-01 0.23493E+01 Friction velocity uk : 0.11475E-01 0.23493E+01 Dimensionless distance yplus : 0.11045E-01 0.23101E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 3.250727821e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29797E+08 1 0.21538E-09 0.58466E+02 0.28054E+04 c Velocity[X] 0.33255E+02 c Velocity[Y] 0.25210E+02 c Velocity[Z] 0.10963E-05 c Pressure 0.17710E-03 18 0.55408E-04 0.94603E-03 0.42721E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -36.498 49.743 5.6056 7.9977 v Velocity[Y] -36.866 40.035 -0.22287 -0.23558 v Velocity[Z] -3.2394 3.198 2.0447e-06 -5.3946e-08 v ǁVelocityǁ 0.001997 50.102 9.3824 8.3152 v Pressure -6.4774e+05 2.6063e+05 -1.053e+05 -1.2635e+05 v TurbVisc 2.093e-18 0.032443 0.00023879 0.00011273 v CourantNb 1.9999e-08 0.011919 0.00017427 4.998e-06 v FourierNb 1.2477e-07 0.055373 0.00015906 9.0243e-07 v total_pressure -5.4641e+05 3.6196e+05 -3972.8 -25025 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3101 0.13211 0.0034146 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 8.9396e-07 0.056336 0.00033333 5.9004e-06 INSTANT 0.876935000E-01 TIME STEP NUMBER 57133 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283175353E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.862951241E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13689E-01 0.23499E+01 Friction velocity uk : 0.13689E-01 0.23499E+01 Dimensionless distance yplus : 0.13176E-01 0.23107E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 3.039018614e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29798E+08 1 0.21546E-09 0.58539E+02 0.28069E+04 c Velocity[X] 0.33295E+02 c Velocity[Y] 0.25244E+02 c Velocity[Z] 0.10816E-05 c Pressure 0.18302E-03 24 0.99898E-04 0.97683E-03 0.64750E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -36.512 49.756 5.6056 7.9978 v Velocity[Y] -36.877 40.049 -0.22304 -0.23609 v Velocity[Z] -3.2397 3.1981 2.0443e-06 -5.3946e-08 v ǁVelocityǁ 0.0018855 50.115 9.3839 8.3156 v Pressure -6.4845e+05 2.6096e+05 -1.0677e+05 -1.2754e+05 v TurbVisc 1.0067e-18 0.032456 0.00023886 0.00011285 v CourantNb 1.8212e-08 0.01192 0.00017428 4.9981e-06 v FourierNb 1.2477e-07 0.055415 0.00015908 9.0326e-07 v total_pressure -5.4712e+05 3.6229e+05 -5441.4 -26214 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3107 0.13217 0.003416 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 8.9472e-07 0.056381 0.00033336 5.9014e-06 INSTANT 0.876936000E-01 TIME STEP NUMBER 57134 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283180246E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.863322290E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15550E-01 0.23506E+01 Friction velocity uk : 0.15550E-01 0.23506E+01 Dimensionless distance yplus : 0.14967E-01 0.23113E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 3.114312169e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29800E+08 1 0.21557E-09 0.58614E+02 0.28084E+04 c Velocity[X] 0.33334E+02 c Velocity[Y] 0.25279E+02 c Velocity[Z] 0.10655E-05 c Pressure 0.18519E-03 228 0.84690E-04 0.98749E-03 0.46739E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -36.527 49.769 5.6057 7.9979 v Velocity[Y] -36.889 40.062 -0.22321 -0.23661 v Velocity[Z] -3.24 3.1982 2.0438e-06 -5.3946e-08 v ǁVelocityǁ 0.0018804 50.128 9.3854 8.316 v Pressure -6.4915e+05 2.613e+05 -1.0821e+05 -1.2841e+05 v TurbVisc 2.1107e-18 0.032469 0.00023894 0.00011297 v CourantNb 1.7622e-08 0.011921 0.0001743 4.9983e-06 v FourierNb 1.2477e-07 0.055457 0.0001591 9.0408e-07 v total_pressure -5.4783e+05 3.6262e+05 -6885.3 -27090 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3113 0.13223 0.0034174 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 8.9548e-07 0.056426 0.00033339 5.9024e-06 INSTANT 0.876937000E-01 TIME STEP NUMBER 57135 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283185117E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.863688238E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.17109E-01 0.23512E+01 Friction velocity uk : 0.17109E-01 0.23512E+01 Dimensionless distance yplus : 0.16468E-01 0.23119E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 2.830549102e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29802E+08 1 0.21566E-09 0.58705E+02 0.28103E+04 c Velocity[X] 0.33363E+02 c Velocity[Y] 0.25342E+02 c Velocity[Z] 0.10747E-05 c Pressure 0.18651E-03 9 0.56260E-04 0.99367E-03 0.47813E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -36.542 49.781 5.6057 7.9979 v Velocity[Y] -36.901 40.076 -0.22338 -0.23712 v Velocity[Z] -3.2403 3.1983 2.0434e-06 -5.3947e-08 v ǁVelocityǁ 0.0020213 50.141 9.3869 8.3164 v Pressure -6.4979e+05 2.6163e+05 -1.0975e+05 -1.2926e+05 v TurbVisc 1.1499e-19 0.032482 0.00023901 0.00011309 v CourantNb 1.6191e-08 0.011923 0.00017431 4.9984e-06 v FourierNb 1.2477e-07 0.055499 0.00015911 9.049e-07 v total_pressure -5.4847e+05 3.6296e+05 -8429.3 -27932 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3119 0.13229 0.0034189 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 8.9624e-07 0.05647 0.00033342 5.9033e-06 INSTANT 0.876938000E-01 TIME STEP NUMBER 57136 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283189923E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.864046245E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.16893E-01 0.23518E+01 Friction velocity uk : 0.16893E-01 0.23518E+01 Dimensionless distance yplus : 0.16275E-01 0.23125E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 2.808071379e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29804E+08 1 0.21575E-09 0.58786E+02 0.28120E+04 c Velocity[X] 0.33431E+02 c Velocity[Y] 0.25355E+02 c Velocity[Z] 0.10702E-05 c Pressure 0.19225E-03 116 0.77754E-04 0.10233E-02 0.63889E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -36.556 49.794 5.6058 7.998 v Velocity[Y] -36.912 40.09 -0.22355 -0.23764 v Velocity[Z] -3.2406 3.1984 2.0429e-06 -5.3947e-08 v ǁVelocityǁ 0.0020506 50.154 9.3884 8.3169 v Pressure -6.5158e+05 2.6196e+05 -1.1124e+05 -1.3022e+05 v TurbVisc 1.1529e-18 0.032495 0.00023909 0.00011321 v CourantNb 1.5034e-08 0.011924 0.00017432 4.9986e-06 v FourierNb 1.2477e-07 0.055541 0.00015913 9.0572e-07 v total_pressure -5.5026e+05 3.6329e+05 -9919.1 -28898 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3125 0.13234 0.0034202 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 8.97e-07 0.056515 0.00033345 5.9043e-06 INSTANT 0.876939000E-01 TIME STEP NUMBER 57137 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283194434E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.864400063E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19803E-01 0.23525E+01 Friction velocity uk : 0.19803E-01 0.23525E+01 Dimensionless distance yplus : 0.19079E-01 0.23131E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 2.768086296e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29806E+08 1 0.21586E-09 0.58876E+02 0.28139E+04 c Velocity[X] 0.33458E+02 c Velocity[Y] 0.25417E+02 c Velocity[Z] 0.10655E-05 c Pressure 0.19544E-03 533 0.82463E-04 0.10394E-02 0.72165E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -36.571 49.807 5.6058 7.9981 v Velocity[Y] -36.924 40.103 -0.22371 -0.23815 v Velocity[Z] -3.2409 3.1985 2.0425e-06 -5.3947e-08 v ǁVelocityǁ 0.0022643 50.167 9.3899 8.3173 v Pressure -6.5163e+05 2.623e+05 -1.1287e+05 -1.3134e+05 v TurbVisc 1.6304e-18 0.032508 0.00023917 0.00011333 v CourantNb 1.3654e-08 0.011926 0.00017433 4.9987e-06 v FourierNb 1.2477e-07 0.055583 0.00015915 9.0655e-07 v total_pressure -5.503e+05 3.6363e+05 -11546 -30017 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3131 0.1324 0.0034216 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 8.9776e-07 0.05656 0.00033348 5.9053e-06 INSTANT 0.876940000E-01 TIME STEP NUMBER 57138 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283199070E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.864744665E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15522E-01 0.23531E+01 Friction velocity uk : 0.15522E-01 0.23531E+01 Dimensionless distance yplus : 0.14959E-01 0.23137E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 2.657791088e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29807E+08 1 0.21596E-09 0.58956E+02 0.28156E+04 c Velocity[X] 0.33515E+02 c Velocity[Y] 0.25441E+02 c Velocity[Z] 0.10678E-05 c Pressure 0.19955E-03 121 0.96544E-04 0.10603E-02 0.60756E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -36.585 49.82 5.6059 7.9982 v Velocity[Y] -36.935 40.117 -0.22388 -0.23867 v Velocity[Z] -3.2412 3.1986 2.042e-06 -5.3947e-08 v ǁVelocityǁ 0.0026145 50.18 9.3915 8.3177 v Pressure -6.5372e+05 2.6262e+05 -1.144e+05 -1.3206e+05 v TurbVisc 1.7973e-18 0.032521 0.00023924 0.00011345 v CourantNb 1.2495e-08 0.011927 0.00017435 4.9988e-06 v FourierNb 1.2477e-07 0.055625 0.00015917 9.0737e-07 v total_pressure -5.5239e+05 3.6394e+05 -13077 -30736 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3137 0.13246 0.003423 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 8.9853e-07 0.056604 0.00033351 5.9062e-06 INSTANT 0.876941000E-01 TIME STEP NUMBER 57139 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283203258E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.865086093E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11189E-01 0.23537E+01 Friction velocity uk : 0.11189E-01 0.23537E+01 Dimensionless distance yplus : 0.10783E-01 0.23143E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 2.607467762e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29809E+08 1 0.21604E-09 0.59014E+02 0.28167E+04 c Velocity[X] 0.33545E+02 c Velocity[Y] 0.25469E+02 c Velocity[Z] 0.10701E-05 c Pressure 0.20348E-03 107 0.81758E-04 0.10802E-02 0.70812E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -36.6 49.832 5.6059 7.9982 v Velocity[Y] -36.947 40.131 -0.22405 -0.23918 v Velocity[Z] -3.2415 3.1987 2.0416e-06 -5.3947e-08 v ǁVelocityǁ 0.0027448 50.193 9.393 8.3181 v Pressure -6.541e+05 2.6295e+05 -1.1608e+05 -1.3331e+05 v TurbVisc 1.617e-18 0.032534 0.00023932 0.00011357 v CourantNb 1.2574e-08 0.011929 0.00017436 4.999e-06 v FourierNb 1.2477e-07 0.055666 0.00015918 9.082e-07 v total_pressure -5.5278e+05 3.6427e+05 -14759 -31986 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3143 0.13251 0.0034243 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 8.9929e-07 0.056648 0.00033354 5.9072e-06 INSTANT 0.876942000E-01 TIME STEP NUMBER 57140 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283207517E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.865415738E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.18541E-01 0.23543E+01 Friction velocity uk : 0.18541E-01 0.23543E+01 Dimensionless distance yplus : 0.17868E-01 0.23149E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 2.522206300e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29811E+08 1 0.21614E-09 0.59107E+02 0.28187E+04 c Velocity[X] 0.33578E+02 c Velocity[Y] 0.25529E+02 c Velocity[Z] 0.10796E-05 c Pressure 0.20072E-03 9 0.57700E-04 0.10646E-02 0.47567E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -36.615 49.845 5.6059 7.9983 v Velocity[Y] -36.958 40.144 -0.22422 -0.2397 v Velocity[Z] -3.2417 3.1988 2.0411e-06 -5.3947e-08 v ǁVelocityǁ 0.0029043 50.206 9.3945 8.3184 v Pressure -6.5467e+05 2.6327e+05 -1.1771e+05 -1.3416e+05 v TurbVisc 1.4154e-18 0.032547 0.00023939 0.0001137 v CourantNb 1.1582e-08 0.01193 0.00017437 4.9991e-06 v FourierNb 1.2477e-07 0.055707 0.0001592 9.0902e-07 v total_pressure -5.5334e+05 3.646e+05 -16384 -32838 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3149 0.13257 0.0034257 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 9.0006e-07 0.056693 0.00033357 5.9081e-06 INSTANT 0.876943000E-01 TIME STEP NUMBER 57141 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283211685E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.865739933E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13908E-01 0.23549E+01 Friction velocity uk : 0.13908E-01 0.23549E+01 Dimensionless distance yplus : 0.13403E-01 0.23155E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 2.407770941e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29813E+08 1 0.21623E-09 0.59189E+02 0.28204E+04 c Velocity[X] 0.33643E+02 c Velocity[Y] 0.25546E+02 c Velocity[Z] 0.10800E-05 c Pressure 0.20581E-03 373 0.78046E-04 0.10906E-02 0.70701E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -36.629 49.858 5.606 7.9984 v Velocity[Y] -36.97 40.158 -0.22439 -0.24022 v Velocity[Z] -3.242 3.1989 2.0407e-06 -5.3947e-08 v ǁVelocityǁ 0.0025535 50.219 9.396 8.3188 v Pressure -6.5655e+05 2.636e+05 -1.1939e+05 -1.353e+05 v TurbVisc 1.9198e-18 0.03256 0.00023947 0.00011382 v CourantNb 1.0602e-08 0.011932 0.00017438 4.9993e-06 v FourierNb 1.2477e-07 0.055749 0.00015922 9.0985e-07 v total_pressure -5.5523e+05 3.6493e+05 -18064 -33979 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3155 0.13262 0.0034269 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 9.0083e-07 0.056737 0.0003336 5.9091e-06 INSTANT 0.876944000E-01 TIME STEP NUMBER 57142 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283215547E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.866056609E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10192E-01 0.23555E+01 Friction velocity uk : 0.10192E-01 0.23555E+01 Dimensionless distance yplus : 0.98221E-02 0.23161E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 2.365487222e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29815E+08 1 0.21633E-09 0.59280E+02 0.28223E+04 c Velocity[X] 0.33674E+02 c Velocity[Y] 0.25606E+02 c Velocity[Z] 0.10750E-05 c Pressure 0.20871E-03 324 0.83554E-04 0.11050E-02 0.72084E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -36.644 49.87 5.606 7.9984 v Velocity[Y] -36.982 40.171 -0.22456 -0.24074 v Velocity[Z] -3.2423 3.199 2.0402e-06 -5.3947e-08 v ǁVelocityǁ 0.0025365 50.232 9.3975 8.3192 v Pressure -6.5654e+05 2.6394e+05 -1.2113e+05 -1.3643e+05 v TurbVisc 1.3533e-18 0.032573 0.00023954 0.00011394 v CourantNb 9.2097e-09 0.011933 0.0001744 4.9994e-06 v FourierNb 1.2477e-07 0.05579 0.00015924 9.1068e-07 v total_pressure -5.5522e+05 3.6527e+05 -19807 -35109 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3161 0.13267 0.0034283 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 9.016e-07 0.056781 0.00033364 5.9101e-06 INSTANT 0.876945000E-01 TIME STEP NUMBER 57143 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283219556E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.866367828E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10164E-01 0.23561E+01 Friction velocity uk : 0.10164E-01 0.23561E+01 Dimensionless distance yplus : 0.97954E-02 0.23167E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 2.322991055e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29816E+08 1 0.21644E-09 0.59361E+02 0.28240E+04 c Velocity[X] 0.33730E+02 c Velocity[Y] 0.25632E+02 c Velocity[Z] 0.10701E-05 c Pressure 0.21236E-03 235 0.97670E-04 0.11233E-02 0.66146E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -36.658 49.883 5.606 7.9985 v Velocity[Y] -36.993 40.185 -0.22473 -0.24126 v Velocity[Z] -3.2426 3.1991 2.0398e-06 -5.3947e-08 v ǁVelocityǁ 0.002821 50.244 9.399 8.3196 v Pressure -6.5874e+05 2.6425e+05 -1.2283e+05 -1.3733e+05 v TurbVisc 1.0995e-18 0.032586 0.00023962 0.00011406 v CourantNb 8.0769e-09 0.011934 0.00017441 4.9995e-06 v FourierNb 1.2477e-07 0.055831 0.00015926 9.115e-07 v total_pressure -5.5742e+05 3.6557e+05 -21504 -36006 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3167 0.13274 0.0034298 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 9.0237e-07 0.056825 0.00033367 5.911e-06 INSTANT 0.876946000E-01 TIME STEP NUMBER 57144 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283223061E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.866674703E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10557E-01 0.23567E+01 Friction velocity uk : 0.10557E-01 0.23567E+01 Dimensionless distance yplus : 0.10174E-01 0.23173E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 2.266020808e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29818E+08 1 0.21652E-09 0.59418E+02 0.28251E+04 c Velocity[X] 0.33767E+02 c Velocity[Y] 0.25652E+02 c Velocity[Z] 0.10774E-05 c Pressure 0.21591E-03 536 0.82988E-04 0.11411E-02 0.65280E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -36.673 49.895 5.6061 7.9985 v Velocity[Y] -37.005 40.198 -0.2249 -0.24178 v Velocity[Z] -3.2429 3.1992 2.0393e-06 -5.3947e-08 v ǁVelocityǁ 0.0031599 50.257 9.4005 8.32 v Pressure -6.5902e+05 2.6459e+05 -1.2459e+05 -1.3849e+05 v TurbVisc 9.8504e-19 0.032599 0.0002397 0.00011418 v CourantNb 6.9571e-09 0.011936 0.00017442 4.9997e-06 v FourierNb 1.2477e-07 0.055872 0.00015928 9.1233e-07 v total_pressure -5.5769e+05 3.6591e+05 -23269 -37166 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3173 0.1328 0.0034313 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 9.0314e-07 0.056868 0.0003337 5.912e-06 INSTANT 0.876947000E-01 TIME STEP NUMBER 57145 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283226694E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.866969943E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.85743E-02 0.23573E+01 Friction velocity uk : 0.85743E-02 0.23573E+01 Dimensionless distance yplus : 0.82631E-02 0.23179E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 2.214662341e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29820E+08 1 0.21662E-09 0.59512E+02 0.28271E+04 c Velocity[X] 0.33787E+02 c Velocity[Y] 0.25725E+02 c Velocity[Z] 0.10901E-05 c Pressure 0.21280E-03 9 0.59528E-04 0.11236E-02 0.58020E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -36.687 49.908 5.6061 7.9986 v Velocity[Y] -37.016 40.212 -0.22507 -0.2423 v Velocity[Z] -3.2432 3.1993 2.0389e-06 -5.3947e-08 v ǁVelocityǁ 0.0031576 50.27 9.402 8.3204 v Pressure -6.5976e+05 2.649e+05 -1.2639e+05 -1.3957e+05 v TurbVisc 8.7958e-19 0.032612 0.00023977 0.0001143 v CourantNb 5.882e-09 0.011937 0.00017443 4.9998e-06 v FourierNb 1.2477e-07 0.055913 0.00015929 9.1316e-07 v total_pressure -5.5844e+05 3.6623e+05 -25067 -38243 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3179 0.13286 0.0034327 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 9.0391e-07 0.056912 0.00033373 5.913e-06 INSTANT 0.876948000E-01 TIME STEP NUMBER 57146 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283230133E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.867255937E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13988E-01 0.23578E+01 Friction velocity uk : 0.13988E-01 0.23578E+01 Dimensionless distance yplus : 0.13481E-01 0.23184E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 2.093622290e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29822E+08 1 0.21671E-09 0.59597E+02 0.28289E+04 c Velocity[X] 0.33864E+02 c Velocity[Y] 0.25733E+02 c Velocity[Z] 0.10826E-05 c Pressure 0.21745E-03 172 0.79298E-04 0.11471E-02 0.69367E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -36.702 49.92 5.6061 7.9986 v Velocity[Y] -37.027 40.225 -0.22525 -0.24282 v Velocity[Z] -3.2435 3.1994 2.0385e-06 -5.3947e-08 v ǁVelocityǁ 0.0033085 50.283 9.4035 8.3208 v Pressure -6.6152e+05 2.6523e+05 -1.2816e+05 -1.4068e+05 v TurbVisc 1.2332e-18 0.032625 0.00023985 0.00011442 v CourantNb 5.2931e-09 0.011939 0.00017445 4.9999e-06 v FourierNb 1.2477e-07 0.055954 0.00015931 9.1399e-07 v total_pressure -5.602e+05 3.6656e+05 -26834 -39350 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3184 0.13292 0.0034343 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 9.0469e-07 0.056955 0.00033376 5.9139e-06 INSTANT 0.876949000E-01 TIME STEP NUMBER 57147 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283233332E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.867534070E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.92843E-02 0.23584E+01 Friction velocity uk : 0.92843E-02 0.23584E+01 Dimensionless distance yplus : 0.89474E-02 0.23190E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 2.051805357e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29823E+08 1 0.21682E-09 0.59688E+02 0.28308E+04 c Velocity[X] 0.33897E+02 c Velocity[Y] 0.25791E+02 c Velocity[Z] 0.10815E-05 c Pressure 0.21988E-03 67 0.84717E-04 0.11589E-02 0.73677E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -36.716 49.933 5.6062 7.9987 v Velocity[Y] -37.039 40.239 -0.22542 -0.24335 v Velocity[Z] -3.2438 3.1995 2.038e-06 -5.3948e-08 v ǁVelocityǁ 0.0031827 50.296 9.4051 8.3212 v Pressure -6.615e+05 2.6556e+05 -1.3002e+05 -1.4187e+05 v TurbVisc 9.2476e-19 0.032638 0.00023992 0.00011455 v CourantNb 3.9121e-09 0.01194 0.00017446 5.0001e-06 v FourierNb 1.2477e-07 0.055994 0.00015933 9.1482e-07 v total_pressure -5.6018e+05 3.6689e+05 -28693 -40545 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.319 0.13298 0.0034357 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 9.0546e-07 0.056998 0.00033379 5.9149e-06 INSTANT 0.876950000E-01 TIME STEP NUMBER 57148 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283236666E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.867805222E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12598E-01 0.23590E+01 Friction velocity uk : 0.12598E-01 0.23590E+01 Dimensionless distance yplus : 0.12140E-01 0.23196E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.996292595e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29825E+08 1 0.21692E-09 0.59770E+02 0.28325E+04 c Velocity[X] 0.33945E+02 c Velocity[Y] 0.25825E+02 c Velocity[Z] 0.10730E-05 c Pressure 0.22301E-03 234 0.99216E-04 0.11743E-02 0.71825E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -36.731 49.945 5.6062 7.9987 v Velocity[Y] -37.05 40.252 -0.22559 -0.24387 v Velocity[Z] -3.2441 3.1996 2.0376e-06 -5.3948e-08 v ǁVelocityǁ 0.0031616 50.308 9.4066 8.3215 v Pressure -6.6384e+05 2.6587e+05 -1.3187e+05 -1.4297e+05 v TurbVisc 7.3401e-19 0.032651 0.00024 0.00011467 v CourantNb 2.9462e-09 0.011942 0.00017447 5.0002e-06 v FourierNb 1.2477e-07 0.056034 0.00015935 9.1564e-07 v total_pressure -5.6251e+05 3.6719e+05 -30547 -41643 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3196 0.13304 0.0034372 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 9.0624e-07 0.057041 0.00033382 5.9159e-06 INSTANT 0.876951000E-01 TIME STEP NUMBER 57149 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283239423E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.868070270E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.79918E-02 0.23596E+01 Friction velocity uk : 0.79918E-02 0.23596E+01 Dimensionless distance yplus : 0.76923E-02 0.23202E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.931920164e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29827E+08 1 0.21700E-09 0.59827E+02 0.28336E+04 c Velocity[X] 0.33988E+02 c Velocity[Y] 0.25840E+02 c Velocity[Z] 0.10749E-05 c Pressure 0.22618E-03 551 0.84314E-04 0.11900E-02 0.63427E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -36.745 49.958 5.6062 7.9988 v Velocity[Y] -37.062 40.266 -0.22576 -0.24439 v Velocity[Z] -3.2444 3.1997 2.0371e-06 -5.3948e-08 v ǁVelocityǁ 0.0028732 50.321 9.4081 8.3219 v Pressure -6.6405e+05 2.662e+05 -1.3372e+05 -1.4411e+05 v TurbVisc 6.657e-19 0.032664 0.00024007 0.00011479 v CourantNb 2.1947e-09 0.011943 0.00017449 5.0003e-06 v FourierNb 1.2478e-07 0.056074 0.00015937 9.1647e-07 v total_pressure -5.6272e+05 3.6753e+05 -32396 -42785 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3202 0.1331 0.0034386 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 9.0701e-07 0.057084 0.00033385 5.9168e-06 INSTANT 0.876952000E-01 TIME STEP NUMBER 57150 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283242347E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.868326045E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.77209E-02 0.23602E+01 Friction velocity uk : 0.77209E-02 0.23602E+01 Dimensionless distance yplus : 0.74317E-02 0.23207E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.862392287e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29828E+08 1 0.21711E-09 0.59923E+02 0.28356E+04 c Velocity[X] 0.34008E+02 c Velocity[Y] 0.25915E+02 c Velocity[Z] 0.10869E-05 c Pressure 0.22261E-03 9 0.60559E-04 0.11701E-02 0.59692E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -36.76 49.97 5.6063 7.9988 v Velocity[Y] -37.073 40.279 -0.22594 -0.24492 v Velocity[Z] -3.2447 3.1997 2.0367e-06 -5.3948e-08 v ǁVelocityǁ 0.0026458 50.334 9.4096 8.3223 v Pressure -6.6481e+05 2.6652e+05 -1.3562e+05 -1.4524e+05 v TurbVisc 6.1786e-19 0.032677 0.00024015 0.00011491 v CourantNb 2.1923e-09 0.011944 0.0001745 5.0005e-06 v FourierNb 1.2478e-07 0.056114 0.00015939 9.1731e-07 v total_pressure -5.6349e+05 3.6784e+05 -34297 -43919 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3207 0.13316 0.0034401 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 9.0779e-07 0.057127 0.00033389 5.9178e-06 INSTANT 0.876953000E-01 TIME STEP NUMBER 57151 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283245050E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.868570930E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11747E-01 0.23607E+01 Friction velocity uk : 0.11747E-01 0.23607E+01 Dimensionless distance yplus : 0.11299E-01 0.23213E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.716283109e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29830E+08 1 0.21719E-09 0.60009E+02 0.28374E+04 c Velocity[X] 0.34087E+02 c Velocity[Y] 0.25922E+02 c Velocity[Z] 0.10846E-05 c Pressure 0.22677E-03 257 0.80595E-04 0.11909E-02 0.72316E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -36.774 49.982 5.6063 7.9988 v Velocity[Y] -37.084 40.292 -0.22611 -0.24544 v Velocity[Z] -3.245 3.1998 2.0362e-06 -5.3948e-08 v ǁVelocityǁ 0.0025656 50.346 9.4111 8.3227 v Pressure -6.666e+05 2.6684e+05 -1.375e+05 -1.4644e+05 v TurbVisc 8.9581e-19 0.03269 0.00024023 0.00011503 v CourantNb 2.3374e-09 0.011946 0.00017451 5.0006e-06 v FourierNb 1.2478e-07 0.056154 0.00015941 9.1814e-07 v total_pressure -5.6528e+05 3.6816e+05 -36170 -45112 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3213 0.13323 0.0034418 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 9.0857e-07 0.05717 0.00033392 5.9187e-06 INSTANT 0.876954000E-01 TIME STEP NUMBER 57152 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283247510E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.868807018E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.82650E-02 0.23613E+01 Friction velocity uk : 0.82650E-02 0.23613E+01 Dimensionless distance yplus : 0.79494E-02 0.23219E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.655786393e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29832E+08 1 0.21730E-09 0.60102E+02 0.28394E+04 c Velocity[X] 0.34115E+02 c Velocity[Y] 0.25986E+02 c Velocity[Z] 0.10768E-05 c Pressure 0.22876E-03 610 0.86325E-04 0.12003E-02 0.78086E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -36.788 49.995 5.6063 7.9989 v Velocity[Y] -37.095 40.306 -0.22629 -0.24597 v Velocity[Z] -3.2453 3.1999 2.0358e-06 -5.3948e-08 v ǁVelocityǁ 0.0023358 50.359 9.4126 8.323 v Pressure -6.6663e+05 2.6717e+05 -1.3947e+05 -1.4775e+05 v TurbVisc 6.6572e-19 0.032703 0.0002403 0.00011515 v CourantNb 3.2094e-09 0.011947 0.00017452 5.0007e-06 v FourierNb 1.2478e-07 0.056194 0.00015943 9.1897e-07 v total_pressure -5.6531e+05 3.685e+05 -38142 -46427 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3219 0.13329 0.0034433 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 9.0935e-07 0.057212 0.00033395 5.9197e-06 INSTANT 0.876955000E-01 TIME STEP NUMBER 57153 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283250061E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.869036436E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.31348E-02 0.23619E+01 Friction velocity uk : 0.31348E-02 0.23619E+01 Dimensionless distance yplus : 0.30151E-02 0.23224E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.575000095e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29834E+08 1 0.21741E-09 0.60159E+02 0.28405E+04 c Velocity[X] 0.34174E+02 c Velocity[Y] 0.25985E+02 c Velocity[Z] 0.10690E-05 c Pressure 0.23147E-03 273 0.75670E-04 0.12134E-02 0.52815E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -36.803 50.007 5.6063 7.9989 v Velocity[Y] -37.107 40.319 -0.22646 -0.2465 v Velocity[Z] -3.2456 3.2 2.0353e-06 -5.3948e-08 v ǁVelocityǁ 0.0018578 50.371 9.4141 8.3234 v Pressure -6.6817e+05 2.6749e+05 -1.4134e+05 -1.4869e+05 v TurbVisc 5.1129e-19 0.032715 0.00024038 0.00011528 v CourantNb 2.9953e-09 0.011949 0.00017454 5.0009e-06 v FourierNb 1.2478e-07 0.056233 0.00015944 9.198e-07 v total_pressure -5.6685e+05 3.6881e+05 -40017 -47365 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3224 0.13335 0.0034448 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 9.1013e-07 0.057255 0.00033398 5.9207e-06 INSTANT 0.876956000E-01 TIME STEP NUMBER 57154 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283252302E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.869260003E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.46683E-02 0.23624E+01 Friction velocity uk : 0.46683E-02 0.23624E+01 Dimensionless distance yplus : 0.44900E-02 0.23230E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.474993316e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29835E+08 1 0.21750E-09 0.60252E+02 0.28425E+04 c Velocity[X] 0.34205E+02 c Velocity[Y] 0.26047E+02 c Velocity[Z] 0.10819E-05 c Pressure 0.22860E-03 9 0.57984E-04 0.11973E-02 0.54793E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -36.817 50.019 5.6064 7.9989 v Velocity[Y] -37.118 40.332 -0.22664 -0.24702 v Velocity[Z] -3.2459 3.2001 2.0349e-06 -5.3948e-08 v ǁVelocityǁ 0.0019319 50.384 9.4156 8.3237 v Pressure -6.6987e+05 2.6779e+05 -1.4329e+05 -1.4979e+05 v TurbVisc 5.0635e-19 0.032728 0.00024045 0.0001154 v CourantNb 3.7475e-09 0.01195 0.00017455 5.001e-06 v FourierNb 1.2478e-07 0.056273 0.00015946 9.2063e-07 v total_pressure -5.6855e+05 3.6911e+05 -41970 -48469 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.323 0.13341 0.0034465 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 9.1092e-07 0.057297 0.00033401 5.9216e-06 INSTANT 0.876957000E-01 TIME STEP NUMBER 57155 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283254188E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.869468990E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10845E-01 0.23630E+01 Friction velocity uk : 0.10845E-01 0.23630E+01 Dimensionless distance yplus : 0.10431E-01 0.23235E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.292784182e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29837E+08 1 0.21757E-09 0.60333E+02 0.28441E+04 c Velocity[X] 0.34262E+02 c Velocity[Y] 0.26071E+02 c Velocity[Z] 0.10736E-05 c Pressure 0.23188E-03 145 0.98012E-04 0.12133E-02 0.73179E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -36.831 50.031 5.6064 7.9989 v Velocity[Y] -37.129 40.346 -0.22681 -0.24755 v Velocity[Z] -3.2462 3.2002 2.0345e-06 -5.3948e-08 v ǁVelocityǁ 0.0022267 50.396 9.4171 8.3241 v Pressure -6.704e+05 2.6811e+05 -1.4526e+05 -1.5125e+05 v TurbVisc 7.0945e-19 0.032741 0.00024053 0.00011552 v CourantNb 3.356e-09 0.011952 0.00017456 5.0011e-06 v FourierNb 1.2478e-07 0.056313 0.00015948 9.2146e-07 v total_pressure -5.6907e+05 3.6943e+05 -43934 -49925 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3235 0.13348 0.0034482 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 9.117e-07 0.05734 0.00033404 5.9226e-06 INSTANT 0.876958000E-01 TIME STEP NUMBER 57156 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283256101E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.869666925E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.14057E-01 0.23635E+01 Friction velocity uk : 0.14057E-01 0.23635E+01 Dimensionless distance yplus : 0.13520E-01 0.23240E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.181273319e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29839E+08 1 0.21770E-09 0.60411E+02 0.28457E+04 c Velocity[X] 0.34306E+02 c Velocity[Y] 0.26105E+02 c Velocity[Z] 0.10661E-05 c Pressure 0.23222E-03 410 0.81842E-04 0.12140E-02 0.60506E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -36.846 50.043 5.6064 7.999 v Velocity[Y] -37.14 40.359 -0.22699 -0.24808 v Velocity[Z] -3.2465 3.2003 2.034e-06 -5.3948e-08 v ǁVelocityǁ 0.0014395 50.409 9.4186 8.3245 v Pressure -6.7119e+05 2.6843e+05 -1.4728e+05 -1.5249e+05 v TurbVisc 2.4092e-19 0.032754 0.0002406 0.00011564 v CourantNb 3.1853e-09 0.011953 0.00017457 5.0012e-06 v FourierNb 1.2478e-07 0.056352 0.0001595 9.223e-07 v total_pressure -5.6987e+05 3.6975e+05 -45955 -51168 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.324 0.13354 0.0034499 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 9.1249e-07 0.057382 0.00033408 5.9235e-06 INSTANT 0.876959000E-01 TIME STEP NUMBER 57157 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283257905E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.869856034E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.17016E-01 0.23641E+01 Friction velocity uk : 0.17016E-01 0.23641E+01 Dimensionless distance yplus : 0.16366E-01 0.23246E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.145346653e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29840E+08 1 0.21779E-09 0.60506E+02 0.28477E+04 c Velocity[X] 0.34330E+02 c Velocity[Y] 0.26175E+02 c Velocity[Z] 0.10806E-05 c Pressure 0.23201E-03 9 0.54678E-04 0.12118E-02 0.57634E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -36.86 50.056 5.6064 7.999 v Velocity[Y] -37.151 40.372 -0.22716 -0.24861 v Velocity[Z] -3.2468 3.2004 2.0336e-06 -5.3948e-08 v ǁVelocityǁ 0.00082224 50.421 9.4201 8.3248 v Pressure -6.7199e+05 2.6875e+05 -1.4929e+05 -1.5364e+05 v TurbVisc 3.8503e-19 0.032767 0.00024068 0.00011577 v CourantNb 3.349e-09 0.011954 0.00017459 5.0014e-06 v FourierNb 1.2478e-07 0.056391 0.00015952 9.2313e-07 v total_pressure -5.7066e+05 3.7008e+05 -47962 -52314 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3246 0.1336 0.0034516 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 9.1327e-07 0.057424 0.00033411 5.9245e-06 INSTANT 0.876960000E-01 TIME STEP NUMBER 57158 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283259581E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.870041093E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19744E-01 0.23646E+01 Friction velocity uk : 0.19744E-01 0.23646E+01 Dimensionless distance yplus : 0.19063E-01 0.23251E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 8.347284569e-03 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29842E+08 1 0.21787E-09 0.60584E+02 0.28493E+04 c Velocity[X] 0.34399E+02 c Velocity[Y] 0.26186E+02 c Velocity[Z] 0.10726E-05 c Pressure 0.23513E-03 147 0.99005E-04 0.12270E-02 0.61563E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -36.874 50.068 5.6064 7.999 v Velocity[Y] -37.162 40.385 -0.22734 -0.24914 v Velocity[Z] -3.2471 3.2005 2.0331e-06 -5.3948e-08 v ǁVelocityǁ 0.0012483 50.434 9.4216 8.3252 v Pressure -6.7315e+05 2.6908e+05 -1.5122e+05 -1.5487e+05 v TurbVisc 5.2465e-19 0.03278 0.00024075 0.00011589 v CourantNb 3.5386e-09 0.011956 0.0001746 5.0015e-06 v FourierNb 1.2478e-07 0.056431 0.00015954 9.2397e-07 v total_pressure -5.7183e+05 3.704e+05 -49895 -53541 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3251 0.13366 0.0034532 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 9.1406e-07 0.057467 0.00033414 5.9254e-06 INSTANT 0.876961000E-01 TIME STEP NUMBER 57159 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283261036E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.870215308E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.20123E-01 0.23652E+01 Friction velocity uk : 0.20123E-01 0.23652E+01 Dimensionless distance yplus : 0.19429E-01 0.23256E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 8.059274492e-03 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29844E+08 1 0.21799E-09 0.60666E+02 0.28510E+04 c Velocity[X] 0.34450E+02 c Velocity[Y] 0.26216E+02 c Velocity[Z] 0.10603E-05 c Pressure 0.23520E-03 27 0.84194E-04 0.12262E-02 0.56022E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -36.888 50.08 5.6064 7.999 v Velocity[Y] -37.173 40.398 -0.22752 -0.24967 v Velocity[Z] -3.2474 3.2006 2.0327e-06 -5.3949e-08 v ǁVelocityǁ 0.0013295 50.446 9.4231 8.3255 v Pressure -6.744e+05 2.6939e+05 -1.5324e+05 -1.5604e+05 v TurbVisc 3.9273e-19 0.032793 0.00024083 0.00011601 v CourantNb 3.5145e-09 0.011957 0.00017461 5.0016e-06 v FourierNb 1.2478e-07 0.056471 0.00015956 9.248e-07 v total_pressure -5.7308e+05 3.7072e+05 -51918 -54710 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3256 0.13372 0.0034548 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 9.1485e-07 0.057509 0.00033417 5.9264e-06 INSTANT 0.876962000E-01 TIME STEP NUMBER 57160 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283262333E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.870376152E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.20821E-01 0.23657E+01 Friction velocity uk : 0.20821E-01 0.23657E+01 Dimensionless distance yplus : 0.20103E-01 0.23262E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 6.287882648e-03 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29845E+08 1 0.21808E-09 0.60763E+02 0.28531E+04 c Velocity[X] 0.34494E+02 c Velocity[Y] 0.26269E+02 c Velocity[Z] 0.10729E-05 c Pressure 0.23451E-03 9 0.58425E-04 0.12215E-02 0.55458E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -36.903 50.092 5.6065 7.999 v Velocity[Y] -37.184 40.411 -0.2277 -0.2502 v Velocity[Z] -3.2476 3.2007 2.0322e-06 -5.3949e-08 v ǁVelocityǁ 0.0015167 50.458 9.4246 8.3259 v Pressure -6.7595e+05 2.697e+05 -1.5529e+05 -1.5717e+05 v TurbVisc 4.0045e-19 0.032806 0.0002409 0.00011613 v CourantNb 4.0016e-09 0.011959 0.00017463 5.0017e-06 v FourierNb 1.2478e-07 0.05651 0.00015958 9.2564e-07 v total_pressure -5.7463e+05 3.7102e+05 -53968 -55846 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3262 0.13378 0.0034564 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 9.1563e-07 0.057552 0.00033421 5.9274e-06 INSTANT 