The Jenkins Controller is preparing for shutdown. No new builds can be started.
Skipping 599 KB.. Full LogRestart file name: restart_flow_pyCAPS_SU2_aflr2.dat. ------------- Config File Boundary Information ( Zone 0 ) --------------- +-----------------------------------------------------------------------+ | Marker Type| Marker Name| +-----------------------------------------------------------------------+ | Euler wall| BC_5| | | BC_2| +-----------------------------------------------------------------------+ | Inlet boundary| BC_4| +-----------------------------------------------------------------------+ | Outlet boundary| BC_3| +-----------------------------------------------------------------------+ -------------------- Output Preprocessing ( Zone 0 ) -------------------- WARNING: SURFACE_PRESSURE_DROP can only be computed for at least 2 surfaces (outlet, inlet, ...) Screen output fields: TIME_ITER, OUTER_ITER, INNER_ITER, CUR_TIME, TIME_STEP, WALL_TIME, RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_ENERGY, EFFICIENCY History output group(s): ITER, TIME_DOMAIN, WALL_TIME, RMS_RES, AERO_COEFF Convergence field(s): RMS_DENSITY Warning: No (valid) fields chosen for time convergence monitoring. Time convergence monitoring inactive. Volume output fields: COORDINATES, SOLUTION, PRIMITIVE ------------------- Geometry Preprocessing ( Zone 0 ) ------------------- Two dimensional problem. 3715 grid points. 7206 volume elements. 4 surface markers. 98 boundary elements in index 0 (Marker = BC_2). 24 boundary elements in index 1 (Marker = BC_3). 24 boundary elements in index 2 (Marker = BC_4). 78 boundary elements in index 3 (Marker = BC_5). 7206 triangles. Setting point connectivity. Renumbering points (Reverse Cuthill McKee Ordering). Recomputing point connectivity. Setting element connectivity. Checking the numerical grid orientation. There has been a re-orientation of 7206 TRIANGLE volume elements. There has been a re-orientation of 73 LINE surface elements. Identifying edges and vertices. Setting the control volume structure. Area of the computational grid: 999.917. Searching for the closest normal neighbors to the surfaces. Storing a mapping from global to local point index. Compute the surface curvature. Max K: 177.06. Mean K: 1.97231. Standard deviation K: 13.0434. Checking for periodicity. Computing mesh quality statistics for the dual control volumes. +--------------------------------------------------------------+ | Mesh Quality Metric| Minimum| Maximum| +--------------------------------------------------------------+ | Orthogonality Angle (deg.)| 63.4343| 90| | CV Face Area Aspect Ratio| 1| 5.23543| | CV Sub-Volume Ratio| 1| 3.11804| +--------------------------------------------------------------+ Setting the multigrid structure. +-------------------------------------------+ | MG Level| CVs|Aggl. Rate| CFL| +-------------------------------------------+ | 0| 3715| 1/1.00| 10| | 1| 1048| 1/3.54| 7.96696| | 2| 298| 1/3.52| 6.37252| +-------------------------------------------+ Finding max control volume width. Wetted area = 2.06136 m. Area projection in the x-plane = 0.178383 m, y-plane = 0.994925 m. Max. coordinate in the x-direction = 1 m, y-direction = 0.138389 m. Min. coordinate in the x-direction = -0.000250564 m, y-direction = -0.0151999 m. Checking if Euler & Symmetry markers are straight/plane: Boundary marker BC_5 is NOT a single straight. Boundary marker BC_2 is NOT a single straight. Computing wall distances. -------------------- Solver Preprocessing ( Zone 0 ) -------------------- Inviscid flow: Computing density based on free-stream temperature and pressure using the ideal gas law. Force coefficients computed using free-stream values. -- Models: +------------------------------------------------------------------------------+ | Viscosity Model| Conductivity Model| Fluid Model| +------------------------------------------------------------------------------+ | -| -| STANDARD_AIR| +------------------------------------------------------------------------------+ -- Fluid properties: +------------------------------------------------------------------------------+ | Name| Dim. value| Ref. value| Unit|Non-dim. value| +------------------------------------------------------------------------------+ | Gas Constant| 287.058| 1| N.m/kg.K| 287.058| | Spec. Heat Ratio| -| -| -| 1.4| +------------------------------------------------------------------------------+ -- Initial and free-stream conditions: +------------------------------------------------------------------------------+ | Name| Dim. value| Ref. value| Unit|Non-dim. value| +------------------------------------------------------------------------------+ | Static Pressure| 101325| 1| Pa| 101325| | Density| 1.22498| 1| kg/m^3| 1.22498| | Temperature| 288.15| 1| K| 288.15| | Total Energy| 216054| 1| m^2/s^2| 216054| | Velocity-X| 136.119| 1| m/s| 136.119| | Velocity-Y| 0| 1| m/s| 0| | Velocity Magnitude| 136.119| 1| m/s| 136.119| +------------------------------------------------------------------------------+ | Mach Number| -| -| -| 0.4| +------------------------------------------------------------------------------+ Initialize Jacobian structure (Euler). MG level: 0. Initialize Jacobian structure (Euler). MG level: 1. Initialize Jacobian structure (Euler). MG level: 2. ------------------- Numerics Preprocessing ( Zone 0 ) ------------------- ----------------- Integration Preprocessing ( Zone 0 ) ------------------ ------------------- Iteration Preprocessing ( Zone 0 ) ------------------ Euler/Navier-Stokes/RANS fluid iteration. ------------------------------ Begin Solver ----------------------------- Simulation Run using the Single-zone Driver WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better, see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better, see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better, see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations +----------------------------------------------------------------------------------------------------------------------------------------------+ | Time_Iter| Outer_Iter| Inner_Iter| Cur_Time| Time_Step| Time(sec)| rms[Rho]| rms[RhoU]| rms[RhoV]| rms[RhoE]| CEff| +----------------------------------------------------------------------------------------------------------------------------------------------+ | 0| 0| 0| 0.0000e+00| 0.0000e+00| 3.0693e-02| -0.385358| 2.453598| 1.625650| 5.369499| 0.360138| | 0| 0| 1| 0.0000e+00| 0.0000e+00| 2.9247e-02| -0.512634| 2.087781| 1.374671| 4.973554| 1.183036| | 0| 0| 2| 0.0000e+00| 0.0000e+00| 2.7141e-02| -0.792582| 1.733529| 1.142729| 4.657622| 3.896320| | 0| 0| 3| 0.0000e+00| 0.0000e+00| 2.6609e-02| -0.880738| 1.486539| 1.023158| 4.334759| 14.592265| | 0| 0| 4| 0.0000e+00| 0.0000e+00| 2.9356e-02| -0.987528| 1.351478| 0.932491| 4.191092| 111.166022| | 0| 0| 5| 0.0000e+00| 0.0000e+00| 3.1298e-02| -1.104038| 1.188715| 0.874764| 3.951825| -483.924340| | 0| 0| 6| 0.0000e+00| 0.0000e+00| 3.0717e-02| -1.178622| 1.124587| 0.844310| 3.820426| 127.331200| | 0| 0| 7| 0.0000e+00| 0.0000e+00| 3.0254e-02| -1.243517| 1.097463| 0.824869| 3.768858| 40.162273| | 0| 0| 8| 0.0000e+00| 0.0000e+00| 3.0584e-02| -1.287932| 1.075843| 0.810639| 3.733440| 25.154653| | 0| 0| 9| 0.0000e+00| 0.0000e+00| 3.0229e-02| -1.300689| 1.046363| 0.775886| 3.684245| 21.097801| ----------------------------- Solver Exit ------------------------------- Maximum number of iterations reached (ITER = 10) before convergence. +-----------------------------------------------------------------------+ | Convergence Field | Value | Criterion | Converged | +-----------------------------------------------------------------------+ | rms[Rho]| -1.30069| < -14| No| +-----------------------------------------------------------------------+ ------------------------------------------------------------------------- +-----------------------------------------------------------------------+ | File Writing Summary | Filename | +-----------------------------------------------------------------------+ |SU2 binary restart |restart_flow_pyCAPS_SU2_aflr2.dat | Writing the forces breakdown file (forces_breakdown_pyCAPS_SU2_aflr2.dat). |CSV file |surface_flow_pyCAPS_SU2_aflr2.csv | Writing the forces breakdown file (forces_breakdown_pyCAPS_SU2_aflr2.dat). |Tecplot binary |flow_pyCAPS_SU2_aflr2.szplt | Writing the forces breakdown file (forces_breakdown_pyCAPS_SU2_aflr2.dat). |Tecplot binary surface |surface_flow_pyCAPS_SU2_aflr2.szplt| Error in tecFileWriterClose: Not all node map values for zone 1 have been written. Currently need 352 more values.0: Error finishing Tecplot file output. Writing the forces breakdown file (forces_breakdown_pyCAPS_SU2_aflr2.dat). +-----------------------------------------------------------------------+ ------------------------- Solver Postprocessing ------------------------- Deleted CNumerics container. Deleted CIntegration container. Deleted CSolver container. Deleted CIteration container. Deleted CInterface container. Deleted CGeometry container. Deleted CFreeFormDefBox class. Deleted CSurfaceMovement class. Deleted CVolumetricMovement class. Deleted CConfig container. Deleted nInst container. Deleted COutput class. ------------------------------------------------------------------------- ------------------------- Exit Success (SU2_CFD) ------------------------ Total Force - Pressure + Viscous Cl = 0.650457 Cd = 0.030831 Cmz = 0.373226 Cx = 0.030831 Cy = 0.650457 Pressure Contribution Cl_p = 0.650457 Cd_p = 0.030831 Cmz_p = 0.373226 Cx_p = 0.030831 Cy_p = 0.650457 Viscous Contribution Cl_v = 0.0 Cd_v = 0.0 Cmz_v = 0.0 Cx_v = 0.0 Cy_v = 0.0 real 0m2.905s user 0m1.878s sys 0m0.418s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case su2_and_AFLR2_NodeDist_PyTest.py passed (as expected) ================================================= ================================================= + echo 'su2_and_AFLR2_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/CFD/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/pyCAPSlog.txt su2_and_AFLR2_PyTest.py test; + python -u su2_and_AFLR2_PyTest.py -outLevel=0 + tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/CFD/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/pyCAPSlog.txt Saving geometry Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 5 Name = 2DSlice, index = 1 Name = TunnelWall, index = 2 Name = OutFlow, index = 3 Name = InFlow, index = 4 Name = Airfoil, index = 5 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = TunnelWall, index = 1 Name = OutFlow, index = 2 Name = InFlow, index = 3 Name = Airfoil, index = 4 Getting mesh sizing parameters Mesh sizing name - 2DSlice Mesh sizing name - Airfoil Mesh sizing name - InFlow Mesh sizing name - OutFlow Mesh sizing name - TunnelWall Done getting mesh sizing parameters Getting 2D mesh for body 1 (of 1) AFLR2 : --------------------------------------- AFLR2 : AFLR2 LIBRARY AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR2 : TRIA/QUAD GRID GENERATOR AFLR2 : Version Number 9.14.7 AFLR2 : Version Date 07/16/23 @ 01:42PM AFLR2 : Compile OS Darwin 22.5.0 arm64 AFLR2 : Compile Date 07/16/23 @ 01:42PM AFLR2 : Copyright 1994-2021, D.L. Marcum AFLR2 : --------------------------------------- AFLR2 IC : INPUT DATA CHECK AFLR2 IC : Nodes, Faces = 545 0 AFLR2 : CPU Time = 0.000 seconds AFLR2 EG : EDGE GRID RE-GENERATION AFLR2 EG : Nodes, Edges = 545 545 AFLR2 : CPU Time = 0.000 seconds AFLR2 IG : INITIAL GRID GENERATION AFLR2 IG : Nodes, Faces = 0 2 AFLR2 IG : Nodes, Faces = 110 222 AFLR2 IG : Nodes, Faces = 220 442 AFLR2 IG : Nodes, Faces = 330 662 AFLR2 IG : Nodes, Faces = 440 882 AFLR2 IG : Nodes, Faces = 517 1036 AFLR2 IG : Nodes, Faces = 545 1092 AFLR2 IG : Nodes, Faces = 549 1092 AFLR2 IG : Nodes, Faces = 545 545 AFLR2 : CPU Time = 0.002 seconds AFLR2 GG : FIELD GRID GENERATION AFLR2 GGp: Nodes, Faces = 545 545 AFLR2 GGp: Nodes, Faces = 1083 1621 AFLR2 GGp: Nodes, Faces = 1616 2687 AFLR2 GGp: Nodes, Faces = 2144 3743 AFLR2 GGp: Nodes, Faces = 2661 4777 AFLR2 GGp: Nodes, Faces = 3171 5797 AFLR2 GGp: Nodes, Faces = 3672 6799 AFLR2 GGp: Nodes, Faces = 4158 7771 AFLR2 GGp: Nodes, Faces = 4653 8761 AFLR2 GGp: Nodes, Faces = 5142 9739 AFLR2 GGp: Nodes, Faces = 5608 10671 AFLR2 GGp: Nodes, Faces = 6055 11565 AFLR2 GGp: Nodes, Faces = 6482 12419 AFLR2 GGp: Nodes, Faces = 6880 13215 AFLR2 GGp: Nodes, Faces = 7257 13969 AFLR2 GGp: Nodes, Faces = 7614 14683 AFLR2 GGp: Nodes, Faces = 7947 15349 AFLR2 GGp: Nodes, Faces = 8276 16007 AFLR2 GGp: Nodes, Faces = 8575 16605 AFLR2 GGp: Nodes, Faces = 8869 17193 AFLR2 GGp: Nodes, Faces = 9140 17735 AFLR2 GGp: Nodes, Faces = 9401 18257 AFLR2 GGp: Nodes, Faces = 9654 18763 AFLR2 GGp: Nodes, Faces = 9887 19229 AFLR2 GGp: Nodes, Faces = 10110 19675 AFLR2 GGp: Nodes, Faces = 10315 20085 AFLR2 GGp: Nodes, Faces = 10497 20449 AFLR2 GGp: Nodes, Faces = 10656 20767 AFLR2 GGp: Nodes, Faces = 10791 21037 AFLR2 GGp: Nodes, Faces = 10919 21293 AFLR2 GGp: Nodes, Faces = 11022 21499 AFLR2 GGp: Nodes, Faces = 11092 21639 AFLR2 GGp: Nodes, Faces = 11145 21745 AFLR2 GGp: Nodes, Faces = 11156 21767 AFLR2 : CPU Time = 0.092 seconds AFLR2 QI : QUALITY IMPROVEMENT AFLR2 QI : Nodes, Faces = 11156 21767 AFLR2 QI : Nodes, Faces = 11155 819 AFLR2 QI : Nodes, Faces = 11155 10473 AFLR2 QI : Nodes, Faces = 11155 21765 AFLR2 QI : Nodes, Faces = 11154 811 AFLR2 QI : Nodes, Faces = 11154 10476 AFLR2 QI : Nodes, Faces = 11154 21763 AFLR2 QI : Nodes, Faces = 11154 805 AFLR2 QI : Nodes, Faces = 11154 10479 AFLR2 QI : Nodes, Faces = 11154 21763 AFLR2 QI : Nodes, Faces = 11154 911 AFLR2 QI : Nodes, Faces = 11154 10426 AFLR2 QI : Nodes, Faces = 11154 21763 AFLR2 QI : Nodes, Faces = 11153 915 AFLR2 QI : Nodes, Faces = 11153 10423 AFLR2 QI : Nodes, Faces = 11153 917 AFLR2 QI : Nodes, Faces = 11153 10423 AFLR2 : CPU Time = 0.008 seconds AFLR2 : DONE EGADS Internal: Face 1, Side 11077 11153 complete [but 18248] (EG_makeConnect)! EGADS Internal: Face 1, Side 10985 11077 complete [but 18248] (EG_makeConnect)! EGADS Internal: Face 1, Side 10985 11152 complete [but 18249] (EG_makeConnect)! EGADS Internal: Face 1, Side 11152 11153 complete [but 19022] (EG_makeConnect)! Writing AFLR3 file .... Finished writing AFLR3 file Number of nodes = 11153 Number of elements = 11885 Number of tris = 917 Number of quad = 10423 Writing TECPLOT file: pyCAPS_su2_aflr2.dat .... Finished writing TECPLOT file EGADS Internal: Face 1, Side 11077 11153 complete [but 