0.876963000E-01 TIME STEP NUMBER 57161 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283263357E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.870529480E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.21676E-01 0.23662E+01 Friction velocity uk : 0.21676E-01 0.23662E+01 Dimensionless distance yplus : 0.20928E-01 0.23267E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 2.970770427e-03 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29847E+08 1 0.21815E-09 0.60857E+02 0.28550E+04 c Velocity[X] 0.34544E+02 c Velocity[Y] 0.26313E+02 c Velocity[Z] 0.10741E-05 c Pressure 0.23755E-03 54 0.77683E-04 0.12363E-02 0.84041E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -36.917 50.103 5.6065 7.999 v Velocity[Y] -37.195 40.424 -0.22787 -0.25073 v Velocity[Z] -3.2479 3.2008 2.0318e-06 -5.3949e-08 v ǁVelocityǁ 0.0018685 50.47 9.4261 8.3262 v Pressure -6.759e+05 2.7004e+05 -1.5731e+05 -1.5872e+05 v TurbVisc 5.6955e-19 0.032818 0.00024098 0.00011626 v CourantNb 4.4578e-09 0.01196 0.00017464 5.0018e-06 v FourierNb 1.2478e-07 0.056552 0.0001596 9.2647e-07 v total_pressure -5.7458e+05 3.7137e+05 -55988 -57395 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3267 0.13384 0.003458 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 9.1643e-07 0.057596 0.00033424 5.9283e-06 INSTANT 0.876964000E-01 TIME STEP NUMBER 57162 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283264545E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.870674793E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.22761E-01 0.23668E+01 Friction velocity uk : 0.22761E-01 0.23668E+01 Dimensionless distance yplus : 0.21976E-01 0.23272E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 2.208752457e-03 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29848E+08 1 0.21828E-09 0.60942E+02 0.28568E+04 c Velocity[X] 0.34593E+02 c Velocity[Y] 0.26349E+02 c Velocity[Z] 0.10893E-05 c Pressure 0.23837E-03 65 0.82747E-04 0.12394E-02 0.63197E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -36.931 50.115 5.6065 7.999 v Velocity[Y] -37.206 40.438 -0.22805 -0.25126 v Velocity[Z] -3.2482 3.2009 2.0313e-06 -5.3949e-08 v ǁVelocityǁ 0.0023005 50.482 9.4276 8.3265 v Pressure -6.7808e+05 2.7035e+05 -1.5935e+05 -1.5981e+05 v TurbVisc 4.4188e-19 0.032831 0.00024105 0.00011638 v CourantNb 4.7801e-09 0.011961 0.00017465 5.002e-06 v FourierNb 1.2478e-07 0.056592 0.00015962 9.2731e-07 v total_pressure -5.7675e+05 3.7167e+05 -58025 -58487 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3272 0.1339 0.0034595 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 9.1722e-07 0.057639 0.00033427 5.9293e-06 INSTANT 0.876965000E-01 TIME STEP NUMBER 57163 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283265172E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.870809609E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.23968E-01 0.23673E+01 Friction velocity uk : 0.23968E-01 0.23673E+01 Dimensionless distance yplus : 0.23141E-01 0.23277E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.404958063e-04 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29850E+08 1 0.21836E-09 0.61038E+02 0.28588E+04 c Velocity[X] 0.34632E+02 c Velocity[Y] 0.26406E+02 c Velocity[Z] 0.10666E-05 c Pressure 0.23988E-03 34 0.96540E-04 0.12461E-02 0.78629E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -36.945 50.127 5.6065 7.999 v Velocity[Y] -37.217 40.451 -0.22823 -0.2518 v Velocity[Z] -3.2485 3.201 2.0309e-06 -5.3949e-08 v ǁVelocityǁ 0.0027751 50.495 9.4291 8.3269 v Pressure -6.779e+05 2.7067e+05 -1.614e+05 -1.6116e+05 v TurbVisc 3.8896e-19 0.032844 0.00024113 0.0001165 v CourantNb 5.1881e-09 0.011963 0.00017466 5.0021e-06 v FourierNb 1.2478e-07 0.056633 0.00015964 9.2815e-07 v total_pressure -5.7657e+05 3.72e+05 -60072 -59835 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3277 0.13396 0.003461 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 9.1801e-07 0.057682 0.0003343 5.9302e-06 INSTANT 0.876966000E-01 TIME STEP NUMBER 57164 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283265969E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.870936127E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.25217E-01 0.23678E+01 Friction velocity uk : 0.25217E-01 0.23678E+01 Dimensionless distance yplus : 0.24347E-01 0.23282E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.831658342e-03 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29852E+08 1 0.21847E-09 0.61095E+02 0.28599E+04 c Velocity[X] 0.34689E+02 c Velocity[Y] 0.26406E+02 c Velocity[Z] 0.10561E-05 c Pressure 0.24132E-03 199 0.82224E-04 0.12524E-02 0.56439E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -36.959 50.139 5.6065 7.999 v Velocity[Y] -37.228 40.464 -0.22841 -0.25233 v Velocity[Z] -3.2488 3.2011 2.0305e-06 -5.3949e-08 v ǁVelocityǁ 0.002761 50.507 9.4306 8.3272 v Pressure -6.7955e+05 2.71e+05 -1.6341e+05 -1.6222e+05 v TurbVisc 3.7145e-19 0.032857 0.0002412 0.00011662 v CourantNb 5.4206e-09 0.011964 0.00017468 5.0022e-06 v FourierNb 1.2478e-07 0.056673 0.00015966 9.2898e-07 v total_pressure -5.7823e+05 3.7232e+05 -62083 -60893 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3282 0.13401 0.0034625 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 9.188e-07 0.057725 0.00033434 5.9312e-06 INSTANT 0.876967000E-01 TIME STEP NUMBER 57165 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283266454E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.871050389E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.24386E-01 0.23683E+01 Friction velocity uk : 0.24386E-01 0.23683E+01 Dimensionless distance yplus : 0.23544E-01 0.23287E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -4.171168403e-03 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29853E+08 1 0.21856E-09 0.61193E+02 0.28620E+04 c Velocity[X] 0.34728E+02 c Velocity[Y] 0.26466E+02 c Velocity[Z] 0.10742E-05 c Pressure 0.23664E-03 9 0.60414E-04 0.12270E-02 0.52935E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -36.973 50.151 5.6065 7.999 v Velocity[Y] -37.239 40.476 -0.22859 -0.25287 v Velocity[Z] -3.2491 3.2011 2.03e-06 -5.3949e-08 v ǁVelocityǁ 0.0019841 50.519 9.4321 8.3275 v Pressure -6.8122e+05 2.713e+05 -1.6544e+05 -1.6333e+05 v TurbVisc 3.6715e-19 0.03287 0.00024128 0.00011675 v CourantNb 5.5725e-09 0.011966 0.00017469 5.0023e-06 v FourierNb 1.2478e-07 0.056714 0.00015968 9.2982e-07 v total_pressure -5.7989e+05 3.7263e+05 -64119 -62009 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3287 0.13407 0.003464 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 9.196e-07 0.057769 0.00033437 5.9321e-06 INSTANT 0.876968000E-01 TIME STEP NUMBER 57166 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283266579E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.871153733E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.23311E-01 0.23687E+01 Friction velocity uk : 0.23311E-01 0.23687E+01 Dimensionless distance yplus : 0.22507E-01 0.23291E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -7.476804027e-03 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29855E+08 1 0.21863E-09 0.61291E+02 0.28640E+04 c Velocity[X] 0.34788E+02 c Velocity[Y] 0.26503E+02 c Velocity[Z] 0.10641E-05 c Pressure 0.23901E-03 53 0.78259E-04 0.12382E-02 0.84577E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -36.987 50.162 5.6065 7.999 v Velocity[Y] -37.249 40.489 -0.22877 -0.2534 v Velocity[Z] -3.2494 3.2012 2.0296e-06 -5.3949e-08 v ǁVelocityǁ 0.0011705 50.531 9.4336 8.3279 v Pressure -6.8103e+05 2.7164e+05 -1.6752e+05 -1.6493e+05 v TurbVisc 4.6246e-19 0.032882 0.00024135 0.00011687 v CourantNb 5.582e-09 0.011967 0.0001747 5.0024e-06 v FourierNb 1.2479e-07 0.056756 0.0001597 9.3066e-07 v total_pressure -5.7971e+05 3.7297e+05 -66196 -63605 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3291 0.13412 0.0034654 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 9.204e-07 0.057814 0.0003344 5.9331e-06 INSTANT 0.876969000E-01 TIME STEP NUMBER 57167 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283266959E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.871247044E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11769E-01 0.23692E+01 Friction velocity uk : 0.11769E-01 0.23692E+01 Dimensionless distance yplus : 0.11353E-01 0.23296E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -8.830681056e-03 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29856E+08 1 0.21877E-09 0.61377E+02 0.28658E+04 c Velocity[X] 0.34837E+02 c Velocity[Y] 0.26541E+02 c Velocity[Z] 0.10829E-05 c Pressure 0.23937E-03 279 0.84045E-04 0.12389E-02 0.65809E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -37.001 50.174 5.6065 7.999 v Velocity[Y] -37.26 40.502 -0.22895 -0.25394 v Velocity[Z] -3.2497 3.2013 2.0291e-06 -5.3949e-08 v ǁVelocityǁ 0.00098126 50.543 9.4351 8.3282 v Pressure -6.8326e+05 2.7195e+05 -1.696e+05 -1.6612e+05 v TurbVisc 4.0969e-19 0.032895 0.00024143 0.00011699 v CourantNb 5.5787e-09 0.011968 0.00017471 5.0025e-06 v FourierNb 1.2479e-07 0.056798 0.00015972 9.315e-07 v total_pressure -5.8194e+05 3.7327e+05 -68272 -64793 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3296 0.13418 0.0034668 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 9.2119e-07 0.057858 0.00033444 5.934e-06 INSTANT 0.876970000E-01 TIME STEP NUMBER 57168 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283266757E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.871334565E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19984E-01 0.23697E+01 Friction velocity uk : 0.19984E-01 0.23697E+01 Dimensionless distance yplus : 0.19279E-01 0.23301E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.190749858e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29858E+08 1 0.21884E-09 0.61475E+02 0.28678E+04 c Velocity[X] 0.34879E+02 c Velocity[Y] 0.26596E+02 c Velocity[Z] 0.10585E-05 c Pressure 0.24044E-03 33 0.97698E-04 0.12433E-02 0.73509E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -37.014 50.185 5.6065 7.9989 v Velocity[Y] -37.271 40.515 -0.22913 -0.25448 v Velocity[Z] -3.25 3.2014 2.0287e-06 -5.3949e-08 v ǁVelocityǁ 0.0016375 50.554 9.4366 8.3285 v Pressure -6.8301e+05 2.7229e+05 -1.7162e+05 -1.6736e+05 v TurbVisc 3.8722e-19 0.032908 0.0002415 0.00011712 v CourantNb 5.5818e-09 0.01197 0.00017473 5.0026e-06 v FourierNb 1.2479e-07 0.05684 0.00015974 9.3234e-07 v total_pressure -5.8169e+05 3.7361e+05 -70298 -66032 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3301 0.13424 0.0034684 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 9.2199e-07 0.057903 0.00033447 5.935e-06 INSTANT 0.876971000E-01 TIME STEP NUMBER 57169 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283266771E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.871416282E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.21112E-01 0.23702E+01 Friction velocity uk : 0.21112E-01 0.23702E+01 Dimensionless distance yplus : 0.20384E-01 0.23305E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.392017575e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29859E+08 1 0.21895E-09 0.61532E+02 0.28689E+04 c Velocity[X] 0.34936E+02 c Velocity[Y] 0.26596E+02 c Velocity[Z] 0.10439E-05 c Pressure 0.24133E-03 322 0.83310E-04 0.12468E-02 0.58000E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -37.028 50.197 5.6064 7.9989 v Velocity[Y] -37.281 40.528 -0.22931 -0.25501 v Velocity[Z] -3.2503 3.2015 2.0282e-06 -5.3949e-08 v ǁVelocityǁ 0.0014326 50.566 9.4381 8.3288 v Pressure -6.8472e+05 2.7261e+05 -1.7366e+05 -1.6848e+05 v TurbVisc 3.927e-19 0.032921 0.00024157 0.00011724 v CourantNb 5.4002e-09 0.011971 0.00017474 5.0027e-06 v FourierNb 1.2479e-07 0.056882 0.00015976 9.3318e-07 v total_pressure -5.8339e+05 3.7394e+05 -72335 -67154 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3305 0.1343 0.00347 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 9.2279e-07 0.057948 0.0003345 5.9359e-06 INSTANT 0.876972000E-01 TIME STEP NUMBER 57170 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283266432E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.871482717E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.21051E-01 0.23706E+01 Friction velocity uk : 0.21051E-01 0.23706E+01 Dimensionless distance yplus : 0.20324E-01 0.23310E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.688169428e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29861E+08 1 0.21904E-09 0.61633E+02 0.28711E+04 c Velocity[X] 0.34978E+02 c Velocity[Y] 0.26655E+02 c Velocity[Z] 0.10582E-05 c Pressure 0.23594E-03 9 0.61021E-04 0.12178E-02 0.51265E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -37.042 50.208 5.6064 7.9989 v Velocity[Y] -37.292 40.541 -0.22949 -0.25555 v Velocity[Z] -3.2506 3.2016 2.0278e-06 -5.3949e-08 v ǁVelocityǁ 0.0012748 50.578 9.4396 8.3292 v Pressure -6.8636e+05 2.7291e+05 -1.7569e+05 -1.6958e+05 v TurbVisc 4.0468e-19 0.032934 0.00024165 0.00011736 v CourantNb 5.1145e-09 0.011972 0.00017475 5.0029e-06 v FourierNb 1.2479e-07 0.056925 0.00015978 9.3402e-07 v total_pressure -5.8503e+05 3.7424e+05 -74366 -68255 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.331 0.13435 0.0034716 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 9.2359e-07 0.057993 0.00033454 5.9369e-06 INSTANT 0.876973000E-01 TIME STEP NUMBER 57171 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283265758E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.871537763E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.21437E-01 0.23710E+01 Friction velocity uk : 0.21437E-01 0.23710E+01 Dimensionless distance yplus : 0.20698E-01 0.23314E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -2.066504061e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29862E+08 1 0.21911E-09 0.61732E+02 0.28731E+04 c Velocity[X] 0.35035E+02 c Velocity[Y] 0.26697E+02 c Velocity[Z] 0.10494E-05 c Pressure 0.23785E-03 88 0.79394E-04 0.12265E-02 0.86597E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -37.056 50.22 5.6064 7.9989 v Velocity[Y] -37.303 40.553 -0.22967 -0.25609 v Velocity[Z] -3.2509 3.2017 2.0274e-06 -5.395e-08 v ǁVelocityǁ 0.001601 50.59 9.4411 8.3295 v Pressure -6.8625e+05 2.7325e+05 -1.7779e+05 -1.7127e+05 v TurbVisc 4.5676e-19 0.032946 0.00024172 0.00011748 v CourantNb 4.6447e-09 0.011974 0.00017476 5.003e-06 v FourierNb 1.2479e-07 0.056969 0.00015981 9.3486e-07 v total_pressure -5.8492e+05 3.7457e+05 -76461 -69944 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3314 0.13441 0.0034731 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 9.2439e-07 0.058039 0.00033457 5.9378e-06 INSTANT 0.876974000E-01 TIME STEP NUMBER 57172 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283265264E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.871581776E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.22185E-01 0.23715E+01 Friction velocity uk : 0.22185E-01 0.23715E+01 Dimensionless distance yplus : 0.21420E-01 0.23319E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -2.248534963e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29864E+08 1 0.21924E-09 0.61821E+02 0.28750E+04 c Velocity[X] 0.35093E+02 c Velocity[Y] 0.26728E+02 c Velocity[Z] 0.10421E-05 c Pressure 0.23772E-03 280 0.85376E-04 0.12247E-02 0.60062E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -37.069 50.231 5.6064 7.9988 v Velocity[Y] -37.313 40.566 -0.22985 -0.25663 v Velocity[Z] -3.2512 3.2018 2.0269e-06 -5.395e-08 v ǁVelocityǁ 0.0011574 50.601 9.4425 8.3298 v Pressure -6.8836e+05 2.7357e+05 -1.7982e+05 -1.7229e+05 v TurbVisc 4.6121e-19 0.032959 0.0002418 0.00011761 v CourantNb 4.3635e-09 0.011975 0.00017478 5.0031e-06 v FourierNb 1.2479e-07 0.057012 0.00015983 9.357e-07 v total_pressure -5.8703e+05 3.7489e+05 -78495 -70962 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3319 0.13446 0.0034746 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 9.252e-07 0.058085 0.0003346 5.9388e-06 INSTANT 0.876975000E-01 TIME STEP NUMBER 57173 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283264317E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.871620130E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.17153E-01 0.23719E+01 Friction velocity uk : 0.17153E-01 0.23719E+01 Dimensionless distance yplus : 0.16550E-01 0.23323E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -2.593610114e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29865E+08 1 0.21932E-09 0.61920E+02 0.28771E+04 c Velocity[X] 0.35133E+02 c Velocity[Y] 0.26788E+02 c Velocity[Z] 0.10370E-05 c Pressure 0.23825E-03 33 0.99286E-04 0.12263E-02 0.74886E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -37.083 50.242 5.6064 7.9988 v Velocity[Y] -37.323 40.579 -0.23003 -0.25717 v Velocity[Z] -3.2514 3.2019 2.0265e-06 -5.395e-08 v ǁVelocityǁ 0.0011284 50.613 9.444 8.3301 v Pressure -6.8816e+05 2.739e+05 -1.8185e+05 -1.7359e+05 v TurbVisc 4.5452e-19 0.032972 0.00024187 0.00011773 v CourantNb 4.5427e-09 0.011976 0.00017479 5.0032e-06 v FourierNb 1.2479e-07 0.057056 0.00015985 9.3654e-07 v total_pressure -5.8684e+05 3.7523e+05 -80520 -72268 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3323 0.13451 0.003476 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 9.26e-07 0.058132 0.00033464 5.9397e-06 INSTANT 0.876976000E-01 TIME STEP NUMBER 57174 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283263514E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.871651295E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11499E-01 0.23724E+01 Friction velocity uk : 0.11499E-01 0.23724E+01 Dimensionless distance yplus : 0.11084E-01 0.23327E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -2.859299340e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29867E+08 1 0.21943E-09 0.61979E+02 0.28782E+04 c Velocity[X] 0.35189E+02 c Velocity[Y] 0.26789E+02 c Velocity[Z] 0.10329E-05 c Pressure 0.23868E-03 631 0.84672E-04 0.12274E-02 0.59115E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -37.097 50.254 5.6063 7.9988 v Velocity[Y] -37.334 40.591 -0.23021 -0.25771 v Velocity[Z] -3.2517 3.202 2.026e-06 -5.395e-08 v ǁVelocityǁ 0.0016001 50.624 9.4455 8.3304 v Pressure -6.899e+05 2.7422e+05 -1.8388e+05 -1.7478e+05 v TurbVisc 4.6864e-19 0.032985 0.00024194 0.00011786 v CourantNb 4.6001e-09 0.011978 0.0001748 5.0033e-06 v FourierNb 1.2479e-07 0.057101 0.00015987 9.3738e-07 v total_pressure -5.8857e+05 3.7555e+05 -82560 -73452 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3327 0.13457 0.0034775 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 9.268e-07 0.058179 0.00033467 5.9407e-06 INSTANT 0.876977000E-01 TIME STEP NUMBER 57175 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283262350E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.871667542E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12464E-01 0.23728E+01 Friction velocity uk : 0.12464E-01 0.23728E+01 Dimensionless distance yplus : 0.12014E-01 0.23331E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -3.189457312e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29868E+08 1 0.21952E-09 0.62082E+02 0.28803E+04 c Velocity[X] 0.35240E+02 c Velocity[Y] 0.26842E+02 c Velocity[Z] 0.10415E-05 c Pressure 0.23254E-03 9 0.61395E-04 0.11948E-02 0.44778E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -37.11 50.265 5.6063 7.9987 v Velocity[Y] -37.344 40.604 -0.23039 -0.25825 v Velocity[Z] -3.252 3.2021 2.0256e-06 -5.395e-08 v ǁVelocityǁ 0.0014578 50.636 9.447 8.3307 v Pressure -6.9146e+05 2.7453e+05 -1.8585e+05 -1.7573e+05 v TurbVisc 4.9978e-19 0.032997 0.00024202 0.00011798 v CourantNb 4.6664e-09 0.011979 0.00017481 5.0034e-06 v FourierNb 1.2479e-07 0.057146 0.00015989 9.3822e-07 v total_pressure -5.9013e+05 3.7585e+05 -84527 -74410 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3331 0.13464 0.0034792 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 9.2761e-07 0.058226 0.00033471 5.9416e-06 INSTANT 0.876978000E-01 TIME STEP NUMBER 57176 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283260894E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.871674281E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19489E-01 0.23731E+01 Friction velocity uk : 0.19489E-01 0.23731E+01 Dimensionless distance yplus : 0.18839E-01 0.23335E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -3.614095027e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29870E+08 1 0.21959E-09 0.62182E+02 0.28824E+04 c Velocity[X] 0.35293E+02 c Velocity[Y] 0.26889E+02 c Velocity[Z] 0.10374E-05 c Pressure 0.23398E-03 86 0.80604E-04 0.12010E-02 0.87011E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -37.123 50.276 5.6063 7.9987 v Velocity[Y] -37.355 40.616 -0.23057 -0.2588 v Velocity[Z] -3.2523 3.2022 2.0251e-06 -5.395e-08 v ǁVelocityǁ 0.00085249 50.647 9.4484 8.331 v Pressure -6.9141e+05 2.7487e+05 -1.8794e+05 -1.7746e+05 v TurbVisc 5.2329e-19 0.03301 0.00024209 0.0001181 v CourantNb 4.5581e-09 0.01198 0.00017483 5.0035e-06 v FourierNb 1.2479e-07 0.057192 0.00015991 9.3907e-07 v total_pressure -5.9008e+05 3.7619e+05 -86614 -76139 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3335 0.13471 0.0034811 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 9.2842e-07 0.058274 0.00033474 5.9425e-06 INSTANT 0.876979000E-01 TIME STEP NUMBER 57177 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283259594E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.871667612E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.16831E-01 0.23736E+01 Friction velocity uk : 0.16831E-01 0.23736E+01 Dimensionless distance yplus : 0.16270E-01 0.23339E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -3.807203416e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29871E+08 1 0.21972E-09 0.62273E+02 0.28843E+04 c Velocity[X] 0.35357E+02 c Velocity[Y] 0.26915E+02 c Velocity[Z] 0.10273E-05 c Pressure 0.23337E-03 719 0.86700E-04 0.11968E-02 0.57685E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -37.137 50.287 5.6062 7.9986 v Velocity[Y] -37.365 40.629 -0.23075 -0.25934 v Velocity[Z] -3.2526 3.2022 2.0247e-06 -5.395e-08 v ǁVelocityǁ 0.00026121 50.659 9.4499 8.3313 v Pressure -6.9348e+05 2.7519e+05 -1.8992e+05 -1.7841e+05 v TurbVisc 5.593e-19 0.033023 0.00024216 0.00011823 v CourantNb 3.7592e-09 0.011982 0.00017484 5.0036e-06 v FourierNb 1.2478e-07 0.057238 0.00015994 9.3991e-07 v total_pressure -5.9215e+05 3.7651e+05 -88599 -77082 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3339 0.13478 0.0034829 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 9.2923e-07 0.058322 0.00033477 5.9435e-06 INSTANT 0.876980000E-01 TIME STEP NUMBER 57178 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283257866E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.871656531E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.17378E-01 0.23739E+01 Friction velocity uk : 0.17378E-01 0.23739E+01 Dimensionless distance yplus : 0.16798E-01 0.23343E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -4.169709066e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29873E+08 1 0.21979E-09 0.62340E+02 0.28857E+04 c Velocity[X] 0.35391E+02 c Velocity[Y] 0.26949E+02 c Velocity[Z] 0.10202E-05 c Pressure 0.23343E-03 77 0.75683E-04 0.11960E-02 0.65467E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -37.15 50.298 5.6062 7.9986 v Velocity[Y] -37.375 40.641 -0.23093 -0.25988 v Velocity[Z] -3.2529 3.2023 2.0243e-06 -5.395e-08 v ǁVelocityǁ 0.00085022 50.67 9.4514 8.3316 v Pressure -6.9398e+05 2.7552e+05 -1.9194e+05 -1.7978e+05 v TurbVisc 5.2985e-19 0.033036 0.00024224 0.00011835 v CourantNb 3.9122e-09 0.011983 0.00017485 5.0037e-06 v FourierNb 1.2478e-07 0.057284 0.00015996 9.4075e-07 v total_pressure -5.9265e+05 3.7684e+05 -90613 -78452 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3343 0.13484 0.0034846 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 9.3004e-07 0.058371 0.00033481 5.9444e-06 INSTANT 0.876981000E-01 TIME STEP NUMBER 57179 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283256111E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.871637650E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.20635E-01 0.23743E+01 Friction velocity uk : 0.20635E-01 0.23743E+01 Dimensionless distance yplus : 0.19946E-01 0.23346E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -4.473772970e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29874E+08 1 0.21989E-09 0.62442E+02 0.28878E+04 c Velocity[X] 0.35436E+02 c Velocity[Y] 0.27006E+02 c Velocity[Z] 0.10332E-05 c Pressure 0.22779E-03 9 0.55706E-04 0.11661E-02 0.48125E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -37.164 50.309 5.6061 7.9985 v Velocity[Y] -37.385 40.654 -0.23111 -0.26043 v Velocity[Z] -3.2532 3.2024 2.0238e-06 -5.395e-08 v ǁVelocityǁ 0.0016441 50.681 9.4528 8.3319 v Pressure -6.9455e+05 2.7583e+05 -1.939e+05 -1.8082e+05 v TurbVisc 5.7273e-19 0.033048 0.00024231 0.00011847 v CourantNb 2.8358e-09 0.011984 0.00017486 5.0038e-06 v FourierNb 1.2478e-07 0.057331 0.00015998 9.416e-07 v total_pressure -5.9323e+05 3.7716e+05 -92574 -79496 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3346 0.13491 0.0034863 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 9.3085e-07 0.058419 0.00033484 5.9454e-06 INSTANT 0.876982000E-01 TIME STEP NUMBER 57180 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283254234E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.871605704E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.21793E-01 0.23746E+01 Friction velocity uk : 0.21793E-01 0.23746E+01 Dimensionless distance yplus : 0.21042E-01 0.23350E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -4.924072403e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29876E+08 1 0.21998E-09 0.62528E+02 0.28895E+04 c Velocity[X] 0.35504E+02 c Velocity[Y] 0.27024E+02 c Velocity[Z] 0.10242E-05 c Pressure 0.22843E-03 140 0.97640E-04 0.11683E-02 0.58144E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -37.177 50.32 5.6061 7.9985 v Velocity[Y] -37.395 40.666 -0.23129 -0.26097 v Velocity[Z] -3.2535 3.2025 2.0234e-06 -5.395e-08 v ǁVelocityǁ 0.0017891 50.693 9.4543 8.3322 v Pressure -6.9586e+05 2.7616e+05 -1.9584e+05 -1.8211e+05 v TurbVisc 6.0867e-19 0.033061 0.00024238 0.0001186 v CourantNb 3.6925e-09 0.011985 0.00017487 5.0039e-06 v FourierNb 1.2478e-07 0.057378 0.00016 9.4244e-07 v total_pressure -5.9454e+05 3.7748e+05 -94514 -80780 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.335 0.13497 0.003488 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 9.3166e-07 0.058469 0.00033487 5.9463e-06 INSTANT 0.876983000E-01 TIME STEP NUMBER 57181 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283252139E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.871560904E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19948E-01 0.23750E+01 Friction velocity uk : 0.19948E-01 0.23750E+01 Dimensionless distance yplus : 0.19260E-01 0.23353E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -5.108458942e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29877E+08 1 0.22009E-09 0.62617E+02 0.28914E+04 c Velocity[X] 0.35562E+02 c Velocity[Y] 0.27055E+02 c Velocity[Z] 0.10173E-05 c Pressure 0.22607E-03 32 0.81645E-04 0.11551E-02 0.50813E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -37.19 50.331 5.606 7.9984 v Velocity[Y] -37.405 40.678 -0.23147 -0.26152 v Velocity[Z] -3.2538 3.2026 2.0229e-06 -5.395e-08 v ǁVelocityǁ 0.0020028 50.704 9.4558 8.3325 v Pressure -6.9708e+05 2.7648e+05 -1.9782e+05 -1.8327e+05 v TurbVisc 6.1316e-19 0.033074 0.00024246 0.00011872 v CourantNb 3.355e-09 0.011987 0.00017489 5.004e-06 v FourierNb 1.2478e-07 0.057426 0.00016002 9.4329e-07 v total_pressure -5.9576e+05 3.778e+05 -96496 -81942 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3353 0.13503 0.0034896 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 9.3247e-07 0.058519 0.00033491 5.9472e-06 INSTANT 0.876984000E-01 TIME STEP NUMBER 57182 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283249913E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.871505557E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.18562E-01 0.23754E+01 Friction velocity uk : 0.18562E-01 0.23754E+01 Dimensionless distance yplus : 0.17922E-01 0.23357E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -5.455552246e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29879E+08 1 0.22018E-09 0.62720E+02 0.28935E+04 c Velocity[X] 0.35614E+02 c Velocity[Y] 0.27106E+02 c Velocity[Z] 0.10263E-05 c Pressure 0.22301E-03 9 0.55168E-04 0.11384E-02 0.48848E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -37.203 50.342 5.606 7.9983 v Velocity[Y] -37.415 40.691 -0.23165 -0.26206 v Velocity[Z] -3.254 3.2027 2.0225e-06 -5.395e-08 v ǁVelocityǁ 0.0022276 50.715 9.4572 8.3327 v Pressure -6.9859e+05 2.7679e+05 -1.998e+05 -1.8436e+05 v TurbVisc 6.2283e-19 0.033087 0.00024253 0.00011885 v CourantNb 4.4714e-09 0.011988 0.0001749 5.004e-06 v FourierNb 1.2478e-07 0.057473 0.00016004 9.4413e-07 v total_pressure -5.9727e+05 3.7812e+05 -98472 -83038 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3357 0.13509 0.0034912 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 9.3329e-07 0.058568 0.00033494 5.9482e-06 INSTANT 0.876985000E-01 TIME STEP NUMBER 57183 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283247425E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.871443208E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.17933E-01 0.23757E+01 Friction velocity uk : 0.17933E-01 0.23757E+01 Dimensionless distance yplus : 0.17314E-01 0.23360E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -5.981484924e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29880E+08 1 0.22025E-09 0.62806E+02 0.28953E+04 c Velocity[X] 0.35671E+02 c Velocity[Y] 0.27135E+02 c Velocity[Z] 0.10171E-05 c Pressure 0.22372E-03 16 0.99133E-04 0.11410E-02 0.63200E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -37.216 50.352 5.6059 7.9983 v Velocity[Y] -37.425 40.703 -0.23183 -0.26261 v Velocity[Z] -3.2543 3.2028 2.022e-06 -5.3951e-08 v ǁVelocityǁ 0.0021247 50.726 9.4587 8.333 v Pressure -6.9923e+05 2.7713e+05 -2.0172e+05 -1.8577e+05 v TurbVisc 6.62e-19 0.033099 0.0002426 0.00011897 v CourantNb 6.3185e-09 0.011989 0.00017491 5.0041e-06 v FourierNb 1.2478e-07 0.057523 0.00016007 9.4498e-07 v total_pressure -5.979e+05 3.7845e+05 -1.0039e+05 -84447 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.336 0.13515 0.0034928 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 9.341e-07 0.05862 0.00033498 5.9491e-06 INSTANT 0.876986000E-01 TIME STEP NUMBER 57184 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283244887E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.871372791E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11304E-01 0.23761E+01 Friction velocity uk : 0.11304E-01 0.23761E+01 Dimensionless distance yplus : 0.11010E-01 0.23363E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -6.059336587e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29881E+08 1 0.22037E-09 0.62892E+02 0.28971E+04 c Velocity[X] 0.35719E+02 c Velocity[Y] 0.27173E+02 c Velocity[Z] 0.10035E-05 c Pressure 0.22110E-03 165 0.84177E-04 0.11266E-02 0.51484E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -37.229 50.363 5.6059 7.9982 v Velocity[Y] -37.435 40.715 -0.23201 -0.26316 v Velocity[Z] -3.2546 3.2029 2.0216e-06 -5.3951e-08 v ǁVelocityǁ 0.0021097 50.737 9.4601 8.3333 v Pressure -7.0003e+05 2.7745e+05 -2.0362e+05 -1.8697e+05 v TurbVisc 6.2392e-19 0.033112 0.00024267 0.00011909 v CourantNb 8.1598e-09 0.011991 0.00017492 5.0042e-06 v FourierNb 1.2477e-07 0.057571 0.00016009 9.4583e-07 v total_pressure -5.9871e+05 3.7877e+05 -1.023e+05 -85641 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3363 0.13521 0.0034944 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 9.3492e-07 0.058671 0.00033501 5.9501e-06 INSTANT 0.876987000E-01 TIME STEP NUMBER 57185 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283242226E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.871290578E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.16965E-01 0.23764E+01 Friction velocity uk : 0.16965E-01 0.23764E+01 Dimensionless distance yplus : 0.16524E-01 0.23366E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -6.532463436e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29883E+08 1 0.22046E-09 0.62997E+02 0.28993E+04 c Velocity[X] 0.35758E+02 c Velocity[Y] 0.27239E+02 c Velocity[Z] 0.10142E-05 c Pressure 0.21764E-03 9 0.56513E-04 0.11080E-02 0.48134E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -37.242 50.374 5.6058 7.9981 v Velocity[Y] -37.445 40.727 -0.23219 -0.26371 v Velocity[Z] -3.2549 3.203 2.0212e-06 -5.3951e-08 v ǁVelocityǁ 0.0014391 50.748 9.4616 8.3336 v Pressure -7.0071e+05 2.7778e+05 -2.0557e+05 -1.8803e+05 v TurbVisc 7.2934e-19 0.033125 0.00024274 0.00011922 v CourantNb 9.8494e-09 0.011992 0.00017493 5.0043e-06 v FourierNb 1.2477e-07 0.05762 0.00016011 9.4667e-07 v total_pressure -5.9938e+05 3.791e+05 -1.0424e+05 -86707 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3366 0.13527 0.003496 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 9.3574e-07 0.058721 0.00033504 5.951e-06 INSTANT 0.876988000E-01 TIME STEP NUMBER 57186 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283239476E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.871200056E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.21490E-01 0.23767E+01 Friction velocity uk : 0.21490E-01 0.23767E+01 Dimensionless distance yplus : 0.20749E-01 0.23369E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -6.925888468e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29884E+08 1 0.22054E-09 0.63092E+02 0.29012E+04 c Velocity[X] 0.35841E+02 c Velocity[Y] 0.27251E+02 c Velocity[Z] 0.10084E-05 c Pressure 0.21827E-03 247 0.77383E-04 0.11102E-02 0.59028E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -37.255 50.384 5.6057 7.998 v Velocity[Y] -37.455 40.739 -0.23237 -0.26425 v Velocity[Z] -3.2552 3.2031 2.0207e-06 -5.3951e-08 v ǁVelocityǁ 0.0019294 50.759 9.463 8.3338 v Pressure -7.0255e+05 2.7811e+05 -2.0738e+05 -1.8917e+05 v TurbVisc 7.1668e-19 0.033137 0.00024282 0.00011934 v CourantNb 1.1935e-08 0.011993 0.00017495 5.0044e-06 v FourierNb 1.2477e-07 0.057671 0.00016013 9.4752e-07 v total_pressure -6.0122e+05 3.7943e+05 -1.0605e+05 -87841 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3369 0.13532 0.0034975 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 9.3656e-07 0.058774 0.00033508 5.9519e-06 INSTANT 0.876989000E-01 TIME STEP NUMBER 57187 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283236416E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.871100799E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.23607E-01 0.23770E+01 Friction velocity uk : 0.23607E-01 0.23770E+01 Dimensionless distance yplus : 0.22793E-01 0.23373E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -7.043562797e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29886E+08 1 0.22065E-09 0.63195E+02 0.29034E+04 c Velocity[X] 0.35880E+02 c Velocity[Y] 0.27315E+02 c Velocity[Z] 0.10018E-05 c Pressure 0.21653E-03 454 0.82122E-04 0.11003E-02 0.66176E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -37.268 50.395 5.6057 7.998 v Velocity[Y] -37.465 40.751 -0.23255 -0.26481 v Velocity[Z] -3.2555 3.2032 2.0203e-06 -5.3951e-08 v ǁVelocityǁ 0.0017134 50.77 9.4645 8.3341 v Pressure -7.026e+05 2.7845e+05 -2.093e+05 -1.9047e+05 v TurbVisc 6.6332e-19 0.03315 0.00024289 0.00011947 v CourantNb 1.3853e-08 0.011994 0.00017496 5.0045e-06 v FourierNb 1.2477e-07 0.05772 0.00016015 9.4837e-07 v total_pressure -6.0128e+05 3.7977e+05 -1.0798e+05 -89142 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3373 0.13538 0.003499 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 9.3738e-07 0.058825 0.00033511 5.9529e-06 INSTANT 0.876990000E-01 TIME STEP NUMBER 57188 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283233449E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.870990664E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.25651E-01 0.23773E+01 Friction velocity uk : 0.25651E-01 0.23773E+01 Dimensionless distance yplus : 0.24766E-01 0.23376E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -7.417630172e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29887E+08 1 0.22075E-09 0.63289E+02 0.29053E+04 c Velocity[X] 0.35948E+02 c Velocity[Y] 0.27341E+02 c Velocity[Z] 0.99743E-06 c Pressure 0.21569E-03 241 0.96272E-04 0.10950E-02 0.55694E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -37.281 50.405 5.6056 7.9979 v Velocity[Y] -37.475 40.763 -0.23273 -0.26535 v Velocity[Z] -3.2558 3.2032 2.0198e-06 -5.3951e-08 v ǁVelocityǁ 0.0014912 50.781 9.4659 8.3344 v Pressure -7.048e+05 2.7876e+05 -2.1109e+05 -1.9137e+05 v TurbVisc 7.2108e-19 0.033163 0.00024296 0.00011959 v CourantNb 1.6019e-08 0.011996 0.00017497 5.0046e-06 v FourierNb 1.2477e-07 0.05777 0.00016018 9.4922e-07 v total_pressure -6.0347e+05 3.8008e+05 -1.0977e+05 -90041 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3376 0.13544 0.0035005 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 9.382e-07 0.058877 0.00033515 5.9538e-06 INSTANT 0.876991000E-01 TIME STEP NUMBER 57189 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283229995E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.870874086E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.21540E-01 0.23776E+01 Friction velocity uk : 0.21540E-01 0.23776E+01 Dimensionless distance yplus : 0.20737E-01 0.23378E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -7.690970371e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29888E+08 1 0.22082E-09 0.63358E+02 0.29067E+04 c Velocity[X] 0.35996E+02 c Velocity[Y] 0.27361E+02 c Velocity[Z] 0.99697E-06 c Pressure 0.21476E-03 468 0.81771E-04 0.10893E-02 0.56032E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -37.294 50.416 5.6055 7.9978 v Velocity[Y] -37.485 40.775 -0.23291 -0.26591 v Velocity[Z] -3.2561 3.2033 2.0194e-06 -5.3951e-08 v ǁVelocityǁ 0.0012798 50.791 9.4673 8.3346 v Pressure -7.0509e+05 2.791e+05 -2.1292e+05 -1.9257e+05 v TurbVisc 8.0385e-19 0.033175 0.00024303 0.00011972 v CourantNb 1.8256e-08 0.011997 0.00017498 5.0047e-06 v FourierNb 1.2477e-07 0.057821 0.0001602 9.5007e-07 v total_pressure -6.0376e+05 3.8042e+05 -1.1159e+05 -91242 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3378 0.13549 0.0035019 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 9.3902e-07 0.058929 0.00033518 5.9547e-06 INSTANT 0.876992000E-01 TIME STEP NUMBER 57190 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283226659E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.870744249E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15953E-01 0.23779E+01 Friction velocity uk : 0.15953E-01 0.23779E+01 Dimensionless distance yplus : 0.15358E-01 0.23381E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -7.969921654e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29890E+08 1 0.22092E-09 0.63465E+02 0.29089E+04 c Velocity[X] 0.36027E+02 c Velocity[Y] 0.27438E+02 c Velocity[Z] 0.10075E-05 c Pressure 0.20670E-03 9 0.58430E-04 0.10474E-02 0.48700E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -37.306 50.426 5.6054 7.9977 v Velocity[Y] -37.494 40.787 -0.23309 -0.26646 v Velocity[Z] -3.2564 3.2034 2.0189e-06 -5.3951e-08 v ǁVelocityǁ 0.0010865 50.802 9.4688 8.3349 v Pressure -7.0584e+05 2.7942e+05 -2.1473e+05 -1.9365e+05 v TurbVisc 8.4095e-19 0.033188 0.0002431 0.00011984 v CourantNb 2.0607e-08 0.011998 0.00017499 5.0047e-06 v FourierNb 1.2477e-07 0.057871 0.00016022 9.5091e-07 v total_pressure -6.0451e+05 3.8075e+05 -1.1341e+05 -92329 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3381 0.13554 0.0035033 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 9.3985e-07 0.058981 0.00033521 5.9557e-06 INSTANT 0.876993000E-01 TIME STEP NUMBER 57191 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283223133E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.870604277E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10409E-01 0.23781E+01 Friction velocity uk : 0.10409E-01 0.23781E+01 Dimensionless distance yplus : 0.10021E-01 0.23384E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -8.342320976e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29891E+08 1 0.22100E-09 0.63562E+02 0.29109E+04 c Velocity[X] 0.36121E+02 c Velocity[Y] 0.27441E+02 c Velocity[Z] 0.99879E-06 c Pressure 0.20700E-03 641 0.78154E-04 0.10480E-02 0.58091E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -37.319 50.436 5.6054 7.9976 v Velocity[Y] -37.504 40.799 -0.23327 -0.26701 v Velocity[Z] -3.2567 3.2035 2.0185e-06 -5.3951e-08 v ǁVelocityǁ 0.00093726 50.813 9.4702 8.3352 v Pressure -7.0759e+05 2.7975e+05 -2.1647e+05 -1.9475e+05 v TurbVisc 5.9929e-19 0.033201 0.00024317 0.00011996 v CourantNb 2.3165e-08 0.011999 0.000175 5.0048e-06 v FourierNb 1.2477e-07 0.057922 0.00016024 9.5176e-07 v total_pressure -6.0626e+05 3.8108e+05 -1.1515e+05 -93421 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3384 0.1356 0.0035047 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 9.4067e-07 0.059034 0.00033525 5.9566e-06 INSTANT 0.876994000E-01 TIME STEP NUMBER 57192 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283219382E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.870456198E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.74713E-02 0.23784E+01 Friction velocity uk : 0.74713E-02 0.23784E+01 Dimensionless distance yplus : 0.71927E-02 0.23387E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -8.494694373e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29892E+08 1 0.22111E-09 0.63665E+02 0.29131E+04 c Velocity[X] 0.36158E+02 c Velocity[Y] 0.27508E+02 c Velocity[Z] 0.99402E-06 c Pressure 0.20497E-03 49 0.83536E-04 0.10367E-02 0.61029E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -37.331 50.447 5.6053 7.9975 v Velocity[Y] -37.513 40.811 -0.23345 -0.26757 v Velocity[Z] -3.2569 3.2036 2.0181e-06 -5.3951e-08 v ǁVelocityǁ 0.00084323 50.823 9.4716 8.3354 v Pressure -7.0762e+05 2.801e+05 -2.1825e+05 -1.959e+05 v TurbVisc 9.256e-19 0.033213 0.00024324 0.00012009 v CourantNb 2.5539e-08 0.012001 0.00017502 5.0049e-06 v FourierNb 1.2476e-07 0.057973 0.00016027 9.5261e-07 v total_pressure -6.063e+05 3.8143e+05 -1.1693e+05 -94580 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3387 0.13565 0.0035062 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 9.415e-07 0.059086 0.00033528 5.9575e-06 INSTANT 0.876995000E-01 TIME STEP NUMBER 57193 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283215751E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.870301344E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.68670E-02 0.23787E+01 Friction velocity uk : 0.68670E-02 0.23787E+01 Dimensionless distance yplus : 0.66109E-02 0.23389E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -8.753771003e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29894E+08 1 0.22121E-09 0.63760E+02 0.29150E+04 c Velocity[X] 0.36221E+02 c Velocity[Y] 0.27540E+02 c Velocity[Z] 0.98139E-06 c Pressure 0.20375E-03 337 0.97778E-04 0.10296E-02 0.58040E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -37.344 50.457 5.6052 7.9974 v Velocity[Y] -37.523 40.823 -0.23363 -0.26812 v Velocity[Z] -3.2572 3.2037 2.0176e-06 -5.3951e-08 v ǁVelocityǁ 0.00082579 50.834 9.4731 8.3357 v Pressure -7.0993e+05 2.8041e+05 -2.1998e+05 -1.9692e+05 v TurbVisc 9.9167e-19 0.033226 0.00024331 0.00012021 v CourantNb 2.8105e-08 0.012002 0.00017503 5.005e-06 v FourierNb 1.2476e-07 0.058023 0.00016029 9.5346e-07 v total_pressure -6.0861e+05 3.8173e+05 -1.1866e+05 -95592 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3389 0.1357 0.0035077 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 9.4232e-07 0.059138 0.00033532 5.9585e-06 INSTANT 0.876996000E-01 TIME STEP NUMBER 57194 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283211569E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.870139236E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11236E-01 0.23789E+01 Friction velocity uk : 0.11236E-01 0.23789E+01 Dimensionless distance yplus : 0.10817E-01 0.23392E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -8.985892781e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29895E+08 1 0.22128E-09 0.63828E+02 0.29163E+04 c Velocity[X] 0.36268E+02 c Velocity[Y] 0.27560E+02 c Velocity[Z] 0.99654E-06 c Pressure 0.20268E-03 78 0.82893E-04 0.10232E-02 0.52198E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -37.356 50.467 5.6051 7.9973 v Velocity[Y] -37.532 40.835 -0.23381 -0.26867 v Velocity[Z] -3.2575 3.2038 2.0172e-06 -5.3951e-08 v ǁVelocityǁ 0.00083434 50.844 9.4745 8.3359 v Pressure -7.1021e+05 2.8075e+05 -2.2168e+05 -1.9803e+05 v TurbVisc 9.2154e-19 0.033239 0.00024338 0.00012034 v CourantNb 3.0753e-08 0.012003 0.00017504 5.0051e-06 v FourierNb 1.2476e-07 0.058074 0.00016031 9.5432e-07 v total_pressure -6.0889e+05 3.8208e+05 -1.2036e+05 -96707 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3392 0.13576 0.0035092 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 9.4315e-07 0.059191 0.00033535 5.9594e-06 INSTANT 0.876997000E-01 TIME STEP NUMBER 57195 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283207536E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.869967900E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.18862E-01 0.23792E+01 Friction velocity uk : 0.18862E-01 0.23792E+01 Dimensionless distance yplus : 0.18159E-01 0.23394E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -9.174575864e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29896E+08 1 0.22138E-09 0.63938E+02 0.29186E+04 c Velocity[X] 0.36312E+02 c Velocity[Y] 0.27625E+02 c Velocity[Z] 0.98698E-06 c Pressure 0.19364E-03 9 0.58285E-04 0.97668E-03 0.40376E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -37.369 50.477 5.605 7.9972 v Velocity[Y] -37.542 40.846 -0.23399 -0.26923 v Velocity[Z] -3.2578 3.2039 2.0167e-06 -5.3952e-08 v ǁVelocityǁ 0.00086332 50.855 9.4759 8.3362 v Pressure -7.1076e+05 2.8108e+05 -2.2334e+05 -1.9893e+05 v TurbVisc 8.9625e-19 0.033251 0.00024345 0.00012046 v CourantNb 3.3455e-08 0.012004 0.00017505 5.0051e-06 v FourierNb 1.2476e-07 0.058125 0.00016034 9.5517e-07 v total_pressure -6.0944e+05 3.8241e+05 -1.2202e+05 -97609 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3394 0.13581 0.0035107 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 9.4398e-07 0.059243 0.00033539 5.9603e-06 INSTANT 0.876998000E-01 TIME STEP NUMBER 57196 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283203398E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.869785818E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.25333E-01 0.23794E+01 Friction velocity uk : 0.25333E-01 0.23794E+01 Dimensionless distance yplus : 0.24459E-01 0.23397E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -9.470818856e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29898E+08 1 0.22147E-09 0.64033E+02 0.29206E+04 c Velocity[X] 0.36393E+02 c Velocity[Y] 0.27640E+02 c Velocity[Z] 0.97699E-06 c Pressure 0.19378E-03 67 0.79104E-04 0.97653E-03 0.55090E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -37.381 50.487 5.6049 7.9971 v Velocity[Y] -37.551 40.858 -0.23417 -0.26978 v Velocity[Z] -3.2581 3.204 2.0163e-06 -5.3952e-08 v ǁVelocityǁ 0.00095934 50.865 9.4773 8.3364 v Pressure -7.1271e+05 2.8142e+05 -2.2496e+05 -1.9999e+05 v TurbVisc 5.6364e-19 0.033264 0.00024352 0.00012059 v CourantNb 3.6267e-08 0.012005 0.00017506 5.0052e-06 v FourierNb 1.2476e-07 0.058175 0.00016036 9.5602e-07 v total_pressure -6.1139e+05 3.8275e+05 -1.2364e+05 -98663 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3397 0.13587 0.0035123 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 9.4481e-07 0.059295 0.00033542 5.9612e-06 INSTANT 0.876999000E-01 TIME STEP NUMBER 57197 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283198965E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.869594281E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.25959E-01 0.23797E+01 Friction velocity uk : 0.25959E-01 0.23797E+01 Dimensionless distance yplus : 0.25063E-01 0.23399E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -9.599923616e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29899E+08 1 0.22157E-09 0.64139E+02 0.29228E+04 c Velocity[X] 0.36440E+02 c Velocity[Y] 0.27699E+02 c Velocity[Z] 0.99236E-06 c Pressure 0.19138E-03 58 0.84860E-04 0.96350E-03 0.59048E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -37.393 50.497 5.6048 7.997 v Velocity[Y] -37.56 40.869 -0.23435 -0.27034 v Velocity[Z] -3.2584 3.2041 2.0158e-06 -5.3952e-08 v ǁVelocityǁ 0.0011197 50.875 9.4788 8.3367 v Pressure -7.1261e+05 2.8176e+05 -2.2663e+05 -2.0111e+05 v TurbVisc 9.5397e-19 0.033276 0.00024359 0.00012071 v CourantNb 3.9048e-08 0.012007 0.00017507 5.0053e-06 v FourierNb 1.2476e-07 0.058226 0.00016038 9.5687e-07 v total_pressure -6.1128e+05 3.8309e+05 -1.2531e+05 -99788 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3399 0.13592 0.0035138 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 9.4565e-07 0.059347 0.00033546 5.9622e-06 INSTANT 0.877000000E-01 TIME STEP NUMBER 57198 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283194706E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.869394630E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.26949E-01 0.23799E+01 Friction velocity uk : 0.26949E-01 0.23799E+01 Dimensionless distance yplus : 0.26020E-01 0.23402E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -9.780176491e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29900E+08 1 0.22167E-09 0.64234E+02 0.29247E+04 c Velocity[X] 0.36501E+02 c Velocity[Y] 0.27733E+02 c Velocity[Z] 0.97258E-06 c Pressure 0.19004E-03 235 0.99255E-04 0.95589E-03 0.54846E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -37.405 50.507 5.6047 7.9969 v Velocity[Y] -37.57 40.881 -0.23453 -0.2709 v Velocity[Z] -3.2587 3.2041 2.0154e-06 -5.3952e-08 v ǁVelocityǁ 0.0013204 50.885 9.4802 8.3369 v Pressure -7.1495e+05 2.8208e+05 -2.2822e+05 -2.0201e+05 v TurbVisc 8.3167e-19 0.033289 0.00024366 0.00012084 v CourantNb 4.1922e-08 0.012008 0.00017508 5.0054e-06 v FourierNb 1.2476e-07 0.058276 0.00016041 9.5772e-07 v total_pressure -6.1363e+05 3.8341e+05 -1.2689e+05 -1.0068e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3402 0.13597 0.0035153 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 9.4648e-07 0.059399 0.00033549 5.9631e-06 INSTANT 0.877001000E-01 TIME STEP NUMBER 57199 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283189911E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.869190114E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.26382E-01 0.23802E+01 Friction velocity uk : 0.26382E-01 0.23802E+01 Dimensionless distance yplus : 0.25438E-01 0.23404E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -9.937625966e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29902E+08 1 0.22175E-09 0.64301E+02 0.29261E+04 c Velocity[X] 0.36547E+02 c Velocity[Y] 0.27754E+02 c Velocity[Z] 0.96067E-06 c Pressure 0.18883E-03 73 0.84417E-04 0.94893E-03 0.50219E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -37.418 50.517 5.6046 7.9968 v Velocity[Y] -37.579 40.893 -0.23471 -0.27145 v Velocity[Z] -3.2589 3.2042 2.015e-06 -5.3952e-08 v ǁVelocityǁ 0.0015471 50.896 9.4816 8.3372 v Pressure -7.1523e+05 2.8243e+05 -2.2978e+05 -2.0308e+05 v TurbVisc 7.4949e-19 0.033302 0.00024373 0.00012096 v CourantNb 4.4831e-08 0.012009 0.0001751 5.0054e-06 v FourierNb 1.2476e-07 0.058326 0.00016043 9.5858e-07 v total_pressure -6.139e+05 3.8375e+05 -1.2846e+05 -1.0176e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3404 0.13602 0.0035167 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 9.4732e-07 0.05945 0.00033553 5.964e-06 INSTANT 0.877002000E-01 TIME STEP NUMBER 57200 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283185244E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.868976406E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12147E-01 0.23804E+01 Friction velocity uk : 0.12147E-01 0.23804E+01 Dimensionless distance yplus : 0.11713E-01 0.23406E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.007867837e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29903E+08 1 0.22184E-09 0.64412E+02 0.29284E+04 c Velocity[X] 0.36592E+02 c Velocity[Y] 0.27820E+02 c Velocity[Z] 0.96888E-06 c Pressure 0.17868E-03 9 0.58996E-04 0.89710E-03 0.36319E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -37.43 50.527 5.6045 7.9967 v Velocity[Y] -37.588 40.904 -0.2349 -0.27202 v Velocity[Z] -3.2592 3.2043 2.0145e-06 -5.3952e-08 v ǁVelocityǁ 0.0012873 50.906 9.483 8.3374 v Pressure -7.1574e+05 2.8276e+05 -2.3129e+05 -2.0389e+05 v TurbVisc 6.9361e-19 0.033314 0.0002438 0.00012109 v CourantNb 4.4565e-08 0.01201 0.00017511 5.0055e-06 v FourierNb 1.2476e-07 0.058375 0.00016046 9.5943e-07 v total_pressure -6.1441e+05 3.8409e+05 -1.2996e+05 -1.0256e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3406 0.13607 0.0035181 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 9.481e-07 0.059501 0.00033557 5.965e-06 INSTANT 0.877003000E-01 TIME STEP NUMBER 57201 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283180515E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.868752958E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.21291E-01 0.23806E+01 Friction velocity uk : 0.21291E-01 0.23806E+01 Dimensionless distance yplus : 0.20629E-01 0.23408E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.026950754e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29904E+08 1 0.22193E-09 0.64507E+02 0.29303E+04 c Velocity[X] 0.36672E+02 c Velocity[Y] 0.27835E+02 c Velocity[Z] 0.95952E-06 c Pressure 0.17894E-03 78 0.80583E-04 0.89754E-03 0.51829E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -37.442 50.536 5.6044 7.9965 v Velocity[Y] -37.597 40.915 -0.23508 -0.27257 v Velocity[Z] -3.2595 3.2044 2.0141e-06 -5.3952e-08 v ǁVelocityǁ 0.00082981 50.916 9.4844 8.3377 v Pressure -7.1772e+05 2.831e+05 -2.3277e+05 -2.0485e+05 v TurbVisc 5.1279e-19 0.033327 0.00024387 0.00012121 v CourantNb 4.0833e-08 0.012011 0.00017512 5.0056e-06 v FourierNb 1.2476e-07 0.058425 0.00016048 9.6028e-07 v total_pressure -6.1639e+05 3.8442e+05 -1.3144e+05 -1.0353e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3408 0.13612 0.0035195 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 9.4883e-07 0.059552 0.0003356 5.9659e-06 INSTANT 0.877004000E-01 TIME STEP NUMBER 57202 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283175484E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.868520763E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15458E-01 0.23809E+01 Friction velocity uk : 0.15458E-01 0.23809E+01 Dimensionless distance yplus : 0.14978E-01 0.23411E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.035687012e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29906E+08 1 0.22203E-09 0.64614E+02 0.29325E+04 c Velocity[X] 0.36720E+02 c Velocity[Y] 0.27894E+02 c Velocity[Z] 0.96007E-06 c Pressure 0.17630E-03 71 0.86418E-04 0.88350E-03 0.56146E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -37.454 50.546 5.6043 7.9964 v Velocity[Y] -37.606 40.927 -0.23526 -0.27314 v Velocity[Z] -3.2598 3.2045 2.0136e-06 -5.3952e-08 v ǁVelocityǁ 0.0003772 50.926 9.4858 8.3379 v Pressure -7.1757e+05 2.8345e+05 -2.3428e+05 -2.059e+05 v TurbVisc 6.9619e-19 0.033339 0.00024394 0.00012134 v CourantNb 3.6567e-08 0.012012 0.00017513 5.0057e-06 v FourierNb 1.2476e-07 0.058474 0.00016051 9.6114e-07 v total_pressure -6.1625e+05 3.8477e+05 -1.3296e+05 -1.0457e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3411 0.13617 0.0035209 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 9.4957e-07 0.059602 0.00033564 5.9668e-06 INSTANT 0.877005000E-01 TIME STEP NUMBER 57203 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283170653E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.868280413E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.62141E-02 0.23811E+01 Friction velocity uk : 0.62141E-02 0.23811E+01 Dimensionless distance yplus : 0.60210E-02 0.23413E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.045632770e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29907E+08 1 0.22213E-09 0.64681E+02 0.29338E+04 c Velocity[X] 0.36777E+02 c Velocity[Y] 0.27904E+02 c Velocity[Z] 0.94387E-06 c Pressure 0.17492E-03 245 0.75744E-04 0.87573E-03 0.38807E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -37.465 50.556 5.6042 7.9963 v Velocity[Y] -37.615 40.938 -0.23544 -0.2737 v Velocity[Z] -3.2601 3.2046 2.0132e-06 -5.3952e-08 v ǁVelocityǁ 0.00019345 50.936 9.4872 8.3381 v Pressure -7.1925e+05 2.8378e+05 -2.357e+05 -2.0672e+05 v TurbVisc 6.3056e-19 0.033352 0.00024401 0.00012147 v CourantNb 3.2513e-08 0.012014 0.00017514 5.0057e-06 v FourierNb 1.2476e-07 0.058523 0.00016053 9.6199e-07 v total_pressure -6.1792e+05 3.851e+05 -1.3438e+05 -1.054e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3413 0.13622 0.0035222 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 9.503e-07 0.059653 0.00033568 5.9677e-06 INSTANT 0.877006000E-01 TIME STEP NUMBER 57204 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283165466E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.868035887E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.36054E-02 0.23813E+01 Friction velocity uk : 0.36054E-02 0.23813E+01 Dimensionless distance yplus : 0.34934E-02 0.23415E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.053597167e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29908E+08 1 0.22222E-09 0.64787E+02 0.29360E+04 c Velocity[X] 0.36825E+02 c Velocity[Y] 0.27962E+02 c Velocity[Z] 0.97246E-06 c Pressure 0.16553E-03 16 0.57153E-04 0.82799E-03 0.30321E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -37.477 50.565 5.6041 7.9962 v Velocity[Y] -37.624 40.949 -0.23562 -0.27426 v Velocity[Z] -3.2604 3.2047 2.0128e-06 -5.3952e-08 v ǁVelocityǁ 0.00018749 50.946 9.4887 8.3384 v Pressure -7.2076e+05 2.8411e+05 -2.3707e+05 -2.0741e+05 v TurbVisc 5.8328e-19 0.033365 0.00024408 0.00012159 v CourantNb 2.8492e-08 0.012015 0.00017515 5.0058e-06 v FourierNb 1.2475e-07 0.058571 0.00016056 9.6285e-07 v total_pressure -6.1943e+05 3.8543e+05 -1.3574e+05 -1.0608e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3415 0.13626 0.0035235 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 9.5103e-07 0.059702 0.00033571 5.9687e-06 INSTANT 0.877007000E-01 TIME STEP NUMBER 57205 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283160095E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.867781861E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.68662E-02 0.23815E+01 Friction velocity uk : 0.68662E-02 0.23815E+01 Dimensionless distance yplus : 0.66529E-02 0.23417E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.067891127e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29909E+08 1 0.22228E-09 0.64876E+02 0.29378E+04 c Velocity[X] 0.36887E+02 c Velocity[Y] 0.27988E+02 c Velocity[Z] 0.96270E-06 c Pressure 0.16533E-03 24 0.98763E-04 0.82618E-03 0.48937E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -37.489 50.575 5.604 7.9961 v Velocity[Y] -37.633 40.961 -0.23581 -0.27482 v Velocity[Z] -3.2607 3.2048 2.0123e-06 -5.3952e-08 v ǁVelocityǁ 0.0003497 50.955 9.4901 8.3386 v Pressure -7.214e+05 2.8444e+05 -2.385e+05 -2.086e+05 v TurbVisc 5.831e-19 0.033377 0.00024415 0.00012172 v CourantNb 1.651e-08 0.012016 0.00017517 5.0059e-06 v FourierNb 1.2475e-07 0.058618 0.00016058 9.637e-07 v total_pressure -6.2007e+05 3.8577e+05 -1.3717e+05 -1.0727e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3417 0.13631 0.0035249 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 9.5177e-07 0.059751 0.00033575 5.9696e-06 INSTANT 0.877008000E-01 TIME STEP NUMBER 57206 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283154673E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.867516118E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.25943E-02 0.23818E+01 Friction velocity uk : 0.25943E-02 0.23818E+01 Dimensionless distance yplus : 0.25407E-02 0.23420E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.060758610e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29911E+08 1 0.22240E-09 0.64965E+02 0.29396E+04 c Velocity[X] 0.36939E+02 c Velocity[Y] 0.28025E+02 c Velocity[Z] 0.93987E-06 c Pressure 0.16082E-03 49 0.82234E-04 0.80291E-03 0.32636E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -37.501 50.584 5.6039 7.9959 v Velocity[Y] -37.642 40.972 -0.23599 -0.27538 v Velocity[Z] -3.2609 3.2049 2.0119e-06 -5.3952e-08 v ǁVelocityǁ 0.00051956 50.965 9.4915 8.3388 v Pressure -7.221e+05 2.8479e+05 -2.3981e+05 -2.0939e+05 v TurbVisc 5.8998e-19 0.03339 0.00024421 0.00012184 v CourantNb 2.0477e-08 0.012017 0.00017518 5.006e-06 v FourierNb 1.2475e-07 0.058666 0.00016061 9.6456e-07 v total_pressure -6.2077e+05 3.8612e+05 -1.3849e+05 -1.0807e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.342 0.13636 0.0035263 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 9.5251e-07 0.0598 0.00033578 5.9705e-06 INSTANT 0.877009000E-01 TIME STEP NUMBER 57207 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283149271E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.867249884E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.14598E-01 0.23820E+01 Friction velocity uk : 0.14598E-01 0.23820E+01 Dimensionless distance yplus : 0.14094E-01 0.23422E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.073476642e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29912E+08 1 0.22249E-09 0.65072E+02 0.29418E+04 c Velocity[X] 0.36983E+02 c Velocity[Y] 0.28089E+02 c Velocity[Z] 0.96538E-06 c Pressure 0.15526E-03 18 0.53769E-04 0.77441E-03 0.31635E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -37.513 50.594 5.6038 7.9958 v Velocity[Y] -37.651 40.983 -0.23617 -0.27595 v Velocity[Z] -3.2612 3.2049 2.0114e-06 -5.3953e-08 v ǁVelocityǁ 0.00080113 50.975 9.4929 8.3391 v Pressure -7.2269e+05 2.8514e+05 -2.4109e+05 -2.101e+05 v TurbVisc 6.3356e-19 0.033402 0.00024428 0.00012197 v CourantNb 1.6271e-08 0.012018 0.00017519 5.006e-06 v FourierNb 1.2475e-07 0.058712 0.00016063 9.6542e-07 v total_pressure -6.2136e+05 3.8646e+05 -1.3977e+05 -1.0878e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3422 0.13642 0.0035277 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 9.5325e-07 0.059848 0.00033582 5.9714e-06 INSTANT 0.877010000E-01 TIME STEP NUMBER 57208 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283143840E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.866975089E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13316E-01 0.23822E+01 Friction velocity uk : 0.13316E-01 0.23822E+01 Dimensionless distance yplus : 0.12857E-01 0.23424E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.090940666e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29913E+08 1 0.22257E-09 0.65166E+02 0.29437E+04 c Velocity[X] 0.37061E+02 c Velocity[Y] 0.28105E+02 c Velocity[Z] 0.94204E-06 c Pressure 0.15537E-03 243 0.75305E-04 0.77429E-03 0.46330E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -37.524 50.603 5.6037 7.9957 v Velocity[Y] -37.66 40.994 -0.23635 -0.27651 v Velocity[Z] -3.2615 3.205 2.011e-06 -5.3953e-08 v ǁVelocityǁ 0.0012024 50.985 9.4943 8.3393 v Pressure -7.2457e+05 2.8549e+05 -2.4236e+05 -2.1097e+05 v TurbVisc 6.4042e-19 0.033415 0.00024435 0.00012209 v CourantNb 1.3822e-08 0.012019 0.0001752 5.0061e-06 v FourierNb 1.2475e-07 0.058759 0.00016066 9.6627e-07 v total_pressure -6.2325e+05 3.8681e+05 -1.4104e+05 -1.0965e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3424 0.13647 0.0035291 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 9.5398e-07 0.059896 0.00033586 5.9724e-06 INSTANT 0.877011000E-01 TIME STEP NUMBER 57209 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283138100E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.866690634E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.14974E-01 0.23824E+01 Friction velocity uk : 0.14974E-01 0.23824E+01 Dimensionless distance yplus : 0.14458E-01 0.23426E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.084786379e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29915E+08 1 0.22267E-09 0.65271E+02 0.29459E+04 c Velocity[X] 0.37108E+02 c Velocity[Y] 0.28163E+02 c Velocity[Z] 0.92920E-06 c Pressure 0.15246E-03 63 0.79663E-04 0.75905E-03 0.45141E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -37.536 50.612 5.6036 7.9955 v Velocity[Y] -37.669 41.005 -0.23654 -0.27708 v Velocity[Z] -3.2618 3.2051 2.0105e-06 -5.3953e-08 v ǁVelocityǁ 0.0016474 50.994 9.4957 8.3395 v Pressure -7.2446e+05 2.8584e+05 -2.4359e+05 -2.1174e+05 v TurbVisc 4.9351e-19 0.033427 0.00024442 0.00012222 v CourantNb 1.3739e-08 0.012021 0.00017521 5.0062e-06 v FourierNb 1.2475e-07 0.058805 0.00016068 9.6713e-07 v total_pressure -6.2314e+05 3.8717e+05 -1.4226e+05 -1.1042e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3426 0.13652 0.0035304 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 9.5472e-07 0.059944 0.00033589 5.9733e-06 INSTANT 0.877012000E-01 TIME STEP NUMBER 57210 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283132599E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.866401291E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13491E-01 0.23827E+01 Friction velocity uk : 0.13491E-01 0.23827E+01 Dimensionless distance yplus : 0.13015E-01 0.23428E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.086519893e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29916E+08 1 0.22277E-09 0.65365E+02 0.29478E+04 c Velocity[X] 0.37165E+02 c Velocity[Y] 0.28201E+02 c Velocity[Z] 0.92944E-06 c Pressure 0.15082E-03 74 0.93386E-04 0.75017E-03 0.45876E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -37.547 50.621 5.6035 7.9954 v Velocity[Y] -37.677 41.016 -0.23672 -0.27764 v Velocity[Z] -3.2621 3.2052 2.0101e-06 -5.3953e-08 v ǁVelocityǁ 0.0021064 51.004 9.4971 8.3397 v Pressure -7.2674e+05 2.8617e+05 -2.4476e+05 -2.1242e+05 v TurbVisc 4.9211e-19 0.03344 0.00024448 0.00012234 v CourantNb 1.3759e-08 0.012022 0.00017522 5.0062e-06 v FourierNb 1.2475e-07 0.05885 0.00016071 9.6799e-07 v total_pressure -6.2542e+05 3.8749e+05 -1.4344e+05 -1.111e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3428 0.13656 0.0035316 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 9.5546e-07 0.059991 0.00033593 5.9742e-06 INSTANT 0.877013000E-01 TIME STEP NUMBER 57211 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283126572E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.866104618E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13312E-01 0.23829E+01 Friction velocity uk : 0.13312E-01 0.23829E+01 Dimensionless distance yplus : 0.12802E-01 0.23431E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.086771385e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29917E+08 1 0.22285E-09 0.65435E+02 0.29492E+04 c Velocity[X] 0.37219E+02 c Velocity[Y] 0.28216E+02 c Velocity[Z] 0.93223E-06 c Pressure 0.14935E-03 453 0.79612E-04 0.74218E-03 0.40520E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -37.559 50.631 5.6034 7.9953 v Velocity[Y] -37.686 41.027 -0.23691 -0.2782 v Velocity[Z] -3.2624 3.2053 2.0097e-06 -5.3953e-08 v ǁVelocityǁ 0.0025726 51.013 9.4984 8.34 v Pressure -7.2694e+05 2.8652e+05 -2.4594e+05 -2.1328e+05 v TurbVisc 4.9487e-19 0.033452 0.00024455 0.00012247 v CourantNb 1.4648e-08 0.012023 0.00017523 5.0063e-06 v FourierNb 1.2475e-07 0.058895 0.00016073 9.6885e-07 v total_pressure -6.2561e+05 3.8785e+05 -1.4462e+05 -1.1196e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3431 0.13662 0.003533 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 9.5621e-07 0.060037 0.00033596 5.9751e-06 INSTANT 0.877014000E-01 TIME STEP NUMBER 57212 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283120759E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.865799684E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.47476E-02 0.23831E+01 Friction velocity uk : 0.47476E-02 0.23831E+01 Dimensionless distance yplus : 0.45658E-02 0.23433E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.086969317e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29918E+08 1 0.22295E-09 0.65543E+02 0.29514E+04 c Velocity[X] 0.37252E+02 c Velocity[Y] 0.28291E+02 c Velocity[Z] 0.94971E-06 c Pressure 0.13781E-03 16 0.56763E-04 0.68418E-03 0.30703E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -37.57 50.64 5.6033 7.9951 v Velocity[Y] -37.694 41.038 -0.23709 -0.27877 v Velocity[Z] -3.2626 3.2054 2.0092e-06 -5.3953e-08 v ǁVelocityǁ 0.0028533 51.023 9.4998 8.3402 v Pressure -7.2756e+05 2.8687e+05 -2.4704e+05 -2.1394e+05 v TurbVisc 4.9859e-19 0.033465 0.00024462 0.0001226 v CourantNb 1.8479e-08 0.012024 0.00017525 5.0064e-06 v FourierNb 1.2475e-07 0.058939 0.00016076 9.697e-07 v total_pressure -6.2624e+05 3.882e+05 -1.4572e+05 -1.1261e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3433 0.13668 0.0035344 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 9.5695e-07 0.060082 0.000336 5.9761e-06 INSTANT 0.877015000E-01 TIME STEP NUMBER 57213 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283114860E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.865489514E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.57280E-02 0.23833E+01 Friction velocity uk : 0.57280E-02 0.23833E+01 Dimensionless distance yplus : 0.55304E-02 0.23435E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.089315710e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29920E+08 1 0.22303E-09 0.65637E+02 0.29533E+04 c Velocity[X] 0.37339E+02 c Velocity[Y] 0.28298E+02 c Velocity[Z] 0.93257E-06 c Pressure 0.13840E-03 532 0.76654E-04 0.68650E-03 0.41540E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -37.582 50.649 5.6032 7.995 v Velocity[Y] -37.703 41.049 -0.23728 -0.27934 v Velocity[Z] -3.2629 3.2055 2.0088e-06 -5.3953e-08 v ǁVelocityǁ 0.0028133 51.032 9.5012 8.3404 v Pressure -7.2936e+05 2.8723e+05 -2.4809e+05 -2.1458e+05 v TurbVisc 6.0033e-19 0.033478 0.00024469 0.00012272 v CourantNb 2.2175e-08 0.012025 0.00017526 5.0064e-06 v FourierNb 1.2475e-07 0.058982 0.00016078 9.7056e-07 v total_pressure -6.2803e+05 3.8856e+05 -1.4677e+05 -1.1326e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3435 0.13674 0.0035362 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 9.577e-07 0.060127 0.00033604 5.977e-06 INSTANT 0.877016000E-01 TIME STEP NUMBER 57214 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283108736E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.865171943E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11950E-01 0.23836E+01 Friction velocity uk : 0.11950E-01 0.23836E+01 Dimensionless distance yplus : 0.11538E-01 0.23437E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.087746857e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29921E+08 1 0.22313E-09 0.65741E+02 0.29554E+04 c Velocity[X] 0.37376E+02 c Velocity[Y] 0.28366E+02 c Velocity[Z] 0.92240E-06 c Pressure 0.13571E-03 54 0.82174E-04 0.67249E-03 0.47064E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -37.593 50.658 5.6031 7.9948 v Velocity[Y] -37.711 41.06 -0.23746 -0.27991 v Velocity[Z] -3.2632 3.2056 2.0083e-06 -5.3953e-08 v ǁVelocityǁ 0.0027931 51.041 9.5026 8.3406 v Pressure -7.2932e+05 2.8759e+05 -2.4916e+05 -2.1538e+05 v TurbVisc 5.2154e-19 0.03349 0.00024475 0.00012285 v CourantNb 2.6135e-08 0.012026 0.00017527 5.0065e-06 v FourierNb 1.2475e-07 0.059026 0.00016081 9.7142e-07 v total_pressure -6.28e+05 3.8892e+05 -1.4783e+05 -1.1406e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3437 0.1368 0.003538 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 9.5844e-07 0.060172 0.00033607 5.9779e-06 INSTANT 0.877017000E-01 TIME STEP NUMBER 57215 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283102803E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.864851652E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.16686E-01 0.23838E+01 Friction velocity uk : 0.16686E-01 0.23838E+01 Dimensionless distance yplus : 0.16110E-01 0.23439E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.085039033e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29922E+08 1 0.22323E-09 0.65835E+02 0.29573E+04 c Velocity[X] 0.37438E+02 c Velocity[Y] 0.28398E+02 c Velocity[Z] 0.91773E-06 c Pressure 0.13447E-03 107 0.96190E-04 0.66572E-03 0.44187E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -37.604 50.667 5.6029 7.9947 v Velocity[Y] -37.72 41.07 -0.23765 -0.28048 v Velocity[Z] -3.2635 3.2056 2.0079e-06 -5.3953e-08 v ǁVelocityǁ 0.0027293 51.051 9.504 8.3408 v Pressure -7.3156e+05 2.8793e+05 -2.5014e+05 -2.1592e+05 v TurbVisc 5.3932e-19 0.033503 0.00024482 0.00012297 v CourantNb 3.0122e-08 0.012028 0.00017528 5.0066e-06 v FourierNb 1.2475e-07 0.059068 0.00016083 9.7228e-07 v total_pressure -6.3023e+05 3.8926e+05 -1.4882e+05 -1.1459e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3439 0.13686 0.0035397 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 9.5919e-07 0.060216 0.00033611 5.9788e-06 INSTANT 0.877018000E-01 TIME STEP NUMBER 57216 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283096416E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.864526028E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.20399E-01 0.23840E+01 Friction velocity uk : 0.20399E-01 0.23840E+01 Dimensionless distance yplus : 0.19696E-01 0.23442E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.081247119e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29924E+08 1 0.22331E-09 0.65902E+02 0.29586E+04 c Velocity[X] 0.37490E+02 c Velocity[Y] 0.28412E+02 c Velocity[Z] 0.91150E-06 c Pressure 0.13357E-03 471 0.81896E-04 0.66065E-03 0.36430E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -37.615 50.675 5.6028 7.9945 v Velocity[Y] -37.728 41.081 -0.23784 -0.28105 v Velocity[Z] -3.2638 3.2057 2.0074e-06 -5.3953e-08 v ǁVelocityǁ 0.0026362 51.06 9.5054 8.3411 v Pressure -7.3172e+05 2.883e+05 -2.5111e+05 -2.1665e+05 v TurbVisc 5.3387e-19 0.033515 0.00024489 0.0001231 v CourantNb 3.4137e-08 0.012029 0.00017529 5.0066e-06 v FourierNb 1.2475e-07 0.05911 0.00016086 9.7314e-07 v total_pressure -6.304e+05 3.8962e+05 -1.4978e+05 -1.1532e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3442 0.13692 0.0035413 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 9.5994e-07 0.06026 0.00033615 5.9798e-06 INSTANT 0.877019000E-01 TIME STEP NUMBER 57217 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283090246E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.864194482E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.23546E-01 0.23842E+01 Friction velocity uk : 0.23546E-01 0.23842E+01 Dimensionless distance yplus : 0.22734E-01 0.23444E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.079475904e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29925E+08 1 0.22341E-09 0.66010E+02 0.29608E+04 c Velocity[X] 0.37522E+02 c Velocity[Y] 0.28488E+02 c Velocity[Z] 0.95374E-06 c Pressure 0.12037E-03 15 0.57900E-04 0.59484E-03 0.28018E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -37.627 50.684 5.6027 7.9944 v Velocity[Y] -37.737 41.092 -0.23802 -0.28162 v Velocity[Z] -3.2641 3.2058 2.007e-06 -5.3953e-08 v ǁVelocityǁ 0.0025496 51.069 9.5068 8.3413 v Pressure -7.323e+05 2.8865e+05 -2.5202e+05 -2.1721e+05 v TurbVisc 5.7615e-19 0.033528 0.00024495 0.00012323 v CourantNb 3.612e-08 0.01203 0.0001753 5.0067e-06 v FourierNb 1.2475e-07 0.059152 0.00016088 9.74e-07 v total_pressure -6.3097e+05 3.8998e+05 -1.5069e+05 -1.1589e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3444 0.13697 0.0035429 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 9.6069e-07 0.060303 0.00033618 5.9807e-06 INSTANT 0.877020000E-01 TIME STEP NUMBER 57218 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283084023E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.863856676E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.26366E-01 0.23844E+01 Friction velocity uk : 0.26366E-01 0.23844E+01 Dimensionless distance yplus : 0.25456E-01 0.23446E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.077631076e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29926E+08 1 0.22349E-09 0.66102E+02 0.29627E+04 c Velocity[X] 0.37607E+02 c Velocity[Y] 0.28496E+02 c Velocity[Z] 0.92244E-06 c Pressure 0.12199E-03 480 0.78659E-04 0.60226E-03 