18248] (EG_makeConnect)! EGADS Internal: Face 1, Side 10985 11077 complete [but 18248] (EG_makeConnect)! EGADS Internal: Face 1, Side 10985 11152 complete [but 18249] (EG_makeConnect)! EGADS Internal: Face 1, Side 11152 11153 complete [but 19022] (EG_makeConnect)! EGADS Internal: Face 1, Side 11077 11153 complete [but 18248] (EG_makeConnect)! EGADS Internal: Face 1, Side 10985 11077 complete [but 18248] (EG_makeConnect)! EGADS Internal: Face 1, Side 10985 11152 complete [but 18249] (EG_makeConnect)! EGADS Internal: Face 1, Side 11152 11153 complete [but 19022] (EG_makeConnect)! Writing SU2 file .... SU2 expects 2D meshes be in the x-y plane... attempting to rotate mesh! Swapping z and y coordinates! Finished writing SU2 file Getting CFD boundary conditions Boundary condition name - Airfoil Boundary condition name - InFlow Boundary condition name - OutFlow Boundary condition name - TunnelWall Done getting CFD boundary conditions Warning: The su2 cfg file will be overwritten! Write SU2 configuration file for version "BlackBird (7.5.1) " Running SU2...... ------------------------------------------------------------------------- | ___ _ _ ___ | | / __| | | |_ ) Release 7.5.1 "Blackbird" | | \__ \ |_| |/ / | | |___/\___//___| Suite (Computational Fluid Dynamics Code) | | | ------------------------------------------------------------------------- | SU2 Project Website: https://su2code.github.io | | | | The SU2 Project is maintained by the SU2 Foundation | | (http://su2foundation.org) | ------------------------------------------------------------------------- | Copyright 2012-2023, SU2 Contributors | | | | SU2 is free software; you can redistribute it and/or | | modify it under the terms of the GNU Lesser General Public | | License as published by the Free Software Foundation; either | | version 2.1 of the License, or (at your option) any later version. | | | | SU2 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 | | Lesser General Public License for more details. | | | | You should have received a copy of the GNU Lesser General Public | | License along with SU2. If not, see <http://www.gnu.org/licenses/>. | ------------------------------------------------------------------------- Parsing config file for zone 0 ----------------- Physical Case Definition ( Zone 0 ) ------------------- Compressible Euler equations. Mach number: 0.4. Angle of attack (AoA): 0 deg, and angle of sideslip (AoS): 0 deg. No restart solution, use the values at infinity (freestream). Dimensional simulation. The reference area is 1 m^2. The semi-span will be computed using the max y(3D) value. The reference length is 1 m. Reference origin for moment evaluation is (0, 0, 0). Surface(s) where the force coefficients are evaluated: BC_5. Surface(s) plotted in the output file: BC_5, BC_2. Input mesh file name: ../aflr2/aflr2.su2 --------------- Space Numerical Integration ( Zone 0 ) ------------------ Roe (with entropy fix = 0.001) solver for the flow inviscid terms. Standard Roe without low-dissipation function. Second order integration in space, with slope limiter. Venkatakrishnan slope-limiting method, with constant: 0.05. The reference element size is: 1. Gradient for upwind reconstruction: inverse-distance weighted Least-Squares. Gradient for viscous and source terms: inverse-distance weighted Least-Squares. --------------- Time Numerical Integration ( Zone 0 ) ------------------ Local time stepping (steady state simulation). Euler implicit method for the flow equations. FGMRES is used for solving the linear system. Using a ILU(0) preconditioning. Convergence criteria of the linear solver: 1e-06. Max number of linear iterations: 10. V Multigrid Cycle, with 2 multigrid levels. Damping factor for the residual restriction: 0.75. Damping factor for the correction prolongation: 0.75. No CFL adaptation. +-------------------------------------------+ | MG Level| Presmooth|PostSmooth|CorrectSmo| +-------------------------------------------+ | 0| 1| 0| 0| | 1| 2| 0| 0| | 2| 3| 0| 0| +-------------------------------------------+ Courant-Friedrichs-Lewy number: 10 ------------------ Convergence Criteria ( Zone 0 ) --------------------- Maximum number of solver subiterations: 10. Begin convergence monitoring at iteration 5. Residual minimum value: 1e-14. Cauchy series min. value: 1e-10. Number of Cauchy elements: 100. Begin windowed time average at iteration 0. -------------------- Output Information ( Zone 0 ) ---------------------- File writing frequency: +------------------------------------+ | File| Frequency| +------------------------------------+ | RESTART| 250| | SURFACE_CSV| 250| | TECPLOT| 250| | SURFACE_TECPLOT| 250| +------------------------------------+ Writing the convergence history file every 1 inner iterations. Writing the screen convergence history every 1 inner iterations. The tabular file format is CSV (.csv). Convergence history file name: history. Forces breakdown file name: forces_breakdown_pyCAPS_su2_aflr2.dat. Surface file name: surface_flow_pyCAPS_su2_aflr2. Volume file name: flow_pyCAPS_su2_aflr2. Restart file name: restart_flow_pyCAPS_su2_aflr2.dat. ------------- Config File Boundary Information ( Zone 0 ) --------------- +-----------------------------------------------------------------------+ | Marker Type| Marker Name| +-----------------------------------------------------------------------+ | Euler wall| BC_5| | | BC_2| +-----------------------------------------------------------------------+ | Inlet boundary| BC_4| +-----------------------------------------------------------------------+ | Outlet boundary| BC_3| +-----------------------------------------------------------------------+ -------------------- Output Preprocessing ( Zone 0 ) -------------------- WARNING: SURFACE_PRESSURE_DROP can only be computed for at least 2 surfaces (outlet, inlet, ...) Screen output fields: TIME_ITER, OUTER_ITER, INNER_ITER, CUR_TIME, TIME_STEP, WALL_TIME, RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_ENERGY, EFFICIENCY History output group(s): ITER, TIME_DOMAIN, WALL_TIME, RMS_RES, AERO_COEFF Convergence field(s): RMS_DENSITY Warning: No (valid) fields chosen for time convergence monitoring. Time convergence monitoring inactive. Volume output fields: COORDINATES, SOLUTION, PRIMITIVE ------------------- Geometry Preprocessing ( Zone 0 ) ------------------- Two dimensional problem. 11153 grid points. 11340 volume elements. 4 surface markers. 98 boundary elements in index 0 (Marker = BC_2). 24 boundary elements in index 1 (Marker = BC_3). 24 boundary elements in index 2 (Marker = BC_4). 399 boundary elements in index 3 (Marker = BC_5). 917 triangles. 10423 quadrilaterals. Setting point connectivity. Renumbering points (Reverse Cuthill McKee Ordering). Recomputing point connectivity. Setting element connectivity. Checking the numerical grid orientation. There has been a re-orientation of 917 TRIANGLE volume elements. There has been a re-orientation of 10423 QUADRILATERAL volume elements. There has been a re-orientation of 73 LINE surface elements. Identifying edges and vertices. Setting the control volume structure. Area of the computational grid: 999.878. Searching for the closest normal neighbors to the surfaces. Storing a mapping from global to local point index. Compute the surface curvature. Max K: 385.665. Mean K: 2.15881. Standard deviation K: 17.7215. Checking for periodicity. Computing mesh quality statistics for the dual control volumes. +--------------------------------------------------------------+ | Mesh Quality Metric| Minimum| Maximum| +--------------------------------------------------------------+ | Orthogonality Angle (deg.)| 49.3184| 90| | CV Face Area Aspect Ratio| 1.00035| 33.4982| | CV Sub-Volume Ratio| 1.00001| 7.89914| +--------------------------------------------------------------+ Setting the multigrid structure. +-------------------------------------------+ | MG Level| CVs|Aggl. Rate| CFL| +-------------------------------------------+ | 0| 11153| 1/1.00| 10| | 1| 2702| 1/4.13| 7.38309| | 2| 549| 1/4.92| 4.99198| +-------------------------------------------+ Finding max control volume width. Wetted area = 2.06265 m. Area projection in the x-plane = 0.211192 m, y-plane = 0.997011 m. Max. coordinate in the x-direction = 1 m, y-direction = 0.102037 m. Min. coordinate in the x-direction = 0.000323229 m, y-direction = -0.108492 m. Checking if Euler & Symmetry markers are straight/plane: Boundary marker BC_5 is NOT a single straight. Boundary marker BC_2 is NOT a single straight. Computing wall distances. -------------------- Solver Preprocessing ( Zone 0 ) -------------------- Inviscid flow: Computing density based on free-stream temperature and pressure using the ideal gas law. Force coefficients computed using free-stream values. -- Models: +------------------------------------------------------------------------------+ | Viscosity Model| Conductivity Model| Fluid Model| +------------------------------------------------------------------------------+ | -| -| STANDARD_AIR| +------------------------------------------------------------------------------+ -- Fluid properties: +------------------------------------------------------------------------------+ | Name| Dim. value| Ref. value| Unit|Non-dim. value| +------------------------------------------------------------------------------+ | Gas Constant| 287.058| 1| N.m/kg.K| 287.058| | Spec. Heat Ratio| -| -| -| 1.4| +------------------------------------------------------------------------------+ -- Initial and free-stream conditions: +------------------------------------------------------------------------------+ | Name| Dim. value| Ref. value| Unit|Non-dim. value| +------------------------------------------------------------------------------+ | Static Pressure| 101325| 1| Pa| 101325| | Density| 1.22498| 1| kg/m^3| 1.22498| | Temperature| 288.15| 1| K| 288.15| | Total Energy| 216054| 1| m^2/s^2| 216054| | Velocity-X| 136.119| 1| m/s| 136.119| | Velocity-Y| 0| 1| m/s| 0| | Velocity Magnitude| 136.119| 1| m/s| 136.119| +------------------------------------------------------------------------------+ | Mach Number| -| -| -| 0.4| +------------------------------------------------------------------------------+ Initialize Jacobian structure (Euler). MG level: 0. Initialize Jacobian structure (Euler). MG level: 1. Initialize Jacobian structure (Euler). MG level: 2. ------------------- Numerics Preprocessing ( Zone 0 ) ------------------- ----------------- Integration Preprocessing ( Zone 0 ) ------------------ ------------------- Iteration Preprocessing ( Zone 0 ) ------------------ Euler/Navier-Stokes/RANS fluid iteration. ------------------------------ Begin Solver ----------------------------- Simulation Run using the Single-zone Driver WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better, see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better, see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better, see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations +----------------------------------------------------------------------------------------------------------------------------------------------+ | Time_Iter| Outer_Iter| Inner_Iter| Cur_Time| Time_Step| Time(sec)| rms[Rho]| rms[RhoU]| rms[RhoV]| rms[RhoE]| CEff| +----------------------------------------------------------------------------------------------------------------------------------------------+ | 0| 0| 0| 0.0000e+00| 0.0000e+00| 7.9688e-02| 0.071067| 2.739763| 1.616077| 5.599701| 0.055267| | 0| 0| 1| 0.0000e+00| 0.0000e+00| 7.9026e-02| -0.447576| 2.193837| 1.571349| 5.070382| 0.046028| | 0| 0| 2| 0.0000e+00| 0.0000e+00| 7.7578e-02| -0.561159| 2.074597| 1.490746| 4.953698| 0.033910| | 0| 0| 3| 0.0000e+00| 0.0000e+00| 7.8062e-02| -0.723326| 1.921155| 1.390756| 4.790278| 0.049695| | 0| 0| 4| 0.0000e+00| 0.0000e+00| 7.8064e-02| -0.876572| 1.825653| 1.275093| 4.637161| 0.133976| | 0| 0| 5| 0.0000e+00| 0.0000e+00| 7.5682e-02| -1.029177| 1.759196| 1.156078| 4.482282| 0.368542| | 0| 0| 6| 0.0000e+00| 0.0000e+00| 7.3483e-02| -1.215334| 1.704909| 1.114966| 4.286060| 0.974759| | 0| 0| 7| 0.0000e+00| 0.0000e+00| 7.1403e-02| -1.329970| 1.644937| 1.145030| 4.116982| 2.716332| | 0| 0| 8| 0.0000e+00| 0.0000e+00| 6.9794e-02| -1.270672| 1.570739| 1.155400| 4.139480| 16.569216| | 0| 0| 9| 0.0000e+00| 0.0000e+00| 6.9870e-02| -1.221243| 1.499646| 1.130319| 4.189559| -6.277653| ----------------------------- Solver Exit ------------------------------- Maximum number of iterations reached (ITER = 10) before convergence. +-----------------------------------------------------------------------+ | Convergence Field | Value | Criterion | Converged | +-----------------------------------------------------------------------+ | rms[Rho]| -1.22124| < -14| No| +-----------------------------------------------------------------------+ ------------------------------------------------------------------------- +-----------------------------------------------------------------------+ | File Writing Summary | Filename | +-----------------------------------------------------------------------+ |SU2 binary restart |restart_flow_pyCAPS_su2_aflr2.dat | Writing the forces breakdown file (forces_breakdown_pyCAPS_su2_aflr2.dat). |CSV file |surface_flow_pyCAPS_su2_aflr2.csv | Writing the forces breakdown file (forces_breakdown_pyCAPS_su2_aflr2.dat). |Tecplot binary |flow_pyCAPS_su2_aflr2.szplt | Writing the forces breakdown file (forces_breakdown_pyCAPS_su2_aflr2.dat). |Tecplot binary surface |surface_flow_pyCAPS_su2_aflr2.szplt| Error in tecFileWriterClose: Not all node map values for zone 1 have been written. Currently need 994 more values.0: Error finishing Tecplot file output. Writing the forces breakdown file (forces_breakdown_pyCAPS_su2_aflr2.dat). +-----------------------------------------------------------------------+ ------------------------- Solver Postprocessing ------------------------- Deleted CNumerics container. Deleted CIntegration container. Deleted CSolver container. Deleted CIteration container. Deleted CInterface container. Deleted CGeometry container. Deleted CFreeFormDefBox class. Deleted CSurfaceMovement class. Deleted CVolumetricMovement class. Deleted CConfig container. Deleted nInst container. Deleted COutput class. ------------------------------------------------------------------------- ------------------------- Exit Success (SU2_CFD) ------------------------ Total Force - Pressure + Viscous