0.38798E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -37.638 50.693 5.6026 7.9943 v Velocity[Y] -37.745 41.102 -0.23821 -0.28219 v Velocity[Z] -3.2644 3.2059 2.0066e-06 -5.3954e-08 v ǁVelocityǁ 0.0024689 51.078 9.5082 8.3415 v Pressure -7.3413e+05 2.8901e+05 -2.5286e+05 -2.1771e+05 v TurbVisc 6.3369e-19 0.03354 0.00024502 0.00012335 v CourantNb 3.6411e-08 0.012031 0.00017532 5.0067e-06 v FourierNb 1.2475e-07 0.059193 0.0001609 9.7487e-07 v total_pressure -6.3281e+05 3.9034e+05 -1.5154e+05 -1.1639e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3446 0.13703 0.0035445 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 9.6144e-07 0.060346 0.00033622 5.9816e-06 INSTANT 0.877021000E-01 TIME STEP NUMBER 57219 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283077568E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.863512839E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.28822E-01 0.23847E+01 Friction velocity uk : 0.28822E-01 0.23847E+01 Dimensionless distance yplus : 0.27828E-01 0.23448E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.075120299e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29927E+08 1 0.22359E-09 0.66207E+02 0.29648E+04 c Velocity[X] 0.37643E+02 c Velocity[Y] 0.28563E+02 c Velocity[Z] 0.90288E-06 c Pressure 0.11964E-03 49 0.84309E-04 0.59009E-03 0.44852E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -37.649 50.702 5.6025 7.9941 v Velocity[Y] -37.753 41.113 -0.2384 -0.28276 v Velocity[Z] -3.2646 3.206 2.0061e-06 -5.3954e-08 v ǁVelocityǁ 0.0023958 51.087 9.5096 8.3417 v Pressure -7.3404e+05 2.8938e+05 -2.5373e+05 -2.1841e+05 v TurbVisc 6.3445e-19 0.033553 0.00024508 0.00012348 v CourantNb 3.6568e-08 0.012032 0.00017533 5.0068e-06 v FourierNb 1.2475e-07 0.059233 0.00016093 9.7573e-07 v total_pressure -6.3272e+05 3.9071e+05 -1.524e+05 -1.1708e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3448 0.13708 0.003546 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 9.6219e-07 0.060388 0.00033626 5.9825e-06 INSTANT 0.877022000E-01 TIME STEP NUMBER 57220 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283071338E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.863166122E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.31135E-01 0.23849E+01 Friction velocity uk : 0.31135E-01 0.23849E+01 Dimensionless distance yplus : 0.30061E-01 0.23451E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.070807963e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29929E+08 1 0.22369E-09 0.66300E+02 0.29667E+04 c Velocity[X] 0.37706E+02 c Velocity[Y] 0.28594E+02 c Velocity[Z] 0.90546E-06 c Pressure 0.11909E-03 249 0.98694E-04 0.58684E-03 0.43813E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -37.66 50.71 5.6024 7.994 v Velocity[Y] -37.761 41.124 -0.23859 -0.28333 v Velocity[Z] -3.2649 3.2061 2.0057e-06 -5.3954e-08 v ǁVelocityǁ 0.0023304 51.096 9.5109 8.3419 v Pressure -7.3627e+05 2.8973e+05 -2.5452e+05 -2.1885e+05 v TurbVisc 6.1718e-19 0.033565 0.00024515 0.00012361 v CourantNb 3.6832e-08 0.012033 0.00017534 5.0069e-06 v FourierNb 1.2475e-07 0.059273 0.00016095 9.7659e-07 v total_pressure -6.3495e+05 3.9105e+05 -1.532e+05 -1.1753e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3451 0.13714 0.0035476 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 9.6294e-07 0.060429 0.00033629 5.9835e-06 INSTANT 0.877023000E-01 TIME STEP NUMBER 57221 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283064680E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.862815279E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.31519E-01 0.23852E+01 Friction velocity uk : 0.31519E-01 0.23852E+01 Dimensionless distance yplus : 0.30432E-01 0.23453E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.066776972e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29930E+08 1 0.22377E-09 0.66363E+02 0.29679E+04 c Velocity[X] 0.37748E+02 c Velocity[Y] 0.28615E+02 c Velocity[Z] 0.88988E-06 c Pressure 0.11902E-03 105 0.84025E-04 0.58597E-03 0.33386E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -37.671 50.719 5.6023 7.9938 v Velocity[Y] -37.77 41.134 -0.23878 -0.28391 v Velocity[Z] -3.2652 3.2062 2.0052e-06 -5.3954e-08 v ǁVelocityǁ 0.002274 51.105 9.5123 8.3421 v Pressure -7.3649e+05 2.901e+05 -2.5527e+05 -2.1946e+05 v TurbVisc 6.0889e-19 0.033578 0.00024521 0.00012373 v CourantNb 3.8906e-08 0.012034 0.00017535 5.0069e-06 v FourierNb 1.2475e-07 0.059312 0.00016098 9.7745e-07 v total_pressure -6.3516e+05 3.9142e+05 -1.5395e+05 -1.1813e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3453 0.13719 0.0035491 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 9.6369e-07 0.06047 0.00033633 5.9844e-06 INSTANT 0.877024000E-01 TIME STEP NUMBER 57222 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283058207E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.862461336E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.29863E-01 0.23854E+01 Friction velocity uk : 0.29863E-01 0.23854E+01 Dimensionless distance yplus : 0.28833E-01 0.23455E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.064061970e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29931E+08 1 0.22387E-09 0.66472E+02 0.29701E+04 c Velocity[X] 0.37791E+02 c Velocity[Y] 0.28681E+02 c Velocity[Z] 0.91005E-06 c Pressure 0.10407E-03 13 0.58165E-04 0.51187E-03 0.20896E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -37.682 50.727 5.6022 7.9937 v Velocity[Y] -37.778 41.145 -0.23896 -0.28448 v Velocity[Z] -3.2655 3.2062 2.0048e-06 -5.3954e-08 v ǁVelocityǁ 0.0022341 51.114 9.5137 8.3424 v Pressure -7.3687e+05 2.9047e+05 -2.5592e+05 -2.198e+05 v TurbVisc 6.0517e-19 0.03359 0.00024528 0.00012386 v CourantNb 4.2842e-08 0.012035 0.00017536 5.007e-06 v FourierNb 1.2475e-07 0.059351 0.000161 9.7831e-07 v total_pressure -6.3555e+05 3.9179e+05 -1.5459e+05 -1.1848e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3455 0.13725 0.0035506 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 9.6445e-07 0.06051 0.00033636 5.9853e-06 INSTANT 0.877025000E-01 TIME STEP NUMBER 57223 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283051809E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.862101378E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.28117E-01 0.23856E+01 Friction velocity uk : 0.28117E-01 0.23856E+01 Dimensionless distance yplus : 0.27147E-01 0.23457E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.063430128e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29932E+08 1 0.22396E-09 0.66561E+02 0.29719E+04 c Velocity[X] 0.37864E+02 c Velocity[Y] 0.28697E+02 c Velocity[Z] 0.90725E-06 c Pressure 0.10706E-03 85 0.80140E-04 0.52607E-03 0.38493E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -37.693 50.736 5.6021 7.9935 v Velocity[Y] -37.786 41.155 -0.23915 -0.28505 v Velocity[Z] -3.2658 3.2063 2.0043e-06 -5.3954e-08 v ǁVelocityǁ 0.0021879 51.123 9.5151 8.3426 v Pressure -7.3888e+05 2.9082e+05 -2.5665e+05 -2.2033e+05 v TurbVisc 5.348e-19 0.033602 0.00024534 0.00012399 v CourantNb 4.6627e-08 0.012037 0.00017537 5.0071e-06 v FourierNb 1.2475e-07 0.05939 0.00016102 9.7918e-07 v total_pressure -6.3756e+05 3.9214e+05 -1.5533e+05 -1.19e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3457 0.1373 0.0035521 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 9.6521e-07 0.060551 0.0003364 5.9862e-06 INSTANT 0.877026000E-01 TIME STEP NUMBER 57224 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283045058E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.861736694E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.26956E-01 0.23859E+01 Friction velocity uk : 0.26956E-01 0.23859E+01 Dimensionless distance yplus : 0.26026E-01 0.23460E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.058280232e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29934E+08 1 0.22406E-09 0.66666E+02 0.29740E+04 c Velocity[X] 0.37902E+02 c Velocity[Y] 0.28763E+02 c Velocity[Z] 0.88836E-06 c Pressure 0.10536E-03 560 0.85913E-04 0.51725E-03 0.42949E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -37.704 50.744 5.602 7.9933 v Velocity[Y] -37.794 41.165 -0.23934 -0.28563 v Velocity[Z] -3.266 3.2064 2.0039e-06 -5.3954e-08 v ǁVelocityǁ 0.0021597 51.131 9.5164 8.3428 v Pressure -7.3872e+05 2.9119e+05 -2.5729e+05 -2.2092e+05 v TurbVisc 6.0184e-19 0.033615 0.00024541 0.00012411 v CourantNb 4.642e-08 0.012038 0.00017539 5.0071e-06 v FourierNb 1.2475e-07 0.059428 0.00016104 9.8004e-07 v total_pressure -6.3739e+05 3.9252e+05 -1.5596e+05 -1.196e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.346 0.13735 0.0035536 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 9.6596e-07 0.06059 0.00033643 5.9872e-06 INSTANT 0.877027000E-01 TIME STEP NUMBER 57225 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283038606E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.861369369E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.25930E-01 0.23861E+01 Friction velocity uk : 0.25930E-01 0.23861E+01 Dimensionless distance yplus : 0.25036E-01 0.23462E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.054933929e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29935E+08 1 0.22416E-09 0.66728E+02 0.29752E+04 c Velocity[X] 0.37968E+02 c Velocity[Y] 0.28761E+02 c Velocity[Z] 0.88130E-06 c Pressure 0.10589E-03 111 0.75167E-04 0.51938E-03 0.23305E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -37.714 50.753 5.6018 7.9932 v Velocity[Y] -37.802 41.176 -0.23953 -0.28621 v Velocity[Z] -3.2663 3.2065 2.0035e-06 -5.3954e-08 v ǁVelocityǁ 0.0021415 51.14 9.5178 8.343 v Pressure -7.4016e+05 2.9156e+05 -2.578e+05 -2.2109e+05 v TurbVisc 6.1552e-19 0.033627 0.00024547 0.00012424 v CourantNb 4.6676e-08 0.012039 0.0001754 5.0072e-06 v FourierNb 1.2475e-07 0.059465 0.00016107 9.8091e-07 v total_pressure -6.3883e+05 3.9288e+05 -1.5648e+05 -1.1976e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3462 0.13741 0.003555 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 9.6672e-07 0.06063 0.00033646 5.9881e-06 INSTANT 0.877028000E-01 TIME STEP NUMBER 57226 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283031971E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.861001772E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.25380E-01 0.23864E+01 Friction velocity uk : 0.25380E-01 0.23864E+01 Dimensionless distance yplus : 0.24505E-01 0.23465E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.053908504e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29936E+08 1 0.22425E-09 0.66831E+02 0.29773E+04 c Velocity[X] 0.38007E+02 c Velocity[Y] 0.28824E+02 c Velocity[Z] 0.88596E-06 c Pressure 0.92596E-04 7 0.55805E-04 0.45373E-03 0.18593E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -37.725 50.761 5.6017 7.993 v Velocity[Y] -37.81 41.186 -0.23973 -0.28678 v Velocity[Z] -3.2666 3.2066 2.003e-06 -5.3954e-08 v ǁVelocityǁ 0.0021348 51.149 9.5192 8.3432 v Pressure -7.4165e+05 2.9192e+05 -2.5828e+05 -2.2138e+05 v TurbVisc 6.2668e-19 0.03364 0.00024554 0.00012437 v CourantNb 4.6694e-08 0.01204 0.00017541 5.0073e-06 v FourierNb 1.2475e-07 0.059502 0.00016109 9.8177e-07 v total_pressure -6.4032e+05 3.9325e+05 -1.5695e+05 -1.2006e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3465 0.13746 0.0035565 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 9.6748e-07 0.060668 0.0003365 5.989e-06 INSTANT 0.877029000E-01 TIME STEP NUMBER 57227 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283025210E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.860627252E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.25044E-01 0.23866E+01 Friction velocity uk : 0.25044E-01 0.23866E+01 Dimensionless distance yplus : 0.24173E-01 0.23467E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.059304774e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29938E+08 1 0.22432E-09 0.66913E+02 0.29789E+04 c Velocity[X] 0.38065E+02 c Velocity[Y] 0.28848E+02 c Velocity[Z] 0.88425E-06 c Pressure 0.95799E-04 65 0.97481E-04 0.46898E-03 0.29255E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -37.736 50.769 5.6016 7.9929 v Velocity[Y] -37.818 41.196 -0.23992 -0.28736 v Velocity[Z] -3.2669 3.2067 2.0026e-06 -5.3954e-08 v ǁVelocityǁ 0.002136 51.157 9.5206 8.3434 v Pressure -7.4223e+05 2.9228e+05 -2.5894e+05 -2.221e+05 v TurbVisc 6.3227e-19 0.033652 0.0002456 0.00012449 v CourantNb 4.6607e-08 0.012041 0.00017542 5.0073e-06 v FourierNb 1.2475e-07 0.059539 0.00016111 9.8263e-07 v total_pressure -6.4091e+05 3.936e+05 -1.5761e+05 -1.2078e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3467 0.13751 0.0035579 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 9.6824e-07 0.060707 0.00033654 5.99e-06 INSTANT 0.877030000E-01 TIME STEP NUMBER 57228 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283018440E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.860242975E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.22899E-01 0.23868E+01 Friction velocity uk : 0.22899E-01 0.23868E+01 Dimensionless distance yplus : 0.22102E-01 0.23470E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.038955763e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29939E+08 1 0.22443E-09 0.66998E+02 0.29806E+04 c Velocity[X] 0.38107E+02 c Velocity[Y] 0.28891E+02 c Velocity[Z] 0.88183E-06 c Pressure 0.91669E-04 207 0.81184E-04 0.44834E-03 0.14110E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -37.747 50.777 5.6015 7.9927 v Velocity[Y] -37.826 41.207 -0.24011 -0.28794 v Velocity[Z] -3.2672 3.2068 2.0021e-06 -5.3954e-08 v ǁVelocityǁ 0.0021479 51.166 9.5219 8.3436 v Pressure -7.4288e+05 2.9266e+05 -2.5932e+05 -2.2236e+05 v TurbVisc 6.4999e-19 0.033665 0.00024567 0.00012462 v CourantNb 4.6255e-08 0.012042 0.00017543 5.0074e-06 v FourierNb 1.2475e-07 0.059575 0.00016114 9.835e-07 v total_pressure -6.4156e+05 3.9398e+05 -1.58e+05 -1.2104e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.347 0.13756 0.0035593 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 9.69e-07 0.060745 0.00033657 5.9909e-06 INSTANT 0.877031000E-01 TIME STEP NUMBER 57229 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283011769E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.859870340E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.20663E-01 0.23871E+01 Friction velocity uk : 0.20663E-01 0.23871E+01 Dimensionless distance yplus : 0.19945E-01 0.23472E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.055979917e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29940E+08 1 0.22453E-09 0.67102E+02 0.29827E+04 c Velocity[X] 0.38147E+02 c Velocity[Y] 0.28955E+02 c Velocity[Z] 0.88216E-06 c Pressure 0.85793E-04 7 0.51600E-04 0.41921E-03 0.16639E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -37.757 50.786 5.6014 7.9926 v Velocity[Y] -37.833 41.217 -0.2403 -0.28852 v Velocity[Z] -3.2675 3.2069 2.0017e-06 -5.3954e-08 v ǁVelocityǁ 0.002166 51.175 9.5233 8.3439 v Pressure -7.4334e+05 2.9304e+05 -2.5965e+05 -2.2257e+05 v TurbVisc 5.8737e-19 0.033677 0.00024573 0.00012475 v CourantNb 4.6412e-08 0.012043 0.00017545 5.0074e-06 v FourierNb 1.2475e-07 0.059611 0.00016116 9.8437e-07 v total_pressure -6.4202e+05 3.9436e+05 -1.5833e+05 -1.2124e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3472 0.13761 0.0035607 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 9.6977e-07 0.060783 0.00033661 5.9918e-06 INSTANT 0.877032000E-01 TIME STEP NUMBER 57230 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283005178E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.859490413E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.18611E-01 0.23873E+01 Friction velocity uk : 0.18611E-01 0.23873E+01 Dimensionless distance yplus : 0.17964E-01 0.23474E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.052067371e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29942E+08 1 0.22462E-09 0.67179E+02 0.29842E+04 c Velocity[X] 0.38207E+02 c Velocity[Y] 0.28972E+02 c Velocity[Z] 0.87283E-06 c Pressure 0.90153E-04 30 0.97905E-04 0.44010E-03 0.17062E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -37.768 50.794 5.6013 7.9924 v Velocity[Y] -37.841 41.227 -0.24049 -0.2891 v Velocity[Z] -3.2677 3.2069 2.0013e-06 -5.3955e-08 v ǁVelocityǁ 0.0022038 51.183 9.5247 8.3441 v Pressure -7.4463e+05 2.934e+05 -2.6009e+05 -2.2291e+05 v TurbVisc 6.3162e-19 0.03369 0.00024579 0.00012488 v CourantNb 4.6397e-08 0.012044 0.00017546 5.0075e-06 v FourierNb 1.2475e-07 0.059647 0.00016119 9.8523e-07 v total_pressure -6.4331e+05 3.9473e+05 -1.5877e+05 -1.2159e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3474 0.13766 0.0035621 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 9.7053e-07 0.06082 0.00033665 5.9927e-06 INSTANT 0.877033000E-01 TIME STEP NUMBER 57231 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282998395E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.859100800E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15559E-01 0.23876E+01 Friction velocity uk : 0.15559E-01 0.23876E+01 Dimensionless distance yplus : 0.15018E-01 0.23477E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.048880651e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29943E+08 1 0.22472E-09 0.67268E+02 0.29859E+04 c Velocity[X] 0.38265E+02 c Velocity[Y] 0.29002E+02 c Velocity[Z] 0.86736E-06 c Pressure 0.86722E-04 52 0.83501E-04 0.42295E-03 0.12805E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -37.779 50.802 5.6012 7.9923 v Velocity[Y] -37.849 41.237 -0.24069 -0.28968 v Velocity[Z] -3.268 3.207 2.0008e-06 -5.3955e-08 v ǁVelocityǁ 0.0022002 51.191 9.526 8.3443 v Pressure -7.4571e+05 2.9377e+05 -2.604e+05 -2.2315e+05 v TurbVisc 6.5438e-19 0.033702 0.00024586 0.000125 v CourantNb 4.6362e-08 0.012045 0.00017547 5.0076e-06 v FourierNb 1.2475e-07 0.059682 0.00016121 9.861e-07 v total_pressure -6.4439e+05 3.951e+05 -1.5907e+05 -1.2182e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3477 0.13771 0.0035634 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 9.713e-07 0.060857 0.00033668 5.9937e-06 INSTANT 0.877034000E-01 TIME STEP NUMBER 57232 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282991641E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.858716831E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12272E-01 0.23879E+01 Friction velocity uk : 0.12272E-01 0.23879E+01 Dimensionless distance yplus : 0.11845E-01 0.23479E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.054797236e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29944E+08 1 0.22482E-09 0.67372E+02 0.29880E+04 c Velocity[X] 0.38314E+02 c Velocity[Y] 0.29058E+02 c Velocity[Z] 0.89617E-06 c Pressure 0.81197E-04 13 0.56092E-04 0.39563E-03 0.15867E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -37.789 50.81 5.6011 7.9921 v Velocity[Y] -37.857 41.247 -0.24088 -0.29026 v Velocity[Z] -3.2683 3.2071 2.0004e-06 -5.3955e-08 v ǁVelocityǁ 0.0021278 51.2 9.5274 8.3445 v Pressure -7.4703e+05 2.9415e+05 -2.6057e+05 -2.2325e+05 v TurbVisc 7.2042e-19 0.033715 0.00024592 0.00012513 v CourantNb 4.6328e-08 0.012047 0.00017548 5.0076e-06 v FourierNb 1.2476e-07 0.059718 0.00016124 9.8697e-07 v total_pressure -6.4571e+05 3.9547e+05 -1.5925e+05 -1.2192e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3479 0.13776 0.0035647 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 9.7207e-07 0.060894 0.00033672 5.9946e-06 INSTANT 0.877035000E-01 TIME STEP NUMBER 57233 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282984868E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.858329975E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.51946E-02 0.23881E+01 Friction velocity uk : 0.51946E-02 0.23881E+01 Dimensionless distance yplus : 0.50395E-02 0.23482E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.057410449e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29945E+08 1 0.22489E-09 0.67465E+02 0.29899E+04 c Velocity[X] 0.38361E+02 c Velocity[Y] 0.29104E+02 c Velocity[Z] 0.87537E-06 c Pressure 0.87445E-04 35 0.77640E-04 0.42568E-03 0.37385E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -37.8 50.818 5.601 7.992 v Velocity[Y] -37.864 41.257 -0.24107 -0.29084 v Velocity[Z] -3.2686 3.2072 1.9999e-06 -5.3955e-08 v ǁVelocityǁ 0.0019938 51.208 9.5288 8.3447 v Pressure -7.4699e+05 2.9452e+05 -2.6099e+05 -2.2382e+05 v TurbVisc 7.0695e-19 0.033728 0.00024599 0.00012526 v CourantNb 4.6214e-08 0.012048 0.00017549 5.0077e-06 v FourierNb 1.2476e-07 0.059753 0.00016127 9.8783e-07 v total_pressure -6.4566e+05 3.9585e+05 -1.5967e+05 -1.2249e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3482 0.1378 0.0035659 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 9.7283e-07 0.060932 0.00033676 5.9955e-06 INSTANT 0.877036000E-01 TIME STEP NUMBER 57234 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282978222E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.857934249E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19330E-02 0.23883E+01 Friction velocity uk : 0.19330E-02 0.23883E+01 Dimensionless distance yplus : 0.18658E-02 0.23484E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.044103477e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29947E+08 1 0.22501E-09 0.67554E+02 0.29916E+04 c Velocity[X] 0.38407E+02 c Velocity[Y] 0.29147E+02 c Velocity[Z] 0.87607E-06 c Pressure 0.87793E-04 45 0.82500E-04 0.42697E-03 0.33680E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -37.81 50.826 5.6009 7.9918 v Velocity[Y] -37.872 41.267 -0.24127 -0.29142 v Velocity[Z] -3.2689 3.2073 1.9995e-06 -5.3955e-08 v ǁVelocityǁ 0.0018981 51.217 9.5301 8.3449 v Pressure -7.4904e+05 2.949e+05 -2.6109e+05 -2.2383e+05 v TurbVisc 6.3979e-19 0.03374 0.00024605 0.00012538 v CourantNb 4.6144e-08 0.012049 0.00017551 5.0078e-06 v FourierNb 1.2476e-07 0.059787 0.00016129 9.887e-07 v total_pressure -6.4772e+05 3.9622e+05 -1.5976e+05 -1.225e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3484 0.13785 0.0035672 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 9.736e-07 0.060968 0.0003368 5.9965e-06 INSTANT 0.877037000E-01 TIME STEP NUMBER 57235 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282971280E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.857551397E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.46664E-02 0.23886E+01 Friction velocity uk : 0.46664E-02 0.23886E+01 Dimensionless distance yplus : 0.44878E-02 0.23487E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.055650196e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29948E+08 1 0.22509E-09 0.67653E+02 0.29936E+04 c Velocity[X] 0.38454E+02 c Velocity[Y] 0.29199E+02 c Velocity[Z] 0.87463E-06 c Pressure 0.90666E-04 72 0.95833E-04 0.44052E-03 0.39183E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -37.821 50.834 5.6007 7.9916 v Velocity[Y] -37.88 41.277 -0.24146 -0.29201 v Velocity[Z] -3.2691 3.2074 1.999e-06 -5.3955e-08 v ǁVelocityǁ 0.001808 51.225 9.5315 8.3451 v Pressure -7.4851e+05 2.953e+05 -2.612e+05 -2.2398e+05 v TurbVisc 6.4462e-19 0.033753 0.00024611 0.00012551 v CourantNb 4.6283e-08 0.01205 0.00017552 5.0078e-06 v FourierNb 1.2476e-07 0.059822 0.00016132 9.8957e-07 v total_pressure -6.4719e+05 3.9662e+05 -1.5988e+05 -1.2266e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3487 0.1379 0.0035686 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 9.7438e-07 0.061004 0.00033683 5.9974e-06 INSTANT 0.877038000E-01 TIME STEP NUMBER 57236 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282964779E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.857161437E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11110E-01 0.23888E+01 Friction velocity uk : 0.11110E-01 0.23888E+01 Dimensionless distance yplus : 0.10724E-01 0.23489E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.060355782e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29949E+08 1 0.22521E-09 0.67707E+02 0.29946E+04 c Velocity[X] 0.38504E+02 c Velocity[Y] 0.29203E+02 c Velocity[Z] 0.86632E-06 c Pressure 0.93853E-04 495 0.81261E-04 0.45557E-03 0.23282E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -37.831 50.842 5.6006 7.9915 v Velocity[Y] -37.887 41.287 -0.24165 -0.29259 v Velocity[Z] -3.2694 3.2075 1.9986e-06 -5.3955e-08 v ǁVelocityǁ 0.0017248 51.233 9.5328 8.3454 v Pressure -7.5017e+05 2.9567e+05 -2.6131e+05 -2.241e+05 v TurbVisc 6.4372e-19 0.033765 0.00024617 0.00012564 v CourantNb 4.6234e-08 0.012051 0.00017553 5.0079e-06 v FourierNb 1.2476e-07 0.059856 0.00016134 9.9044e-07 v total_pressure -6.4884e+05 3.9699e+05 -1.5999e+05 -1.2277e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3489 0.13797 0.0035704 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 9.7515e-07 0.06104 0.00033687 5.9983e-06 INSTANT 0.877039000E-01 TIME STEP NUMBER 57237 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282958014E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.856767626E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.14691E-01 0.23891E+01 Friction velocity uk : 0.14691E-01 0.23891E+01 Dimensionless distance yplus : 0.14180E-01 0.23492E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.063737714e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29951E+08 1 0.22529E-09 0.67810E+02 0.29966E+04 c Velocity[X] 0.38547E+02 c Velocity[Y] 0.29263E+02 c Velocity[Z] 0.85723E-06 c Pressure 0.78896E-04 6 0.57458E-04 0.38261E-03 0.16159E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -37.841 50.85 5.6005 7.9913 v Velocity[Y] -37.895 41.297 -0.24185 -0.29317 v Velocity[Z] -3.2697 3.2075 1.9982e-06 -5.3955e-08 v ǁVelocityǁ 0.0016538 51.241 9.5342 8.3456 v Pressure -7.5156e+05 2.9605e+05 -2.6134e+05 -2.2418e+05 v TurbVisc 6.4123e-19 0.033778 0.00024624 0.00012577 v CourantNb 4.6192e-08 0.012052 0.00017554 5.008e-06 v FourierNb 1.2476e-07 0.05989 0.00016136 9.9131e-07 v total_pressure -6.5024e+05 3.9737e+05 -1.6002e+05 -1.2285e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3492 0.13803 0.0035722 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 9.7592e-07 0.061076 0.00033691 5.9993e-06 INSTANT 0.877040000E-01 TIME STEP NUMBER 57238 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282951199E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.856374597E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.17461E-01 0.23893E+01 Friction velocity uk : 0.17461E-01 0.23893E+01 Dimensionless distance yplus : 0.16854E-01 0.23494E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.069820908e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29952E+08 1 0.22537E-09 0.67901E+02 0.29984E+04 c Velocity[X] 0.38598E+02 c Velocity[Y] 0.29303E+02 c Velocity[Z] 0.84908E-06 c Pressure 0.86761E-04 95 0.77428E-04 0.42036E-03 0.31329E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -37.852 50.857 5.6004 7.9912 v Velocity[Y] -37.902 41.307 -0.24204 -0.29376 v Velocity[Z] -3.27 3.2076 1.9977e-06 -5.3955e-08 v ǁVelocityǁ 0.0015844 51.249 9.5355 8.3458 v Pressure -7.5133e+05 2.9644e+05 -2.6139e+05 -2.2438e+05 v TurbVisc 6.6142e-19 0.033791 0.0002463 0.00012589 v CourantNb 4.2061e-08 0.012053 0.00017555 5.008e-06 v FourierNb 1.2476e-07 0.059925 0.00016139 9.9218e-07 v total_pressure -6.5e+05 3.9776e+05 -1.6007e+05 -1.2305e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3494 0.13809 0.003574 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 9.767e-07 0.061112 0.00033694 6.0002e-06 INSTANT 0.877041000E-01 TIME STEP NUMBER 57239 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282944664E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.855978796E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.18599E-01 0.23896E+01 Friction velocity uk : 0.18599E-01 0.23896E+01 Dimensionless distance yplus : 0.17992E-01 0.23497E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.070995647e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29954E+08 1 0.22550E-09 0.67989E+02 0.30002E+04 c Velocity[X] 0.38643E+02 c Velocity[Y] 0.29347E+02 c Velocity[Z] 0.84582E-06 c Pressure 0.88377E-04 58 0.83075E-04 0.42778E-03 0.33721E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -37.862 50.865 5.6003 7.991 v Velocity[Y] -37.91 41.317 -0.24224 -0.29434 v Velocity[Z] -3.2703 3.2077 1.9973e-06 -5.3955e-08 v ǁVelocityǁ 0.0015299 51.258 9.5369 8.346 v Pressure -7.5344e+05 2.9681e+05 -2.6136e+05 -2.2441e+05 v TurbVisc 6.4938e-19 0.033803 0.00024636 0.00012602 v CourantNb 3.769e-08 0.012054 0.00017557 5.0081e-06 v FourierNb 1.2476e-07 0.059959 0.00016141 9.9305e-07 v total_pressure -6.5211e+05 3.9814e+05 -1.6003e+05 -1.2308e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3497 0.13815 0.0035757 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 9.7747e-07 0.061148 0.00033698 6.0011e-06 INSTANT 0.877042000E-01 TIME STEP NUMBER 57240 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282937794E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.855587144E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.22238E-01 0.23899E+01 Friction velocity uk : 0.22238E-01 0.23899E+01 Dimensionless distance yplus : 0.21464E-01 0.23499E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.076863044e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29955E+08 1 0.22557E-09 0.68088E+02 0.30021E+04 c Velocity[X] 0.38690E+02 c Velocity[Y] 0.29398E+02 c Velocity[Z] 0.84510E-06 c Pressure 0.92484E-04 104 0.96281E-04 0.44724E-03 0.39004E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -37.873 50.873 5.6002 7.9909 v Velocity[Y] -37.917 41.327 -0.24243 -0.29493 v Velocity[Z] -3.2705 3.2078 1.9968e-06 -5.3955e-08 v ǁVelocityǁ 0.0014881 51.266 9.5382 8.3462 v Pressure -7.5286e+05 2.9722e+05 -2.6126e+05 -2.2446e+05 v TurbVisc 6.5347e-19 0.033816 0.00024643 0.00012615 v CourantNb 3.6313e-08 0.012055 0.00017558 5.0082e-06 v FourierNb 1.2476e-07 0.059993 0.00016144 9.9392e-07 v total_pressure -6.5154e+05 3.9854e+05 -1.5994e+05 -1.2314e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3499 0.1382 0.0035774 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 9.7825e-07 0.061184 0.00033702 6.0021e-06 INSTANT 0.877043000E-01 TIME STEP NUMBER 57241 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282931397E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.855195331E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.24252E-01 0.23901E+01 Friction velocity uk : 0.24252E-01 0.23901E+01 Dimensionless distance yplus : 0.23409E-01 0.23501E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.082927932e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29956E+08 1 0.22569E-09 0.68139E+02 0.30030E+04 c Velocity[X] 0.38731E+02 c Velocity[Y] 0.29408E+02 c Velocity[Z] 0.84864E-06 c Pressure 0.96933E-04 459 0.82036E-04 0.46831E-03 0.23394E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -37.883 50.881 5.6001 7.9907 v Velocity[Y] -37.925 41.337 -0.24262 -0.29552 v Velocity[Z] -3.2708 3.2079 1.9964e-06 -5.3956e-08 v ǁVelocityǁ 0.0014596 51.274 9.5396 8.3464 v Pressure -7.5457e+05 2.976e+05 -2.6115e+05 -2.2445e+05 v TurbVisc 6.7489e-19 0.033828 0.00024649 0.00012628 v CourantNb 3.7237e-08 0.012056 0.00017559 5.0082e-06 v FourierNb 1.2477e-07 0.060027 0.00016146 9.9479e-07 v total_pressure -6.5325e+05 3.9893e+05 -1.5982e+05 -1.2313e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3501 0.13826 0.003579 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 9.7903e-07 0.061219 0.00033705 6.003e-06 INSTANT 0.877044000E-01 TIME STEP NUMBER 57242 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282924731E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.854801904E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.26114E-01 0.23904E+01 Friction velocity uk : 0.26114E-01 0.23904E+01 Dimensionless distance yplus : 0.25206E-01 0.23504E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.087967794e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29958E+08 1 0.22578E-09 0.68242E+02 0.30051E+04 c Velocity[X] 0.38786E+02 c Velocity[Y] 0.29456E+02 c Velocity[Z] 0.85459E-06 c Pressure 0.83511E-04 11 0.57903E-04 0.40308E-03 0.16005E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -37.893 50.888 5.6 7.9906 v Velocity[Y] -37.932 41.346 -0.24282 -0.29611 v Velocity[Z] -3.2711 3.208 1.996e-06 -5.3956e-08 v ǁVelocityǁ 0.0014399 51.282 9.5409 8.3467 v Pressure -7.5583e+05 2.9798e+05 -2.6105e+05 -2.2447e+05 v TurbVisc 6.9192e-19 0.033841 0.00024655 0.00012641 v CourantNb 3.7629e-08 0.012057 0.0001756 5.0083e-06 v FourierNb 1.2477e-07 0.06006 0.00016149 9.9566e-07 v total_pressure -6.545e+05 3.993e+05 -1.5972e+05 -1.2314e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3504 0.13832 0.0035806 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 9.7981e-07 0.061255 0.00033709 6.0039e-06 INSTANT 0.877045000E-01 TIME STEP NUMBER 57243 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282918060E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.854410369E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.28106E-01 0.23906E+01 Friction velocity uk : 0.28106E-01 0.23906E+01 Dimensionless distance yplus : 0.27129E-01 0.23506E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.084482141e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29959E+08 1 0.22586E-09 0.68330E+02 0.30068E+04 c Velocity[X] 0.38828E+02 c Velocity[Y] 0.29503E+02 c Velocity[Z] 0.84299E-06 c Pressure 0.92268E-04 40 0.78373E-04 0.44493E-03 0.31309E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -37.903 50.896 5.5999 7.9904 v Velocity[Y] -37.94 41.356 -0.24301 -0.2967 v Velocity[Z] -3.2714 3.2081 1.9955e-06 -5.3956e-08 v ǁVelocityǁ 0.0014471 51.29 9.5423 8.3469 v Pressure -7.5563e+05 2.9839e+05 -2.6072e+05 -2.244e+05 v TurbVisc 5.9309e-19 0.033853 0.00024661 0.00012653 v CourantNb 4.5644e-08 0.012058 0.00017561 5.0083e-06 v FourierNb 1.2477e-07 0.060094 0.00016152 9.9653e-07 v total_pressure -6.5431e+05 3.9971e+05 -1.594e+05 -1.2307e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3506 0.13837 0.0035822 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 9.8059e-07 0.06129 0.00033713 6.0049e-06 INSTANT 0.877046000E-01 TIME STEP NUMBER 57244 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282911715E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.854025702E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.27472E-01 0.23909E+01 Friction velocity uk : 0.27472E-01 0.23909E+01 Dimensionless distance yplus : 0.26452E-01 0.23509E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.107925083e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29961E+08 1 0.22599E-09 0.68418E+02 0.30085E+04 c Velocity[X] 0.38871E+02 c Velocity[Y] 0.29547E+02 c Velocity[Z] 0.84161E-06 c Pressure 0.95114E-04 121 0.84284E-04 0.45822E-03 0.34732E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -37.913 50.904 5.5997 7.9903 v Velocity[Y] -37.947 41.366 -0.24321 -0.29728 v Velocity[Z] -3.2716 3.2081 1.9951e-06 -5.3956e-08 v ǁVelocityǁ 0.0014639 51.298 9.5436 8.3471 v Pressure -7.5772e+05 2.9877e+05 -2.6052e+05 -2.2431e+05 v TurbVisc 7.3957e-19 0.033866 0.00024667 0.00012666 v CourantNb 3.9307e-08 0.01206 0.00017563 5.0084e-06 v FourierNb 1.2477e-07 0.060128 0.00016154 9.9741e-07 v total_pressure -6.564e+05 4.0009e+05 -1.5919e+05 -1.2299e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3509 0.13842 0.0035838 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 9.8138e-07 0.061326 0.00033717 6.0058e-06 INSTANT 0.877047000E-01 TIME STEP NUMBER 57245 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282905033E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.853630762E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.25918E-01 0.23911E+01 Friction velocity uk : 0.25918E-01 0.23911E+01 Dimensionless distance yplus : 0.24955E-01 0.23511E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.105384585e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29962E+08 1 0.22606E-09 0.68516E+02 0.30104E+04 c Velocity[X] 0.38915E+02 c Velocity[Y] 0.29601E+02 c Velocity[Z] 0.83985E-06 c Pressure 0.10015E-03 104 0.97808E-04 0.48204E-03 0.39822E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -37.924 50.911 5.5996 7.9901 v Velocity[Y] -37.955 41.376 -0.2434 -0.29788 v Velocity[Z] -3.2719 3.2082 1.9946e-06 -5.3956e-08 v ǁVelocityǁ 0.0014956 51.306 9.545 8.3473 v Pressure -7.5714e+05 2.9918e+05 -2.6024e+05 -2.243e+05 v TurbVisc 7.5418e-19 0.033878 0.00024673 0.00012679 v CourantNb 3.7856e-08 0.012061 0.00017564 5.0085e-06 v FourierNb 1.2477e-07 0.060162 0.00016157 9.9828e-07 v total_pressure -6.5582e+05 4.005e+05 -1.5891e+05 -1.2298e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3511 0.13848 0.0035853 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 9.8216e-07 0.061362 0.0003372 6.0068e-06 INSTANT 0.877048000E-01 TIME STEP NUMBER 57246 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282898821E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.853241823E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.18561E-01 0.23914E+01 Friction velocity uk : 0.18561E-01 0.23914E+01 Dimensionless distance yplus : 0.18078E-01 0.23514E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.113584294e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29963E+08 1 0.22619E-09 0.68565E+02 0.30113E+04 c Velocity[X] 0.38957E+02 c Velocity[Y] 0.29608E+02 c Velocity[Z] 0.83794E-06 c Pressure 0.10537E-03 488 0.83253E-04 0.50667E-03 0.24803E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -37.934 50.919 5.5995 7.99 v Velocity[Y] -37.962 41.386 -0.2436 -0.29847 v Velocity[Z] -3.2722 3.2083 1.9942e-06 -5.3956e-08 v ǁVelocityǁ 0.0015418 51.314 9.5463 8.3476 v Pressure -7.5882e+05 2.9956e+05 -2.599e+05 -2.2415e+05 v TurbVisc 8.4864e-19 0.033891 0.0002468 0.00012692 v CourantNb 3.8523e-08 0.012062 0.00017565 5.0086e-06 v FourierNb 1.2477e-07 0.060196 0.00016159 9.9915e-07 v total_pressure -6.575e+05 4.0089e+05 -1.5858e+05 -1.2283e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3514 0.13853 0.0035868 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 9.8295e-07 0.061397 0.00033724 6.0077e-06 INSTANT 0.877049000E-01 TIME STEP NUMBER 57247 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282892372E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.852854403E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13733E-01 0.23916E+01 Friction velocity uk : 0.13733E-01 0.23916E+01 Dimensionless distance yplus : 0.13376E-01 0.23516E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.116476517e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29965E+08 1 0.22628E-09 0.68668E+02 0.30133E+04 c Velocity[X] 0.39014E+02 c Velocity[Y] 0.29655E+02 c Velocity[Z] 0.84553E-06 c Pressure 0.93656E-04 6 0.58609E-04 0.44991E-03 0.17081E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -37.944 50.927 5.5994 7.9898 v Velocity[Y] -37.969 41.395 -0.24379 -0.29905 v Velocity[Z] -3.2725 3.2084 1.9938e-06 -5.3956e-08 v ǁVelocityǁ 0.001616 51.322 9.5477 8.3478 v Pressure -7.6005e+05 2.9994e+05 -2.5959e+05 -2.2407e+05 v TurbVisc 8.5838e-19 0.033903 0.00024686 0.00012705 v CourantNb 3.8584e-08 0.012063 0.00017566 5.0086e-06 v FourierNb 1.2477e-07 0.06023 0.00016162 1e-06 v total_pressure -6.5872e+05 4.0127e+05 -1.5826e+05 -1.2274e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3516 0.13858 0.0035884 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 9.8373e-07 0.061433 0.00033728 6.0086e-06 INSTANT 0.877050000E-01 TIME STEP NUMBER 57248 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282885951E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.852470219E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15349E-01 0.23919E+01 Friction velocity uk : 0.15349E-01 0.23919E+01 Dimensionless distance yplus : 0.14964E-01 0.23519E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.117583052e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29966E+08 1 0.22636E-09 0.68755E+02 0.30150E+04 c Velocity[X] 0.39048E+02 c Velocity[Y] 0.29707E+02 c Velocity[Z] 0.84210E-06 c Pressure 0.10268E-03 109 0.79332E-04 0.49278E-03 0.33292E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -37.954 50.934 5.5993 7.9897 v Velocity[Y] -37.977 41.405 -0.24399 -0.29965 v Velocity[Z] -3.2728 3.2085 1.9933e-06 -5.3956e-08 v ǁVelocityǁ 0.0016731 51.33 9.549 8.348 v Pressure -7.5988e+05 3.0036e+05 -2.5907e+05 -2.2389e+05 v TurbVisc 8.1402e-19 0.033916 0.00024692 0.00012717 v CourantNb 3.6761e-08 0.012064 0.00017567 5.0087e-06 v FourierNb 1.2478e-07 0.060263 0.00016164 1.0009e-06 v total_pressure -6.5855e+05 4.0169e+05 -1.5775e+05 -1.2257e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3519 0.13863 0.0035899 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 9.8452e-07 0.061468 0.00033732 6.0096e-06 INSTANT 0.877051000E-01 TIME STEP NUMBER 57249 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282879842E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.852094420E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.39465E-02 0.23921E+01 Friction velocity uk : 0.39465E-02 0.23921E+01 Dimensionless distance yplus : 0.38474E-02 0.23521E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.130245308e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29968E+08 1 0.22648E-09 0.68842E+02 0.30167E+04 c Velocity[X] 0.39094E+02 c Velocity[Y] 0.29748E+02 c Velocity[Z] 0.82992E-06 c Pressure 0.10620E-03 56 0.85086E-04 0.50920E-03 0.36658E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -37.964 50.942 5.5992 7.9895 v Velocity[Y] -37.984 41.415 -0.24418 -0.30024 v Velocity[Z] -3.273 3.2086 1.9929e-06 -5.3956e-08 v ǁVelocityǁ 0.0017559 51.338 9.5503 8.3482 v Pressure -7.6193e+05 3.0074e+05 -2.5865e+05 -2.2367e+05 v TurbVisc 9.2845e-19 0.033928 0.00024698 0.0001273 v CourantNb 4.0157e-08 0.012065 0.00017569 5.0088e-06 v FourierNb 1.2478e-07 0.060297 0.00016167 1.0018e-06 v total_pressure -6.6061e+05 4.0207e+05 -1.5733e+05 -1.2234e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3521 0.13868 0.0035913 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 9.8531e-07 0.061504 0.00033735 6.0105e-06 INSTANT 0.877052000E-01 TIME STEP NUMBER 57250 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282873427E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.851709474E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.74462E-02 0.23924E+01 Friction velocity uk : 0.74462E-02 0.23924E+01 Dimensionless distance yplus : 0.72593E-02 0.23524E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.131411235e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29969E+08 1 0.22656E-09 0.68939E+02 0.30186E+04 c Velocity[X] 0.39137E+02 c Velocity[Y] 0.29802E+02 c Velocity[Z] 0.83467E-06 c Pressure 0.11155E-03 118 0.98665E-04 0.53437E-03 0.40736E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -37.974 50.949 5.5991 7.9894 v Velocity[Y] -37.991 41.424 -0.24438 -0.30083 v Velocity[Z] -3.2733 3.2086 1.9924e-06 -5.3956e-08 v ǁVelocityǁ 0.001847 51.346 9.5517 8.3485 v Pressure -7.6132e+05 3.0116e+05 -2.5815e+05 -2.2355e+05 v TurbVisc 8.9935e-19 0.033941 0.00024704 0.00012743 v CourantNb 4.4922e-08 0.012066 0.0001757 5.0088e-06 v FourierNb 1.2478e-07 0.060331 0.00016169 1.0027e-06 v total_pressure -6.5999e+05 4.0248e+05 -1.5683e+05 -1.2222e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3524 0.13873 0.0035928 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 9.8611e-07 0.061539 0.00033739 6.0115e-06 INSTANT 0.877053000E-01 TIME STEP NUMBER 57251 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282867520E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.851332105E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13337E-01 0.23926E+01 Friction velocity uk : 0.13337E-01 0.23926E+01 Dimensionless distance yplus : 0.12958E-01 0.23527E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.135930192e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29971E+08 1 0.22669E-09 0.68986E+02 0.30194E+04 c Velocity[X] 0.39182E+02 c Velocity[Y] 0.29804E+02 c Velocity[Z] 0.82561E-06 c Pressure 0.11709E-03 123 0.84062E-04 0.56034E-03 0.28501E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -37.984 50.957 5.599 7.9892 v Velocity[Y] -37.999 41.434 -0.24457 -0.30143 v Velocity[Z] -3.2736 3.2087 1.992e-06 -5.3956e-08 v ǁVelocityǁ 0.0019473 51.354 9.553 8.3487 v Pressure -7.6293e+05 3.0155e+05 -2.576e+05 -2.232e+05 v TurbVisc 8.3602e-19 0.033953 0.0002471 0.00012756 v CourantNb 4.8711e-08 0.012067 0.00017571 5.0089e-06 v FourierNb 1.2478e-07 0.060365 0.00016172 1.0035e-06 v total_pressure -6.6161e+05 4.0288e+05 -1.5628e+05 -1.2188e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3527 0.13879 0.0035943 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 9.869e-07 0.061575 0.00033743 6.0124e-06 INSTANT 0.877054000E-01 TIME STEP NUMBER 57252 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282861405E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.850956736E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.83400E-02 0.23929E+01 Friction velocity uk : 0.83400E-02 0.23929E+01 Dimensionless distance yplus : 0.81029E-02 0.23529E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.137720353e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29972E+08 1 0.22678E-09 0.69089E+02 0.30214E+04 c Velocity[X] 0.39227E+02 c Velocity[Y] 0.29862E+02 c Velocity[Z] 0.83365E-06 c Pressure 0.10709E-03 7 0.59324E-04 0.51200E-03 0.17234E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -37.994 50.965 5.5988 7.9891 v Velocity[Y] -38.006 41.444 -0.24477 -0.30202 v Velocity[Z] -3.2739 3.2088 1.9915e-06 -5.3957e-08 v ǁVelocityǁ 0.0018955 51.362 9.5543 8.3489 v Pressure -7.6428e+05 3.0194e+05 -2.5713e+05 -2.2313e+05 v TurbVisc 8.3073e-19 0.033966 0.00024716 0.00012769 v CourantNb 4.7649e-08 0.012068 0.00017572 5.009e-06 v FourierNb 1.2479e-07 0.060399 0.00016175 1.0044e-06 v total_pressure -6.6296e+05 4.0326e+05 -1.5581e+05 -1.2181e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3529 0.13884 0.0035958 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 9.8769e-07 0.06161 0.00033747 6.0134e-06 INSTANT 0.877055000E-01 TIME STEP NUMBER 57253 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282855285E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.850585092E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.31280E-02 0.23932E+01 Friction velocity uk : 0.31280E-02 0.23932E+01 Dimensionless distance yplus : 0.30391E-02 0.23532E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.133173944e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29974E+08 1 0.22686E-09 0.69176E+02 0.30231E+04 c Velocity[X] 0.39265E+02 c Velocity[Y] 0.29910E+02 c Velocity[Z] 0.82434E-06 c Pressure 0.11582E-03 189 0.80313E-04 0.55322E-03 0.35514E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -38.004 50.972 5.5987 7.9889 v Velocity[Y] -38.013 41.453 -0.24496 -0.30262 v Velocity[Z] -3.2741 3.2089 1.9911e-06 -5.3957e-08 v ǁVelocityǁ 0.0018126 51.369 9.5557 8.3492 v Pressure -7.6402e+05 3.0236e+05 -2.5638e+05 -2.2281e+05 v TurbVisc 7.6637e-19 0.033978 0.00024723 0.00012782 v CourantNb 4.69e-08 0.012069 0.00017573 5.0091e-06 v FourierNb 1.2479e-07 0.060432 0.00016177 1.0053e-06 v total_pressure -6.627e+05 4.0368e+05 -1.5505e+05 -1.2148e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3532 0.1389 0.0035974 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 9.8849e-07 0.061646 0.00033751 6.0143e-06 INSTANT 0.877056000E-01 TIME STEP NUMBER 57254 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282849509E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.850225330E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.51333E-02 0.23934E+01 Friction velocity uk : 0.51333E-02 0.23934E+01 Dimensionless distance yplus : 0.49873E-02 0.23534E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.145382854e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29975E+08 1 0.22699E-09 0.69262E+02 0.30248E+04 c Velocity[X] 0.39317E+02 c Velocity[Y] 0.29945E+02 c Velocity[Z] 0.82685E-06 c Pressure 0.11971E-03 378 0.86489E-04 0.57127E-03 0.41714E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -38.014 50.98 5.5986 7.9888 v Velocity[Y] -38.021 41.463 -0.24516 -0.30321 v Velocity[Z] -3.2744 3.209 1.9907e-06 -5.3957e-08 v ǁVelocityǁ 0.0016856 51.377 9.557 8.3494 v Pressure -7.6598e+05 3.0275e+05 -2.5574e+05 -2.2234e+05 v TurbVisc 7.8406e-19 0.033991 0.00024729 0.00012795 v CourantNb 4.5505e-08 0.01207 0.00017575 5.0091e-06 v FourierNb 1.2479e-07 0.060466 0.0001618 1.0062e-06 v total_pressure -6.6466e+05 4.0407e+05 -1.5441e+05 -1.2101e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3534 0.13895 0.0035988 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 9.8928e-07 0.061681 0.00033755 6.0153e-06 INSTANT 0.877057000E-01 TIME STEP NUMBER 57255 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282843505E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.849854664E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13817E-01 0.23937E+01 Friction velocity uk : 0.13817E-01 0.23937E+01 Dimensionless distance yplus : 0.13424E-01 0.23537E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.144369615e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29977E+08 1 0.22708E-09 0.69320E+02 0.30258E+04 c Velocity[X] 0.39343E+02 c Velocity[Y] 0.29977E+02 c Velocity[Z] 0.82433E-06 c Pressure 0.12525E-03 60 0.75313E-04 0.59710E-03 0.24174E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -38.024 50.987 5.5985 7.9887 v Velocity[Y] -38.028 41.473 -0.24535 -0.30381 v Velocity[Z] -3.2747 3.2091 1.9902e-06 -5.3957e-08 v ǁVelocityǁ 0.0015617 51.385 9.5583 8.3497 v Pressure -7.6623e+05 3.0315e+05 -2.5511e+05 -2.2229e+05 v TurbVisc 7.75e-19 0.034003 0.00024735 0.00012807 v CourantNb 4.4492e-08 0.012071 0.00017576 5.0092e-06 v FourierNb 1.2479e-07 0.0605 0.00016182 1.007e-06 v total_pressure -6.649e+05 4.0448e+05 -1.5378e+05 -1.2096e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3537 0.139 0.0036003 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 9.9008e-07 0.061716 0.00033758 6.0162e-06 INSTANT 0.877058000E-01 TIME STEP NUMBER 57256 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282837743E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.849492088E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.18154E-01 0.23940E+01 Friction velocity uk : 0.18154E-01 0.23940E+01 Dimensionless distance yplus : 0.17665E-01 0.23540E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.139729620e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29978E+08 1 0.22718E-09 0.69421E+02 0.30278E+04 c Velocity[X] 0.39391E+02 c Velocity[Y] 0.30030E+02 c Velocity[Z] 0.82828E-06 c Pressure 0.11868E-03 7 0.53244E-04 0.56525E-03 0.17621E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -38.034 50.995 5.5984 7.9885 v Velocity[Y] -38.035 41.482 -0.24555 -0.30441 v Velocity[Z] -3.275 3.2092 1.9898e-06 -5.3957e-08 v ǁVelocityǁ 0.0014115 51.393 9.5597 8.3499 v Pressure -7.6637e+05 3.0356e+05 -2.5443e+05 -2.2207e+05 v TurbVisc 7.6671e-19 0.034016 0.00024741 0.0001282 v CourantNb 4.3472e-08 0.012072 0.00017577 5.0093e-06 v FourierNb 1.248e-07 0.060533 0.00016185 1.0079e-06 v total_pressure -6.6504e+05 4.0489e+05 -1.531e+05 -1.2074e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.354 0.13905 0.0036018 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 9.9089e-07 0.061752 0.00033762 6.0172e-06 INSTANT 0.877059000E-01 TIME STEP NUMBER 57257 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282832228E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.849136977E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10747E-01 0.23943E+01 Friction velocity uk : 0.10747E-01 0.23943E+01 Dimensionless distance yplus : 0.10457E-01 0.23543E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.134591146e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29980E+08 1 0.22729E-09 0.69487E+02 0.30290E+04 c Velocity[X] 0.39439E+02 c Velocity[Y] 0.30048E+02 c Velocity[Z] 0.82030E-06 c Pressure 0.12593E-03 78 0.96917E-04 0.59919E-03 0.31486E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -38.044 51.002 5.5983 7.9884 v Velocity[Y] -38.042 41.492 -0.24574 -0.30501 v Velocity[Z] -3.2753 3.2092 1.9893e-06 -5.3957e-08 v ǁVelocityǁ 0.001332 51.401 9.561 8.3501 v Pressure -7.6753e+05 3.0398e+05 -2.5353e+05 -2.2137e+05 v TurbVisc 7.8623e-19 0.034028 0.00024747 0.00012833 v CourantNb 4.2702e-08 0.012073 0.00017578 5.0094e-06 v FourierNb 1.248e-07 0.060567 0.00016188 1.0088e-06 v total_pressure -6.6621e+05 4.053e+05 -1.522e+05 -1.2005e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3543 0.13911 0.0036034 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 9.9169e-07 0.061787 0.00033766 6.0182e-06 INSTANT 0.877060000E-01 TIME STEP NUMBER 57258 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282826692E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.848791749E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.50783E-02 0.23945E+01 Friction velocity uk : 0.50783E-02 0.23945E+01 Dimensionless distance yplus : 0.49415E-02 0.23545E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.144602922e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29982E+08 1 0.22740E-09 0.69570E+02 0.30306E+04 c Velocity[X] 0.39479E+02 c Velocity[Y] 0.30091E+02 c Velocity[Z] 0.81730E-06 c Pressure 0.12747E-03 350 0.81209E-04 0.60597E-03 0.17647E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -38.054 51.01 5.5982 7.9883 v Velocity[Y] -38.05 41.502 -0.24594 -0.30561 v Velocity[Z] -3.2755 3.2093 1.9889e-06 -5.3957e-08 v ǁVelocityǁ 0.0012357 51.409 9.5623 8.3504 v Pressure -7.687e+05 3.0438e+05 -2.5276e+05 -2.2107e+05 v TurbVisc 8.1525e-19 0.034041 0.00024753 0.00012846 v CourantNb 4.1385e-08 0.012074 0.0001758 5.0094e-06 v FourierNb 1.248e-07 0.0606 0.0001619 1.0097e-06 v total_pressure -6.6738e+05 4.057e+05 -1.5144e+05 -1.1975e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3545 0.13915 0.0036047 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 9.9249e-07 0.061822 0.0003377 6.0191e-06 INSTANT 0.877061000E-01 TIME STEP NUMBER 57259 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282821142E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.848439988E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.32515E-02 0.23948E+01 Friction velocity uk : 0.32515E-02 0.23948E+01 Dimensionless distance yplus : 0.31640E-02 0.23548E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.119305120e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29983E+08 1 0.22750E-09 0.69671E+02 0.30325E+04 c Velocity[X] 0.39531E+02 c Velocity[Y] 0.30140E+02 c Velocity[Z] 0.84733E-06 c Pressure 0.12761E-03 13 0.52749E-04 0.60602E-03 0.19477E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -38.064 51.017 5.5981 7.9881 v Velocity[Y] -38.057 41.511 -0.24614 -0.3062 v Velocity[Z] -3.2758 3.2094 1.9885e-06 -5.3957e-08 v ǁVelocityǁ 0.0011295 51.417 9.5636 8.3506 v Pressure -7.6988e+05 3.0476e+05 -2.5198e+05 -2.2079e+05 v TurbVisc 7.723e-19 0.034053 0.00024759 0.00012859 v CourantNb 4.0404e-08 0.012075 0.00017581 5.0095e-06 v FourierNb 1.248e-07 0.060633 0.00016193 1.0105e-06 v total_pressure -6.6855e+05 4.0609e+05 -1.5065e+05 -1.1946e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3548 0.13921 0.0036062 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 9.9329e-07 0.061857 0.00033774 6.0201e-06 INSTANT 0.877062000E-01 TIME STEP NUMBER 57260 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282815660E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.848095229E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.33579E-02 0.23951E+01 Friction velocity uk : 0.33579E-02 0.23951E+01 Dimensionless distance yplus : 0.32717E-02 0.23551E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.130612813e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29985E+08 1 0.22759E-09 0.69740E+02 0.30338E+04 c Velocity[X] 0.39568E+02 c Velocity[Y] 0.30171E+02 c Velocity[Z] 0.82706E-06 c Pressure 0.13505E-03 280 0.98354E-04 0.64078E-03 0.27948E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -38.074 51.025 5.598 7.988 v Velocity[Y] -38.064 41.521 -0.24633 -0.3068 v Velocity[Z] -3.2761 3.2095 1.988e-06 -5.3957e-08 v ǁVelocityǁ 0.00077946 51.425 9.565 8.3509 v Pressure -7.7038e+05 3.0518e+05 -2.5101e+05 -2.202e+05 v TurbVisc 7.7165e-19 0.034066 0.00024765 0.00012872 v CourantNb 3.9706e-08 0.012076 0.00017582 5.0096e-06 v FourierNb 1.2481e-07 0.060666 0.00016196 1.0114e-06 v total_pressure -6.6906e+05 4.0651e+05 -1.4969e+05 -1.1888e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3551 0.13927 0.0036078 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 9.941e-07 0.061891 0.00033778 6.021e-06 INSTANT 0.877063000E-01 TIME STEP NUMBER 57261 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282810372E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.847756445E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.48075E-02 0.23953E+01 Friction velocity uk : 0.48075E-02 0.23953E+01 Dimensionless distance yplus : 0.46751E-02 0.23553E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.120286226e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29986E+08 1 0.22770E-09 0.69819E+02 0.30353E+04 c Velocity[X] 0.39603E+02 c Velocity[Y] 0.30216E+02 c Velocity[Z] 0.81432E-06 c Pressure 0.13645E-03 32 0.83197E-04 0.64681E-03 0.15357E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -38.084 51.032 5.5978 7.9879 v Velocity[Y] -38.071 41.53 -0.24652 -0.3074 v Velocity[Z] -3.2764 3.2096 1.9876e-06 -5.3957e-08 v ǁVelocityǁ 0.0005276 51.432 9.5663 8.3512 v Pressure -7.7096e+05 3.0559e+05 -2.5018e+05 -2.1997e+05 v TurbVisc 7.9506e-19 0.034078 0.00024771 0.00012885 v CourantNb 3.8479e-08 0.012078 0.00017583 5.0097e-06 v FourierNb 1.2481e-07 0.060698 0.00016198 1.0123e-06 v total_pressure -6.6963e+05 4.0691e+05 -1.4885e+05 -1.1865e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3553 0.13932 0.0036093 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 9.9491e-07 0.061926 0.00033782 6.022e-06 INSTANT 0.877064000E-01 TIME STEP NUMBER 57262 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282805178E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.847422863E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.86151E-02 0.23956E+01 Friction velocity uk : 0.86151E-02 0.23956E+01 Dimensionless distance yplus : 0.83778E-02 0.23556E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.106539253e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29988E+08 1 0.22781E-09 0.69922E+02 0.30373E+04 c Velocity[X] 0.39635E+02 c Velocity[Y] 0.30287E+02 c Velocity[Z] 0.81863E-06 c Pressure 0.13649E-03 64 0.53999E-04 0.64636E-03 0.21917E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -38.094 51.04 5.5977 7.9878 v Velocity[Y] -38.079 41.54 -0.24672 -0.30801 v Velocity[Z] -3.2766 3.2096 1.9871e-06 -5.3957e-08 v ǁVelocityǁ 0.00053746 51.44 9.5676 8.3514 v Pressure -7.713e+05 3.06e+05 -2.4925e+05 -2.1965e+05 v TurbVisc 7.98e-19 0.034091 0.00024777 0.00012898 v CourantNb 3.7476e-08 0.012079 0.00017584 5.0098e-06 v FourierNb 1.2481e-07 0.060731 0.00016201 1.0132e-06 v total_pressure -6.6998e+05 4.0732e+05 -1.4793e+05 -1.1833e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3556 0.13938 0.0036109 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 9.9572e-07 0.06196 0.00033786 6.023e-06 INSTANT 0.877065000E-01 TIME STEP NUMBER 57263 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282800183E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.847096091E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15774E-01 0.23959E+01 Friction velocity uk : 0.15774E-01 0.23959E+01 Dimensionless distance yplus : 0.15339E-01 0.23558E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.097310068e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29990E+08 1 0.22791E-09 0.69997E+02 0.30387E+04 c Velocity[X] 0.39696E+02 c Velocity[Y] 0.30301E+02 c Velocity[Z] 0.81033E-06 c Pressure 0.14376E-03 40 0.76744E-04 0.68013E-03 0.50213E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -38.103 51.047 5.5976 7.9876 v Velocity[Y] -38.086 41.55 -0.24692 -0.30861 v Velocity[Z] -3.2769 3.2097 1.9867e-06 -5.3957e-08 v ǁVelocityǁ 0.00085866 51.448 9.5689 8.3517 v Pressure -7.7312e+05 3.064e+05 -2.4817e+05 -2.1875e+05 v TurbVisc 4.6797e-19 0.034103 0.00024783 0.00012911 v CourantNb 3.6495e-08 0.012079 0.00017586 5.0098e-06 v FourierNb 1.2482e-07 0.060762 0.00016204 1.0141e-06 v total_pressure -6.7179e+05 4.0773e+05 -1.4684e+05 -1.1743e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3558 0.13944 0.0036124 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 9.9653e-07 0.061993 0.0003379 6.0239e-06 INSTANT 0.877066000E-01 TIME STEP NUMBER 57264 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282795028E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.846776558E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13630E-01 0.23962E+01 Friction velocity uk : 0.13630E-01 0.23962E+01 Dimensionless distance yplus : 0.13311E-01 0.23562E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.092871407e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29991E+08 1 0.22802E-09 0.70096E+02 0.30406E+04 c Velocity[X] 0.39731E+02 c Velocity[Y] 0.30365E+02 c Velocity[Z] 0.80305E-06 c Pressure 0.14733E-03 82 0.80832E-04 0.69633E-03 0.37005E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -38.113 51.055 5.5975 7.9875 v Velocity[Y] -38.093 41.559 -0.24711 -0.30921 v Velocity[Z] -3.2772 3.2098 1.9863e-06 -5.3958e-08 v ǁVelocityǁ 0.00099373 51.456 9.5703 8.3519 v Pressure -7.7275e+05 3.0682e+05 -2.4721e+05 -2.1845e+05 v TurbVisc 8.741e-19 0.034115 0.00024789 0.00012924 v CourantNb 3.5938e-08 0.012081 0.00017587 5.0099e-06 v FourierNb 1.2482e-07 0.060794 0.00016207 1.015e-06 v total_pressure -6.7142e+05 4.0815e+05 -1.4588e+05 -1.1713e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3562 0.1395 0.003614 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 9.9734e-07 0.062027 0.00033794 6.0249e-06 INSTANT 0.877067000E-01 TIME STEP NUMBER 57265 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282790357E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.846454966E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.51805E-02 0.23965E+01 Friction velocity uk : 0.51805E-02 0.23965E+01 Dimensionless distance yplus : 0.50592E-02 0.23565E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.075439570e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29993E+08 1 0.22814E-09 0.70181E+02 0.30422E+04 c Velocity[X] 0.39782E+02 c Velocity[Y] 0.30398E+02 c Velocity[Z] 0.80423E-06 c Pressure 0.15204E-03 101 0.94931E-04 0.71794E-03 0.47810E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -38.123 51.062 5.5974 7.9874 v Velocity[Y] -38.101 41.569 -0.24731 -0.30981 v Velocity[Z] -3.2775 3.2099 1.9858e-06 -5.3958e-08 v ǁVelocityǁ 0.0010258 51.464 9.5716 8.3522 v Pressure -7.7482e+05 3.0723e+05 -2.4615e+05 -2.1786e+05 v TurbVisc 8.9014e-19 0.034128 0.00024795 0.00012937 v CourantNb 3.5148e-08 0.012082 0.00017588 5.01e-06 v FourierNb 1.2482e-07 0.060826 0.00016209 1.0158e-06 v total_pressure -6.735e+05 4.0855e+05 -1.4483e+05 -1.1653e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3565 0.13956 0.0036155 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 9.9815e-07 0.06206 0.00033797 6.0259e-06 INSTANT 0.877068000E-01 TIME STEP NUMBER 57266 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282785421E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.846141714E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.31631E-02 0.23968E+01 Friction velocity uk : 0.31631E-02 0.23968E+01 Dimensionless distance yplus : 0.30890E-02 0.23568E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.062888895e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29995E+08 1 0.22823E-09 0.70237E+02 0.30432E+04 c Velocity[X] 0.39811E+02 c Velocity[Y] 0.30426E+02 c Velocity[Z] 0.80223E-06 c Pressure 0.15681E-03 273 0.80383E-04 0.73975E-03 0.29892E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -38.133 51.07 5.5973 7.9873 v Velocity[Y] -38.108 41.578 -0.2475 -0.31042 v Velocity[Z] -3.2777 3.21 1.9854e-06 -5.3958e-08 v ǁVelocityǁ 0.0010755 51.472 9.5729 8.3525 v Pressure -7.7495e+05 3.0764e+05 -2.4511e+05 -2.175e+05 v TurbVisc 9.4136e-19 0.03414 0.00024801 0.0001295 v CourantNb 3.4648e-08 0.012083 0.00017589 5.0101e-06 v FourierNb 1.2483e-07 0.060857 0.00016212 1.0167e-06 v total_pressure -6.7362e+05 4.0897e+05 -1.4378e+05 -1.1617e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3568 0.13961 0.003617 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 9.9897e-07 0.062093 0.00033801 6.0268e-06 INSTANT 0.877069000E-01 TIME STEP NUMBER 57267 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282780780E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.845835960E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.91856E-02 0.23972E+01 Friction velocity uk : 0.91856E-02 0.23972E+01 Dimensionless distance yplus : 0.89705E-02 0.23571E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.047080677e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29997E+08 1 0.22834E-09 0.70341E+02 0.30452E+04 c Velocity[X] 0.39856E+02 c Velocity[Y] 0.30485E+02 c Velocity[Z] 0.81921E-06 c Pressure 0.15071E-03 9 0.55244E-04 0.71027E-03 0.21757E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -38.143 51.078 5.5972 7.9872 v Velocity[Y] -38.115 41.588 -0.2477 -0.31103 v Velocity[Z] -3.278 3.2101 1.9849e-06 -5.3958e-08 v ǁVelocityǁ 0.0011451 51.48 9.5742 8.3527 v Pressure -7.7507e+05 3.0806e+05 -2.4404e+05 -2.1713e+05 v TurbVisc 9.6933e-19 0.034153 0.00024807 0.00012963 v CourantNb 3.4536e-08 0.012084 0.00017591 5.0102e-06 v FourierNb 1.2483e-07 0.060888 0.00016215 1.0176e-06 v total_pressure -6.7374e+05 4.0938e+05 -1.4272e+05 -1.158e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3571 0.13967 0.0036186 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 9.9979e-07 0.062126 0.00033805 6.0278e-06 INSTANT 0.877070000E-01 TIME STEP NUMBER 57268 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282776420E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.845537029E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13031E-01 0.23975E+01 Friction velocity uk : 0.13031E-01 0.23975E+01 Dimensionless distance yplus : 0.12725E-01 0.23575E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.022538192e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.29998E+08 1 0.22845E-09 0.70416E+02 0.30466E+04 c Velocity[X] 0.39904E+02 c Velocity[Y] 0.30511E+02 c Velocity[Z] 0.81027E-06 c Pressure 0.15730E-03 48 0.76633E-04 0.74063E-03 0.52115E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -38.153 51.085 5.5971 7.9871 v Velocity[Y] -38.122 41.598 -0.2479 -0.31163 v Velocity[Z] -3.2783 3.2101 1.9845e-06 -5.3958e-08 v ǁVelocityǁ 0.0012166 51.488 9.5755 8.353 v Pressure -7.7708e+05 3.0848e+05 -2.4283e+05 -2.1618e+05 v TurbVisc 1.0479e-18 0.034165 0.00024813 0.00012976 v CourantNb 3.4488e-08 0.012085 0.00017592 5.0103e-06 v FourierNb 1.2483e-07 0.060918 0.00016218 1.0185e-06 v total_pressure -6.7575e+05 4.098e+05 -1.415e+05 -1.1486e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3575 0.13973 0.0036201 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0006e-06 0.062158 0.00033809 6.0288e-06 INSTANT 0.877071000E-01 TIME STEP NUMBER 57269 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282771840E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.845246274E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.37262E-02 0.23978E+01 Friction velocity uk : 0.37262E-02 0.23978E+01 Dimensionless distance yplus : 0.36174E-02 0.23577E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.017943164e-01 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.30000E+08 1 0.22855E-09 0.70517E+02 0.30485E+04 c Velocity[X] 0.39942E+02 c Velocity[Y] 0.30575E+02 c Velocity[Z] 0.81709E-06 c Pressure 0.16059E-03 72 0.81865E-04 0.75537E-03 0.39861E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -38.163 51.093 5.597 7.987 v Velocity[Y] -38.13 41.607 -0.24809 -0.31224 v Velocity[Z] -3.2786 3.2102 1.9841e-06 -5.3958e-08 v ǁVelocityǁ 0.001302 51.496 9.5769 8.3533 v Pressure -7.7665e+05 3.089e+05 -2.4169e+05 -2.1575e+05 v TurbVisc 9.8441e-19 0.034178 0.00024819 0.00012989 v CourantNb 3.4436e-08 0.012086 0.00017593 5.0104e-06 v FourierNb 1.2484e-07 0.060948 0.0001622 1.0194e-06 v total_pressure -6.7532e+05 4.1022e+05 -1.4036e+05 -1.1442e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3577 0.13979 0.0036216 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0014e-06 0.062189 0.00033814 6.0297e-06 INSTANT 0.877072000E-01 TIME STEP NUMBER 57270 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282767763E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.844957831E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.62916E-02 0.23981E+01 Friction velocity uk : 0.62916E-02 0.23981E+01 Dimensionless distance yplus : 0.61078E-02 0.23581E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -9.912133223e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.30002E+08 1 0.22867E-09 0.70602E+02 0.30501E+04 c Velocity[X] 0.39994E+02 c Velocity[Y] 0.30609E+02 c Velocity[Z] 0.80179E-06 c Pressure 0.16499E-03 107 0.95666E-04 0.77531E-03 0.51359E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -38.172 51.1 5.597 7.9868 v Velocity[Y] -38.137 41.617 -0.24829 -0.31284 v Velocity[Z] -3.2788 3.2103 1.9836e-06 -5.3958e-08 v ǁVelocityǁ 0.0011865 51.504 9.5782 8.3536 v Pressure -7.7876e+05 3.093e+05 -2.4048e+05 -2.1504e+05 v TurbVisc 9.8712e-19 0.03419 0.00024825 0.00013002 v CourantNb 3.4411e-08 0.012087 0.00017594 5.0105e-06 v FourierNb 1.2484e-07 0.060977 0.00016223 1.0203e-06 v total_pressure -6.7743e+05 4.1063e+05 -1.3915e+05 -1.1372e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3581 0.13985 0.0036231 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0022e-06 0.062221 0.00033818 6.0307e-06 INSTANT 0.877073000E-01 TIME STEP NUMBER 57271 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282763426E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.844674958E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.71743E-02 0.23985E+01 Friction velocity uk : 0.71743E-02 0.23985E+01 Dimensionless distance yplus : 0.69648E-02 0.23584E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -9.735491982e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.30004E+08 1 0.22876E-09 0.70658E+02 0.30511E+04 c Velocity[X] 0.40023E+02 c Velocity[Y] 0.30635E+02 c Velocity[Z] 0.80768E-06 c Pressure 0.16941E-03 177 0.81332E-04 0.79535E-03 0.31730E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -38.182 51.108 5.5969 7.9867 v Velocity[Y] -38.144 41.627 -0.24849 -0.31345 v Velocity[Z] -3.2791 3.2104 1.9832e-06 -5.3958e-08 v ǁVelocityǁ 0.0010828 51.512 9.5795 8.3538 v Pressure -7.7884e+05 3.0972e+05 -2.393e+05 -2.1463e+05 v TurbVisc 1.0092e-18 0.034202 0.00024831 0.00013015 v CourantNb 3.4376e-08 0.012088 0.00017596 5.0106e-06 v FourierNb 1.2485e-07 0.061006 0.00016226 1.0211e-06 v total_pressure -6.7752e+05 4.1104e+05 -1.3797e+05 -1.1331e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3584 0.13991 0.0036246 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0029e-06 0.062252 0.00033822 6.0317e-06 INSTANT 0.877074000E-01 TIME STEP NUMBER 57272 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282759407E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.844400638E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.54957E-02 0.23988E+01 Friction velocity uk : 0.54957E-02 0.23988E+01 Dimensionless distance yplus : 0.53804E-02 0.23587E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -9.513660831e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.30005E+08 1 0.22888E-09 0.70765E+02 0.30531E+04 c Velocity[X] 0.40069E+02 c Velocity[Y] 0.30696E+02 c Velocity[Z] 0.82692E-06 c Pressure 0.16342E-03 9 0.56253E-04 0.76647E-03 0.24476E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -38.192 51.116 5.5968 7.9866 v Velocity[Y] -38.152 41.636 -0.24869 -0.31406 v Velocity[Z] -3.2794 3.2105 1.9827e-06 -5.3958e-08 v ǁVelocityǁ 0.0010139 51.519 9.5808 8.3541 v Pressure -7.7894e+05 3.1014e+05 -2.3809e+05 -2.1417e+05 v TurbVisc 1.0303e-18 0.034215 0.00024837 0.00013028 v CourantNb 3.4322e-08 0.012089 0.00017597 5.0106e-06 v FourierNb 1.2485e-07 0.061035 0.00016229 1.022e-06 v total_pressure -6.7761e+05 4.1147e+05 -1.3676e+05 -1.1285e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3587 0.13997 0.0036262 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0037e-06 0.062282 0.00033826 6.0327e-06 INSTANT 0.877075000E-01 TIME STEP NUMBER 57273 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282755681E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.844135423E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.56136E-02 0.23993E+01 Friction velocity uk : 0.56136E-02 0.23993E+01 Dimensionless distance yplus : 0.54959E-02 0.23591E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -9.185565601e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.30007E+08 1 0.22899E-09 0.70840E+02 0.30545E+04 c Velocity[X] 0.40116E+02 c Velocity[Y] 0.30723E+02 c Velocity[Z] 0.80194E-06 c Pressure 0.16953E-03 63 0.77695E-04 0.79437E-03 0.56775E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -38.202 51.123 5.5967 7.9865 v Velocity[Y] -38.159 41.646 -0.24888 -0.31467 v Velocity[Z] -3.2796 3.2106 1.9823e-06 -5.3958e-08 v ǁVelocityǁ 0.00098987 51.527 9.5822 8.3544 v Pressure -7.8097e+05 3.1056e+05 -2.3673e+05 -2.131e+05 v TurbVisc 1.1368e-18 0.034227 0.00024843 0.00013041 v CourantNb 3.4275e-08 0.01209 0.00017598 5.0107e-06 v FourierNb 1.2486e-07 0.061063 0.00016232 1.0229e-06 v total_pressure -6.7964e+05 4.1189e+05 -1.354e+05 -1.1178e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3591 0.14002 0.0036277 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0044e-06 0.062312 0.0003383 6.0337e-06 INSTANT 0.877076000E-01 TIME STEP NUMBER 57274 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282751740E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.843878833E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.60449E-02 0.23996E+01 Friction velocity uk : 0.60449E-02 0.23996E+01 Dimensionless distance yplus : 0.59181E-02 0.23595E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -9.098408773e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.30009E+08 1 0.22908E-09 0.70943E+02 0.30565E+04 c Velocity[X] 0.40154E+02 c Velocity[Y] 0.30789E+02 c Velocity[Z] 0.80683E-06 c Pressure 0.17248E-03 333 0.82976E-04 0.80740E-03 0.42218E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -38.212 51.131 5.5966 7.9865 v Velocity[Y] -38.166 41.655 -0.24908 -0.31528 v Velocity[Z] -3.2799 3.2106 1.9819e-06 -5.3958e-08 v ǁVelocityǁ 0.00099505 51.535 9.5835 8.3547 v Pressure -7.8052e+05 3.1099e+05 -2.3544e+05 -2.1259e+05 v TurbVisc 1.088e-18 0.03424 0.00024849 0.00013054 v CourantNb 3.4191e-08 0.012091 0.00017599 5.0108e-06 v FourierNb 1.2486e-07 0.06109 0.00016234 1.0238e-06 v total_pressure -6.7919e+05 4.1232e+05 -1.3412e+05 -1.1126e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3595 0.14008 0.0036292 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0051e-06 0.062341 0.00033834 6.0346e-06 INSTANT 0.877077000E-01 TIME STEP NUMBER 57275 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282748320E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.843625212E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10291E-01 0.23999E+01 Friction velocity uk : 0.10291E-01 0.23999E+01 Dimensionless distance yplus : 0.10075E-01 0.23598E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Incoming flow detained for 20 outlet faces on 2100 Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -8.782514523e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.30011E+08 1 0.22927E-09 0.71497E+02 0.30681E+04 c Velocity[X] 0.39980E+02 c Velocity[Y] 0.31517E+02 c Velocity[Z] 0.79902E-06 c Pressure 0.27337E-02 482 0.80471E-04 0.13242E-01 0.71838E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -38.222 51.139 5.5965 7.9864 v Velocity[Y] -38.174 41.665 -0.24928 -0.31589 v Velocity[Z] -3.2802 3.2107 1.9814e-06 -5.3959e-08 v ǁVelocityǁ 0.00099935 51.544 9.5848 8.355 v Pressure -7.8199e+05 3.1028e+05 -2.3415e+05 -2.1219e+05 v TurbVisc 1.1459e-18 0.034252 0.00024855 0.00013067 v CourantNb 3.4161e-08 0.012092 0.00017601 5.0109e-06 v FourierNb 1.2486e-07 0.061116 0.00016237 1.0247e-06 v total_pressure -6.8066e+05 4.116e+05 -1.3283e+05 -1.1086e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3598 