Cl = 0.072253 Cd = -0.01151 Cmz = 0.070975 Cx = -0.01151 Cy = 0.072253 Pressure Contribution Cl_p = 0.072253 Cd_p = -0.01151 Cmz_p = 0.070975 Cx_p = -0.01151 Cy_p = 0.072253 Viscous Contribution Cl_v = 0.0 Cd_v = 0.0 Cmz_v = 0.0 Cx_v = 0.0 Cy_v = 0.0 real 0m5.278s user 0m2.872s sys 0m0.612s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case su2_and_AFLR2_PyTest.py passed (as expected) ================================================= ================================================= + tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/CFD/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/pyCAPSlog.txt + echo 'su2_and_AFLR4_AFLR3_PyTest.py test;' su2_and_AFLR4_AFLR3_PyTest.py test; + python -u su2_and_AFLR4_AFLR3_PyTest.py -outLevel=0 + tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/CFD/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/pyCAPSlog.txt Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Wake, index = 3 Name = Farfield, index = 4 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 4 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Wake, index = 3 Name = Farfield, index = 4 AFLR4 : Proximity BG Surface Grid Generation Skipped AFLR4 : No Modifications Required Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Writing TECPLOT file: AFLR4_Mesh.dat .... Finished writing TECPLOT file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 4 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Wake, index = 3 Name = Farfield, index = 4 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Wake, index = 3 Name = Farfield, index = 4 Getting volume mesh AFLR2 : --------------------------------------- AFLR2 : AFLR2 LIBRARY AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR2 : TRIA/QUAD GRID GENERATOR AFLR2 : Version Number 9.14.7 AFLR2 : Version Date 07/16/23 @ 01:42PM AFLR2 : Compile OS Darwin 22.5.0 arm64 AFLR2 : Compile Date 07/16/23 @ 01:42PM AFLR2 : Copyright 1994-2021, D.L. Marcum AFLR2 : --------------------------------------- AFLR4 : --------------------------------------- AFLR4 : AFLR4 LIBRARY AFLR4 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR4 : TRIA/QUAD SURFACE GRID GENERATOR AFLR4 : Version Number 11.5.8 AFLR4 : Version Date 07/24/23 @ 06:11PM AFLR4 : Compile OS Darwin 22.5.0 arm64 AFLR4 : Compile Date 07/24/23 @ 06:11PM AFLR4 : Copyright 1994-2021, D.L. Marcum AFLR4 : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.24 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.24 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- : XYZ DEVIATION > TOLERANCE AT 1 NODES ON EDGE 2 : MAX XYZ DEVIATION 0.0130791 TOLERANCE 0.00207194 AT NODE 14 : INPUT EDGE COORDINATE T 0.997092 : INPUT X,Y,Z COORDINATES 0, 0, 0 : EVALUATED X,Y,Z COORDINATES -0.00349719, 7.71706e-19, 0.0126029 : XYZ DEVIATION > TOLERANCE AT 1 NODES ON EDGE 4 : MAX XYZ DEVIATION 0.0105131 TOLERANCE 0.00180609 AT NODE 39 : INPUT EDGE COORDINATE T 0.995234 : INPUT X,Y,Z COORDINATES 4.56435, 7.90569, 0.137994 : EVALUATED X,Y,Z COORDINATES 4.56765, 7.90569, 0.147977 : XYZ DEVIATION > TOLERANCE AT 13 NODES ON EDGE 5 : MAX XYZ DEVIATION 0.0116919 TOLERANCE 0.00366054 AT NODE 13 : INPUT EDGE COORDINATE T 0.997249 : INPUT X,Y,Z COORDINATES 4.215, -3.14321e-19, -0.00513325 : EVALUATED X,Y,Z COORDINATES 4.2034, -2.2476e-19, -0.00367061 : XYZ DEVIATION > TOLERANCE AT 39 NODES ON EDGE 7 : MAX XYZ DEVIATION 0.0107541 TOLERANCE 6.07701e-05 AT NODE 39 : INPUT EDGE COORDINATE T 0.995118 : INPUT X,Y,Z COORDINATES 6.59956, 7.90569, -0.41192 : EVALUATED X,Y,Z COORDINATES 6.58881, 7.90569, -0.411568 : XYZ DEVIATION > TOLERANCE AT 1 NODES ON EDGE 12 : MAX XYZ DEVIATION 0.010541 TOLERANCE 0.00180944 AT NODE 39 : INPUT EDGE COORDINATE T 0.995222 : INPUT X,Y,Z COORDINATES 4.56435, -7.90569, 0.137994 : EVALUATED X,Y,Z COORDINATES 4.56766, -7.90569, 0.148003 : XYZ DEVIATION > TOLERANCE AT 39 NODES ON EDGE 14 : MAX XYZ DEVIATION 0.0107663 TOLERANCE 6.0313e-05 AT NODE 39 : INPUT EDGE COORDINATE T 0.995113 : INPUT X,Y,Z COORDINATES 6.59956, -7.90569, -0.41192 : EVALUATED X,Y,Z COORDINATES 6.5888, -7.90569, -0.411568 : XYZ DEVIATION > TOLERANCE AT 1 NODES ON EDGE 17 : MAX XYZ DEVIATION 0.0188854 TOLERANCE 0.00360043 AT NODE 5 : INPUT EDGE COORDINATE T 0.989329 : INPUT X,Y,Z COORDINATES 10, 0, 0 : EVALUATED X,Y,Z COORDINATES 9.99962, 1.15617e-18, 0.0188817 : XYZ DEVIATION > TOLERANCE AT 1 NODES ON EDGE 19 : MAX XYZ DEVIATION 0.00275272 TOLERANCE 0.000709873 AT NODE 39 : INPUT EDGE COORDINATE T 0.996882 : INPUT X,Y,Z COORDINATES 11.8257, 3.16228, 0.0551978 : EVALUATED X,Y,Z COORDINATES 11.8266, 3.16228, 0.0578281 : XYZ DEVIATION > TOLERANCE AT 5 NODES ON EDGE 20 : MAX XYZ DEVIATION 0.00942488 TOLERANCE 0.00313697 AT NODE 5 : INPUT EDGE COORDINATE T 0.994455 : INPUT X,Y,Z COORDINATES 11.686, -1.25728e-19, -0.0020533 : EVALUATED X,Y,Z COORDINATES 11.6766, -5.37476e-20, -0.000877765 : XYZ DEVIATION > TOLERANCE AT 38 NODES ON EDGE 22 : MAX XYZ DEVIATION 0.0026872 TOLERANCE 2.48071e-05 AT NODE 38 : INPUT EDGE COORDINATE T 0.99695 : INPUT X,Y,Z COORDINATES 12.6398, 3.16228, -0.164768 : EVALUATED X,Y,Z COORDINATES 12.6371, 3.16228, -0.164681 : XYZ DEVIATION > TOLERANCE AT 1 NODES ON EDGE 27 : MAX XYZ DEVIATION 0.00280378 TOLERANCE 0.000715677 AT NODE 39 : INPUT EDGE COORDINATE T 0.996824 : INPUT X,Y,Z COORDINATES 11.8257, -3.16228, 0.0551978 : EVALUATED X,Y,Z COORDINATES 11.8266, -3.16228, 0.0578763 : XYZ DEVIATION > TOLERANCE AT 38 NODES ON EDGE 29 : MAX XYZ DEVIATION 0.00266676 TOLERANCE 2.47043e-05 AT NODE 38 : INPUT EDGE COORDINATE T 0.996974 : INPUT X,Y,Z COORDINATES 12.6398, -3.16228, -0.164768 : EVALUATED X,Y,Z COORDINATES 12.6372, -3.16228, -0.164682 : XYZ DEVIATION > TOLERANCE AT 6 NODES ON EDGE 36 : MAX XYZ DEVIATION 0.450685 TOLERANCE 0.231543 AT NODE 11 : INPUT EDGE COORDINATE T 1.56516 : INPUT X,Y,Z COORDINATES 4.89859e-15, -1.19981e-30, 80 : EVALUATED X,Y,Z COORDINATES -0.450683, 5.51928e-17, 79.9987 : XYZ DEVIATION > TOLERANCE AT 6 NODES ON EDGE 38 : MAX XYZ DEVIATION 0.450695 TOLERANCE 0.231783 AT NODE 11 : INPUT EDGE COORDINATE T 7.84835 : INPUT X,Y,Z COORDINATES 4.89859e-15, -1.19981e-30, 80 : EVALUATED X,Y,Z COORDINATES 0.450694, -1.10388e-16, 79.9987 *** NON-FATAL EGADS ERROR 3299 *** *** COORDINATES FOUND THAT DEVIATE FROM EGADS GEOMETRY *** Volume mesh: Number of nodes = 39523 Number of elements = 227963 Number of triangles = 12446 Number of quadrilatarals = 0 Number of tetrahedrals = 215517 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing TECPLOT file: AFLR3_Mesh.dat .... Finished writing TECPLOT file Writing SU2 file .... Finished writing SU2 file Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wake Boundary condition name - Wing1 Boundary condition name - Wing2 Done getting CFD boundary conditions Warning: The su2 cfg file will be overwritten! Write SU2 configuration file for version "BlackBird (7.5.1) " Running SU2...... ------------------------------------------------------------------------- | ___ _ _ ___ | | / __| | | |_ ) Release 7.5.1 "Blackbird" | | \__ \ |_| |/ / | | |___/\___//___| Suite (Computational Fluid Dynamics Code) | | | ------------------------------------------------------------------------- | SU2 Project Website: https://su2code.github.io | | | | The SU2 Project is maintained by the SU2 Foundation | | (http://su2foundation.org) | ------------------------------------------------------------------------- | Copyright 2012-2023, SU2 Contributors | | | | SU2 is free software; you can redistribute it and/or | | modify it under the terms of the GNU Lesser General Public | | License as published by the Free Software Foundation; either | | version 2.1 of the License, or (at your option) any later version. | | | | SU2 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 | | Lesser General Public License for more details. | | | | You should have received a copy of the GNU Lesser General Public | | License along with SU2. If not, see <http://www.gnu.org/licenses/>. | ------------------------------------------------------------------------- Parsing config file for zone 0 ----------------- Physical Case Definition ( Zone 0 ) ------------------- Compressible Euler equations. Mach number: 0.5901. Angle of attack (AoA): 1 deg, and angle of sideslip (AoS): 0 deg. No restart solution, use the values at infinity (freestream). Dimensional simulation. The reference area is 50 m^2. The semi-span will be computed using the max y(3D) value. The reference length is 15.8114 m. Surface(s) where the force coefficients are evaluated and their reference origin for moment computation: - BC_1 (0, 0, 0). - BC_2 (0, 0, 0) m. Surface(s) plotted in the output file: BC_1, BC_2. Input mesh file name: ../aflr3/aflr3_0.su2 --------------- Space Numerical Integration ( Zone 0 ) ------------------ Roe (with entropy fix = 0.001) solver for the flow inviscid terms. Standard Roe without low-dissipation function. Second order integration in space, with slope limiter. Venkatakrishnan slope-limiting method, with constant: 0.05. The reference element size is: 1. Gradient for upwind reconstruction: inverse-distance weighted Least-Squares. Gradient for viscous and source terms: inverse-distance weighted Least-Squares. --------------- Time Numerical Integration ( Zone 0 ) ------------------ Local time stepping (steady state simulation). Euler implicit method for the flow equations. FGMRES is used for solving the linear system. Using a ILU(0) preconditioning. Convergence criteria of the linear solver: 1e-06. Max number of linear iterations: 10. V Multigrid Cycle, with 2 multigrid levels. Damping factor for the residual restriction: 0.75. Damping factor for the correction prolongation: 0.75. No CFL adaptation. +-------------------------------------------+ | MG Level| Presmooth|PostSmooth|CorrectSmo| +-------------------------------------------+ | 0| 1| 0| 0| | 1| 2| 0| 0| | 2| 3| 0| 0| +-------------------------------------------+ Courant-Friedrichs-Lewy number: 10 ------------------ Convergence Criteria ( Zone 0 ) --------------------- Maximum number of solver subiterations: 10. Begin convergence monitoring at iteration 5. Residual minimum value: 1e-8. Cauchy series min. value: 1e-10. Number of Cauchy elements: 100. Begin windowed time average at iteration 0. -------------------- Output Information ( Zone 0 ) ---------------------- File writing frequency: +------------------------------------+ | File| Frequency| +------------------------------------+ | RESTART| 250| | SURFACE_CSV| 250| | PARAVIEW| 250| | SURFACE_PARAVIEW| 250| +------------------------------------+ Writing the convergence history file every 1 inner iterations. Writing the screen convergence history every 1 inner iterations. The tabular file format is CSV (.csv). Convergence history file name: history. Forces breakdown file name: forces_breakdown_su2AFLRTest.dat. Surface file name: surface_flow_su2AFLRTest. Volume file name: flow_su2AFLRTest. Restart file name: restart_flow_su2AFLRTest.dat. ------------- Config File Boundary Information ( Zone 0 ) --------------- +-----------------------------------------------------------------------+ | Marker Type| Marker Name| +-----------------------------------------------------------------------+ | Euler wall| BC_1| | | BC_2| +-----------------------------------------------------------------------+ | Far-field| BC_4| +-----------------------------------------------------------------------+ | Internal boundary| BC_3| +-----------------------------------------------------------------------+ -------------------- Output Preprocessing ( Zone 0 ) -------------------- WARNING: SURFACE_PRESSURE_DROP can only be computed for at least 2 surfaces (outlet, inlet, ...) Screen output fields: TIME_ITER, OUTER_ITER, INNER_ITER, CUR_TIME, TIME_STEP, WALL_TIME, RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_ENERGY, EFFICIENCY History output group(s): ITER, TIME_DOMAIN, WALL_TIME, RMS_RES, AERO_COEFF Convergence field(s): RMS_DENSITY Warning: No (valid) fields chosen for time convergence monitoring. Time convergence monitoring inactive. Volume output fields: COORDINATES, SOLUTION, PRIMITIVE ------------------- Geometry Preprocessing ( Zone 0 ) ------------------- Three dimensional problem. 39523 grid points. 215517 volume elements. 4 surface markers. 6594 boundary elements in index 0 (Marker = BC_1). 5358 boundary elements in index 1 (Marker = BC_2). 74 boundary elements in index 2 (Marker = BC_3). 420 boundary elements in index 3 (Marker = BC_4). 215517 tetrahedra. Setting point connectivity. Renumbering points (Reverse Cuthill McKee Ordering). Recomputing point connectivity. Setting element connectivity. Checking the numerical grid orientation. All volume elements are correctly orientend. All surface elements are correctly orientend. Identifying edges and vertices. Setting the control volume structure. Volume of the computational grid: 2.08667e+06. Searching for the closest normal neighbors to the surfaces. Storing a mapping from global to local point index. Compute the surface curvature. Max K: 4873.1. Mean K: 61.8682. Standard deviation K: 266.942. Checking for periodicity. Computing mesh quality statistics for the dual control volumes. +--------------------------------------------------------------+ | Mesh Quality Metric| Minimum| Maximum| +--------------------------------------------------------------+ | Orthogonality Angle (deg.)