0.14015 0.0036307 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0059e-06 0.06237 0.00033838 6.0356e-06 INSTANT 0.877078000E-01 TIME STEP NUMBER 57276 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282744836E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.843376616E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.14364E-01 0.24003E+01 Friction velocity uk : 0.14364E-01 0.24003E+01 Dimensionless distance yplus : 0.14062E-01 0.23602E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -8.514022182e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.30013E+08 1 0.23308E-09 0.71227E+02 0.30621E+04 c Velocity[X] 0.40414E+02 c Velocity[Y] 0.30812E+02 c Velocity[Z] 0.80476E-06 c Pressure 0.31584E-02 507 0.51523E-04 0.14764E-01 0.88216E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -38.232 51.146 5.5965 7.9863 v Velocity[Y] -38.181 41.675 -0.24948 -0.31649 v Velocity[Z] -3.2805 3.2108 1.981e-06 -5.3959e-08 v ǁVelocityǁ 0.00098105 51.552 9.5861 8.3553 v Pressure -7.8321e+05 3.0933e+05 -2.3305e+05 -2.1287e+05 v TurbVisc 1.1914e-18 0.034264 0.00024861 0.00013086 v CourantNb 3.4105e-08 0.012093 0.00017602 5.011e-06 v FourierNb 1.2487e-07 0.061143 0.0001624 1.026e-06 v total_pressure -6.8188e+05 4.1066e+05 -1.3173e+05 -1.1155e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3602 0.14021 0.0036323 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0066e-06 0.062398 0.00033842 6.0371e-06 INSTANT 0.877079000E-01 TIME STEP NUMBER 57277 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282741756E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.843139839E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.17415E-01 0.24007E+01 Friction velocity uk : 0.17415E-01 0.24007E+01 Dimensionless distance yplus : 0.17049E-01 0.23606E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Incoming flow detained for 20 outlet faces on 2100 Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -8.259110200e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.30015E+08 1 0.23042E-09 0.71306E+02 0.30635E+04 c Velocity[X] 0.39933E+02 c Velocity[Y] 0.31373E+02 c Velocity[Z] 0.80231E-06 c Pressure 0.29953E-02 163 0.46774E-04 0.14483E-01 0.97926E+05 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -38.242 51.154 5.5964 7.9862 v Velocity[Y] -38.189 41.685 -0.24968 -0.31709 v Velocity[Z] -3.2807 3.2109 1.9805e-06 -5.3959e-08 v ǁVelocityǁ 0.00097288 51.56 9.5875 8.3556 v Pressure -7.8384e+05 3.0779e+05 -2.3164e+05 -2.1222e+05 v TurbVisc 1.2457e-18 0.034277 0.00024867 0.00013091 v CourantNb 3.4043e-08 0.012094 0.00017603 5.0111e-06 v FourierNb 1.2487e-07 0.061168 0.00016243 1.0264e-06 v total_pressure -6.8252e+05 4.0911e+05 -1.3031e+05 -1.1089e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3606 0.14027 0.0036338 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0073e-06 0.062426 0.00033846 6.0375e-06 INSTANT 0.877080000E-01 TIME STEP NUMBER 57278 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282738766E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.842925350E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.16576E-01 0.24011E+01 Friction velocity uk : 0.16576E-01 0.24011E+01 Dimensionless distance yplus : 0.16044E-01 0.23610E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -7.977357118e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.30017E+08 1 0.23207E-09 0.71602E+02 0.30696E+04 c Velocity[X] 0.40612E+02 c Velocity[Y] 0.30990E+02 c Velocity[Z] 0.78919E-06 c Pressure 0.32396E-02 191 0.47255E-04 0.15120E-01 0.11268E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -38.252 51.162 5.5963 7.9861 v Velocity[Y] -38.196 41.694 -0.24987 -0.31769 v Velocity[Z] -3.281 3.211 1.9801e-06 -5.3959e-08 v ǁVelocityǁ 0.00096865 51.568 9.5888 8.3559 v Pressure -7.8439e+05 3.149e+05 -2.3017e+05 -2.1078e+05 v TurbVisc 1.306e-18 0.034289 0.00024873 0.00013112 v CourantNb 3.3976e-08 0.012095 0.00017605 5.0112e-06 v FourierNb 1.2488e-07 0.061194 0.00016246 1.0278e-06 v total_pressure -6.8307e+05 4.1622e+05 -1.2885e+05 -1.0945e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.361 0.14032 0.0036353 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0081e-06 0.062453 0.0003385 6.039e-06 INSTANT 0.877081000E-01 TIME STEP NUMBER 57279 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282736032E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.842717802E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15191E-01 0.24015E+01 Friction velocity uk : 0.15191E-01 0.24015E+01 Dimensionless distance yplus : 0.14703E-01 0.23614E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Incoming flow detained for 20 outlet faces on 2100 Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -7.687584697e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.30019E+08 1 0.23144E-09 0.71394E+02 0.30649E+04 c Velocity[X] 0.40035E+02 c Velocity[Y] 0.31359E+02 c Velocity[Z] 0.78590E-06 c Pressure 0.31881E-02 364 0.48388E-04 0.15387E-01 0.20045E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -38.262 51.17 5.5963 7.986 v Velocity[Y] -38.204 41.704 -0.25007 -0.31827 v Velocity[Z] -3.2813 3.211 1.9797e-06 -5.3959e-08 v ǁVelocityǁ 0.00097419 51.576 9.5901 8.3562 v Pressure -7.8561e+05 3.041e+05 -2.2921e+05 -2.1326e+05 v TurbVisc 1.3763e-18 0.034301 0.00024879 0.00013117 v CourantNb 3.3905e-08 0.012096 0.00017606 5.0113e-06 v FourierNb 1.2488e-07 0.061218 0.00016249 1.0281e-06 v total_pressure -6.8429e+05 4.0543e+05 -1.2788e+05 -1.1193e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3614 0.14038 0.0036368 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0088e-06 0.06248 0.00033855 6.0394e-06 INSTANT 0.877082000E-01 TIME STEP NUMBER 57280 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282733809E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.842514597E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.16037E-01 0.24020E+01 Friction velocity uk : 0.16037E-01 0.24020E+01 Dimensionless distance yplus : 0.15522E-01 0.23618E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -7.385786272e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.30020E+08 1 0.23183E-09 0.72064E+02 0.30790E+04 c Velocity[X] 0.40910E+02 c Velocity[Y] 0.31154E+02 c Velocity[Z] 0.79289E-06 c Pressure 0.33630E-02 288 0.50072E-04 0.15670E-01 0.25123E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -38.272 51.177 5.5962 7.986 v Velocity[Y] -38.211 41.714 -0.25027 -0.31888 v Velocity[Z] -3.2816 3.2111 1.9792e-06 -5.3959e-08 v ǁVelocityǁ 0.00097658 51.584 9.5915 8.3565 v Pressure -7.8569e+05 3.2895e+05 -2.2726e+05 -2.0876e+05 v TurbVisc 1.4477e-18 0.034314 0.00024885 0.00013137 v CourantNb 3.383e-08 0.012098 0.00017607 5.0114e-06 v FourierNb 1.2489e-07 0.061242 0.00016252 1.0295e-06 v total_pressure -6.8437e+05 4.3028e+05 -1.2594e+05 -1.0743e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3618 0.14044 0.0036382 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0095e-06 0.062506 0.00033859 6.0409e-06 INSTANT 0.877083000E-01 TIME STEP NUMBER 57281 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282731151E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.842341752E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.18279E-01 0.24024E+01 Friction velocity uk : 0.18279E-01 0.24024E+01 Dimensionless distance yplus : 0.17693E-01 0.23622E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Incoming flow detained for 20 outlet faces on 2100 Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -7.083298521e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.30023E+08 1 0.23227E-09 0.71622E+02 0.30693E+04 c Velocity[X] 0.40198E+02 c Velocity[Y] 0.31424E+02 c Velocity[Z] 0.78514E-06 c Pressure 0.33697E-02 256 0.53147E-04 0.16235E-01 0.35096E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -38.282 51.185 5.5961 7.9859 v Velocity[Y] -38.219 41.724 -0.25047 -0.31945 v Velocity[Z] -3.2818 3.2112 1.9788e-06 -5.3959e-08 v ǁVelocityǁ 0.0010023 51.593 9.5928 8.3568 v Pressure -7.8756e+05 2.9972e+05 -2.2671e+05 -2.1428e+05 v TurbVisc 1.5244e-18 0.034326 0.00024891 0.00013142 v CourantNb 3.3751e-08 0.012099 0.00017609 5.0116e-06 v FourierNb 1.2489e-07 0.061265 0.00016254 1.0298e-06 v total_pressure -6.8623e+05 4.0105e+05 -1.2538e+05 -1.1296e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3622 0.1405 0.0036397 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0103e-06 0.062532 0.00033863 6.0414e-06 INSTANT 0.877084000E-01 TIME STEP NUMBER 57282 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282729725E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.842153048E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.20796E-01 0.24028E+01 Friction velocity uk : 0.20796E-01 0.24028E+01 Dimensionless distance yplus : 0.20129E-01 0.23627E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -6.769779334e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.30024E+08 1 0.23189E-09 0.72632E+02 0.30906E+04 c Velocity[X] 0.41290E+02 c Velocity[Y] 0.31343E+02 c Velocity[Z] 0.78471E-06 c Pressure 0.35075E-02 269 0.56344E-04 0.16316E-01 0.41269E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -38.292 51.193 5.5961 7.9858 v Velocity[Y] -38.226 41.734 -0.25067 -0.32007 v Velocity[Z] -3.2821 3.2113 1.9783e-06 -5.3959e-08 v ǁVelocityǁ 0.0010446 51.601 9.5941 8.3572 v Pressure -7.8704e+05 3.4327e+05 -2.2429e+05 -2.067e+05 v TurbVisc 1.6155e-18 0.034338 0.00024897 0.00013162 v CourantNb 3.367e-08 0.0121 0.0001761 5.0117e-06 v FourierNb 1.2489e-07 0.061288 0.00016257 1.0312e-06 v total_pressure -6.8571e+05 4.4459e+05 -1.2296e+05 -1.0538e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3627 0.14056 0.0036412 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.011e-06 0.062557 0.00033867 6.0429e-06 INSTANT 0.877085000E-01 TIME STEP NUMBER 57283 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282727205E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.842014698E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.23204E-01 0.24033E+01 Friction velocity uk : 0.23204E-01 0.24033E+01 Dimensionless distance yplus : 0.22459E-01 0.23631E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Incoming flow detained for 20 outlet faces on 2100 Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -6.441563299e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.30027E+08 1 0.23301E-09 0.71975E+02 0.30763E+04 c Velocity[X] 0.40431E+02 c Velocity[Y] 0.31544E+02 c Velocity[Z] 0.78919E-06 c Pressure 0.35481E-02 196 0.62554E-04 0.17064E-01 0.51013E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -38.303 51.201 5.596 7.9858 v Velocity[Y] -38.234 41.744 -0.25086 -0.32062 v Velocity[Z] -3.2824 3.2114 1.9779e-06 -5.3959e-08 v ǁVelocityǁ 0.0011068 51.609 9.5955 8.3575 v Pressure -7.8936e+05 2.9518e+05 -2.2413e+05 -2.1522e+05 v TurbVisc 1.6603e-18 0.034351 0.00024903 0.00013168 v CourantNb 3.3584e-08 0.012101 0.00017611 5.0118e-06 v FourierNb 1.2489e-07 0.06131 0.0001626 1.0316e-06 v total_pressure -6.8804e+05 3.965e+05 -1.228e+05 -1.1389e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3631 0.14062 0.0036427 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0117e-06 0.062582 0.00033871 6.0434e-06 INSTANT 0.877086000E-01 TIME STEP NUMBER 57284 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282726700E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.841840988E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.24238E-01 0.24038E+01 Friction velocity uk : 0.24238E-01 0.24038E+01 Dimensionless distance yplus : 0.23355E-01 0.23636E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -6.108978126e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.30028E+08 1 0.23212E-09 0.73311E+02 0.31044E+04 c Velocity[X] 0.41764E+02 c Velocity[Y] 0.31547E+02 c Velocity[Z] 0.80051E-06 c Pressure 0.36664E-02 148 0.66369E-04 0.17025E-01 0.56929E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -38.313 51.209 5.596 7.9857 v Velocity[Y] -38.242 41.754 -0.25106 -0.32125 v Velocity[Z] -3.2826 3.2115 1.9775e-06 -5.3959e-08 v ǁVelocityǁ 0.0011835 51.617 9.5968 8.3578 v Pressure -7.8835e+05 3.5763e+05 -2.2135e+05 -2.0498e+05 v TurbVisc 1.6597e-18 0.034363 0.00024909 0.00013188 v CourantNb 3.3631e-08 0.012102 0.00017613 5.0119e-06 v FourierNb 1.2489e-07 0.061331 0.00016263 1.033e-06 v total_pressure -6.8702e+05 4.5895e+05 -1.2002e+05 -1.0366e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3636 0.14067 0.0036441 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0124e-06 0.062606 0.00033876 6.0448e-06 INSTANT 0.877087000E-01 TIME STEP NUMBER 57285 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282724070E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.841738820E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.21021E-01 0.24042E+01 Friction velocity uk : 0.21021E-01 0.24042E+01 Dimensionless distance yplus : 0.20255E-01 0.23641E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Incoming flow detained for 20 outlet faces on 2100 Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -5.761236472e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.30031E+08 1 0.23371E-09 0.72450E+02 0.30859E+04 c Velocity[X] 0.40738E+02 c Velocity[Y] 0.31712E+02 c Velocity[Z] 0.78929E-06 c Pressure 0.37271E-02 616 0.72938E-04 0.17892E-01 0.66381E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -38.323 51.218 5.5959 7.9857 v Velocity[Y] -38.249 41.764 -0.25126 -0.32178 v Velocity[Z] -3.2829 3.2115 1.977e-06 -5.3959e-08 v ǁVelocityǁ 0.0012697 51.626 9.5982 8.3582 v Pressure -7.9102e+05 2.9028e+05 -2.215e+05 -2.1613e+05 v TurbVisc 1.6592e-18 0.034375 0.00024915 0.00013194 v CourantNb 3.4473e-08 0.012103 0.00017614 5.012e-06 v FourierNb 1.249e-07 0.061352 0.00016266 1.0333e-06 v total_pressure -6.897e+05 3.916e+05 -1.2018e+05 -1.148e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3641 0.14073 0.0036456 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0132e-06 0.062629 0.0003388 6.0453e-06 INSTANT 0.877088000E-01 TIME STEP NUMBER 57286 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282724567E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.841586714E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.17446E-01 0.24047E+01 Friction velocity uk : 0.17446E-01 0.24047E+01 Dimensionless distance yplus : 0.16810E-01 0.23645E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -5.410302766e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.30032E+08 1 0.23245E-09 0.74117E+02 0.31209E+04 c Velocity[X] 0.42328E+02 c Velocity[Y] 0.31789E+02 c Velocity[Z] 0.78296E-06 c Pressure 0.38353E-02 456 0.76825E-04 0.17779E-01 0.73831E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -38.334 51.226 5.5959 7.9856 v Velocity[Y] -38.257 41.774 -0.25146 -0.32241 v Velocity[Z] -3.2832 3.2116 1.9766e-06 -5.396e-08 v ǁVelocityǁ 0.001362 51.634 9.5995 8.3585 v Pressure -7.8939e+05 3.7253e+05 -2.183e+05 -2.0292e+05 v TurbVisc 1.6633e-18 0.034388 0.00024921 0.00013214 v CourantNb 3.5414e-08 0.012104 0.00017615 5.0121e-06 v FourierNb 1.249e-07 0.061372 0.00016269 1.0347e-06 v total_pressure -6.8806e+05 4.7385e+05 -1.1698e+05 -1.0159e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3645 0.14079 0.003647 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0139e-06 0.062652 0.00033884 6.0468e-06 INSTANT 0.877089000E-01 TIME STEP NUMBER 57287 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282722020E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.841520887E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13558E-01 0.24052E+01 Friction velocity uk : 0.13558E-01 0.24052E+01 Dimensionless distance yplus : 0.13064E-01 0.23650E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Incoming flow detained for 20 outlet faces on 2100 Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -5.044913650e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.30035E+08 1 0.23441E-09 0.73053E+02 0.30982E+04 c Velocity[X] 0.41131E+02 c Velocity[Y] 0.31922E+02 c Velocity[Z] 0.78400E-06 c Pressure 0.39080E-02 650 0.83582E-04 0.18727E-01 0.82778E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -38.344 51.234 5.5959 7.9856 v Velocity[Y] -38.265 41.784 -0.25165 -0.32294 v Velocity[Z] -3.2835 3.2117 1.9762e-06 -5.396e-08 v ǁVelocityǁ 0.0014569 51.643 9.6008 8.3589 v Pressure -7.925e+05 2.8556e+05 -2.1887e+05 -2.1711e+05 v TurbVisc 1.6613e-18 0.0344 0.00024927 0.00013219 v CourantNb 3.6461e-08 0.012105 0.00017617 5.0122e-06 v FourierNb 1.249e-07 0.061392 0.00016272 1.0351e-06 v total_pressure -6.9118e+05 3.8689e+05 -1.1754e+05 -1.1579e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.365 0.14084 0.0036485 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0146e-06 0.062674 0.00033888 6.0473e-06 INSTANT 0.877090000E-01 TIME STEP NUMBER 57288 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282723385E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.841386885E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.90748E-02 0.24057E+01 Friction velocity uk : 0.90748E-02 0.24057E+01 Dimensionless distance yplus : 0.88560E-02 0.23655E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -4.677797160e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.30037E+08 1 0.23283E-09 0.75048E+02 0.31399E+04 c Velocity[X] 0.42985E+02 c Velocity[Y] 0.32063E+02 c Velocity[Z] 0.78442E-06 c Pressure 0.40109E-02 1066 0.87007E-04 0.18560E-01 0.91322E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -38.354 51.242 5.5958 7.9856 v Velocity[Y] -38.273 41.794 -0.25185 -0.32357 v Velocity[Z] -3.2837 3.2118 1.9757e-06 -5.396e-08 v ǁVelocityǁ 0.0015526 51.652 9.6022 8.3592 v Pressure -7.9019e+05 3.8784e+05 -2.1522e+05 -2.008e+05 v TurbVisc 1.662e-18 0.034412 0.00024934 0.0001324 v CourantNb 3.7608e-08 0.012106 0.00017618 5.0123e-06 v FourierNb 1.249e-07 0.061411 0.00016274 1.0365e-06 v total_pressure -6.8886e+05 4.8917e+05 -1.139e+05 -99478 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3655 0.1409 0.0036499 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0153e-06 0.062696 0.00033893 6.0488e-06 INSTANT 0.877091000E-01 TIME STEP NUMBER 57289 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282720882E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.841358752E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13493E-01 0.24063E+01 Friction velocity uk : 0.13493E-01 0.24063E+01 Dimensionless distance yplus : 0.13001E-01 0.23661E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Incoming flow detained for 20 outlet faces on 2100 Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -4.295900573e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.30040E+08 1 0.23510E-09 0.73780E+02 0.31130E+04 c Velocity[X] 0.41605E+02 c Velocity[Y] 0.32175E+02 c Velocity[Z] 0.78594E-06 c Pressure 0.40912E-02 226 0.94912E-04 0.19570E-01 0.99052E+06 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -38.365 51.251 5.5958 7.9855 v Velocity[Y] -38.281 41.804 -0.25205 -0.32408 v Velocity[Z] -3.284 3.2119 1.9753e-06 -5.396e-08 v ǁVelocityǁ 0.0016473 51.66 9.6035 8.3596 v Pressure -7.9366e+05 2.8086e+05 -2.1621e+05 -2.1798e+05 v TurbVisc 1.6628e-18 0.034425 0.0002494 0.00013245 v CourantNb 3.8859e-08 0.012107 0.0001762 5.0125e-06 v FourierNb 1.249e-07 0.06143 0.00016277 1.0369e-06 v total_pressure -6.9234e+05 3.8218e+05 -1.1488e+05 -1.1666e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3661 0.14096 0.0036514 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0161e-06 0.062718 0.00033897 6.0494e-06 INSTANT 0.877092000E-01 TIME STEP NUMBER 57290 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282723138E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.841242738E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.17034E-01 0.24068E+01 Friction velocity uk : 0.17034E-01 0.24068E+01 Dimensionless distance yplus : 0.16413E-01 0.23666E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -3.917237353e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.30041E+08 1 0.23326E-09 0.76109E+02 0.31614E+04 c Velocity[X] 0.43736E+02 c Velocity[Y] 0.32372E+02 c Velocity[Z] 0.80754E-06 c Pressure 0.41914E-02 219 0.98483E-04 0.19361E-01 0.10900E+07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -38.375 51.259 5.5958 7.9855 v Velocity[Y] -38.288 41.814 -0.25225 -0.32473 v Velocity[Z] -3.2843 3.2119 1.9748e-06 -5.396e-08 v ǁVelocityǁ 0.0017397 51.669 9.6049 8.36 v Pressure -7.9068e+05 4.037e+05 -2.1213e+05 -1.9862e+05 v TurbVisc 1.6632e-18 0.034437 0.00024946 0.00013265 v CourantNb 4.0209e-08 0.012109 0.00017621 5.0126e-06 v FourierNb 1.249e-07 0.061448 0.0001628 1.0382e-06 v total_pressure -6.8935e+05 5.0502e+05 -1.1081e+05 -97298 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3666 0.14101 0.0036528 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0167e-06 0.062739 0.00033901 6.0508e-06 INSTANT 0.877093000E-01 TIME STEP NUMBER 57291 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282720650E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.841252063E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.20145E-01 0.24074E+01 Friction velocity uk : 0.20145E-01 0.24074E+01 Dimensionless distance yplus : 0.19411E-01 0.23671E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Incoming flow detained for 20 outlet faces on 2100 Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -3.522253815e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.30044E+08 1 0.23581E-09 0.74776E+02 0.31334E+04 c Velocity[X] 0.42215E+02 c Velocity[Y] 0.32561E+02 c Velocity[Z] 0.80090E-06 c Pressure 0.42772E-02 262 0.85713E-04 0.20423E-01 0.11439E+07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -38.386 51.267 5.5958 7.9855 v Velocity[Y] -38.296 41.824 -0.25244 -0.32522 v Velocity[Z] -3.2845 3.212 1.9744e-06 -5.396e-08 v ǁVelocityǁ 0.0018289 51.678 9.6062 8.3603 v Pressure -7.9423e+05 2.7663e+05 -2.134e+05 -2.1816e+05 v TurbVisc 1.6669e-18 0.034449 0.00024952 0.00013271 v CourantNb 4.1662e-08 0.01211 0.00017622 5.0127e-06 v FourierNb 1.249e-07 0.061466 0.00016283 1.0386e-06 v total_pressure -6.929e+05 3.7795e+05 -1.1207e+05 -1.1684e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3671 0.14107 0.0036542 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0175e-06 0.062759 0.00033905 6.0514e-06 INSTANT 0.877094000E-01 TIME STEP NUMBER 57292 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282723372E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.841152664E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.22818E-01 0.24079E+01 Friction velocity uk : 0.22818E-01 0.24079E+01 Dimensionless distance yplus : 0.21987E-01 0.23677E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -3.136481952e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.30045E+08 1 0.23375E-09 0.77629E+02 0.31923E+04 c Velocity[X] 0.44896E+02 c Velocity[Y] 0.32732E+02 c Velocity[Z] 0.78332E-06 c Pressure 0.43782E-02 328 0.55122E-04 0.20188E-01 0.12127E+07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -38.396 51.276 5.5957 7.9855 v Velocity[Y] -38.304 41.835 -0.25264 -0.32587 v Velocity[Z] -3.2848 3.2121 1.974e-06 -5.396e-08 v ǁVelocityǁ 0.0018768 51.686 9.6076 8.3607 v Pressure -7.9119e+05 4.2566e+05 -2.0929e+05 -1.9774e+05 v TurbVisc 1.6683e-18 0.034462 0.00024958 0.00013291 v CourantNb 4.3211e-08 0.012111 0.00017624 5.0128e-06 v FourierNb 1.249e-07 0.061483 0.00016286 1.04e-06 v total_pressure -6.8987e+05 5.2699e+05 -1.0796e+05 -96410 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3677 0.14112 0.0036556 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0182e-06 0.062779 0.0003391 6.0528e-06 INSTANT 0.877095000E-01 TIME STEP NUMBER 57293 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282721654E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.841188311E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.21262E-01 0.24085E+01 Friction velocity uk : 0.21262E-01 0.24085E+01 Dimensionless distance yplus : 0.20816E-01 0.23682E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Incoming flow detained for 20 outlet faces on 2100 Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -2.740467875e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.30049E+08 1 0.23655E-09 0.75772E+02 0.31536E+04 c Velocity[X] 0.42800E+02 c Velocity[Y] 0.32972E+02 c Velocity[Z] 0.77532E-06 c Pressure 0.44558E-02 335 0.48856E-04 0.21237E-01 0.12264E+07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -38.407 51.284 5.5957 7.9855 v Velocity[Y] -38.312 41.845 -0.25283 -0.32635 v Velocity[Z] -3.2851 3.2122 1.9735e-06 -5.396e-08 v ǁVelocityǁ 0.0018377 51.696 9.609 8.3611 v Pressure -7.9454e+05 2.7311e+05 -2.1053e+05 -2.1754e+05 v TurbVisc 1.6704e-18 0.034474 0.00024964 0.00013297 v CourantNb 4.4859e-08 0.012112 0.00017625 5.013e-06 v FourierNb 1.249e-07 0.0615 0.00016289 1.0404e-06 v total_pressure -6.9321e+05 3.7443e+05 -1.0921e+05 -1.1621e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3682 0.14118 0.003657 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0189e-06 0.062799 0.00033914 6.0534e-06 INSTANT 0.877096000E-01 TIME STEP NUMBER 57294 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282724850E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.841121725E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19112E-01 0.24091E+01 Friction velocity uk : 0.19112E-01 0.24091E+01 Dimensionless distance yplus : 0.18711E-01 0.23688E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -2.344620382e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.30050E+08 1 0.23418E-09 0.78959E+02 0.32189E+04 c Velocity[X] 0.45876E+02 c Velocity[Y] 0.33083E+02 c Velocity[Z] 0.78616E-06 c Pressure 0.45556E-02 460 0.43443E-04 0.20969E-01 0.13289E+07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -38.418 51.293 5.5957 7.9855 v Velocity[Y] -38.32 41.855 -0.25303 -0.327 v Velocity[Z] -3.2853 3.2123 1.9731e-06 -5.396e-08 v ǁVelocityǁ 0.0017994 51.704 9.6103 8.3615 v Pressure -7.9089e+05 4.4249e+05 -2.0621e+05 -1.9565e+05 v TurbVisc 1.6733e-18 0.034486 0.0002497 0.00013317 v CourantNb 4.66e-08 0.012113 0.00017627 5.0131e-06 v FourierNb 1.249e-07 0.061516 0.00016292 1.0417e-06 v total_pressure -6.8956e+05 5.4382e+05 -1.0488e+05 -94321 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3688 0.14123 0.0036584 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0196e-06 0.062818 0.00033918 6.0548e-06 INSTANT 0.877097000E-01 TIME STEP NUMBER 57295 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282723132E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.841187913E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.16345E-01 0.24097E+01 Friction velocity uk : 0.16345E-01 0.24097E+01 Dimensionless distance yplus : 0.16002E-01 0.23694E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Incoming flow detained for 20 outlet faces on 2100 Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.937765386e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.30053E+08 1 0.23730E-09 0.76959E+02 0.31776E+04 c Velocity[X] 0.43564E+02 c Velocity[Y] 0.33396E+02 c Velocity[Z] 0.80255E-06 c Pressure 0.46485E-02 334 0.51204E-04 0.22115E-01 0.13693E+07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -38.429 51.302 5.5957 7.9855 v Velocity[Y] -38.329 41.866 -0.25322 -0.32747 v Velocity[Z] -3.2856 3.2123 1.9726e-06 -5.396e-08 v ǁVelocityǁ 0.001762 51.713 9.6117 8.3618 v Pressure -7.9457e+05 2.6958e+05 -2.0779e+05 -2.1782e+05 v TurbVisc 1.6763e-18 0.034499 0.00024976 0.00013323 v CourantNb 4.8436e-08 0.012114 0.00017628 5.0133e-06 v FourierNb 1.249e-07 0.061532 0.00016294 1.0422e-06 v total_pressure -6.9324e+05 3.709e+05 -1.0647e+05 -1.165e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3694 0.14128 0.0036597 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0204e-06 0.062837 0.00033923 6.0554e-06 INSTANT 0.877098000E-01 TIME STEP NUMBER 57296 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282727015E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.841135807E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12656E-01 0.24103E+01 Friction velocity uk : 0.12656E-01 0.24103E+01 Dimensionless distance yplus : 0.12391E-01 0.23700E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.538365927e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.30054E+08 1 0.23473E-09 0.80491E+02 0.32494E+04 c Velocity[X] 0.46976E+02 c Velocity[Y] 0.33515E+02 c Velocity[Z] 0.78688E-06 c Pressure 0.47467E-02 280 0.51436E-04 0.21809E-01 0.14998E+07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -38.44 51.31 5.5957 7.9855 v Velocity[Y] -38.337 41.876 -0.25342 -0.32813 v Velocity[Z] -3.2859 3.2124 1.9722e-06 -5.396e-08 v ǁVelocityǁ 0.0017252 51.722 9.613 8.3622 v Pressure -7.9031e+05 4.606e+05 -2.0313e+05 -1.9325e+05 v TurbVisc 1.6795e-18 0.034511 0.00024983 0.00013343 v CourantNb 4.7325e-08 0.012115 0.0001763 5.0133e-06 v FourierNb 1.249e-07 0.061547 0.00016297 1.0435e-06 v total_pressure -6.8899e+05 5.6193e+05 -1.018e+05 -91921 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.37 0.14134 0.003661 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.021e-06 0.062856 0.00033927 6.0568e-06 INSTANT 0.877099000E-01 TIME STEP NUMBER 57297 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282725369E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.841233562E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.75677E-02 0.24109E+01 Friction velocity uk : 0.75677E-02 0.24109E+01 Dimensionless distance yplus : 0.74089E-02 0.23706E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Incoming flow detained for 20 outlet faces on 2100 Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -1.132474490e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.30058E+08 1 0.23807E-09 0.78273E+02 0.32040E+04 c Velocity[X] 0.44409E+02 c Velocity[Y] 0.33864E+02 c Velocity[Z] 0.79729E-06 c Pressure 0.48409E-02 372 0.55763E-04 0.22989E-01 0.15216E+07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -38.451 51.319 5.5957 7.9855 v Velocity[Y] -38.345 41.887 -0.2536 -0.32858 v Velocity[Z] -3.2861 3.2125 1.9718e-06 -5.3961e-08 v ǁVelocityǁ 0.001689 51.732 9.6144 8.3626 v Pressure -7.9428e+05 2.6638e+05 -2.0507e+05 -2.1796e+05 v TurbVisc 1.6832e-18 0.034523 0.00024989 0.00013349 v CourantNb 4.2973e-08 0.012117 0.00017631 5.0135e-06 v FourierNb 1.2491e-07 0.061563 0.000163 1.0439e-06 v total_pressure -6.9295e+05 3.6771e+05 -1.0374e+05 -1.1663e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3706 0.14139 0.0036623 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0218e-06 0.062874 0.00033931 6.0574e-06 INSTANT 0.877100000E-01 TIME STEP NUMBER 57298 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282729920E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.841196773E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.45030E-02 0.24116E+01 Friction velocity uk : 0.45030E-02 0.24116E+01 Dimensionless distance yplus : 0.44085E-02 0.23712E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -7.397464050e-03 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.30059E+08 1 0.23530E-09 0.82171E+02 0.32825E+04 c Velocity[X] 0.48181E+02 c Velocity[Y] 0.33990E+02 c Velocity[Z] 0.79367E-06 c Pressure 0.49403E-02 264 0.56453E-04 0.22658E-01 0.16709E+07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -38.461 51.328 5.5957 7.9855 v Velocity[Y] -38.353 41.897 -0.2538 -0.32925 v Velocity[Z] -3.2864 3.2126 1.9713e-06 -5.3961e-08 v ǁVelocityǁ 0.0016533 51.74 9.6158 8.363 v Pressure -7.8944e+05 4.7927e+05 -2.0006e+05 -1.9074e+05 v TurbVisc 1.6874e-18 0.034535 0.00024995 0.00013369 v CourantNb 3.8627e-08 0.012118 0.00017633 5.0136e-06 v FourierNb 1.2491e-07 0.061578 0.00016303 1.0453e-06 v total_pressure -6.8811e+05 5.8059e+05 -98737 -89412 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3712 0.14143 0.0036635 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0224e-06 0.062892 0.00033936 6.0589e-06 INSTANT 0.877101000E-01 TIME STEP NUMBER 57299 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282728305E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.841325146E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.38477E-02 0.24122E+01 Friction velocity uk : 0.38477E-02 0.24122E+01 Dimensionless distance yplus : 0.37670E-02 0.23719E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Incoming flow detained for 20 outlet faces on 2100 Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan -3.435390055e-03 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.30063E+08 1 0.23886E-09 0.79728E+02 0.32331E+04 c Velocity[X] 0.45347E+02 c Velocity[Y] 0.34381E+02 c Velocity[Z] 0.79139E-06 c Pressure 0.50354E-02 475 0.61373E-04 0.23869E-01 0.16744E+07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -38.473 51.337 5.5957 7.9855 v Velocity[Y] -38.362 41.908 -0.25398 -0.32969 v Velocity[Z] -3.2867 3.2127 1.9709e-06 -5.3961e-08 v ǁVelocityǁ 0.001618 51.75 9.6172 8.3634 v Pressure -7.9372e+05 2.6352e+05 -2.0236e+05 -2.1799e+05 v TurbVisc 1.6917e-18 0.034548 0.00025001 0.00013375 v CourantNb 3.4318e-08 0.012119 0.00017634 5.0138e-06 v FourierNb 1.2491e-07 0.061592 0.00016306 1.0457e-06 v total_pressure -6.924e+05 3.6484e+05 -1.0103e+05 -1.1667e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3719 0.14149 0.0036651 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0232e-06 0.06291 0.0003394 6.0595e-06 INSTANT 0.877102000E-01 TIME STEP NUMBER 57300 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282733496E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.841302755E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.82875E-02 0.24129E+01 Friction velocity uk : 0.82875E-02 0.24129E+01 Dimensionless distance yplus : 0.80454E-02 0.23725E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 3.622786467e-04 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.30064E+08 1 0.23590E-09 0.84001E+02 0.33182E+04 c Velocity[X] 0.49489E+02 c Velocity[Y] 0.34512E+02 c Velocity[Z] 0.80209E-06 c Pressure 0.51358E-02 482 0.61646E-04 0.23513E-01 0.18434E+07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -38.483 51.346 5.5957 7.9855 v Velocity[Y] -38.37 41.918 -0.25418 -0.33036 v Velocity[Z] -3.287 3.2127 1.9705e-06 -5.3961e-08 v ǁVelocityǁ 0.001583 51.759 9.6185 8.3638 v Pressure -7.8833e+05 4.984e+05 -1.9703e+05 -1.8815e+05 v TurbVisc 1.6966e-18 0.03456 0.00025008 0.00013395 v CourantNb 3.0059e-08 0.01212 0.00017636 5.0139e-06 v FourierNb 1.2491e-07 0.061607 0.00016309 1.047e-06 v total_pressure -6.8701e+05 5.9973e+05 -95702 -86828 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3725 0.14156 0.0036667 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0238e-06 0.062928 0.00033944 6.0609e-06 INSTANT 0.877103000E-01 TIME STEP NUMBER 57301 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282731875E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.841459954E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.14391E-01 0.24135E+01 Friction velocity uk : 0.14391E-01 0.24135E+01 Dimensionless distance yplus : 0.13971E-01 0.23732E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Incoming flow detained for 20 outlet faces on 2100 Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 4.179457120e-03 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.30068E+08 1 0.23969E-09 0.81330E+02 0.32648E+04 c Velocity[X] 0.46381E+02 c Velocity[Y] 0.34949E+02 c Velocity[Z] 0.79363E-06 c Pressure 0.52321E-02 314 0.66552E-04 0.24757E-01 0.18275E+07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -38.495 51.355 5.5958 7.9855 v Velocity[Y] -38.378 41.929 -0.25436 -0.33078 v Velocity[Z] -3.2872 3.2128 1.97e-06 -5.3961e-08 v ǁVelocityǁ 0.0015483 51.768 9.6199 8.3642 v Pressure -7.9295e+05 2.6106e+05 -1.9967e+05 -2.1794e+05 v TurbVisc 1.7016e-18 0.034572 0.00025014 0.00013401 v CourantNb 2.5826e-08 0.012121 0.00017637 5.0141e-06 v FourierNb 1.2491e-07 0.061621 0.00016312 1.0475e-06 v total_pressure -6.9162e+05 3.6238e+05 -98348 -1.1662e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3732 0.14162 0.0036682 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0246e-06 0.062946 0.00033949 6.0615e-06 INSTANT 0.877104000E-01 TIME STEP NUMBER 57302 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282737698E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.841450988E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.18018E-01 0.24142E+01 Friction velocity uk : 0.18018E-01 0.24142E+01 Dimensionless distance yplus : 0.17596E-01 0.23739E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 7.798938458e-03 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.30068E+08 1 0.23652E-09 0.85981E+02 0.33565E+04 c Velocity[X] 0.50900E+02 c Velocity[Y] 0.35081E+02 c Velocity[Z] 0.80518E-06 c Pressure 0.53333E-02 228 0.66924E-04 0.24373E-01 0.20179E+07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -38.506 51.363 5.5958 7.9856 v Velocity[Y] -38.386 41.94 -0.25456 -0.33146 v Velocity[Z] -3.2875 3.2129 1.9696e-06 -5.3961e-08 v ǁVelocityǁ 0.0015137 51.777 9.6213 8.3647 v Pressure -7.8705e+05 5.1795e+05 -1.9402e+05 -1.8548e+05 v TurbVisc 1.707e-18 0.034584 0.0002502 0.0001342 v CourantNb 2.1627e-08 0.012123 0.00017639 5.0141e-06 v FourierNb 1.2491e-07 0.061635 0.00016315 1.0488e-06 v total_pressure -6.8572e+05 6.1927e+05 -92698 -84152 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3739 0.14168 0.0036697 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0252e-06 0.062963 0.00033953 6.0629e-06 INSTANT 0.877105000E-01 TIME STEP NUMBER 57303 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282736067E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.841635915E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12228E-01 0.24149E+01 Friction velocity uk : 0.12228E-01 0.24149E+01 Dimensionless distance yplus : 0.11942E-01 0.23746E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Incoming flow detained for 20 outlet faces on 2100 Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.141770314e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.30073E+08 1 0.24054E-09 0.83083E+02 0.32991E+04 c Velocity[X] 0.47514E+02 c Velocity[Y] 0.35569E+02 c Velocity[Z] 0.79541E-06 c Pressure 0.54305E-02 443 0.71982E-04 0.25648E-01 