| 22.4743| 85.7834| | CV Face Area Aspect Ratio| 1.08187| 5872.03| | CV Sub-Volume Ratio| 1.02366| 63630.9| +--------------------------------------------------------------+ Setting the multigrid structure. +-------------------------------------------+ | MG Level| CVs|Aggl. Rate| CFL| +-------------------------------------------+ | 0| 39523| 1/1.00| 10| | 1| 6562| 1/6.02| 8.24429| | 2| 1021| 1/6.43| 6.65132| +-------------------------------------------+ Finding max control volume width. Semi-span length = 7.90569 m. Wetted area = 118.038 m^2. Area projection in the x-plane = 11.1419 m^2, y-plane = 4.96714 m^2, z-plane = 55.4182 m^2. Max. coordinate in the x-direction = 12.6407 m, y-direction = 7.90569 m, z-direction = 0.582636 m. Min. coordinate in the x-direction = 0 m, y-direction = -7.90569 m, z-direction = -0.41192 m. Checking if Euler & Symmetry markers are straight/plane: Boundary marker BC_1 is NOT a single plane. Boundary marker BC_2 is NOT a single plane. Computing wall distances. -------------------- Solver Preprocessing ( Zone 0 ) -------------------- Inviscid flow: Computing density based on free-stream temperature and pressure using the ideal gas law. Force coefficients computed using free-stream values. -- Models: +------------------------------------------------------------------------------+ | Viscosity Model| Conductivity Model| Fluid Model| +------------------------------------------------------------------------------+ | -| -| STANDARD_AIR| +------------------------------------------------------------------------------+ -- Fluid properties: +------------------------------------------------------------------------------+ | Name| Dim. value| Ref. value| Unit|Non-dim. value| +------------------------------------------------------------------------------+ | Gas Constant| 287.058| 1| N.m/kg.K| 287.058| | Spec. Heat Ratio| -| -| -| 1.4| +------------------------------------------------------------------------------+ -- Initial and free-stream conditions: +------------------------------------------------------------------------------+ | Name| Dim. value| Ref. value| Unit|Non-dim. value| +------------------------------------------------------------------------------+ | Static Pressure| 101325| 1| Pa| 101325| | Density| 1.22498| 1| kg/m^3| 1.22498| | Temperature| 288.15| 1| K| 288.15| | Total Energy| 226952| 1| m^2/s^2| 226952| | Velocity-X| 200.779| 1| m/s| 200.779| | Velocity-Y| 0| 1| m/s| 0| | Velocity-Z| 3.50461| 1| m/s| 3.50461| | Velocity Magnitude| 200.809| 1| m/s| 200.809| +------------------------------------------------------------------------------+ | Mach Number| -| -| -| 0.5901| +------------------------------------------------------------------------------+ Initialize Jacobian structure (Euler). MG level: 0. Initialize Jacobian structure (Euler). MG level: 1. Initialize Jacobian structure (Euler). MG level: 2. ------------------- Numerics Preprocessing ( Zone 0 ) ------------------- ----------------- Integration Preprocessing ( Zone 0 ) ------------------ ------------------- Iteration Preprocessing ( Zone 0 ) ------------------ Euler/Navier-Stokes/RANS fluid iteration. ------------------------------ Begin Solver ----------------------------- Simulation Run using the Single-zone Driver WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better, see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better, see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better, see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations +----------------------------------------------------------------------------------------------------------------------------------------------+ | Time_Iter| Outer_Iter| Inner_Iter| Cur_Time| Time_Step| Time(sec)| rms[Rho]| rms[RhoU]| rms[RhoV]| rms[RhoE]| CEff| +----------------------------------------------------------------------------------------------------------------------------------------------+ | 0| 0| 0| 0.0000e+00| 0.0000e+00| 8.8729e-01| -0.065748| 2.296513| 2.032138| 5.425147| 1.981988| | 0| 0| 1| 0.0000e+00| 0.0000e+00| 8.7729e-01| -0.013435| 2.467910| 2.178447| 5.486323| 2.686472| | 0| 0| 2| 0.0000e+00| 0.0000e+00| 9.0732e-01| 0.026977| 2.551156| 2.399385| 5.520423| 4.113528| | 0| 0| 3| 0.0000e+00| 0.0000e+00| 9.3181e-01| -0.018024| 2.574278| 2.534654| 5.461497| 6.055033| | 0| 0| 4| 0.0000e+00| 0.0000e+00| 9.4522e-01| -0.063766| 2.579967| 2.596760| 5.407698| 7.773086| | 0| 0| 5| 0.0000e+00| 0.0000e+00| 9.3114e-01| -0.091729| 2.577148| 2.617164| 5.388634| 9.049441| | 0| 0| 6| 0.0000e+00| 0.0000e+00| 9.1848e-01| -0.130606| 2.547958| 2.625760| 5.359277| 10.020686| | 0| 0| 7| 0.0000e+00| 0.0000e+00| 9.2217e-01| -0.181405| 2.484434| 2.629292| 5.304802| 10.588909| | 0| 0| 8| 0.0000e+00| 0.0000e+00| 9.1932e-01| -0.228419| 2.399906| 2.617227| 5.240734| 10.696697| | 0| 0| 9| 0.0000e+00| 0.0000e+00| 9.0244e-01| -0.278669| 2.326761| 2.579891| 5.178244| 10.453460| ----------------------------- Solver Exit ------------------------------- Maximum number of iterations reached (ITER = 10) before convergence. +-----------------------------------------------------------------------+ | Convergence Field | Value | Criterion | Converged | +-----------------------------------------------------------------------+ | rms[Rho]| -0.278669| < -8| No| +-----------------------------------------------------------------------+ ------------------------------------------------------------------------- +-----------------------------------------------------------------------+ | File Writing Summary | Filename | +-----------------------------------------------------------------------+ |SU2 binary restart |restart_flow_su2AFLRTest.dat | Writing the forces breakdown file (forces_breakdown_su2AFLRTest.dat). |CSV file |surface_flow_su2AFLRTest.csv | Writing the forces breakdown file (forces_breakdown_su2AFLRTest.dat). |Paraview |flow_su2AFLRTest.vtu | Writing the forces breakdown file (forces_breakdown_su2AFLRTest.dat). |Paraview surface |surface_flow_su2AFLRTest.vtu | Writing the forces breakdown file (forces_breakdown_su2AFLRTest.dat). +-----------------------------------------------------------------------+ ------------------------- Solver Postprocessing ------------------------- Deleted CNumerics container. Deleted CIntegration container. Deleted CSolver container. Deleted CIteration container. Deleted CInterface container. Deleted CGeometry container. Deleted CFreeFormDefBox class. Deleted CSurfaceMovement class. Deleted CVolumetricMovement class. Deleted CConfig container. Deleted nInst container. Deleted COutput class. ------------------------------------------------------------------------- ------------------------- Exit Success (SU2_CFD) ------------------------ Total Force - Pressure + Viscous Cl = 0.796018 Cd = 0.076149 Cmx = 0.000363 Cmy = -0.203375 Cmz = -0.000159 Cx = 0.062245 Cy = 8.9e-05 Cz = 0.797225 Pressure Contribution Cl_p = 0.796018 Cd_p = 0.076149 Cmx_p = 0.000363 Cmy_p = -0.203375 Cmz_p = -0.000159 Cx_p = 0.062245 Cy_p = 8.9e-05 Cz_p = 0.797225 Viscous Contribution Cl_v = 0.0 Cd_v = 0.0 Cmx_v = 0.0 Cmy_v = 0.0 Cmz_v = 0.0 Cx_v = 0.0 Cy_v = 0.0 Cz_v = 0.0 real 0m48.571s user 0m27.826s sys 0m0.637s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case su2_and_AFLR4_AFLR3_PyTest.py passed (as expected) ================================================= delaundo: /Users/jenkins/util/delaundo/delaundo/src/delaundo ================================================= + echo 'su2_and_Delaundo_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/CFD/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/pyCAPSlog.txt su2_and_Delaundo_PyTest.py test; + python -u su2_and_Delaundo_PyTest.py -outLevel=0 + tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/CFD/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/pyCAPSlog.txt Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 5 Name = 2DSlice, index = 1 Name = TunnelWall, index = 2 Name = OutFlow, index = 3 Name = InFlow, index = 4 Name = Airfoil, index = 5 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 5 Name = 2DSlice, index = 1 Name = TunnelWall, index = 2 Name = OutFlow, index = 3 Name = InFlow, index = 4 Name = Airfoil, index = 5 Getting mesh sizing parameters Mesh sizing name - 2DSlice Mesh sizing name - Airfoil Mesh sizing name - InFlow Mesh sizing name - OutFlow Mesh sizing name - TunnelWall Done getting mesh sizing parameters Getting edge discretization for body 1 Delaundo expects 2D meshes be in the x-y plane... attempting to rotate mesh through node swapping! Swapping z and y coordinates! Writing delaundo control file - delaundo.ctr Writing out *.pts file Reading delaundo mesh file - delaundoMesh.mesh Swapping y and z coordinates! Writing TECPLOT file: delaundoMesh.dat .... Finished writing TECPLOT file Writing SU2 file .... SU2 expects 2D meshes be in the x-y plane... attempting to rotate mesh! Swapping z and y coordinates! Finished writing SU2 file Getting CFD boundary conditions Boundary condition name - Airfoil Boundary condition name - InFlow Boundary condition name - OutFlow Boundary condition name - TunnelWall Warning: No boundary condition specified for capsGroup 2DSlice! Done getting CFD boundary conditions Warning: The su2 cfg file will be overwritten! Write SU2 configuration file for version "BlackBird (7.5.1) " Running SU2...... ------------------------------------------------------------------------- | ___ _ _ ___ | | / __| | | |_ ) Release 7.5.1 "Blackbird" | | \__ \ |_| |/ / | | |___/\___//___| Suite (Computational Fluid Dynamics Code) | | | ------------------------------------------------------------------------- | SU2 Project Website: https://su2code.github.io | | | | The SU2 Project is maintained by the SU2 Foundation | | (http://su2foundation.org) | ------------------------------------------------------------------------- | Copyright 2012-2023, SU2 Contributors | | | | SU2 is free software; you can redistribute it and/or | | modify it under the terms of the GNU Lesser General Public | | License as published by the Free Software Foundation; either | | version 2.1 of the License, or (at your option) any later version. | | | | SU2 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 | | Lesser General Public License for more details. | | | | You should have received a copy of the GNU Lesser General Public | | License along with SU2. If not, see <http://www.gnu.org/licenses/>. | ------------------------------------------------------------------------- Parsing config file for zone 0 ----------------- Physical Case Definition ( Zone 0 ) ------------------- Compressible Euler equations. Mach number: 0.4. Angle of attack (AoA): 0 deg, and angle of sideslip (AoS): 0 deg. No restart solution, use the values at infinity (freestream). Dimensional simulation. The reference area is 1 m^2. The semi-span will be computed using the max y(3D) value. The reference length is 1 m. Reference origin for moment evaluation is (0, 0, 0). Surface(s) where the force coefficients are evaluated: BC_5. Surface(s) plotted in the output file: BC_5, BC_2. Input mesh file name: ../delaundo/delaundoMesh.su2 --------------- Space Numerical Integration ( Zone 0 ) ------------------ Roe (with entropy fix = 0.001) solver for the flow inviscid terms. Standard Roe without low-dissipation function. Second order integration in space, with slope limiter. Venkatakrishnan slope-limiting method, with constant: 0.05. The reference element size is: 1. Gradient for upwind reconstruction: inverse-distance weighted Least-Squares. Gradient for viscous and source terms: inverse-distance weighted Least-Squares. --------------- Time Numerical Integration ( Zone 0 ) ------------------ Local time stepping (steady state simulation). Euler implicit method for the flow equations. FGMRES is used for solving the linear system. Using a ILU(0) preconditioning. Convergence criteria of the linear solver: 1e-06. Max number of linear iterations: 10. V Multigrid Cycle, with 2 multigrid levels. Damping factor for the residual restriction: 0.75. Damping factor for the correction prolongation: 0.75. No CFL adaptation. +-------------------------------------------+ | MG Level| Presmooth|PostSmooth|CorrectSmo| +-------------------------------------------+ | 0| 1| 0| 0| | 1| 2| 0| 0| | 2| 3| 0| 0| +-------------------------------------------+ Courant-Friedrichs-Lewy number: 10 ------------------ Convergence Criteria ( Zone 0 ) --------------------- Maximum number of solver subiterations: 10. Begin convergence monitoring at iteration 5. Residual minimum value: 1e-14. Cauchy series min. value: 1e-10. Number of Cauchy elements: 100. Begin windowed time average at iteration 0. -------------------- Output Information ( Zone 0 ) ---------------------- File writing frequency: +------------------------------------+ | File| Frequency| +------------------------------------+ | RESTART| 250| | SURFACE_CSV| 250| | TECPLOT| 250| | SURFACE_TECPLOT| 250| +------------------------------------+ Writing the convergence history file every 1 inner iterations. Writing the screen convergence history every 1 inner iterations. The tabular file format is CSV (.csv). Convergence history file name: history. Forces breakdown file name: forces_breakdown_delaundoMesh.dat. Surface file name: surface_flow_delaundoMesh. Volume file name: flow_delaundoMesh. Restart file name: restart_flow_delaundoMesh.dat. ------------- Config File Boundary Information ( Zone 0 ) --------------- +-----------------------------------------------------------------------+ | Marker Type| Marker Name| +-----------------------------------------------------------------------+ | Euler wall| BC_5| | | BC_2| +-----------------------------------------------------------------------+ | Inlet boundary| BC_4| +-----------------------------------------------------------------------+ | Outlet boundary| BC_3| +-----------------------------------------------------------------------+ -------------------- Output Preprocessing ( Zone 0 ) -------------------- WARNING: SURFACE_PRESSURE_DROP can only be computed for at least 2 surfaces (outlet, inlet, ...) Screen output fields: TIME_ITER, OUTER_ITER, INNER_ITER, CUR_TIME, TIME_STEP, WALL_TIME, RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_ENERGY, EFFICIENCY History output group(s): ITER, TIME_DOMAIN, WALL_TIME, RMS_RES, AERO_COEFF Convergence field(s): RMS_DENSITY Warning: No (valid) fields chosen for time convergence monitoring. Time convergence monitoring inactive. Volume output fields: COORDINATES, SOLUTION, PRIMITIVE ------------------- Geometry Preprocessing ( Zone 0 ) ------------------- Two dimensional problem. 6317 grid points. 12340 volume elements. 5 surface markers. 24 boundary elements in index 0 (Marker = BC_2). 24 boundary elements in index 1 (Marker = BC_3). 24 boundary elements in index 2 (Marker = BC_2). 24 boundary elements in index 3 (Marker = BC_4). 198 boundary elements in index 4 (Marker = BC_5). 12340 triangles. Setting point connectivity. Renumbering points (Reverse Cuthill McKee Ordering). Recomputing point connectivity. Setting element connectivity. Checking the numerical grid orientation. All volume elements are correctly orientend. There has been a re-orientation of 294 LINE surface elements. Identifying edges and vertices. Setting the control volume structure. Area of the computational grid: 999.917. Searching for the closest normal neighbors to the surfaces. Storing a mapping from global to local point index. Compute the surface curvature. Max K: 1792.95. Mean K: 10.8142. Standard deviation K: 104.33. Checking for periodicity. Computing mesh quality statistics for the dual control volumes. +--------------------------------------------------------------+ | Mesh Quality Metric| Minimum| Maximum| +--------------------------------------------------------------+ | Orthogonality Angle (deg.)| 45.3524| 89.2595| | CV Face Area Aspect Ratio| 1.03245| 15.7138| | CV Sub-Volume Ratio| 1| 7.93643| +--------------------------------------------------------------+ Setting the multigrid structure. +-------------------------------------------+ | MG Level| CVs|Aggl. Rate| CFL| +-------------------------------------------+ | 0| 6317| 1/1.00| 10| | 1| 1792| 1/3.53| 7.98923| | 2| 509| 1/3.52| 6.38684| +-------------------------------------------+ Finding max control volume width. Wetted area = 2.07206 m. Area projection in the x-plane = 0.179342 m, y-plane = 1.00053 m. Max. coordinate in the x-direction = 1 m, y-direction = 0.138492 m. Min. coordinate in the x-direction = -0.00104578 m, y-direction = -0.0151891 m. Checking if Euler & Symmetry markers are straight/plane: Boundary marker BC_5 is NOT a single straight. Boundary marker BC_2 is a single straight. Computing wall distances. -------------------- Solver Preprocessing ( Zone 0 ) -------------------- Inviscid flow: Computing density based on free-stream temperature and pressure using the ideal gas law. Force coefficients computed using free-stream values. -- Models: +------------------------------------------------------------------------------+ | Viscosity Model| Conductivity Model| Fluid Model| +------------------------------------------------------------------------------+ | -| -| STANDARD_AIR| +------------------------------------------------------------------------------+ -- Fluid properties: +------------------------------------------------------------------------------+ | Name| Dim. value| Ref. value| Unit|Non-dim. value| +------------------------------------------------------------------------------+ | Gas Constant| 287.058| 1| N.m/kg.K| 287.058| | Spec. Heat Ratio| -| -| -| 1.4| +------------------------------------------------------------------------------+ -- Initial and free-stream conditions: +------------------------------------------------------------------------------+ | Name| Dim. value| Ref. value| Unit|Non-dim. value| +------------------------------------------------------------------------------+ | Static Pressure| 101325| 1| Pa| 101325| | Density| 1.22498| 1| kg/m^3| 1.22498| | Temperature| 288.15| 1| K| 288.15| | Total Energy| 216054| 1| m^2/s^2| 216054| | Velocity-X| 136.119| 1| m/s| 136.119| | Velocity-Y| 0| 1| m/s| 0| | Velocity Magnitude| 136.119| 1| m/s| 136.119| +------------------------------------------------------------------------------+ | Mach Number| -| -| -| 0.4| +------------------------------------------------------------------------------+ Initialize Jacobian structure (Euler). MG level: 0. Initialize Jacobian structure (Euler). MG level: 1. Initialize Jacobian structure (Euler). MG level: 2. ------------------- Numerics Preprocessing ( Zone 0 ) ------------------- ----------------- Integration Preprocessing ( Zone 0 ) ------------------ ------------------- Iteration Preprocessing ( Zone 0 ) ------------------ Euler/Navier-Stokes/RANS fluid iteration. ------------------------------ Begin Solver ----------------------------- Simulation Run using the Single-zone Driver WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better, see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better, see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better, see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations +----------------------------------------------------------------------------------------------------------------------------------------------+ | Time_Iter| Outer_Iter| Inner_Iter| Cur_Time| Time_Step| Time(sec)| rms[Rho]| rms[RhoU]| rms[RhoV]| rms[RhoE]| CEff| +----------------------------------------------------------------------------------------------------------------------------------------------+ | 0| 0| 0| 0.0000e+00| 0.0000e+00| 6.1407e-02| -1.163068| 1.073873| 1.341547| 4.312268| 0.062082| | 0| 0| 1| 0.0000e+00| 0.0000e+00| 5.9417e-02| -1.558471| 0.813117| 0.969484| 3.926501| 0.143132| | 0| 0| 2| 0.0000e+00| 0.0000e+00| 5.7024e-02| -1.599269| 0.950037| 1.012154| 3.879885| 0.386300| | 0| 0| 3| 0.0000e+00| 0.0000e+00| 5.4977e-02| -1.661284| 1.005970| 1.023067| 3.797319| 0.981260| | 0| 0| 4| 0.0000e+00| 0.0000e+00| 5.3320e-02| -1.658421| 1.009907| 0.965279| 3.792658| 2.399755| | 0| 0| 5| 0.0000e+00| 0.0000e+00| 5.3145e-02| -1.630602| 0.996801| 0.859556| 3.833204| 6.390579| | 0| 0| 6| 0.0000e+00| 0.0000e+00| 5.2524e-02| -1.628009| 1.002770| 0.822847| 3.846297| 27.872536| | 0| 0| 7| 0.0000e+00| 0.0000e+00| 5.1756e-02| -1.646113| 1.024424| 0.882502| 3.830202| -48.293527| | 0| 0| 8| 0.0000e+00| 0.0000e+00| 5.1500e-02| -1.672152| 1.033657| 0.939200| 3.797228| -22.113788| | 0| 0| 9| 0.0000e+00| 0.0000e+00| 5.4244e-02| -1.695131| 1.018255| 0.944150| 3.765919| -19.281368| ----------------------------- Solver Exit ------------------------------- Maximum number of iterations reached (ITER = 10) before convergence. +-----------------------------------------------------------------------+ | Convergence Field | Value | Criterion | Converged | +-----------------------------------------------------------------------+ | rms[Rho]| -1.69513| < -14| No| +-----------------------------------------------------------------------+ ------------------------------------------------------------------------- +-----------------------------------------------------------------------+ | File Writing Summary | Filename | +-----------------------------------------------------------------------+ |SU2 binary restart |restart_flow_delaundoMesh.dat | Writing the forces breakdown file (forces_breakdown_delaundoMesh.dat). |CSV file |surface_flow_delaundoMesh.csv | Writing the forces breakdown file (forces_breakdown_delaundoMesh.dat). |Tecplot binary |flow_delaundoMesh.szplt | Writing the forces breakdown file (forces_breakdown_delaundoMesh.dat). |Tecplot binary surface |surface_flow_delaundoMesh.szplt | Error in tecFileWriterClose: Not all node map values for zone 1 have been written. Currently need 492 more values.0: Error finishing Tecplot file output. Writing the forces breakdown file (forces_breakdown_delaundoMesh.dat). +-----------------------------------------------------------------------+ ------------------------- Solver Postprocessing ------------------------- Deleted CNumerics container. Deleted CIntegration container. Deleted CSolver container. Deleted CIteration container. Deleted CInterface container. Deleted CGeometry container. Deleted CFreeFormDefBox class. Deleted CSurfaceMovement class. Deleted CVolumetricMovement class. Deleted CConfig container. Deleted nInst container. Deleted COutput class. ------------------------------------------------------------------------- ------------------------- Exit Success (SU2_CFD) ------------------------ Total Force - Pressure + Viscous Cl = 0.805707 Cd = -0.041787 Cmz = 0.408515 Cx = -0.041787 Cy = 0.805707 Pressure Contribution Cl_p = 0.805707 Cd_p = -0.041787 Cmz_p = 0.408515 Cx_p = -0.041787 Cy_p = 0.805707 Viscous Contribution Cl_v = 0.0 Cd_v = 0.0 Cmz_v = 0.0 Cx_v = 0.0 Cy_v = 0.0 real 0m1.966s user 0m1.936s sys 0m0.408s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case su2_and_Delaundo_PyTest.py passed (as expected) ================================================= ================================================= + echo 'su2_and_Tetgen_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/CFD/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/pyCAPSlog.txt su2_and_Tetgen_PyTest.py test; + python -u su2_and_Tetgen_PyTest.py -outLevel=0 + tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/CFD/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/pyCAPSlog.txt Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Getting surface mesh for body 1 (of 3) Getting surface mesh for body 2 (of 3) Getting surface mesh for body 3 (of 3) Body 1 (of 3) Number of nodes = 2236 Number of elements = 4468 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 4468 Number of quadrilateral elements = 0 Body 2 (of 3) Number of nodes = 636 Number of elements = 1268 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 1268 Number of quadrilateral elements = 0 Body 3 (of 3) Number of nodes = 258 Number of elements = 512 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 512 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 3130 Total number of elements = 6248 Writing TECPLOT file: egadsTessMesh_Surf_0.dat .... Finished writing TECPLOT file Writing TECPLOT file: egadsTessMesh_Surf_1.dat .... Finished writing TECPLOT file Writing TECPLOT file: egadsTessMesh_Surf_2.dat .... Finished writing TECPLOT file Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Number of surface: nodes - 3130, elements - 6248 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000T1.00e-16A Delaunizing vertices... Delaunay seconds: 0.036205 Creating surface mesh ... Surface mesh seconds: 0.006305 Recovering boundaries... Boundary recovery seconds: 0.096589 Removing exterior tetrahedra ... Spreading region attributes. Exterior tets removal seconds: 0.006057 Suppressing Steiner points ... Steiner suppression seconds: 5e-06 Recovering Delaunayness... Delaunay recovery seconds: 0.011169 Refining mesh... 4180 insertions, added 2061 points, 130359 tetrahedra in queue. 1391 insertions, added 425 points, 134059 tetrahedra in queue. 1855 insertions, added 465 points, 131734 tetrahedra in queue. 2472 insertions, added 531 points, 115562 tetrahedra in queue. 3296 insertions, added 526 points, 67935 tetrahedra in queue. 4393 insertions, added 433 points, 372 tetrahedra in queue. 5856 insertions, added 571 points, 794 tetrahedra in queue. Refinement seconds: 1.07632 Smoothing vertices... Mesh smoothing seconds: 0.875959 Improving mesh... Mesh improvement seconds: 0.047421 Jettisoning redundant points. Writing nodes. Writing elements. Writing faces. Writing edges. Output seconds: 0.00231 Total running seconds: 2.15861 Statistics: Input points: 3130 Input facets: 6248 Input segments: 9372 Input holes: 2 Input regions: 0 Mesh points: 8154 Mesh tetrahedra: 40351 Mesh faces: 83827 Mesh faces on exterior boundary: 6250 Mesh faces on input facets: 6250 Mesh edges on input segments: 9373 Steiner points on input segments: 1 Steiner points inside domain: 5023 Done meshing using TetGen! Volume mesher did not preserve surface elements - data transfer will NOT be possible. Writing SU2 file .... Finished writing SU2 file Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - Wing2 Done getting CFD boundary conditions Warning: The su2 cfg file will be overwritten! Write SU2 configuration file for version "BlackBird (7.5.1) " Running SU2...... ------------------------------------------------------------------------- | ___ _ _ ___ | | / __| | | |_ ) Release 7.5.1 "Blackbird" | | \__ \ |_| |/ / | | |___/\___//___| Suite (Computational Fluid Dynamics Code) | | | ------------------------------------------------------------------------- | SU2 Project Website: https://su2code.github.io | | | | The SU2 Project is maintained by the SU2 Foundation | | (http://su2foundation.org) | ------------------------------------------------------------------------- | Copyright 2012-2023, SU2 Contributors | | | | SU2 is free software; you can redistribute it and/or | | modify it under the terms of the GNU Lesser General Public | | License as published by the Free Software Foundation; either | | version 2.1 of the License, or (at your option) any later version. | | | | SU2 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 | | Lesser General Public License for more details. | | | | You should have received a copy of the GNU Lesser General Public | | License along with SU2. If not, see <http://www.gnu.org/licenses/>. | ------------------------------------------------------------------------- Parsing config file for zone 0 ----------------- Physical Case Definition ( Zone 0 ) ------------------- Compressible Euler equations. Mach number: 0.5901. Angle of attack (AoA): 1 deg, and angle of sideslip (AoS): 0 deg. No restart solution, use the values at infinity (freestream). Dimensional simulation. The reference area is 50 m^2. The semi-span will be computed using the max y(3D) value. The reference length is 15.8114 m. Surface(s) where the force coefficients are evaluated and their reference origin for moment computation: - BC_1 (0, 0, 0). - BC_2 (0, 0, 0) m. Surface(s) plotted in the output file: BC_1, BC_2. Input mesh file name: ../myMesh/tetgen_0.su2 --------------- Space Numerical Integration ( Zone 0 ) ------------------ Roe (with entropy fix = 0.001) solver for the flow inviscid terms. Standard Roe without low-dissipation function. Second order integration in space, with slope limiter. Venkatakrishnan slope-limiting method, with constant: 0.05. The reference element size is: 1. Gradient for upwind reconstruction: inverse-distance weighted Least-Squares. Gradient for viscous and source terms: inverse-distance weighted Least-Squares. --------------- Time Numerical Integration ( Zone 0 ) ------------------ Local time stepping (steady state simulation). Euler implicit method for the flow equations. FGMRES is used for solving the linear system. Using a ILU(0) preconditioning. Convergence criteria of the linear solver: 1e-06. Max number of linear iterations: 10. V Multigrid Cycle, with 2 multigrid levels. Damping factor for the residual restriction: 0.75. Damping factor for the correction prolongation: 0.75. No CFL adaptation. +-------------------------------------------+ | MG Level| Presmooth|PostSmooth|CorrectSmo| +-------------------------------------------+ | 0| 1| 0| 0| | 1| 2| 0| 0| | 2| 3| 0| 0| +-------------------------------------------+ Courant-Friedrichs-Lewy number: 10 ------------------ Convergence Criteria ( Zone 0 ) --------------------- Maximum number of solver subiterations: 5. Begin convergence monitoring at iteration 5. Residual minimum value: 1e-14. Cauchy series min. value: 1e-10. Number of Cauchy elements: 100. Begin windowed time average at iteration 0. -------------------- Output Information ( Zone 0 ) ---------------------- File writing frequency: +------------------------------------+ | File| Frequency| +------------------------------------+ | RESTART| 250| | SURFACE_CSV| 250| | PARAVIEW| 250| | SURFACE_PARAVIEW| 250| +------------------------------------+ Writing the convergence history file every 1 inner iterations. Writing the screen convergence history every 1 inner iterations. The tabular file format is CSV (.csv). Convergence history file name: history. Forces breakdown file name: forces_breakdown_pyCAPS_SU2_Tetgen.dat. Surface file name: surface_flow_pyCAPS_SU2_Tetgen. Volume file name: flow_pyCAPS_SU2_Tetgen. Restart file name: restart_flow_pyCAPS_SU2_Tetgen.dat. ------------- Config File Boundary Information ( Zone 0 ) --------------- +-----------------------------------------------------------------------+ | Marker Type| Marker Name| +-----------------------------------------------------------------------+ | Euler wall| BC_1| | | BC_2| +-----------------------------------------------------------------------+ | Far-field| BC_3| +-----------------------------------------------------------------------+ -------------------- Output Preprocessing ( Zone 0 ) -------------------- WARNING: SURFACE_PRESSURE_DROP can only be computed for at least 2 surfaces (outlet, inlet, ...) Screen output fields: TIME_ITER, OUTER_ITER, INNER_ITER, CUR_TIME, TIME_STEP, WALL_TIME, RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_ENERGY, EFFICIENCY History output group(s): ITER, TIME_DOMAIN, WALL_TIME, RMS_RES, AERO_COEFF Convergence field(s): RMS_DENSITY Warning: No (valid) fields chosen for time convergence monitoring. Time convergence monitoring inactive. Volume output fields: COORDINATES, SOLUTION, PRIMITIVE ------------------- Geometry Preprocessing ( Zone 0 ) ------------------- Three dimensional problem. 