0.19817E+07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -38.517 51.373 5.5958 7.9856 v Velocity[Y] -38.395 41.951 -0.25473 -0.33187 v Velocity[Z] -3.2878 3.213 1.9692e-06 -5.3961e-08 v ǁVelocityǁ 0.0014792 51.787 9.6227 8.3651 v Pressure -7.9204e+05 2.5897e+05 -1.9703e+05 -2.1784e+05 v TurbVisc 1.7127e-18 0.034597 0.00025026 0.00013427 v CourantNb 1.7478e-08 0.012124 0.0001764 5.0143e-06 v FourierNb 1.2491e-07 0.061649 0.00016318 1.0492e-06 v total_pressure -6.9072e+05 3.6029e+05 -95708 -1.1651e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3746 0.14174 0.0036711 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.026e-06 0.062981 0.00033958 6.0636e-06 INSTANT 0.877106000E-01 TIME STEP NUMBER 57304 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282742488E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.841639090E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.53027E-02 0.24156E+01 Friction velocity uk : 0.53027E-02 0.24156E+01 Dimensionless distance yplus : 0.51785E-02 0.23753E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.480296235e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.30073E+08 1 0.23718E-09 0.88116E+02 0.33972E+04 c Velocity[X] 0.52415E+02 c Velocity[Y] 0.35701E+02 c Velocity[Z] 0.79109E-06 c Pressure 0.55325E-02 350 0.72059E-04 0.25237E-01 0.21934E+07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -38.528 51.382 5.5958 7.9856 v Velocity[Y] -38.403 41.961 -0.25493 -0.33256 v Velocity[Z] -3.288 3.2131 1.9687e-06 -5.3961e-08 v ǁVelocityǁ 0.0014447 51.796 9.624 8.3655 v Pressure -7.8566e+05 5.3785e+05 -1.9107e+05 -1.828e+05 v TurbVisc 1.7186e-18 0.034609 0.00025033 0.00013446 v CourantNb 1.3368e-08 0.012125 0.00017642 5.0144e-06 v FourierNb 1.2491e-07 0.061663 0.0001632 1.0506e-06 v total_pressure -6.8433e+05 6.3918e+05 -89747 -81473 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3753 0.14179 0.0036725 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0265e-06 0.062998 0.00033962 6.065e-06 INSTANT 0.877107000E-01 TIME STEP NUMBER 57305 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282740815E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.841850707E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.47660E-02 0.24164E+01 Friction velocity uk : 0.47660E-02 0.24164E+01 Dimensionless distance yplus : 0.46544E-02 0.23760E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Incoming flow detained for 20 outlet faces on 2100 Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 1.816378169e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.30078E+08 1 0.24141E-09 0.84987E+02 0.33361E+04 c Velocity[X] 0.48744E+02 c Velocity[Y] 0.36243E+02 c Velocity[Z] 0.79610E-06 c Pressure 0.56305E-02 427 0.77524E-04 0.26544E-01 0.21359E+07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -38.54 51.391 5.5959 7.9856 v Velocity[Y] -38.412 41.972 -0.2551 -0.33295 v Velocity[Z] -3.2883 3.2131 1.9683e-06 -5.3961e-08 v ǁVelocityǁ 0.0014102 51.806 9.6254 8.3659 v Pressure -7.9105e+05 2.571e+05 -1.9445e+05 -2.1773e+05 v TurbVisc 1.7248e-18 0.034621 0.00025039 0.00013453 v CourantNb 9.6662e-09 0.012126 0.00017643 5.0146e-06 v FourierNb 1.2491e-07 0.061677 0.00016323 1.051e-06 v total_pressure -6.8973e+05 3.5843e+05 -93128 -1.1641e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.376 0.14185 0.003674 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0273e-06 0.063016 0.00033967 6.0656e-06 INSTANT 0.877108000E-01 TIME STEP NUMBER 57306 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282747844E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.841865366E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.13946E-01 0.24171E+01 Friction velocity uk : 0.13946E-01 0.24171E+01 Dimensionless distance yplus : 0.13620E-01 0.23767E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 2.124455036e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.30078E+08 1 0.23786E-09 0.90408E+02 0.34405E+04 c Velocity[X] 0.54037E+02 c Velocity[Y] 0.36371E+02 c Velocity[Z] 0.79396E-06 c Pressure 0.57333E-02 293 0.77482E-04 0.26106E-01 0.23708E+07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -38.551 51.4 5.5959 7.9857 v Velocity[Y] -38.421 41.983 -0.2553 -0.33365 v Velocity[Z] -3.2886 3.2132 1.9678e-06 -5.3961e-08 v ǁVelocityǁ 0.0013757 51.815 9.6268 8.3663 v Pressure -7.8422e+05 5.5809e+05 -1.8817e+05 -1.8009e+05 v TurbVisc 1.7313e-18 0.034633 0.00025045 0.00013472 v CourantNb 1.4122e-08 0.012127 0.00017645 5.0147e-06 v FourierNb 1.2491e-07 0.061691 0.00016326 1.0523e-06 v total_pressure -6.8289e+05 6.5942e+05 -86850 -78761 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3767 0.14191 0.0036754 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0279e-06 0.063033 0.00033971 6.067e-06 INSTANT 0.877109000E-01 TIME STEP NUMBER 57307 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282746111E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.842103110E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.47777E-02 0.24178E+01 Friction velocity uk : 0.47777E-02 0.24178E+01 Dimensionless distance yplus : 0.46461E-02 0.23774E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Incoming flow detained for 20 outlet faces on 2100 Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 2.427782950e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.30083E+08 1 0.24232E-09 0.87049E+02 0.33756E+04 c Velocity[X] 0.50077E+02 c Velocity[Y] 0.36972E+02 c Velocity[Z] 0.81532E-06 c Pressure 0.58321E-02 294 0.83035E-04 0.27445E-01 0.22905E+07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -38.563 51.409 5.5959 7.9857 v Velocity[Y] -38.429 41.994 -0.25547 -0.33403 v Velocity[Z] -3.2888 3.2133 1.9674e-06 -5.3961e-08 v ǁVelocityǁ 0.0013412 51.825 9.6282 8.3667 v Pressure -7.9004e+05 2.5542e+05 -1.9193e+05 -2.1759e+05 v TurbVisc 1.7379e-18 0.034646 0.00025051 0.00013479 v CourantNb 1.9854e-08 0.012129 0.00017646 5.0149e-06 v FourierNb 1.2491e-07 0.061705 0.00016329 1.0528e-06 v total_pressure -6.8872e+05 3.5675e+05 -90602 -1.1626e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3774 0.14197 0.0036768 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0287e-06 0.063051 0.00033975 6.0677e-06 INSTANT 0.877110000E-01 TIME STEP NUMBER 57308 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282753728E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.842127937E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.42137E-02 0.24186E+01 Friction velocity uk : 0.42137E-02 0.24186E+01 Dimensionless distance yplus : 0.40977E-02 0.23781E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 2.699549331e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.30083E+08 1 0.23858E-09 0.92861E+02 0.34861E+04 c Velocity[X] 0.55766E+02 c Velocity[Y] 0.37095E+02 c Velocity[Z] 0.82461E-06 c Pressure 0.59355E-02 303 0.82761E-04 0.26978E-01 0.25495E+07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -38.574 51.418 5.596 7.9857 v Velocity[Y] -38.438 42.005 -0.25566 -0.33473 v Velocity[Z] -3.2891 3.2134 1.967e-06 -5.3962e-08 v ǁVelocityǁ 0.0013066 51.834 9.6296 8.3672 v Pressure -7.8278e+05 5.786e+05 -1.8534e+05 -1.7737e+05 v TurbVisc 1.7448e-18 0.034658 0.00025058 0.00013498 v CourantNb 2.5585e-08 0.01213 0.00017648 5.015e-06 v FourierNb 1.2491e-07 0.06172 0.00016332 1.0541e-06 v total_pressure -6.8145e+05 6.7993e+05 -84018 -76047 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3781 0.14203 0.0036782 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0293e-06 0.063069 0.0003398 6.0691e-06 INSTANT 0.877111000E-01 TIME STEP NUMBER 57309 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282751920E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.842390629E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11673E-01 0.24193E+01 Friction velocity uk : 0.11673E-01 0.24193E+01 Dimensionless distance yplus : 0.11373E-01 0.23789E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Incoming flow detained for 20 outlet faces on 2100 Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 2.965434139e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.30088E+08 1 0.24324E-09 0.89272E+02 0.34178E+04 c Velocity[X] 0.51514E+02 c Velocity[Y] 0.37758E+02 c Velocity[Z] 0.80490E-06 c Pressure 0.60349E-02 353 0.88032E-04 0.28347E-01 0.24454E+07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -38.586 51.428 5.596 7.9858 v Velocity[Y] -38.447 42.016 -0.25583 -0.3351 v Velocity[Z] -3.2894 3.2135 1.9665e-06 -5.3962e-08 v ǁVelocityǁ 0.0012721 51.844 9.631 8.3676 v Pressure -7.8906e+05 2.5392e+05 -1.8947e+05 -2.1747e+05 v TurbVisc 1.7518e-18 0.03467 0.00025064 0.00013505 v CourantNb 3.131e-08 0.012131 0.00017649 5.0152e-06 v FourierNb 1.2491e-07 0.061734 0.00016335 1.0546e-06 v total_pressure -6.8774e+05 3.5524e+05 -88148 -1.1614e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3789 0.14209 0.0036797 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0301e-06 0.063087 0.00033984 6.0698e-06 INSTANT 0.877112000E-01 TIME STEP NUMBER 57310 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282760116E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.842425066E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.46311E-02 0.24201E+01 Friction velocity uk : 0.46311E-02 0.24201E+01 Dimensionless distance yplus : 0.45123E-02 0.23796E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 3.197039088e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.30088E+08 1 0.23931E-09 0.95478E+02 0.35342E+04 c Velocity[X] 0.57605E+02 c Velocity[Y] 0.37873E+02 c Velocity[Z] 0.80740E-06 c Pressure 0.61390E-02 438 0.87620E-04 0.27852E-01 0.27288E+07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -38.597 51.437 5.596 7.9858 v Velocity[Y] -38.455 42.027 -0.25602 -0.33581 v Velocity[Z] -3.2896 3.2135 1.9661e-06 -5.3962e-08 v ǁVelocityǁ 0.0012376 51.854 9.6323 8.3681 v Pressure -7.8138e+05 5.9937e+05 -1.826e+05 -1.7471e+05 v TurbVisc 1.7589e-18 0.034682 0.00025071 0.00013524 v CourantNb 3.7028e-08 0.012133 0.00017651 5.0153e-06 v FourierNb 1.2492e-07 0.061749 0.00016338 1.0559e-06 v total_pressure -6.8005e+05 7.0069e+05 -81271 -73384 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3796 0.14215 0.0036811 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0306e-06 0.063105 0.00033989 6.0712e-06 INSTANT 0.877113000E-01 TIME STEP NUMBER 57311 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282758231E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.842711972E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10372E-01 0.24209E+01 Friction velocity uk : 0.10372E-01 0.24209E+01 Dimensionless distance yplus : 0.10106E-01 0.23804E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Incoming flow detained for 20 outlet faces on 2100 Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 3.422423331e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.30093E+08 1 0.24419E-09 0.91656E+02 0.34624E+04 c Velocity[X] 0.53056E+02 c Velocity[Y] 0.38600E+02 c Velocity[Z] 0.81029E-06 c Pressure 0.62390E-02 419 0.93547E-04 0.29251E-01 0.25999E+07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -38.609 51.447 5.5961 7.9858 v Velocity[Y] -38.464 42.038 -0.25618 -0.33616 v Velocity[Z] -3.2899 3.2136 1.9657e-06 -5.3962e-08 v ǁVelocityǁ 0.0012032 51.864 9.6338 8.3685 v Pressure -7.8814e+05 2.5255e+05 -1.8709e+05 -2.1736e+05 v TurbVisc 1.7665e-18 0.034694 0.00025077 0.00013531 v CourantNb 4.2727e-08 0.012134 0.00017652 5.0155e-06 v FourierNb 1.2492e-07 0.061764 0.00016341 1.0563e-06 v total_pressure -6.8682e+05 3.5388e+05 -85769 -1.1604e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3804 0.14221 0.0036826 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0314e-06 0.063124 0.00033993 6.0719e-06 INSTANT 0.877114000E-01 TIME STEP NUMBER 57312 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282766987E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.842755892E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15925E-01 0.24217E+01 Friction velocity uk : 0.15925E-01 0.24217E+01 Dimensionless distance yplus : 0.15315E-01 0.23812E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 3.611434531e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.30093E+08 1 0.24007E-09 0.98258E+02 0.35846E+04 c Velocity[X] 0.59552E+02 c Velocity[Y] 0.38706E+02 c Velocity[Z] 0.80420E-06 c Pressure 0.63437E-02 351 0.92977E-04 0.28728E-01 0.29099E+07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -38.62 51.456 5.5961 7.9859 v Velocity[Y] -38.473 42.049 -0.25637 -0.33688 v Velocity[Z] -3.2902 3.2137 1.9652e-06 -5.3962e-08 v ǁVelocityǁ 0.0011692 51.873 9.6351 8.3689 v Pressure -7.8006e+05 6.2035e+05 -1.7992e+05 -1.7204e+05 v TurbVisc 1.774e-18 0.034707 0.00025084 0.0001355 v CourantNb 4.4502e-08 0.012135 0.00017654 5.0156e-06 v FourierNb 1.2492e-07 0.061779 0.00016344 1.0576e-06 v total_pressure -6.7874e+05 7.2167e+05 -78592 -70713 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3812 0.14227 0.003684 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0319e-06 0.063143 0.00033998 6.0732e-06 INSTANT 0.877115000E-01 TIME STEP NUMBER 57313 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282765006E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.843066446E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.14500E-01 0.24225E+01 Friction velocity uk : 0.14500E-01 0.24225E+01 Dimensionless distance yplus : 0.13945E-01 0.23820E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Incoming flow detained for 20 outlet faces on 2100 Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 3.794272673e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.30098E+08 1 0.24517E-09 0.94204E+02 0.35096E+04 c Velocity[X] 0.54703E+02 c Velocity[Y] 0.39501E+02 c Velocity[Z] 0.81540E-06 c Pressure 0.64443E-02 473 0.98986E-04 0.30158E-01 0.27545E+07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -38.632 51.466 5.5962 7.9859 v Velocity[Y] -38.482 42.06 -0.25653 -0.33722 v Velocity[Z] -3.2904 3.2138 1.9648e-06 -5.3962e-08 v ǁVelocityǁ 0.0011356 51.883 9.6365 8.3693 v Pressure -7.8732e+05 2.5132e+05 -1.8481e+05 -2.1731e+05 v TurbVisc 1.7813e-18 0.034719 0.0002509 0.00013557 v CourantNb 4.4528e-08 0.012136 0.00017656 5.0158e-06 v FourierNb 1.2492e-07 0.061795 0.00016346 1.0581e-06 v total_pressure -6.8599e+05 3.5264e+05 -83482 -1.1599e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.382 0.14233 0.0036855 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0328e-06 0.063162 0.00034002 6.0739e-06 INSTANT 0.877116000E-01 TIME STEP NUMBER 57314 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282774319E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.843118264E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12957E-01 0.24233E+01 Friction velocity uk : 0.12957E-01 0.24233E+01 Dimensionless distance yplus : 0.12461E-01 0.23827E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 3.939376897e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.30098E+08 1 0.24086E-09 0.10121E+03 0.36373E+04 c Velocity[X] 0.61612E+02 c Velocity[Y] 0.39597E+02 c Velocity[Z] 0.80977E-06 c Pressure 0.65496E-02 441 0.98050E-04 0.29607E-01 0.30913E+07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -38.644 51.475 5.5962 7.986 v Velocity[Y] -38.491 42.071 -0.25672 -0.33795 v Velocity[Z] -3.2907 3.2138 1.9644e-06 -5.3962e-08 v ǁVelocityǁ 0.0011026 51.893 9.6379 8.3698 v Pressure -7.7886e+05 6.4155e+05 -1.7735e+05 -1.6946e+05 v TurbVisc 1.7891e-18 0.034731 0.00025096 0.00013576 v CourantNb 4.4555e-08 0.012138 0.00017657 5.0159e-06 v FourierNb 1.2492e-07 0.061811 0.00016349 1.0594e-06 v total_pressure -6.7753e+05 7.4287e+05 -76021 -68132 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3827 0.14239 0.0036869 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0333e-06 0.063182 0.00034006 6.0753e-06 INSTANT 0.877117000E-01 TIME STEP NUMBER 57315 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282772257E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.843451857E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11252E-01 0.24241E+01 Friction velocity uk : 0.11252E-01 0.24241E+01 Dimensionless distance yplus : 0.10821E-01 0.23835E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Incoming flow detained for 20 outlet faces on 2100 Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 4.078948382e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.30103E+08 1 0.24617E-09 0.97159E+02 0.35635E+04 c Velocity[X] 0.56560E+02 c Velocity[Y] 0.40599E+02 c Velocity[Z] 0.82146E-06 c Pressure 0.66505E-02 439 0.49083E-04 0.31066E-01 0.28862E+07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -38.656 51.485 5.5963 7.986 v Velocity[Y] -38.5 42.082 -0.25687 -0.33827 v Velocity[Z] -3.291 3.2139 1.9639e-06 -5.3962e-08 v ǁVelocityǁ 0.0010705 51.903 9.6393 8.3702 v Pressure -7.864e+05 2.505e+05 -1.825e+05 -2.1645e+05 v TurbVisc 1.797e-18 0.034743 0.00025103 0.00013583 v CourantNb 4.4585e-08 0.012139 0.00017659 5.0161e-06 v FourierNb 1.2492e-07 0.061828 0.00016352 1.0599e-06 v total_pressure -6.8507e+05 3.5182e+05 -81178 -1.1513e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3835 0.14245 0.0036882 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0341e-06 0.063203 0.00034011 6.076e-06 INSTANT 0.877118000E-01 TIME STEP NUMBER 57316 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282782087E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.843512429E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.92553E-02 0.24249E+01 Friction velocity uk : 0.92553E-02 0.24249E+01 Dimensionless distance yplus : 0.89009E-02 0.23843E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 4.178906553e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.30103E+08 1 0.24168E-09 0.10487E+03 0.37017E+04 c Velocity[X] 0.64225E+02 c Velocity[Y] 0.40641E+02 c Velocity[Z] 0.81608E-06 c Pressure 0.67555E-02 485 0.54164E-04 0.30481E-01 0.31696E+07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -38.668 51.494 5.5963 7.9861 v Velocity[Y] -38.509 42.093 -0.25706 -0.33901 v Velocity[Z] -3.2912 3.214 1.9635e-06 -5.3962e-08 v ǁVelocityǁ 0.0010396 51.913 9.6407 8.3707 v Pressure -7.7822e+05 6.6677e+05 -1.7507e+05 -1.6861e+05 v TurbVisc 1.8046e-18 0.034755 0.00025109 0.00013602 v CourantNb 4.4616e-08 0.01214 0.0001766 5.0162e-06 v FourierNb 1.2492e-07 0.061845 0.00016355 1.0612e-06 v total_pressure -6.769e+05 7.681e+05 -73746 -67288 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3843 0.14251 0.0036896 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0346e-06 0.063224 0.00034016 6.0774e-06 INSTANT 0.877119000E-01 TIME STEP NUMBER 57317 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282779975E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.843864424E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.67193E-02 0.24257E+01 Friction velocity uk : 0.67193E-02 0.24257E+01 Dimensionless distance yplus : 0.64620E-02 0.23851E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Incoming flow detained for 20 outlet faces on 2100 Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 4.271243986e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.30109E+08 1 0.24720E-09 0.10019E+03 0.36179E+04 c Velocity[X] 0.58484E+02 c Velocity[Y] 0.41704E+02 c Velocity[Z] 0.81626E-06 c Pressure 0.68534E-02 516 0.59315E-04 0.31955E-01 0.29619E+07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -38.68 51.504 5.5964 7.9862 v Velocity[Y] -38.518 42.105 -0.25721 -0.33932 v Velocity[Z] -3.2915 3.2141 1.9631e-06 -5.3962e-08 v ǁVelocityǁ 0.0010102 51.923 9.6421 8.3711 v Pressure -7.8561e+05 2.4972e+05 -1.803e+05 -2.1565e+05 v TurbVisc 1.8123e-18 0.034767 0.00025116 0.00013609 v CourantNb 4.4649e-08 0.012142 0.00017662 5.0165e-06 v FourierNb 1.2492e-07 0.061863 0.00016358 1.0617e-06 v total_pressure -6.8428e+05 3.5105e+05 -78970 -1.1433e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3851 0.14257 0.0036909 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0355e-06 0.063245 0.0003402 6.0781e-06 INSTANT 0.877120000E-01 TIME STEP NUMBER 57318 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282790292E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.843940202E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.21760E-02 0.24265E+01 Friction velocity uk : 0.21760E-02 0.24265E+01 Dimensionless distance yplus : 0.20927E-02 0.23859E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 4.331074841e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.30108E+08 1 0.24250E-09 0.10814E+03 0.37584E+04 c Velocity[X] 0.66494E+02 c Velocity[Y] 0.41649E+02 c Velocity[Z] 0.81600E-06 c Pressure 0.69603E-02 467 0.57933E-04 0.31348E-01 0.33201E+07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -38.692 51.514 5.5964 7.9863 v Velocity[Y] -38.527 42.116 -0.2574 -0.34006 v Velocity[Z] -3.2918 3.2142 1.9626e-06 -5.3962e-08 v ǁVelocityǁ 0.00098281 51.933 9.6435 8.3716 v Pressure -7.773e+05 6.8823e+05 -1.7271e+05 -1.6618e+05 v TurbVisc 1.82e-18 0.03478 0.00025122 0.00013628 v CourantNb 4.6401e-08 0.012143 0.00017663 5.0165e-06 v FourierNb 1.2492e-07 0.061881 0.00016361 1.0629e-06 v total_pressure -6.7598e+05 7.8956e+05 -71380 -64856 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3859 0.14262 0.0036922 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.036e-06 0.063267 0.00034025 6.0795e-06 INSTANT 0.877121000E-01 TIME STEP NUMBER 57319 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282788077E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.844310410E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.16828E-02 0.24273E+01 Friction velocity uk : 0.16828E-02 0.24273E+01 Dimensionless distance yplus : 0.16184E-02 0.23868E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Incoming flow detained for 20 outlet faces on 2100 Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 4.385363633e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.30114E+08 1 0.24825E-09 0.10330E+03 0.36728E+04 c Velocity[X] 0.60493E+02 c Velocity[Y] 0.42805E+02 c Velocity[Z] 0.82621E-06 c Pressure 0.70624E-02 434 0.61434E-04 0.32868E-01 0.31122E+07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -38.704 51.524 5.5965 7.9863 v Velocity[Y] -38.536 42.128 -0.25755 -0.34037 v Velocity[Z] -3.292 3.2142 1.9622e-06 -5.3963e-08 v ǁVelocityǁ 0.00095779 51.943 9.6449 8.372 v Pressure -7.8517e+05 2.4892e+05 -1.7829e+05 -2.1568e+05 v TurbVisc 1.8276e-18 0.034792 0.00025129 0.00013635 v CourantNb 4.9523e-08 0.012144 0.00017665 5.0168e-06 v FourierNb 1.2492e-07 0.0619 0.00016364 1.0634e-06 v total_pressure -6.8384e+05 3.5024e+05 -76969 -1.1435e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3868 0.14268 0.0036935 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0368e-06 0.06329 0.00034029 6.0802e-06 INSTANT 0.877122000E-01 TIME STEP NUMBER 57320 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282798925E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.844393943E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.36423E-02 0.24282E+01 Friction velocity uk : 0.36423E-02 0.24282E+01 Dimensionless distance yplus : 0.35029E-02 0.23876E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 4.406302762e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.30113E+08 1 0.24337E-09 0.11165E+03 0.38181E+04 c Velocity[X] 0.68924E+02 c Velocity[Y] 0.42728E+02 c Velocity[Z] 0.83316E-06 c Pressure 0.71691E-02 501 0.60756E-04 0.32229E-01 0.34956E+07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -38.716 51.534 5.5965 7.9864 v Velocity[Y] -38.545 42.139 -0.25774 -0.34112 v Velocity[Z] -3.2923 3.2143 1.9618e-06 -5.3963e-08 v ǁVelocityǁ 0.00093565 51.953 9.6463 8.3725 v Pressure -7.7654e+05 7.101e+05 -1.7044e+05 -1.6383e+05 v TurbVisc 1.8352e-18 0.034804 0.00025135 0.00013654 v CourantNb 5.249e-08 0.012146 0.00017667 5.0168e-06 v FourierNb 1.2492e-07 0.06192 0.00016367 1.0647e-06 v total_pressure -6.7522e+05 8.1143e+05 -69114 -62507 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3876 0.14273 0.0036948 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0373e-06 0.063313 0.00034034 6.0815e-06 INSTANT 0.877123000E-01 TIME STEP NUMBER 57321 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282796592E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.844785510E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.62230E-02 0.24290E+01 Friction velocity uk : 0.62230E-02 0.24290E+01 Dimensionless distance yplus : 0.59847E-02 0.23884E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Incoming flow detained for 20 outlet faces on 2100 Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 4.423574487e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.30119E+08 1 0.24933E-09 0.10657E+03 0.37298E+04 c Velocity[X] 0.62606E+02 c Velocity[Y] 0.43964E+02 c Velocity[Z] 0.83342E-06 c Pressure 0.72718E-02 336 0.64198E-04 0.33780E-01 0.32601E+07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -38.728 51.544 5.5966 7.9864 v Velocity[Y] -38.555 42.15 -0.25788 -0.34141 v Velocity[Z] -3.2926 3.2144 1.9613e-06 -5.3963e-08 v ǁVelocityǁ 0.00091693 51.964 9.6478 8.373 v Pressure -7.8488e+05 2.4822e+05 -1.7641e+05 -2.158e+05 v TurbVisc 1.8427e-18 0.034816 0.00025142 0.00013661 v CourantNb 4.9365e-08 0.012147 0.00017668 5.0171e-06 v FourierNb 1.2492e-07 0.061941 0.0001637 1.0652e-06 v total_pressure -6.8356e+05 3.4954e+05 -75084 -1.1447e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3884 0.14279 0.0036962 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0381e-06 0.063337 0.00034038 6.0823e-06 INSTANT 0.877124000E-01 TIME STEP NUMBER 57322 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282807950E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.844875569E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.89908E-02 0.24298E+01 Friction velocity uk : 0.89908E-02 0.24298E+01 Dimensionless distance yplus : 0.86466E-02 0.23892E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 4.408293233e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.30119E+08 1 0.24426E-09 0.11534E+03 0.38798E+04 c Velocity[X] 0.71471E+02 c Velocity[Y] 0.43867E+02 c Velocity[Z] 0.83044E-06 c Pressure 0.73792E-02 366 0.63336E-04 0.33113E-01 0.36717E+07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -38.74 51.553 5.5967 7.9865 v Velocity[Y] -38.564 42.162 -0.25807 -0.34217 v Velocity[Z] -3.2928 3.2145 1.9609e-06 -5.3963e-08 v ǁVelocityǁ 0.00089525 51.974 9.6491 8.3735 v Pressure -7.7594e+05 7.3212e+05 -1.6829e+05 -1.6156e+05 v TurbVisc 1.8501e-18 0.034828 0.00025149 0.0001368 v CourantNb 4.6275e-08 0.012148 0.0001767 5.0172e-06 v FourierNb 1.2492e-07 0.061962 0.00016373 1.0665e-06 v total_pressure -6.7461e+05 8.3344e+05 -66963 -60232 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3892 0.14284 0.0036975 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0386e-06 0.063362 0.00034043 6.0836e-06 INSTANT 0.877125000E-01 TIME STEP NUMBER 57323 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282805497E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.845288224E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11162E-01 0.24307E+01 Friction velocity uk : 0.11162E-01 0.24307E+01 Dimensionless distance yplus : 0.10734E-01 0.23900E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Incoming flow detained for 20 outlet faces on 2100 Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 4.392418523e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.30125E+08 1 0.25043E-09 0.11001E+03 0.37888E+04 c Velocity[X] 0.64829E+02 c Velocity[Y] 0.45184E+02 c Velocity[Z] 0.84276E-06 c Pressure 0.74819E-02 452 0.67100E-04 0.34691E-01 0.34068E+07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -38.753 51.564 5.5967 7.9865 v Velocity[Y] -38.573 42.173 -0.25821 -0.34245 v Velocity[Z] -3.2931 3.2145 1.9605e-06 -5.3963e-08 v ǁVelocityǁ 0.0008403 51.984 9.6506 8.3739 v Pressure -7.8476e+05 2.476e+05 -1.7464e+05 -2.1599e+05 v TurbVisc 1.8573e-18 0.03484 0.00025155 0.00013687 v CourantNb 4.473e-08 0.01215 0.00017671 5.0174e-06 v FourierNb 1.2493e-07 0.061984 0.00016376 1.067e-06 v total_pressure -6.8343e+05 3.4892e+05 -73315 -1.1466e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.39 0.1429 0.0036988 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0395e-06 0.063388 0.00034047 6.0844e-06 INSTANT 0.877126000E-01 TIME STEP NUMBER 57324 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282817363E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.845384323E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.23406E-02 0.24315E+01 Friction velocity uk : 0.23406E-02 0.24315E+01 Dimensionless distance yplus : 0.22592E-02 0.23908E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 4.346181841e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.30124E+08 1 0.24518E-09 0.11920E+03 0.39434E+04 c Velocity[X] 0.74134E+02 c Velocity[Y] 0.45067E+02 c Velocity[Z] 0.84048E-06 c Pressure 0.75897E-02 409 0.66285E-04 0.33995E-01 0.38474E+07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -38.765 51.573 5.5968 7.9867 v Velocity[Y] -38.582 42.185 -0.2584 -0.34321 v Velocity[Z] -3.2933 3.2146 1.9601e-06 -5.3963e-08 v ǁVelocityǁ 0.00081351 51.994 9.652 8.3744 v Pressure -7.7549e+05 7.5428e+05 -1.6626e+05 -1.5937e+05 v TurbVisc 1.8644e-18 0.034852 0.00025162 0.00013706 v CourantNb 4.5054e-08 0.012151 0.00017673 5.0175e-06 v FourierNb 1.2493e-07 0.062007 0.00016379 1.0682e-06 v total_pressure -6.7416e+05 8.556e+05 -64935 -58042 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3908 0.14295 0.0037001 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0399e-06 0.063414 0.00034052 6.0857e-06 INSTANT 0.877127000E-01 TIME STEP NUMBER 57325 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282814775E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.845817615E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.85780E-02 0.24323E+01 Friction velocity uk : 0.85780E-02 0.24323E+01 Dimensionless distance yplus : 0.82797E-02 0.23917E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Incoming flow detained for 20 outlet faces on 2100 Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 4.303774125e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.30130E+08 1 0.25156E-09 0.11363E+03 0.38498E+04 c Velocity[X] 0.67166E+02 c Velocity[Y] 0.46463E+02 c Velocity[Z] 0.84568E-06 c Pressure 0.76927E-02 445 0.69940E-04 0.35602E-01 0.35524E+07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -38.778 51.584 5.5968 7.9867 v Velocity[Y] -38.592 42.196 -0.25854 -0.34348 v Velocity[Z] -3.2936 3.2147 1.9596e-06 -5.3963e-08 v ǁVelocityǁ 0.00081353 52.005 9.6534 8.3748 v Pressure -7.8478e+05 2.4704e+05 -1.7299e+05 -2.1625e+05 v TurbVisc 1.8714e-18 0.034864 0.00025168 0.00013713 v CourantNb 4.5378e-08 0.012152 0.00017674 5.0177e-06 v FourierNb 1.2493e-07 0.06203 0.00016382 1.0688e-06 v total_pressure -6.8345e+05 3.4837e+05 -71664 -1.1492e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3917 0.14301 0.0037015 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0408e-06 0.063441 0.00034056 6.0865e-06 INSTANT 0.877128000E-01 TIME STEP NUMBER 57326 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282827146E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.845919660E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.14910E-01 0.24332E+01 Friction velocity uk : 0.14910E-01 0.24332E+01 Dimensionless distance yplus : 0.14391E-01 0.23925E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 4.234063259e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.30129E+08 1 0.24613E-09 0.12324E+03 0.40088E+04 c Velocity[X] 0.76912E+02 c Velocity[Y] 0.46326E+02 c Velocity[Z] 0.84750E-06 c Pressure 0.78014E-02 369 0.68914E-04 0.34878E-01 0.40229E+07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -38.79 51.594 5.5969 7.9868 v Velocity[Y] -38.601 42.208 -0.25873 -0.34426 v Velocity[Z] -3.2939 3.2148 1.9592e-06 -5.3963e-08 v ǁVelocityǁ 0.00081412 52.015 9.6548 8.3753 v Pressure -7.752e+05 7.7657e+05 -1.6435e+05 -1.5725e+05 v TurbVisc 1.8552e-18 0.034877 0.00025175 0.00013732 v CourantNb 4.5699e-08 0.012153 0.00017676 5.0178e-06 v FourierNb 1.2493e-07 0.062054 0.00016385 1.07e-06 v total_pressure -6.7387e+05 8.779e+05 -63028 -55925 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3925 0.14306 0.0037029 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0413e-06 0.063469 0.00034061 6.0878e-06 INSTANT 0.877129000E-01 TIME STEP NUMBER 57327 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282824412E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.846372797E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.17746E-01 0.24340E+01 Friction velocity uk : 0.17746E-01 0.24340E+01 Dimensionless distance yplus : 0.17067E-01 0.23933E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Incoming flow detained for 20 outlet faces on 2100 Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 4.172257443e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.30136E+08 1 0.25271E-09 0.11742E+03 0.39126E+04 c Velocity[X] 0.69616E+02 c Velocity[Y] 0.47802E+02 c Velocity[Z] 0.86035E-06 c Pressure 0.79047E-02 390 0.72928E-04 0.36515E-01 0.36968E+07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -38.802 51.604 5.597 7.9868 v Velocity[Y] -38.611 42.22 -0.25887 -0.34452 v Velocity[Z] -3.2941 3.2149 1.9588e-06 -5.3963e-08 v ǁVelocityǁ 0.00084641 52.026 9.6562 8.3758 v Pressure -7.8497e+05 2.4655e+05 -1.7147e+05 -2.1661e+05 v TurbVisc 1.6688e-18 0.034889 0.00025181 0.0001374 v CourantNb 4.602e-08 0.012155 0.00017678 5.0181e-06 v FourierNb 1.2493e-07 0.06208 0.00016388 1.0705e-06 v total_pressure -6.8364e+05 3.4788e+05 -70148 -1.1529e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3933 0.14312 0.0037043 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0421e-06 0.063498 0.00034066 6.0886e-06 INSTANT 0.877130000E-01 TIME STEP NUMBER 57328 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282837267E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.846480192E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.19148E-01 0.24348E+01 Friction velocity uk : 0.19148E-01 0.24348E+01 Dimensionless distance yplus : 0.18415E-01 0.23941E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 4.085544484e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.30135E+08 1 0.24709E-09 0.12745E+03 0.40759E+04 c Velocity[X] 0.79805E+02 c Velocity[Y] 0.47647E+02 c Velocity[Z] 0.84971E-06 c Pressure 0.80137E-02 459 0.71707E-04 0.35761E-01 0.41982E+07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -38.815 51.614 5.597 7.987 v Velocity[Y] -38.62 42.231 -0.25905 -0.3453 v Velocity[Z] -3.2944 3.2149 1.9583e-06 -5.3963e-08 v ǁVelocityǁ 0.00089139 52.036 9.6576 8.3763 v Pressure -7.7506e+05 7.99e+05 -1.6258e+05 -1.5522e+05 v TurbVisc 1.495e-18 0.034901 0.00025188 0.00013758 v CourantNb 4.6337e-08 0.012156 0.00017679 5.0181e-06 v FourierNb 1.2493e-07 0.062106 0.00016391 1.0718e-06 v total_pressure -6.7373e+05 9.0032e+05 -61254 -53895 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3941 0.14317 0.0037057 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0426e-06 0.063528 0.0003407 6.0899e-06 INSTANT 0.877131000E-01 TIME STEP NUMBER 57329 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282834375E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.846953454E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.20488E-01 0.24357E+01 Friction velocity uk : 0.20488E-01 0.24357E+01 Dimensionless distance yplus : 0.19704E-01 0.23950E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Incoming flow detained for 20 outlet faces on 2100 Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 4.010702749e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.30141E+08 1 0.25389E-09 0.12138E+03 0.39773E+04 c Velocity[X] 0.72180E+02 c Velocity[Y] 0.49202E+02 c Velocity[Z] 0.84852E-06 c Pressure 0.81173E-02 389 0.75459E-04 0.37427E-01 0.38398E+07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -38.827 51.625 5.5971 7.987 v Velocity[Y] -38.63 42.243 -0.25919 -0.34555 v Velocity[Z] -3.2947 3.215 1.9579e-06 -5.3963e-08 v ǁVelocityǁ 0.00090246 52.048 9.659 8.3767 v Pressure -7.853e+05 2.4612e+05 -1.7008e+05 -2.1705e+05 v TurbVisc 1.3332e-18 0.034913 0.00025195 0.00013766 v CourantNb 4.6653e-08 0.012157 0.00017681 5.0184e-06 v FourierNb 1.2493e-07 0.062132 0.00016394 1.0723e-06 v total_pressure -6.8397e+05 3.4744e+05 -68758 -1.1572e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.395 0.14323 0.003707 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0434e-06 0.063558 0.00034075 6.0907e-06 INSTANT 0.877132000E-01 TIME STEP NUMBER 57330 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282847718E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.847066085E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.17851E-01 0.24365E+01 Friction velocity uk : 0.17851E-01 0.24365E+01 Dimensionless distance yplus : 0.17370E-01 0.23958E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 3.913654531e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.30140E+08 1 0.24809E-09 0.13184E+03 0.41447E+04 c Velocity[X] 0.82814E+02 c Velocity[Y] 0.49027E+02 c Velocity[Z] 0.85423E-06 c Pressure 0.82272E-02 409 0.74412E-04 0.36646E-01 0.43730E+07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -38.84 51.635 5.5971 7.9871 v Velocity[Y] -38.64 42.255 -0.25938 -0.34635 v Velocity[Z] -3.2949 3.2151 1.9575e-06 -5.3964e-08 v ǁVelocityǁ 0.00091946 52.058 9.6604 8.3772 v Pressure -7.7506e+05 8.2155e+05 -1.6093e+05 -1.5326e+05 v TurbVisc 1.1835e-18 0.034925 0.00025202 0.00013784 v CourantNb 4.6966e-08 0.012159 0.00017682 5.0185e-06 v FourierNb 1.2493e-07 0.06216 0.00016397 1.0736e-06 v total_pressure -6.7374e+05 9.2287e+05 -59607 -51937 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3958 0.14328 0.0037084 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0439e-06 0.063589 0.0003408 6.092e-06 INSTANT 0.877133000E-01 TIME STEP NUMBER 57331 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282844661E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.847558536E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.14565E-01 0.24373E+01 Friction velocity uk : 0.14565E-01 0.24373E+01 Dimensionless