8154 grid points. 40351 volume elements. 3 surface markers. 4468 boundary elements in index 0 (Marker = BC_1). 1270 boundary elements in index 1 (Marker = BC_2). 512 boundary elements in index 2 (Marker = BC_3). 40351 tetrahedra. Setting point connectivity. Renumbering points (Reverse Cuthill McKee Ordering). Recomputing point connectivity. Setting element connectivity. Checking the numerical grid orientation. All volume elements are correctly orientend. All surface elements are correctly orientend. Identifying edges and vertices. Setting the control volume structure. Volume of the computational grid: 2.08741e+06. Searching for the closest normal neighbors to the surfaces. Storing a mapping from global to local point index. Compute the surface curvature. Max K: 414.134. Mean K: 30.6158. Standard deviation K: 37.5195. Checking for periodicity. Computing mesh quality statistics for the dual control volumes. +--------------------------------------------------------------+ | Mesh Quality Metric| Minimum| Maximum| +--------------------------------------------------------------+ | Orthogonality Angle (deg.)| 1.93303| 83.8522| | CV Face Area Aspect Ratio| 1.66492| 8220.52| | CV Sub-Volume Ratio| 1.0945| 249103| +--------------------------------------------------------------+ Setting the multigrid structure. +-------------------------------------------+ | MG Level| CVs|Aggl. Rate| CFL| +-------------------------------------------+ | 0| 8154| 1/1.00| 10| | 1| 1365| 1/5.97| 8.26695| | 2| 222| 1/6.15| 6.76877| +-------------------------------------------+ Finding max control volume width. Semi-span length = 7.90569 m. Wetted area = 120.046 m^2. Area projection in the x-plane = 10.7914 m^2, y-plane = 4.5843 m^2, z-plane = 57.287 m^2. Max. coordinate in the x-direction = 12.6407 m, y-direction = 7.90569 m, z-direction = 0.557773 m. Min. coordinate in the x-direction = -0.00409054 m, y-direction = -7.90569 m, z-direction = -0.41192 m. Checking if Euler & Symmetry markers are straight/plane: Boundary marker BC_1 is NOT a single plane. Boundary marker BC_2 is NOT a single plane. Computing wall distances. -------------------- Solver Preprocessing ( Zone 0 ) -------------------- Inviscid flow: Computing density based on free-stream temperature and pressure using the ideal gas law. Force coefficients computed using free-stream values. -- Models: +------------------------------------------------------------------------------+ | Viscosity Model| Conductivity Model| Fluid Model| +------------------------------------------------------------------------------+ | -| -| STANDARD_AIR| +------------------------------------------------------------------------------+ -- Fluid properties: +------------------------------------------------------------------------------+ | Name| Dim. value| Ref. value| Unit|Non-dim. value| +------------------------------------------------------------------------------+ | Gas Constant| 287.058| 1| N.m/kg.K| 287.058| | Spec. Heat Ratio| -| -| -| 1.4| +------------------------------------------------------------------------------+ -- Initial and free-stream conditions: +------------------------------------------------------------------------------+ | Name| Dim. value| Ref. value| Unit|Non-dim. value| +------------------------------------------------------------------------------+ | Static Pressure| 101325| 1| Pa| 101325| | Density| 1.22498| 1| kg/m^3| 1.22498| | Temperature| 288.15| 1| K| 288.15| | Total Energy| 226952| 1| m^2/s^2| 226952| | Velocity-X| 200.779| 1| m/s| 200.779| | Velocity-Y| 0| 1| m/s| 0| | Velocity-Z| 3.50461| 1| m/s| 3.50461| | Velocity Magnitude| 200.809| 1| m/s| 200.809| +------------------------------------------------------------------------------+ | Mach Number| -| -| -| 0.5901| +------------------------------------------------------------------------------+ Initialize Jacobian structure (Euler). MG level: 0. Initialize Jacobian structure (Euler). MG level: 1. Initialize Jacobian structure (Euler). MG level: 2. ------------------- Numerics Preprocessing ( Zone 0 ) ------------------- ----------------- Integration Preprocessing ( Zone 0 ) ------------------ ------------------- Iteration Preprocessing ( Zone 0 ) ------------------ Euler/Navier-Stokes/RANS fluid iteration. ------------------------------ Begin Solver ----------------------------- Simulation Run using the Single-zone Driver WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better, see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better, see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better, see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations +----------------------------------------------------------------------------------------------------------------------------------------------+ | Time_Iter| Outer_Iter| Inner_Iter| Cur_Time| Time_Step| Time(sec)| rms[Rho]| rms[RhoU]| rms[RhoV]| rms[RhoE]| CEff| +----------------------------------------------------------------------------------------------------------------------------------------------+ | 0| 0| 0| 0.0000e+00| 0.0000e+00| 1.9814e-01| 0.616284| 3.048260| 2.091357| 6.107180| 1.815389| | 0| 0| 1| 0.0000e+00| 0.0000e+00| 1.8937e-01| 0.741001| 3.258088| 2.952168| 6.243294| 2.156707| | 0| 0| 2| 0.0000e+00| 0.0000e+00| 2.1824e-01| 0.650783| 3.322878| 3.201040| 6.147243| 3.157692| | 0| 0| 3| 0.0000e+00| 0.0000e+00| 2.1266e-01| 0.569960| 3.293032| 3.250810| 6.036360| 4.529265| | 0| 0| 4| 0.0000e+00| 0.0000e+00| 2.1610e-01| 0.533226| 3.191940| 3.195181| 5.994483| 5.686317| ----------------------------- Solver Exit ------------------------------- Maximum number of iterations reached (ITER = 5) before convergence. +-----------------------------------------------------------------------+ | Convergence Field | Value | Criterion | Converged | +-----------------------------------------------------------------------+ | rms[Rho]| 0.533226| < -14| No| +-----------------------------------------------------------------------+ ------------------------------------------------------------------------- +-----------------------------------------------------------------------+ | File Writing Summary | Filename | +-----------------------------------------------------------------------+ |SU2 binary restart |restart_flow_pyCAPS_SU2_Tetgen.dat | Writing the forces breakdown file (forces_breakdown_pyCAPS_SU2_Tetgen.dat). |CSV file |surface_flow_pyCAPS_SU2_Tetgen.csv | Writing the forces breakdown file (forces_breakdown_pyCAPS_SU2_Tetgen.dat). |Paraview |flow_pyCAPS_SU2_Tetgen.vtu | Writing the forces breakdown file (forces_breakdown_pyCAPS_SU2_Tetgen.dat). |Paraview surface |surface_flow_pyCAPS_SU2_Tetgen.vtu | Writing the forces breakdown file (forces_breakdown_pyCAPS_SU2_Tetgen.dat). +-----------------------------------------------------------------------+ ------------------------- Solver Postprocessing ------------------------- Deleted CNumerics container. Deleted CIntegration container. Deleted CSolver container. Deleted CIteration container. Deleted CInterface container. Deleted CGeometry container. Deleted CFreeFormDefBox class. Deleted CSurfaceMovement class. Deleted CVolumetricMovement class. Deleted CConfig container. Deleted nInst container. Deleted COutput class. ------------------------------------------------------------------------- ------------------------- Exit Success (SU2_CFD) ------------------------ Total Force - Pressure + Viscous Cl = 0.757437 Cd = 0.133203 Cmx = -0.003663 Cmy = -0.214942 Cmz = 0.000732 Cx = 0.119964 Cy = 0.000385 Cz = 0.759646 real 0m9.512s user 0m6.966s sys 0m0.381s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case su2_and_Tetgen_PyTest.py passed (as expected) ================================================= ================================================= + echo 'su2_X43a_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/CFD/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/pyCAPSlog.txt su2_X43a_PyTest.py test; + python -u su2_X43a_PyTest.py -outLevel=0 + tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/CFD/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/pyCAPSlog.txt Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = x43A, index = 1 Name = Farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting surface mesh for body 1 (of 2) Getting surface mesh for body 2 (of 2) Body 1 (of 2) Number of nodes = 3801 Number of elements = 7602 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 7602 Number of quadrilateral elements = 0 Body 2 (of 2) Number of nodes = 5678 Number of elements = 11352 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 11352 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 9479 Total number of elements = 18954 Writing TECPLOT file: egadsTessMesh_Surf_0.dat .... Finished writing TECPLOT file Writing TECPLOT file: egadsTessMesh_Surf_1.dat .... Finished writing TECPLOT file Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = x43A, index = 1 Name = Farfield, index = 2 Number of surface: nodes - 9479, elements - 18954 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000T1.00e-16A Delaunizing vertices... Delaunay seconds: 0.117448 Creating surface mesh ... Surface mesh seconds: 0.033978 Recovering boundaries... Boundary recovery seconds: 0.291223 Removing exterior tetrahedra ... Spreading region attributes. Exterior tets removal seconds: 0.025965 Recovering Delaunayness... Delaunay recovery seconds: 0.050165 Refining mesh... 12636 insertions, added 5271 points, 44 tetrahedra in queue. Refinement seconds: 1.55227 Smoothing vertices... Mesh smoothing seconds: 1.26243 Improving mesh... Mesh improvement seconds: 0.066635 Jettisoning redundant points. Writing nodes. Writing elements. Writing faces. Writing edges. Output seconds: 0.010919 Total running seconds: 3.41154 Statistics: Input points: 9479 Input facets: 18954 Input segments: 28431 Input holes: 1 Input regions: 0 Mesh points: 14884 Mesh tetrahedra: 61455 Mesh faces: 132387 Mesh faces on exterior boundary: 18954 Mesh faces on input facets: 18954 Mesh edges on input segments: 28431 Steiner points inside domain: 5405 Done meshing using TetGen! Writing SU2 file .... Finished writing SU2 file Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - x43A Done getting CFD boundary conditions Warning: The su2 cfg file will be overwritten! Write SU2 configuration file for version "BlackBird (7.5.1) " Running SU2...... ------------------------------------------------------------------------- | ___ _ _ ___ | | / __| | | |_ ) Release 7.5.1 "Blackbird" | | \__ \ |_| |/ / | | |___/\___//___| Suite (Computational Fluid Dynamics Code) | | | ------------------------------------------------------------------------- | SU2 Project Website: https://su2code.github.io | | | | The SU2 Project is maintained by the SU2 Foundation | | (http://su2foundation.org) | ------------------------------------------------------------------------- | Copyright 2012-2023, SU2 Contributors | | | | SU2 is free software; you can redistribute it and/or | | modify it under the terms of the GNU Lesser General Public | | License as published by the Free Software Foundation; either | | version 2.1 of the License, or (at your option) any later version. | | | | SU2 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 | | Lesser General Public License for more details. | | | | You should have received a copy of the GNU Lesser General Public | | License along with SU2. If not, see <http://www.gnu.org/licenses/>. | ------------------------------------------------------------------------- Parsing config file for zone 0 ----------------- Physical Case Definition ( Zone 0 ) ------------------- Compressible Euler equations. Mach number: 3.5. Angle of attack (AoA): 3 deg, and angle of sideslip (AoS): 0 deg. No restart solution, use the values at infinity (freestream). Dimensional simulation. The reference area is 1 m^2. The semi-span will be computed using the max y(3D) value. The reference length is 1 m. Reference origin for moment evaluation is (0, 0, 0). Surface(s) where the force coefficients are evaluated: BC_1. Surface(s) plotted in the output file: BC_1. Input mesh file name: ../myMesh/tetgen_0.su2 --------------- Space Numerical Integration ( Zone 0 ) ------------------ Roe (with entropy fix = 0.001) solver for the flow inviscid terms. Standard Roe without low-dissipation function. Second order integration in space, with slope limiter. Venkatakrishnan slope-limiting method, with constant: 0.05. The reference element size is: 1. Gradient for upwind reconstruction: inverse-distance weighted Least-Squares. Gradient for viscous and source terms: inverse-distance weighted Least-Squares. --------------- Time Numerical Integration ( Zone 0 ) ------------------ Local time stepping (steady state simulation). Euler implicit method for the flow equations. FGMRES is used for solving the linear system. Using a ILU(0) preconditioning. Convergence criteria of the linear solver: 1e-06. Max number of linear iterations: 10. V Multigrid Cycle, with 2 multigrid levels. Damping factor for the residual restriction: 0.75. Damping factor for the correction prolongation: 0.75. No CFL adaptation. +-------------------------------------------+ | MG Level| Presmooth|PostSmooth|CorrectSmo| +-------------------------------------------+ | 0| 1| 0| 0| | 1| 2| 0| 0| | 2| 3| 0| 0| +-------------------------------------------+ Courant-Friedrichs-Lewy number: 10 ------------------ Convergence Criteria ( Zone 0 ) --------------------- Maximum number of solver subiterations: 5. Begin convergence monitoring at iteration 5. Residual minimum value: 1e-14. Cauchy series min. value: 1e-10. Number of Cauchy elements: 100. Begin windowed time average at iteration 0. -------------------- Output Information ( Zone 0 ) ---------------------- File writing frequency: +------------------------------------+ | File| Frequency| +------------------------------------+ | RESTART| 250| | SURFACE_CSV| 250| | PARAVIEW| 250| | SURFACE_PARAVIEW| 250| +------------------------------------+ Writing the convergence history file every 1 inner iterations. Writing the screen convergence history every 1 inner iterations. The tabular file format is CSV (.csv). Convergence history file name: history. Forces breakdown file name: forces_breakdown_x43a_Test.dat. Surface file name: surface_flow_x43a_Test. Volume file name: flow_x43a_Test. Restart file name: restart_flow_x43a_Test.dat. ------------- Config File Boundary Information ( Zone 0 ) --------------- +-----------------------------------------------------------------------+ | Marker Type| Marker Name| +-----------------------------------------------------------------------+ | Euler wall| BC_1| +-----------------------------------------------------------------------+ | Far-field| BC_2| +-----------------------------------------------------------------------+ -------------------- Output Preprocessing ( Zone 0 ) -------------------- WARNING: SURFACE_PRESSURE_DROP can only be computed for at least 2 surfaces (outlet, inlet, ...) Screen output fields: TIME_ITER, OUTER_ITER, INNER_ITER, CUR_TIME, TIME_STEP, WALL_TIME, RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_ENERGY, EFFICIENCY History output group(s): ITER, TIME_DOMAIN, WALL_TIME, RMS_RES, AERO_COEFF Convergence field(s): RMS_DENSITY Warning: No (valid) fields chosen for time convergence monitoring. Time convergence monitoring inactive. Volume output fields: COORDINATES, SOLUTION, PRIMITIVE ------------------- Geometry Preprocessing ( Zone 0 ) ------------------- Three dimensional problem. 14884 grid points. 61455 volume elements. 2 surface markers. 7602 boundary elements in index 0 (Marker = BC_1). 11352 boundary elements in index 1 (Marker = BC_2). 61455 tetrahedra. Setting point connectivity. Renumbering points (Reverse Cuthill McKee Ordering). Recomputing point connectivity. Setting element connectivity. Checking the numerical grid orientation. All volume elements are correctly orientend. All surface elements are correctly orientend. Identifying edges and vertices. Setting the control volume structure. Volume of the computational grid: 2.67745e+08. Searching for the closest normal neighbors to the surfaces. Storing a mapping from global to local point index. Compute the surface curvature. Max K: 95.6599. Mean K: 0.525135. Standard deviation K: 2.58749. Checking for periodicity. Computing mesh quality statistics for the dual control volumes. +--------------------------------------------------------------+ | Mesh Quality Metric| Minimum| Maximum| +--------------------------------------------------------------+ | Orthogonality Angle (deg.)| 2.08531| 84.4135| | CV Face Area Aspect Ratio| 1.31056| 2090.22| | CV Sub-Volume Ratio| 1| 1.13144e+06| +--------------------------------------------------------------+ Setting the multigrid structure. +-------------------------------------------+ | MG Level| CVs|Aggl. Rate| CFL| +-------------------------------------------+ | 0| 14884| 1/1.00| 10| | 1| 2708| 1/5.5| 8.49965| | 2| 490| 1/5.53| 7.21121| +-------------------------------------------+ Finding max control volume width. Semi-span length = 30 m. Wetted area = 13592.9 m^2. Area projection in the x-plane = 761.52 m^2, y-plane = 2060.65 m^2, z-plane = 5463.74 m^2. Max. coordinate in the x-direction = 150 m, y-direction = 30 m, z-direction = 19 m. Min. coordinate in the x-direction = 0 m, y-direction = -30 m, z-direction = -10.3 m. Checking if Euler & Symmetry markers are straight/plane: Boundary marker BC_1 is NOT a single plane. Computing wall distances. -------------------- Solver Preprocessing ( Zone 0 ) -------------------- Inviscid flow: Computing density based on free-stream temperature and pressure using the ideal gas law. Force coefficients computed using free-stream values. -- Models: +------------------------------------------------------------------------------+ | Viscosity Model| Conductivity Model| Fluid Model| +------------------------------------------------------------------------------+ | -| -| STANDARD_AIR| +------------------------------------------------------------------------------+ -- Fluid properties: +------------------------------------------------------------------------------+ | Name| Dim. value| Ref. value| Unit|Non-dim. value| +------------------------------------------------------------------------------+ | Gas Constant| 287.058| 1| N.m/kg.K| 287.058| | Spec. Heat Ratio| -| -| -| 1.4| +------------------------------------------------------------------------------+ -- Initial and free-stream conditions: +------------------------------------------------------------------------------+ | Name| Dim. value| Ref. value| Unit|Non-dim. value| +------------------------------------------------------------------------------+ | Static Pressure| 101325| 1| Pa| 101325| | Density| 1.22498| 1| kg/m^3| 1.22498| | Temperature| 288.15| 1| K| 288.15| | Total Energy| 916077| 1| m^2/s^2| 916077| | Velocity-X| 1189.41| 1| m/s| 1189.41| | Velocity-Y| 0| 1| m/s| 0| | Velocity-Z| 62.3342| 1| m/s| 62.3342| | Velocity Magnitude| 1191.04| 1| m/s| 1191.04| +------------------------------------------------------------------------------+ | Mach Number| -| -| -| 3.5| +------------------------------------------------------------------------------+ Initialize Jacobian structure (Euler). MG level: 0. Initialize Jacobian structure (Euler). MG level: 1. Initialize Jacobian structure (Euler). MG level: 2. ------------------- Numerics Preprocessing ( Zone 0 ) ------------------- ----------------- Integration Preprocessing ( Zone 0 ) ------------------ ------------------- Iteration Preprocessing ( Zone 0 ) ------------------ Euler/Navier-Stokes/RANS fluid iteration. ------------------------------ Begin Solver ----------------------------- Simulation Run using the Single-zone Driver WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better, see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better, see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better, see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations +----------------------------------------------------------------------------------------------------------------------------------------------+ | Time_Iter| Outer_Iter| Inner_Iter| Cur_Time| Time_Step| Time(sec)| rms[Rho]| rms[RhoU]| rms[RhoV]| rms[RhoE]| CEff| +----------------------------------------------------------------------------------------------------------------------------------------------+ | 0| 0| 0| 0.0000e+00| 0.0000e+00| 3.7945e-01| 2.731008| 5.665319| 4.731467| 8.730483| -0.401144| | 0| 0| 1| 0.0000e+00| 0.0000e+00| 3.9952e-01| 3.170324| 6.219154| 5.698493| 9.178926| -0.118433| | 0| 0| 2| 0.0000e+00| 0.0000e+00| 3.7932e-01| 3.293104| 6.361720| 5.746884| 9.254295| -0.044919| | 0| 0| 3| 0.0000e+00| 0.0000e+00| 3.5850e-01| 3.250958| 6.318931| 5.673519| 9.221763| -0.034783| | 0| 0| 4| 0.0000e+00| 0.0000e+00| 3.3923e-01| 3.162927| 6.214039| 5.564073| 9.142969| -0.051969| ----------------------------- Solver Exit ------------------------------- Maximum number of iterations reached (ITER = 5) before convergence. +-----------------------------------------------------------------------+ | Convergence Field | Value | Criterion | Converged | +-----------------------------------------------------------------------+ | rms[Rho]| 3.16293| < -14| No| +-----------------------------------------------------------------------+ ------------------------------------------------------------------------- +-----------------------------------------------------------------------+ | File Writing Summary | Filename | +-----------------------------------------------------------------------+ |SU2 binary restart |restart_flow_x43a_Test.dat | Writing the forces breakdown file (forces_breakdown_x43a_Test.dat). |CSV file |surface_flow_x43a_Test.csv | Writing the forces breakdown file (forces_breakdown_x43a_Test.dat). |Paraview |flow_x43a_Test.vtu | Writing the forces breakdown file (forces_breakdown_x43a_Test.dat). |Paraview surface |surface_flow_x43a_Test.vtu | Writing the forces breakdown file (forces_breakdown_x43a_Test.dat). +-----------------------------------------------------------------------+ Warning: there are 129 non-physical points in the solution. Warning: 57 reconstructed states for upwinding are non-physical. ------------------------- Solver Postprocessing ------------------------- Deleted CNumerics container. Deleted CIntegration container. Deleted CSolver container. Deleted CIteration container. Deleted CInterface container. Deleted CGeometry container. Deleted CFreeFormDefBox class. Deleted CSurfaceMovement class. Deleted CVolumetricMovement class. Deleted CConfig container. Deleted nInst container. Deleted COutput class. ------------------------------------------------------------------------- ------------------------- Exit Success (SU2_CFD) ------------------------ Total Force - Pressure + Viscous Cl = -5.94765 Cd = 114.445668 Cmx = -14.939628 Cmy = 9349.058596 Cmz = -28.196104 Cx = 114.6001 Cy = -0.864184 Cz = 0.050124 real 0m21.960s user 0m25.330s sys 0m0.767s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case su2_X43a_PyTest.py passed (as expected) ================================================= ./execute_PyTestRegression.sh: line 405: ulimit: stack size: cannot modify limit: Operation not permitted flowCart: /Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC//flowCart ================================================= + echo 'cart3d_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/CFD/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/pyCAPSlog.txt cart3d_PyTest.py test; + python -u cart3d_PyTest.py -outLevel=0 + tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/CFD/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/pyCAPSlog.txt Loading AIM Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = Wing, index = 1 Body size = 3.796888 Tessellating body 1 with MaxEdge = 0.094922 Sag = 0.003797 Angle = 15.000000 Executing: autoInputs -r 30.000000 -nDiv 6 -maxR 9 > autoInputs.out Executing: ./aero.csh > aero.out C_A 0.050108722 C_Y -0.0015626888 C_N 0.0065057682 C_D 0.050305245 C_S -0.0015626888 C_L 0.0047530359 C_l 0.00381162 C_m -0.00346146 C_n -0.0401149 C_M_x 0.00240931 C_M_y -0.00346146 C_M_z -0.0402235 real 0m37.501s user 0m32.447s sys 0m1.784s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case cart3d_PyTest.py passed (as expected) ================================================= ================================================= + echo 'cart3d_OpenMDAO_3_alpha_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/CFD/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/pyCAPSlog.txt cart3d_OpenMDAO_3_alpha_PyTest.py test; + python -u cart3d_OpenMDAO_3_alpha_PyTest.py -outLevel=0 + tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/CFD/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/pyCAPSlog.txt ---------------------------------------- >>> alpha [2.] Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = Wing, index = 1 Getting CFD design variables....... Number of design variables - 1 Design Variable name - alpha Done getting CFD design variables Getting CFD functional....... Number of design variables - 1 Objective name - CL2 Done getting CFD functional Body size = 3.625615 Tessellating body 1 with MaxEdge = 0.090640 Sag = 0.003626 Angle = 15.000000 Executing: autoInputs -r 30.000000 -nDiv 5 -maxR 7 -mesh2d > autoInputs.out o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (00:49:36) Running aero.csh on 2 core(s) in M0.5901A2B0_DP1 (00:49:43) aero.csh done o case M0.5901A2B0_DP1, averaging data over 1 cycle(s) >>> CL2 [0.01631562] CL 0.12773309 ---------------------------------------- ---------------------------------------- >>> alpha [2.] >>> CL2 [0.01631562] CL 0.12773309 ---------------------------------------- ======================================== o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (00:49:44) Running aero.csh on 2 core(s) in M0.5901A2B0_DP1 (00:49:54) aero.csh done Max memory allowed: 32 GB Flow hexes: 2188 Estimated cutter memory: 0.000219 GB / DV Estimated xsensit memory: 0.004157 GB / DV Available threads: 2 # DVs: 1 o Number of simultaneous cutter jobs: 1 (00:49:54) Linearizing cut-cells (00:49:54) ... done o Number of simultaneous xsensit jobs: 1 (00:49:54) Computing gradients (00:49:58) ... done o case M0.5901A2B0_DP1, averaging data over 1 cycle(s) >>> CL2_alpha [[0.01572627]] ======================================== RUNNING THE L-BFGS-B CODE * * * Machine precision = 2.220D-16 N = 1 M = 10 At X0 0 variables are exactly at the bounds At iterate 0 f= 1.63156D-02 |proj g|= 1.57263D-02 ---------------------------------------- >>> alpha [1.98427373] o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (00:49:59) Running aero.csh on 2 core(s) in M0.5901A1.98427B0_DP1 (00:50:09) aero.csh done o case M0.5901A1.98427B0_DP1, averaging data over 1 cycle(s) >>> CL2 [0.01606724] CL 0.12675617 ---------------------------------------- ======================================== o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (00:50:10) Running aero.csh on 2 core(s) in M0.5901A1.98427B0_DP1 (00:50:22) aero.csh done Max memory allowed: 32 GB Flow hexes: 2188 Estimated