distance yplus : 0.14173E-01 0.23966E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Incoming flow detained for 20 outlet faces on 2100 Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 3.832760576e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.30147E+08 1 0.25510E-09 0.12552E+03 0.40437E+04 c Velocity[X] 0.74858E+02 c Velocity[Y] 0.50663E+02 c Velocity[Z] 0.88746E-06 c Pressure 0.83310E-02 331 0.78583E-04 0.38341E-01 0.39814E+07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -38.852 51.646 5.5972 7.9872 v Velocity[Y] -38.65 42.267 -0.25951 -0.34658 v Velocity[Z] -3.2952 3.2152 1.957e-06 -5.3964e-08 v ǁVelocityǁ 0.00094216 52.069 9.6619 8.3777 v Pressure -7.8577e+05 2.4573e+05 -1.6883e+05 -2.1759e+05 v TurbVisc 1.0457e-18 0.034937 0.00025208 0.00013792 v CourantNb 4.7276e-08 0.01216 0.00017684 5.0187e-06 v FourierNb 1.2493e-07 0.062188 0.000164 1.0741e-06 v total_pressure -6.8445e+05 3.4706e+05 -67510 -1.1626e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3966 0.14333 0.0037097 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0448e-06 0.063621 0.00034084 6.0928e-06 INSTANT 0.877134000E-01 TIME STEP NUMBER 57332 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282858470E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.847675427E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10624E-01 0.24382E+01 Friction velocity uk : 0.10624E-01 0.24382E+01 Dimensionless distance yplus : 0.10338E-01 0.23974E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 3.732217480e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.30146E+08 1 0.24911E-09 0.13641E+03 0.42149E+04 c Velocity[X] 0.85937E+02 c Velocity[Y] 0.50469E+02 c Velocity[Z] 0.88025E-06 c Pressure 0.84410E-02 384 0.77289E-04 0.37529E-01 0.45476E+07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -38.865 51.656 5.5972 7.9873 v Velocity[Y] -38.659 42.278 -0.2597 -0.34739 v Velocity[Z] -3.2955 3.2152 1.9566e-06 -5.3964e-08 v ǁVelocityǁ 0.00097026 52.079 9.6632 8.3782 v Pressure -7.752e+05 8.4421e+05 -1.5942e+05 -1.5138e+05 v TurbVisc 9.1922e-19 0.034949 0.00025215 0.0001381 v CourantNb 4.7584e-08 0.012161 0.00017686 5.0188e-06 v FourierNb 1.2493e-07 0.062217 0.00016403 1.0753e-06 v total_pressure -6.7388e+05 9.4554e+05 -58096 -50053 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3974 0.14338 0.003711 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0452e-06 0.063653 0.00034089 6.0941e-06 INSTANT 0.877135000E-01 TIME STEP NUMBER 57333 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282855246E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.848186902E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.72554E-02 0.24390E+01 Friction velocity uk : 0.72554E-02 0.24390E+01 Dimensionless distance yplus : 0.70599E-02 0.23982E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Incoming flow detained for 20 outlet faces on 2100 Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 3.651824086e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.30152E+08 1 0.25633E-09 0.12983E+03 0.41117E+04 c Velocity[X] 0.77650E+02 c Velocity[Y] 0.52182E+02 c Velocity[Z] 0.88904E-06 c Pressure 0.85452E-02 383 0.81359E-04 0.39253E-01 0.41216E+07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -38.878 51.667 5.5973 7.9873 v Velocity[Y] -38.669 42.291 -0.25984 -0.34761 v Velocity[Z] -3.2957 3.2153 1.9562e-06 -5.3964e-08 v ǁVelocityǁ 0.0010033 52.091 9.6647 8.3786 v Pressure -7.8639e+05 2.454e+05 -1.6773e+05 -2.1822e+05 v TurbVisc 8.0341e-19 0.034961 0.00025222 0.00013818 v CourantNb 4.7889e-08 0.012163 0.00017687 5.0191e-06 v FourierNb 1.2493e-07 0.062247 0.00016406 1.0759e-06 v total_pressure -6.8506e+05 3.4672e+05 -66401 -1.1689e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3982 0.14343 0.0037123 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0461e-06 0.063686 0.00034093 6.095e-06 INSTANT 0.877136000E-01 TIME STEP NUMBER 57334 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282869508E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.848307338E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.28873E-02 0.24398E+01 Friction velocity uk : 0.28873E-02 0.24398E+01 Dimensionless distance yplus : 0.28095E-02 0.23990E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 3.554452766e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.30151E+08 1 0.25015E-09 0.14115E+03 0.42867E+04 c Velocity[X] 0.89177E+02 c Velocity[Y] 0.51970E+02 c Velocity[Z] 0.86722E-06 c Pressure 0.86557E-02 352 0.79946E-04 0.38412E-01 0.47209E+07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -38.89 51.677 5.5973 7.9875 v Velocity[Y] -38.679 42.302 -0.26003 -0.34843 v Velocity[Z] -3.296 3.2154 1.9558e-06 -5.3964e-08 v ǁVelocityǁ 0.0010408 52.101 9.6661 8.3792 v Pressure -7.7548e+05 8.67e+05 -1.5805e+05 -1.496e+05 v TurbVisc 6.9821e-19 0.034973 0.00025229 0.00013836 v CourantNb 4.819e-08 0.012164 0.00017689 5.0191e-06 v FourierNb 1.2493e-07 0.062277 0.00016409 1.0771e-06 v total_pressure -6.7415e+05 9.6832e+05 -56729 -48272 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.399 0.14348 0.0037136 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0465e-06 0.06372 0.00034098 6.0962e-06 INSTANT 0.877137000E-01 TIME STEP NUMBER 57335 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282866098E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.848837275E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.53428E-02 0.24406E+01 Friction velocity uk : 0.53428E-02 0.24406E+01 Dimensionless distance yplus : 0.51989E-02 0.23998E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Incoming flow detained for 20 outlet faces on 2100 Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 3.481109029e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.30158E+08 1 0.25759E-09 0.13432E+03 0.41813E+04 c Velocity[X] 0.80558E+02 c Velocity[Y] 0.53762E+02 c Velocity[Z] 0.87352E-06 c Pressure 0.87603E-02 516 0.83897E-04 0.40165E-01 0.42597E+07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -38.903 51.688 5.5974 7.9875 v Velocity[Y] -38.689 42.315 -0.26016 -0.34864 v Velocity[Z] -3.2962 3.2155 1.9553e-06 -5.3964e-08 v ǁVelocityǁ 0.0010823 52.113 9.6675 8.3796 v Pressure -7.8712e+05 2.4511e+05 -1.6675e+05 -2.1891e+05 v TurbVisc 6.0325e-19 0.034985 0.00025235 0.00013844 v CourantNb 4.849e-08 0.012165 0.0001769 5.0194e-06 v FourierNb 1.2493e-07 0.062308 0.00016412 1.0777e-06 v total_pressure -6.8579e+05 3.4643e+05 -65426 -1.1759e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.3998 0.14353 0.0037149 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0474e-06 0.063755 0.00034103 6.0971e-06 INSTANT 0.877138000E-01 TIME STEP NUMBER 57336 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282880820E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.848961014E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.46541E-02 0.24415E+01 Friction velocity uk : 0.46541E-02 0.24415E+01 Dimensionless distance yplus : 0.45287E-02 0.24007E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 3.392976530e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.30157E+08 1 0.25122E-09 0.14606E+03 0.43598E+04 c Velocity[X] 0.92533E+02 c Velocity[Y] 0.53532E+02 c Velocity[Z] 0.87901E-06 c Pressure 0.88712E-02 473 0.82615E-04 0.39295E-01 0.48917E+07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -38.916 51.698 5.5974 7.9876 v Velocity[Y] -38.698 42.326 -0.26035 -0.34947 v Velocity[Z] -3.2965 3.2155 1.9549e-06 -5.3964e-08 v ǁVelocityǁ 0.0011272 52.123 9.6689 8.3801 v Pressure -7.7588e+05 8.899e+05 -1.5684e+05 -1.4794e+05 v TurbVisc 5.1795e-19 0.034997 0.00025242 0.00013862 v CourantNb 4.8786e-08 0.012167 0.00017692 5.0195e-06 v FourierNb 1.2493e-07 0.06234 0.00016416 1.0789e-06 v total_pressure -6.7456e+05 9.9122e+05 -55519 -46615 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.4007 0.14357 0.0037162 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0478e-06 0.06379 0.00034107 6.0984e-06 INSTANT 0.877139000E-01 TIME STEP NUMBER 57337 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282877200E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.849508302E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.37073E-02 0.24423E+01 Friction velocity uk : 0.37073E-02 0.24423E+01 Dimensionless distance yplus : 0.36074E-02 0.24015E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Incoming flow detained for 20 outlet faces on 2100 Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 3.332475591e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.30164E+08 1 0.25887E-09 0.13898E+03 0.42523E+04 c Velocity[X] 0.83582E+02 c Velocity[Y] 0.55400E+02 c Velocity[Z] 0.88427E-06 c Pressure 0.89757E-02 638 0.86878E-04 0.41076E-01 0.43956E+07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -38.929 51.71 5.5975 7.9877 v Velocity[Y] -38.709 42.339 -0.26049 -0.34967 v Velocity[Z] -3.2968 3.2156 1.9545e-06 -5.3964e-08 v ǁVelocityǁ 0.001175 52.135 9.6703 8.3806 v Pressure -7.8797e+05 2.4486e+05 -1.6592e+05 -2.1969e+05 v TurbVisc 4.419e-19 0.035009 0.00025249 0.00013871 v CourantNb 4.9079e-08 0.012168 0.00017693 5.0198e-06 v FourierNb 1.2494e-07 0.062372 0.00016419 1.0795e-06 v total_pressure -6.8665e+05 3.4618e+05 -64596 -1.1837e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.4015 0.14363 0.0037175 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0487e-06 0.063826 0.00034112 6.0992e-06 INSTANT 0.877140000E-01 TIME STEP NUMBER 57338 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282892359E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.849635449E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.86901E-02 0.24431E+01 Friction velocity uk : 0.86901E-02 0.24431E+01 Dimensionless distance yplus : 0.84561E-02 0.24023E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 3.258808333e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.30162E+08 1 0.25232E-09 0.15116E+03 0.44342E+04 c Velocity[X] 0.96005E+02 c Velocity[Y] 0.55155E+02 c Velocity[Z] 0.89283E-06 c Pressure 0.90873E-02 551 0.85180E-04 0.40177E-01 0.50622E+07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -38.941 51.72 5.5975 7.9878 v Velocity[Y] -38.718 42.35 -0.26068 -0.3505 v Velocity[Z] -3.297 3.2157 1.954e-06 -5.3964e-08 v ǁVelocityǁ 0.0012252 52.145 9.6717 8.3811 v Pressure -7.7639e+05 9.1291e+05 -1.5577e+05 -1.4634e+05 v TurbVisc 3.7451e-19 0.035021 0.00025256 0.00013888 v CourantNb 4.937e-08 0.01217 0.00017695 5.0198e-06 v FourierNb 1.2494e-07 0.062405 0.00016422 1.0807e-06 v total_pressure -6.7507e+05 1.0142e+06 -54448 -45016 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.4023 0.1437 0.0037188 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0492e-06 0.063862 0.00034117 6.1005e-06 INSTANT 0.877141000E-01 TIME STEP NUMBER 57339 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282888535E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.850199357E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12553E-01 0.24439E+01 Friction velocity uk : 0.12553E-01 0.24439E+01 Dimensionless distance yplus : 0.12215E-01 0.24031E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Incoming flow detained for 20 outlet faces on 2100 Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 3.215675516e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.30169E+08 1 0.26018E-09 0.14382E+03 0.43248E+04 c Velocity[X] 0.86719E+02 c Velocity[Y] 0.57098E+02 c Velocity[Z] 0.88363E-06 c Pressure 0.91924E-02 625 0.89662E-04 0.41988E-01 0.45299E+07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -38.955 51.731 5.5976 7.9879 v Velocity[Y] -38.729 42.363 -0.26082 -0.3507 v Velocity[Z] -3.2973 3.2158 1.9536e-06 -5.3964e-08 v ǁVelocityǁ 0.0012774 52.157 9.6732 8.3816 v Pressure -7.8893e+05 2.4465e+05 -1.6523e+05 -2.2053e+05 v TurbVisc 3.1529e-19 0.035033 0.00025263 0.00013897 v CourantNb 5.0411e-08 0.012171 0.00017697 5.0201e-06 v FourierNb 1.2494e-07 0.062438 0.00016425 1.0813e-06 v total_pressure -6.8761e+05 3.4598e+05 -63906 -1.1921e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.4031 0.14376 0.0037202 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0501e-06 0.063898 0.00034122 6.1014e-06 INSTANT 0.877142000E-01 TIME STEP NUMBER 57340 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282904130E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.850328629E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.15216E-01 0.24447E+01 Friction velocity uk : 0.15216E-01 0.24447E+01 Dimensionless distance yplus : 0.14673E-01 0.24039E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 3.160339944e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.30168E+08 1 0.25344E-09 0.15643E+03 0.45099E+04 c Velocity[X] 0.99592E+02 c Velocity[Y] 0.56838E+02 c Velocity[Z] 0.88097E-06 c Pressure 0.93042E-02 585 0.87887E-04 0.41059E-01 0.52293E+07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -38.967 51.742 5.5976 7.988 v Velocity[Y] -38.738 42.375 -0.26101 -0.35154 v Velocity[Z] -3.2976 3.2158 1.9532e-06 -5.3964e-08 v ǁVelocityǁ 0.0013311 52.168 9.6746 8.3821 v Pressure -7.7702e+05 9.3603e+05 -1.5487e+05 -1.4488e+05 v TurbVisc 2.6378e-19 0.035045 0.0002527 0.00013915 v CourantNb 5.01e-08 0.012173 0.00017698 5.0201e-06 v FourierNb 1.2494e-07 0.062472 0.00016428 1.0825e-06 v total_pressure -6.7569e+05 1.0374e+06 -53541 -43554 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.4039 0.14382 0.0037215 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0505e-06 0.063936 0.00034126 6.1026e-06 INSTANT 0.877143000E-01 TIME STEP NUMBER 57341 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282900069E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.850907779E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.16192E-01 0.24455E+01 Friction velocity uk : 0.16192E-01 0.24455E+01 Dimensionless distance yplus : 0.15614E-01 0.24047E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Incoming flow detained for 20 outlet faces on 2100 Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 3.138379039e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.30175E+08 1 0.26151E-09 0.14883E+03 0.43986E+04 c Velocity[X] 0.89975E+02 c Velocity[Y] 0.58858E+02 c Velocity[Z] 0.90195E-06 c Pressure 0.94095E-02 584 0.92329E-04 0.42899E-01 0.46618E+07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -38.98 51.753 5.5977 7.9881 v Velocity[Y] -38.749 42.387 -0.26115 -0.35173 v Velocity[Z] -3.2978 3.2159 1.9528e-06 -5.3965e-08 v ǁVelocityǁ 0.0013859 52.179 9.676 8.3825 v Pressure -7.9002e+05 2.4447e+05 -1.6473e+05 -2.2158e+05 v TurbVisc 2.1946e-19 0.035057 0.00025276 0.00013923 v CourantNb 4.7162e-08 0.012174 0.000177 5.0205e-06 v FourierNb 1.2494e-07 0.062506 0.00016431 1.083e-06 v total_pressure -6.8869e+05 3.458e+05 -63404 -1.2026e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.4047 0.14388 0.0037229 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0514e-06 0.063973 0.00034131 6.1035e-06 INSTANT 0.877144000E-01 TIME STEP NUMBER 57342 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282916062E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.851039071E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.17192E-01 0.24463E+01 Friction velocity uk : 0.17192E-01 0.24463E+01 Dimensionless distance yplus : 0.16578E-01 0.24054E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 3.104582254e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.30173E+08 1 0.25459E-09 0.16188E+03 0.45868E+04 c Velocity[X] 0.10330E+03 c Velocity[Y] 0.58582E+02 c Velocity[Z] 0.88592E-06 c Pressure 0.95218E-02 574 0.90623E-04 0.41941E-01 0.53998E+07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -38.993 51.764 5.5977 7.9882 v Velocity[Y] -38.759 42.399 -0.26135 -0.35258 v Velocity[Z] -3.2981 3.216 1.9523e-06 -5.3965e-08 v ǁVelocityǁ 0.0014415 52.19 9.6774 8.3831 v Pressure -7.7773e+05 9.5924e+05 -1.5408e+05 -1.434e+05 v TurbVisc 1.8168e-19 0.03507 0.00025283 0.00013941 v CourantNb 4.422e-08 0.012175 0.00017701 5.0205e-06 v FourierNb 1.2494e-07 0.06254 0.00016434 1.0843e-06 v total_pressure -6.764e+05 1.0606e+06 -52752 -42071 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.4054 0.14394 0.0037242 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0518e-06 0.064011 0.00034136 6.1047e-06 INSTANT 0.877145000E-01 TIME STEP NUMBER 57343 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282911779E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.851635355E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.18168E-01 0.24471E+01 Friction velocity uk : 0.18168E-01 0.24471E+01 Dimensionless distance yplus : 0.17520E-01 0.24062E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Incoming flow detained for 20 outlet faces on 2100 Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 3.105183407e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.30181E+08 1 0.26287E-09 0.15402E+03 0.44737E+04 c Velocity[X] 0.93345E+02 c Velocity[Y] 0.60675E+02 c Velocity[Z] 0.89471E-06 c Pressure 0.96273E-02 669 0.95143E-04 0.43809E-01 0.47929E+07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -39.006 51.775 5.5978 7.9883 v Velocity[Y] -38.769 42.412 -0.26148 -0.35275 v Velocity[Z] -3.2983 3.2161 1.9519e-06 -5.3965e-08 v ǁVelocityǁ 0.0014975 52.202 9.6789 8.3835 v Pressure -7.9118e+05 2.4433e+05 -1.6436e+05 -2.2264e+05 v TurbVisc 1.4997e-19 0.035082 0.0002529 0.00013949 v CourantNb 4.126e-08 0.012177 0.00017703 5.0208e-06 v FourierNb 1.2494e-07 0.062575 0.00016437 1.0848e-06 v total_pressure -6.8986e+05 3.4566e+05 -63030 -1.2132e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.4062 0.144 0.0037255 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0527e-06 0.064049 0.0003414 6.1056e-06 INSTANT 0.877146000E-01 TIME STEP NUMBER 57344 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282928179E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.851766209E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.16993E-01 0.24479E+01 Friction velocity uk : 0.16993E-01 0.24479E+01 Dimensionless distance yplus : 0.16509E-01 0.24070E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 3.094313647e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.30179E+08 1 0.25576E-09 0.16750E+03 0.46648E+04 c Velocity[X] 0.10712E+03 c Velocity[Y] 0.60387E+02 c Velocity[Z] 0.89481E-06 c Pressure 0.97401E-02 575 0.93365E-04 0.42823E-01 0.55655E+07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -39.019 51.786 5.5978 7.9884 v Velocity[Y] -38.779 42.424 -0.26168 -0.35362 v Velocity[Z] -3.2986 3.2162 1.9515e-06 -5.3965e-08 v ǁVelocityǁ 0.0015537 52.213 9.6803 8.3841 v Pressure -7.7853e+05 9.8257e+05 -1.5347e+05 -1.4208e+05 v TurbVisc 1.2373e-19 0.035094 0.00025297 0.00013967 v CourantNb 3.8291e-08 0.012179 0.00017705 5.0208e-06 v FourierNb 1.2494e-07 0.06261 0.00016441 1.086e-06 v total_pressure -6.7721e+05 1.0839e+06 -52143 -40755 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.407 0.14406 0.0037268 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0531e-06 0.064087 0.00034145 6.1069e-06 INSTANT 0.877147000E-01 TIME STEP NUMBER 57345 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282923649E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.852376672E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.14937E-01 0.24487E+01 Friction velocity uk : 0.14937E-01 0.24487E+01 Dimensionless distance yplus : 0.14512E-01 0.24078E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Incoming flow detained for 20 outlet faces on 2100 Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 3.119706719e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.30187E+08 1 0.26425E-09 0.15939E+03 0.45499E+04 c Velocity[X] 0.96832E+02 c Velocity[Y] 0.62553E+02 c Velocity[Z] 0.90379E-06 c Pressure 0.98459E-02 478 0.97904E-04 0.44719E-01 0.49210E+07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -39.033 51.798 5.5979 7.9884 v Velocity[Y] -38.79 42.436 -0.26182 -0.35378 v Velocity[Z] -3.2989 3.2162 1.9511e-06 -5.3965e-08 v ǁVelocityǁ 0.0016098 52.225 9.6817 8.3845 v Pressure -7.9244e+05 2.4422e+05 -1.6415e+05 -2.2384e+05 v TurbVisc 1.0246e-19 0.035106 0.00025304 0.00013976 v CourantNb 3.5299e-08 0.01218 0.00017706 5.0212e-06 v FourierNb 1.2494e-07 0.062645 0.00016444 1.0866e-06 v total_pressure -6.9112e+05 3.4554e+05 -62827 -1.2251e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.4078 0.14412 0.0037281 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0541e-06 0.064126 0.0003415 6.1078e-06 INSTANT 0.877148000E-01 TIME STEP NUMBER 57346 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282940423E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.852507473E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.12737E-01 0.24495E+01 Friction velocity uk : 0.12737E-01 0.24495E+01 Dimensionless distance yplus : 0.12375E-01 0.24086E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 3.133354305e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.30185E+08 1 0.25695E-09 0.17330E+03 0.47439E+04 c Velocity[X] 0.11105E+03 c Velocity[Y] 0.62253E+02 c Velocity[Z] 0.91356E-06 c Pressure 0.99591E-02 452 0.96009E-04 0.43703E-01 0.57317E+07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -39.045 51.808 5.5979 7.9886 v Velocity[Y] -38.799 42.448 -0.26202 -0.35466 v Velocity[Z] -3.2991 3.2163 1.9506e-06 -5.3965e-08 v ǁVelocityǁ 0.0016657 52.236 9.6831 8.3851 v Pressure -7.7942e+05 1.006e+06 -1.5299e+05 -1.4079e+05 v TurbVisc 8.5588e-20 0.035117 0.00025311 0.00013993 v CourantNb 3.2292e-08 0.012182 0.00017708 5.0212e-06 v FourierNb 1.2494e-07 0.062681 0.00016447 1.0878e-06 v total_pressure -6.781e+05 1.1073e+06 -51669 -39462 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.4086 0.14418 0.0037294 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0544e-06 0.064165 0.00034155 6.109e-06 INSTANT 0.877149000E-01 TIME STEP NUMBER 57347 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282935637E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.853132393E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10117E-01 0.24503E+01 Friction velocity uk : 0.10117E-01 0.24503E+01 Dimensionless distance yplus : 0.98289E-02 0.24094E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Incoming flow detained for 20 outlet faces on 2100 Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 3.183741344e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.30193E+08 1 0.26566E-09 0.16558E+03 0.46366E+04 c Velocity[X] 0.10075E+03 c Velocity[Y] 0.64837E+02 c Velocity[Z] 0.91265E-06 c Pressure 0.10065E-01 486 0.98569E-04 0.45628E-01 0.50455E+07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -39.059 51.82 5.598 7.9886 v Velocity[Y] -38.81 42.461 -0.26216 -0.35481 v Velocity[Z] -3.2994 3.2164 1.9502e-06 -5.3965e-08 v ǁVelocityǁ 0.001721 52.248 9.6846 8.3855 v Pressure -7.9363e+05 2.4428e+05 -1.6407e+05 -2.2481e+05 v TurbVisc 7.266e-20 0.035129 0.00025318 0.00014002 v CourantNb 3.1383e-08 0.012184 0.00017709 5.0215e-06 v FourierNb 1.2494e-07 0.062716 0.0001645 1.0884e-06 v total_pressure -6.923e+05 3.4561e+05 -62745 -1.2349e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.4094 0.14423 0.0037307 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0554e-06 0.064204 0.00034159 6.1099e-06 INSTANT 0.877150000E-01 TIME STEP NUMBER 57348 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282952605E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.853260915E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.69094E-02 0.24511E+01 Friction velocity uk : 0.69094E-02 0.24511E+01 Dimensionless distance yplus : 0.67129E-02 0.24102E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 3.221449947e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.30191E+08 1 0.25825E-09 0.18025E+03 0.48370E+04 c Velocity[X] 0.11571E+03 c Velocity[Y] 0.64537E+02 c Velocity[Z] 0.91237E-06 c Pressure 0.10183E-01 662 0.63636E-04 0.44603E-01 0.58508E+07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -39.072 51.831 5.5981 7.9888 v Velocity[Y] -38.82 42.473 -0.26237 -0.3557 v Velocity[Z] -3.2996 3.2165 1.9498e-06 -5.3965e-08 v ǁVelocityǁ 0.0017757 52.259 9.686 8.3861 v Pressure -7.8064e+05 1.0329e+06 -1.5278e+05 -1.4048e+05 v TurbVisc 6.3222e-20 0.035141 0.00025325 0.0001402 v CourantNb 3.1404e-08 0.012186 0.00017711 5.0215e-06 v FourierNb 1.2494e-07 0.062752 0.00016453 1.0896e-06 v total_pressure -6.7932e+05 1.1342e+06 -51451 -39158 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.4102 0.14429 0.003732 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0558e-06 0.064243 0.00034164 6.1112e-06 INSTANT 0.877151000E-01 TIME STEP NUMBER 57349 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282947739E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.853897167E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.41250E-02 0.24519E+01 Friction velocity uk : 0.41250E-02 0.24519E+01 Dimensionless distance yplus : 0.40077E-02 0.24109E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Incoming flow detained for 20 outlet faces on 2100 Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 3.292778643e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.30199E+08 1 0.26714E-09 0.17115E+03 0.47128E+04 c Velocity[X] 0.10440E+03 c Velocity[Y] 0.66747E+02 c Velocity[Z] 0.91947E-06 c Pressure 0.10281E-01 560 0.62007E-04 0.46516E-01 0.51229E+07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -39.085 51.843 5.5981 7.9888 v Velocity[Y] -38.831 42.486 -0.2625 -0.35585 v Velocity[Z] -3.2999 3.2165 1.9493e-06 -5.3965e-08 v ǁVelocityǁ 0.0018295 52.271 9.6874 8.3866 v Pressure -7.9499e+05 2.4449e+05 -1.6414e+05 -2.2554e+05 v TurbVisc 5.6911e-20 0.035153 0.00025332 0.00014028 v CourantNb 3.1425e-08 0.012188 0.00017713 5.0219e-06 v FourierNb 1.2494e-07 0.062788 0.00016457 1.0902e-06 v total_pressure -6.9366e+05 3.4582e+05 -62814 -1.2422e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.4109 0.14435 0.0037333 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0567e-06 0.064282 0.00034169 6.1121e-06 INSTANT 0.877152000E-01 TIME STEP NUMBER 57350 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282965274E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.854026642E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.27838E-02 0.24527E+01 Friction velocity uk : 0.27838E-02 0.24527E+01 Dimensionless distance yplus : 0.27046E-02 0.24117E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 3.352561823e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.30196E+08 1 0.25939E-09 0.18610E+03 0.49138E+04 c Velocity[X] 0.11973E+03 c Velocity[Y] 0.66368E+02 c Velocity[Z] 0.91870E-06 c Pressure 0.10396E-01 583 0.56040E-04 0.45449E-01 0.59684E+07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -39.098 51.853 5.5982 7.989 v Velocity[Y] -38.841 42.498 -0.26271 -0.35675 v Velocity[Z] -3.3002 3.2166 1.9489e-06 -5.3965e-08 v ǁVelocityǁ 0.0018825 52.282 9.6889 8.3871 v Pressure -7.8163e+05 1.0557e+06 -1.5262e+05 -1.3951e+05 v TurbVisc 5.3456e-20 0.035165 0.00025339 0.00014046 v CourantNb 3.1449e-08 0.01219 0.00017714 5.0219e-06 v FourierNb 1.2494e-07 0.062823 0.0001646 1.0914e-06 v total_pressure -6.8031e+05 1.1571e+06 -51298 -38182 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.4117 0.1444 0.0037346 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0571e-06 0.064322 0.00034174 6.1133e-06 INSTANT 0.877153000E-01 TIME STEP NUMBER 57351 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282959857E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.854676297E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.27927E-02 0.24535E+01 Friction velocity uk : 0.27927E-02 0.24535E+01 Dimensionless distance yplus : 0.27133E-02 0.24125E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Incoming flow detained for 20 outlet faces on 2100 Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 3.449068963e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.30205E+08 1 0.26857E-09 0.17715E+03 0.47937E+04 c Velocity[X] 0.10831E+03 c Velocity[Y] 0.68840E+02 c Velocity[Z] 0.95885E-06 c Pressure 0.10504E-01 512 0.59611E-04 0.47434E-01 0.52359E+07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -39.112 51.865 5.5983 7.989 v Velocity[Y] -38.852 42.511 -0.26285 -0.35688 v Velocity[Z] -3.3004 3.2167 1.9485e-06 -5.3966e-08 v ǁVelocityǁ 0.0019343 52.294 9.6903 8.3876 v Pressure -7.9646e+05 2.4446e+05 -1.6441e+05 -2.27e+05 v TurbVisc 5.2684e-20 0.035177 0.00025346 0.00014055 v CourantNb 3.1474e-08 0.012192 0.00017716 5.0222e-06 v FourierNb 1.2494e-07 0.062859 0.00016463 1.092e-06 v total_pressure -6.9513e+05 3.4578e+05 -63085 -1.2568e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.4125 0.14446 0.0037359 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0581e-06 0.064361 0.00034179 6.1143e-06 INSTANT 0.877154000E-01 TIME STEP NUMBER 57352 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282977750E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.854800382E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.38380E-02 0.24543E+01 Friction velocity uk : 0.38380E-02 0.24543E+01 Dimensionless distance yplus : 0.37289E-02 0.24133E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 3.530962129e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.30202E+08 1 0.26068E-09 0.19248E+03 0.49962E+04 c Velocity[X] 0.12405E+03 c Velocity[Y] 0.68431E+02 c Velocity[Z] 0.94829E-06 c Pressure 0.10617E-01 575 0.58216E-04 0.46329E-01 0.61255E+07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -39.125 51.876 5.5983 7.9892 v Velocity[Y] -38.862 42.523 -0.26306 -0.35779 v Velocity[Z] -3.3007 3.2168 1.9481e-06 -5.3966e-08 v ǁVelocityǁ 0.0019567 52.305 9.6917 8.3881 v Pressure -7.8275e+05 1.0795e+06 -1.5265e+05 -1.3858e+05 v TurbVisc 5.457e-20 0.035189 0.00025353 0.00014072 v CourantNb 3.2839e-08 0.012194 0.00017717 5.0222e-06 v FourierNb 1.2495e-07 0.062895 0.00016466 1.0932e-06 v total_pressure -6.8142e+05 1.1808e+06 -51325 -37255 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.4133 0.14452 0.0037372 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0584e-06 0.0644 0.00034184 6.1155e-06 INSTANT 0.877155000E-01 TIME STEP NUMBER 57353 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282972043E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.855461259E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.93833E-02 0.24551E+01 Friction velocity uk : 0.93833E-02 0.24551E+01 Dimensionless distance yplus : 0.91165E-02 0.24141E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Incoming flow detained for 20 outlet faces on 2100 Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 3.646525286e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.30211E+08 1 0.27004E-09 0.18327E+03 0.48747E+04 c Velocity[X] 0.11229E+03 c Velocity[Y] 0.70977E+02 c Velocity[Z] 0.93689E-06 c Pressure 0.10725E-01 692 0.61028E-04 0.48341E-01 0.53540E+07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -39.138 51.888 5.5984 7.9892 v Velocity[Y] -38.873 42.536 -0.2632 -0.35791 v Velocity[Z] -3.3009 3.2168 1.9476e-06 -5.3966e-08 v ǁVelocityǁ 0.0019256 52.318 9.6932 8.3886 v Pressure -7.9799e+05 2.4445e+05 -1.6483e+05 -2.2851e+05 v TurbVisc 5.9188e-20 0.035201 0.0002536 0.00014081 v CourantNb 3.6064e-08 0.012196 0.00017719 5.0226e-06 v FourierNb 1.2495e-07 0.062931 0.0001647 1.0938e-06 v total_pressure -6.9667e+05 3.4577e+05 -63507 -1.2719e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.4141 0.14458 0.0037385 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0594e-06 0.06444 0.00034189 6.1164e-06 INSTANT 0.877156000E-01 TIME STEP NUMBER 57354 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282990283E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.855581893E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.80954E-02 0.24559E+01 Friction velocity uk : 0.80954E-02 0.24559E+01 Dimensionless distance yplus : 0.78652E-02 0.24148E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 3.744356588e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.30208E+08 1 0.26198E-09 0.19903E+03 0.50794E+04 c Velocity[X] 0.12848E+03 c Velocity[Y] 0.70554E+02 c Velocity[Z] 0.92164E-06 c Pressure 0.10839E-01 604 0.59943E-04 0.47209E-01 0.62796E+07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -39.151 51.899 5.5984 7.9894 v Velocity[Y] -38.883 42.548 -0.26341 -0.35884 v Velocity[Z] -3.3012 3.2169 1.9472e-06 -5.3966e-08 v ǁVelocityǁ 0.0018178 52.329 9.6946 8.3892 v Pressure -7.8391e+05 1.1033e+06 -1.5283e+05 -1.3773e+05 v TurbVisc 6.6767e-20 0.035213 0.00025368 0.00014099 v CourantNb 3.337e-08 0.012198 0.00017721 5.0226e-06 v FourierNb 1.2495e-07 0.062967 0.00016473 1.095e-06 v total_pressure -6.8259e+05 1.2047e+06 -51506 -36402 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.4148 0.14463 0.0037398 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0598e-06 0.064479 0.00034194 6.1176e-06 INSTANT 0.877157000E-01 TIME STEP NUMBER 57355 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282984237E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.856253025E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.11223E-01 0.24567E+01 Friction velocity uk : 0.11223E-01 0.24567E+01 Dimensionless distance yplus : 0.10904E-01 0.24156E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Incoming flow detained for 20 outlet faces on 2100 Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 3.875178861e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.30217E+08 1 0.27155E-09 0.18956E+03 0.49567E+04 c Velocity[X] 0.11639E+03 c Velocity[Y] 0.73172E+02 c Velocity[Z] 0.93987E-06 c Pressure 0.10947E-01 420 0.62564E-04 0.49247E-01 0.54696E+07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -39.165 51.911 5.5985 7.9894 v Velocity[Y] -38.894 42.562 -0.26355 -0.35895 v Velocity[Z] -3.3015 3.217 1.9468e-06 -5.3966e-08 v ǁVelocityǁ 0.0017894 52.341 9.6961 8.3896 v Pressure -7.9959e+05 2.4446e+05 -1.6542e+05 -2.3015e+05 v TurbVisc 7.7605e-20 0.035225 0.00025374 0.00014108 v CourantNb 3.0742e-08 0.0122 0.00017722 5.0229e-06 v FourierNb 1.2495e-07 0.063003 0.00016476 1.0956e-06 v total_pressure -6.9827e+05 3.4579e+05 -64099 -1.2882e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.4156 0.14469 0.003741 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0607e-06 0.064519 0.00034199 6.1186e-06 INSTANT 0.877158000E-01 TIME STEP NUMBER 57356 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.283002795E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.856367812E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.14504E-01 0.24575E+01 Friction velocity uk : 0.14504E-01 0.24575E+01 Dimensionless distance yplus : 0.14092E-01 0.24164E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 3.985018129e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.30214E+08 1 0.26330E-09 0.20577E+03 0.51637E+04 c Velocity[X] 0.13304E+03 c Velocity[Y] 0.72739E+02 c Velocity[Z] 0.93492E-06 c Pressure 0.11062E-01 610 0.61170E-04 0.48087E-01 0.64326E+07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -39.178 51.922 5.5985 7.9896 v Velocity[Y] -38.904 42.574 -0.26377 -0.35988 v Velocity[Z] -3.3017 3.2171 1.9464e-06 -5.3966e-08 v ǁVelocityǁ 0.0018224 52.352 9.6975 8.3902 v Pressure -7.8514e+05 1.1273e+06 -1.5317e+05 -1.3695e+05 v TurbVisc 9.2127e-20 0.035237 0.00025382 0.00014125 v CourantNb 3.0758e-08 0.012201 0.00017724 5.023e-06 v FourierNb 1.2495e-07 0.063039 0.0001648 1.0968e-06 v total_pressure -6.8381e+05 1.2286e+06 -51849 -35629 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.4164 0.14474 0.0037422 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0611e-06 0.064558 0.00034204 6.1198e-06 INSTANT 0.877159000E-01 TIME STEP NUMBER 57357 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Inlet 2 2480 -0.282868800E+02 Smooth wall 5 12240 0.215563268E-19 Rough wall 6 0 0.000000000E+00 Symmetry 4 5500 0.000000000E+00 Free outlet 3 2100 0.282996430E+02 Free inlet 14 0 0.000000000E+00 Convective inlet 16 0 0.000000000E+00 Free surface 15 0 0.000000000E+00 Sat/Sat coupling 13 20160 -0.857048610E-02 Undefined 1 0 0.000000000E+00 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.25883E-02 0.24583E+01 Friction velocity uk : 0.25883E-02 0.24583E+01 Dimensionless distance yplus : 0.25003E-02 0.24172E+01 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 12240 Total number of wall faces : 12240 ------------------------------------------------------------ Incoming flow detained for 20 outlet faces on 2100 Turbomachinery characteristics: Flowrate [m3/s] Head [m] Power [W] Efficiency [1] 2.380000000e-01 -nan 4.126133708e-02 -nan ** INFORMATION ON CONVERGENCE -------------------------- ---------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ---------------------------------------------------------------------------- c Velocity 0.30223E+08 1 0.27308E-09 0.19604E+03 0.50396E+04 c Velocity[X] 0.12061E+03 c Velocity[Y] 0.75427E+02 c Velocity[Z] 0.95267E-06 c Pressure 0.11169E-01 665 0.64087E-04 0.50152E-01 0.55834E+07 ---------------------------------------------------------------------------- ** Computed fields on cells ------------------------ field minimum maximum set mean spatial mean - -------------- -------------- -------------- -------------- -------------- v Velocity[X] -39.192 51.934 5.5986 7.9896 v Velocity[Y] -38.915 42.587 -0.26391 -0.35999 v Velocity[Z] -3.302 3.2171 1.9459e-06 -5.3966e-08 v ǁVelocityǁ 0.0017852 52.365 9.699 8.3906 v Pressure -8.1777e+05 2.4449e+05 -1.6617e+05 -2.3186e+05 v TurbVisc 1.1078e-19 0.035249 0.00025389 0.00014134 v CourantNb 3.0778e-08 0.012203 0.00017726 5.0233e-06 v FourierNb 1.2495e-07 0.063075 0.00016483 1.0974e-06 v total_pressure -7.1644e+05 3.4582e+05 -64845 -1.3053e+05 ** Computed fields on boundary_faces --------------------------------- field minimum maximum set mean spatial mean - ----- -------------- -------------- -------------- -------------- v Yplus 0 2.4172 0.14479 0.0037433 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean --------------- -------------- -------------- -------------- -------------- Courant/Fourier 1.0621e-06 0.064598 0.00034209 6.1208e-06 INSTANT 0.877160000E-01 TIME STEP NUMBER 57358 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------