cutter memory: 0.000219 GB / DV Estimated xsensit memory: 0.004157 GB / DV Available threads: 2 # DVs: 1 o Number of simultaneous cutter jobs: 1 (00:50:22) Linearizing cut-cells (00:50:22) ... done o Number of simultaneous xsensit jobs: 1 (00:50:22) Computing gradients (00:50:26) ... done o case M0.5901A1.98427B0_DP1, averaging data over 1 cycle(s) >>> CL2_alpha [[0.01560329]] ======================================== At iterate 1 f= 1.60672D-02 |proj g|= 1.56033D-02 ---------------------------------------- >>> alpha [-0.01099175] o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (00:50:27) Running aero.csh on 2 core(s) in M0.5901A-0.0109917B0_DP1 (00:50:32) aero.csh done o case M0.5901A-0.0109917B0_DP1, averaging data over 1 cycle(s) >>> CL2 [6.05653711e-06] CL 0.00246101 ---------------------------------------- ======================================== o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (00:50:32) Running aero.csh on 2 core(s) in M0.5901A-0.0109917B0_DP1 (00:50:39) aero.csh done Max memory allowed: 32 GB Flow hexes: 2188 Estimated cutter memory: 0.000219 GB / DV Estimated xsensit memory: 0.004157 GB / DV Available threads: 2 # DVs: 1 o Number of simultaneous cutter jobs: 1 (00:50:40) Linearizing cut-cells (00:50:40) ... done o Number of simultaneous xsensit jobs: 1 (00:50:40) Computing gradients (00:50:44) ... done o case M0.5901A-0.0109917B0_DP1, averaging data over 1 cycle(s) >>> CL2_alpha [[0.00031042]] ======================================== At iterate 2 f= 6.05654D-06 |proj g|= 3.10424D-04 ---------------------------------------- >>> alpha [-0.05149286] o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (00:50:45) Running aero.csh on 2 core(s) in M0.5901A-0.0514929B0_DP1 (00:50:49) aero.csh done o case M0.5901A-0.0514929B0_DP1, averaging data over 1 cycle(s) >>> CL2 [2.59817062e-10] CL 1.612e-05 ---------------------------------------- ======================================== o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (00:50:50) Running aero.csh on 2 core(s) in M0.5901A-0.0514929B0_DP1 (00:50:55) aero.csh done Max memory allowed: 32 GB Flow hexes: 2188 Estimated cutter memory: 0.000219 GB / DV Estimated xsensit memory: 0.004157 GB / DV Available threads: 2 # DVs: 1 o Number of simultaneous cutter jobs: 1 (00:50:55) Linearizing cut-cells (00:50:55) ... done o Number of simultaneous xsensit jobs: 1 (00:50:55) Computing gradients (00:50:59) ... done o case M0.5901A-0.0514929B0_DP1, averaging data over 1 cycle(s) >>> CL2_alpha [[2.03612433e-06]] ======================================== At iterate 3 f= 2.59817D-10 |proj g|= 2.03612D-06 ---------------------------------------- >>> alpha [-0.05176027] o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (00:51:00) Running aero.csh on 2 core(s) in M0.5901A-0.0517603B0_DP1 (00:51:04) aero.csh done o case M0.5901A-0.0517603B0_DP1, averaging data over 1 cycle(s) >>> CL2 [9.25766089e-15] CL 1e-07 ---------------------------------------- ======================================== o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (00:51:05) Running aero.csh on 2 core(s) in M0.5901A-0.0517603B0_DP1 (00:51:09) aero.csh done Max memory allowed: 32 GB Flow hexes: 2188 Estimated cutter memory: 0.000219 GB / DV Estimated xsensit memory: 0.004157 GB / DV Available threads: 2 # DVs: 1 o Number of simultaneous cutter jobs: 1 (00:51:09) Linearizing cut-cells (00:51:09) ... done o Number of simultaneous xsensit jobs: 1 (00:51:09) Computing gradients (00:51:13) ... done o case M0.5901A-0.0517603B0_DP1, averaging data over 1 cycle(s) >>> CL2_alpha [[1.21372408e-08]] ======================================== At iterate 4 f= 9.25766D-15 |proj g|= 1.21372D-08 * * * Tit = total number of iterations Tnf = total number of function evaluations Tnint = total number of segments explored during Cauchy searches Skip = number of BFGS updates skipped Nact = number of active bounds at final generalized Cauchy point Projg = norm of the final projected gradient F = final function value * * * N Tit Tnf Tnint Skip Nact Projg F 1 4 5 4 0 0 1.214D-08 9.258D-15 F = 9.2576608860000000E-015 CONVERGENCE: NORM_OF_PROJECTED_GRADIENT_<=_PGTOL Optimization Complete ----------------------------------- Optimized value: [-0.05176027] real 1m44.923s user 0m53.349s sys 0m10.800s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case cart3d_OpenMDAO_3_alpha_PyTest.py passed (as expected) ================================================= ================================================= + echo 'cart3d_OpenMDAO_3_twist_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/CFD/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/pyCAPSlog.txt cart3d_OpenMDAO_3_twist_PyTest.py test; + python -u cart3d_OpenMDAO_3_twist_PyTest.py -outLevel=0 + tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/CFD/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/pyCAPSlog.txt ---------------------------------------- >>> twist [4.] Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = Wing, index = 1 Getting CFD design variables....... Number of design variables - 1 Design Variable name - twist Done getting CFD design variables Getting CFD functional....... Number of design variables - 1 Objective name - CL2 Done getting CFD functional Body size = 3.630958 Tessellating body 1 with MaxEdge = 0.018155 Sag = 0.000908 Angle = 10.000000 Executing: autoInputs -r 5.123450 -nDiv 5 -maxR 7 -symmY -halfBody > autoInputs.out o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (00:51:19) Running aero.csh on 2 core(s) in M0.5901A0B0_DP1 (00:51:41) aero.csh done o case M0.5901A0B0_DP1, averaging data over 1 cycle(s) >>> CL2 [0.00411365] CL 0.0641354 ---------------------------------------- ---------------------------------------- >>> twist [4.] >>> CL2 [0.00411365] CL 0.0641354 ---------------------------------------- ======================================== o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (00:51:43) Running aero.csh on 2 core(s) in M0.5901A0B0_DP1 (00:52:18) aero.csh done Max memory allowed: 32 GB Flow hexes: 37528 Estimated cutter memory: 0.003753 GB / DV Estimated xsensit memory: 0.071303 GB / DV Available threads: 2 # DVs: 1 o Number of simultaneous cutter jobs: 1 (00:52:18) Linearizing cut-cells (00:52:20) ... done o Number of simultaneous xsensit jobs: 1 (00:52:20) Computing gradients (00:52:24) ... done o case M0.5901A0B0_DP1, averaging data over 1 cycle(s) >>> CL2_twist [[0.00210028]] ======================================== RUNNING THE L-BFGS-B CODE * * * Machine precision = 2.220D-16 N = 1 M = 10 At X0 0 variables are exactly at the bounds At iterate 0 f= 4.11365D-03 |proj g|= 2.10028D-03 ---------------------------------------- >>> twist [3.99789972] Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = Wing, index = 1 Body size = 3.630955 Tessellating body 1 with MaxEdge = 0.018155 Sag = 0.000908 Angle = 10.000000 Executing: autoInputs -r 5.123450 -nDiv 5 -maxR 7 -symmY -halfBody > autoInputs.out o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (00:52:29) Running aero.csh on 2 core(s) in M0.5901A0B0_DP1 (00:52:58) aero.csh done o case M0.5901A0B0_DP1, averaging data over 1 cycle(s) >>> CL2 [0.00411054] CL 0.0641174 ---------------------------------------- ======================================== o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (00:53:00) Running aero.csh on 2 core(s) in M0.5901A0B0_DP1 (00:53:38) aero.csh done Max memory allowed: 32 GB Flow hexes: 37527 Estimated cutter memory: 0.003753 GB / DV Estimated xsensit memory: 0.071301 GB / DV Available threads: 2 # DVs: 1 o Number of simultaneous cutter jobs: 1 (00:53:38) Linearizing cut-cells (00:53:40) ... done o Number of simultaneous xsensit jobs: 1 (00:53:40) Computing gradients (00:53:44) ... done o case M0.5901A0B0_DP1, averaging data over 1 cycle(s) >>> CL2_twist [[0.00209952]] ======================================== At iterate 1 f= 4.11054D-03 |proj g|= 2.09952D-03 ---------------------------------------- >>> twist [-1.82261057] Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = Wing, index = 1 Body size = 3.627721 Tessellating body 1 with MaxEdge = 0.018139 Sag = 0.000907 Angle = 10.000000 Executing: autoInputs -r 5.123450 -nDiv 5 -maxR 7 -symmY -halfBody > autoInputs.out o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (00:53:48) Running aero.csh on 2 core(s) in M0.5901A0B0_DP1 (00:54:17) aero.csh done o case M0.5901A0B0_DP1, averaging data over 1 cycle(s) >>> CL2 [0.00078733] CL -0.0280594 ---------------------------------------- ======================================== o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (00:54:19) Running aero.csh on 2 core(s) in M0.5901A0B0_DP1 (00:54:56) aero.csh done Max memory allowed: 32 GB Flow hexes: 37740 Estimated cutter memory: 0.003774 GB / DV Estimated xsensit memory: 0.071706 GB / DV Available threads: 2 # DVs: 1 o Number of simultaneous cutter jobs: 1 (00:54:56) Linearizing cut-cells (00:54:58) ... done o Number of simultaneous xsensit jobs: 1 (00:54:58) Computing gradients (00:55:02) ... done o case M0.5901A0B0_DP1, averaging data over 1 cycle(s) >>> CL2_twist [[-0.00094375]] ======================================== At iterate 2 f= 7.87327D-04 |proj g|= 9.43751D-04 ---------------------------------------- >>> twist [-0.01761029] Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = Wing, index = 1 Body size = 3.625633 Tessellating body 1 with MaxEdge = 0.018128 Sag = 0.000906 Angle = 10.000000 Executing: autoInputs -r 5.123450 -nDiv 5 -maxR 7 -symmY -halfBody > autoInputs.out o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (00:55:07) Running aero.csh on 2 core(s) in M0.5901A0B0_DP1 (00:55:32) aero.csh done o case M0.5901A0B0_DP1, averaging data over 1 cycle(s) >>> CL2 [1.54159154e-06] CL 0.00123667 ---------------------------------------- ======================================== o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (00:55:35) Running aero.csh on 2 core(s) in M0.5901A0B0_DP1 (00:56:05) aero.csh done Max memory allowed: 32 GB Flow hexes: 38636 Estimated cutter memory: 0.003864 GB / DV Estimated xsensit memory: 0.073408 GB / DV Available threads: 2 # DVs: 1 o Number of simultaneous cutter jobs: 1 (00:56:05) Linearizing cut-cells (00:56:07) ... done o Number of simultaneous xsensit jobs: 1 (00:56:07) Computing gradients (00:56:11) ... done o case M0.5901A0B0_DP1, averaging data over 1 cycle(s) >>> CL2_twist [[4.14681618e-05]] ======================================== At iterate 3 f= 1.54159D-06 |proj g|= 4.14682D-05 ---------------------------------------- >>> twist [-0.09358328] Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = Wing, index = 1 Body size = 3.625710 Tessellating body 1 with MaxEdge = 0.018129 Sag = 0.000906 Angle = 10.000000 Executing: autoInputs -r 5.123450 -nDiv 5 -maxR 7 -symmY -halfBody > autoInputs.out o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (00:56:16) Running aero.csh on 2 core(s) in M0.5901A0B0_DP1 (00:56:39) aero.csh done o case M0.5901A0B0_DP1, averaging data over 1 cycle(s) >>> CL2 [6.09327521e-07] CL 0.00078708 ---------------------------------------- ======================================== o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (00:56:41) Running aero.csh on 2 core(s) in M0.5901A0B0_DP1 (00:57:12) aero.csh done Max memory allowed: 32 GB Flow hexes: 37755 Estimated cutter memory: 0.003776 GB / DV Estimated xsensit memory: 0.071735 GB / DV Available threads: 2 # DVs: 1 o Number of simultaneous cutter jobs: 1 (00:57:13) Linearizing cut-cells (00:57:15) ... done o Number of simultaneous xsensit jobs: 1 (00:57:15) Computing gradients (00:57:19) ... done o case M0.5901A0B0_DP1, averaging data over 1 cycle(s) >>> CL2_twist [[2.5850485e-05]] ======================================== At iterate 4 f= 6.09328D-07 |proj g|= 2.58505D-05 * * * Tit = total number of iterations Tnf = total number of function evaluations Tnint = total number of segments explored during Cauchy searches Skip = number of BFGS updates skipped Nact = number of active bounds at final generalized Cauchy point Projg = norm of the final projected gradient F = final function value * * * N Tit Tnf Tnint Skip Nact Projg F 1 4 5 4 0 0 2.585D-05 6.093D-07 F = 6.0932752137000000E-007 CONVERGENCE: REL_REDUCTION_OF_F_<=_FACTR*EPSMCH Optimization Complete ----------------------------------- Optimized values: [-0.09358328] real 6m5.624s user 6m54.434s sys 0m21.786s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case cart3d_OpenMDAO_3_twist_PyTest.py passed (as expected) ================================================= ================================================= + echo 'fun3d_Morph_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/CFD/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/pyCAPSlog.txt fun3d_Morph_PyTest.py test; + python -u fun3d_Morph_PyTest.py -outLevel=0 -noAnalysis + tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/CFD/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/pyCAPSlog.txt Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 AFLR4 : Proximity BG Surface Grid Generation Skipped AFLR4 : No Modifications Required Writing TECPLOT file: pyCAPS_AFLR4_AFLR3.dat .... Finished writing TECPLOT file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Getting volume mesh AFLR2 : --------------------------------------- AFLR2 : AFLR2 LIBRARY AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR2 : TRIA/QUAD GRID GENERATOR AFLR2 : Version Number 9.14.7 AFLR2 : Version Date 07/16/23 @ 01:42PM AFLR2 : Compile OS Darwin 22.5.0 arm64 AFLR2 : Compile Date 07/16/23 @ 01:42PM AFLR2 : Copyright 1994-2021, D.L. Marcum AFLR2 : --------------------------------------- AFLR4 : --------------------------------------- AFLR4 : AFLR4 LIBRARY AFLR4 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR4 : TRIA/QUAD SURFACE GRID GENERATOR AFLR4 : Version Number 11.5.8 AFLR4 : Version Date 07/24/23 @ 06:11PM AFLR4 : Compile OS Darwin 22.5.0 arm64 AFLR4 : Compile Date 07/24/23 @ 06:11PM AFLR4 : Copyright 1994-2021, D.L. Marcum AFLR4 : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.24 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.24 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- : XYZ DEVIATION > TOLERANCE AT 1 NODES ON EDGE 2 : MAX XYZ DEVIATION 0.00694484 TOLERANCE 0.00121633 AT NODE 20 : INPUT EDGE COORDINATE T 0.998276 : INPUT X,Y,Z COORDINATES 0, 0, 0 : EVALUATED X,Y,Z COORDINATES -0.0021459, 4.04439e-19, 0.006605 : XYZ DEVIATION > TOLERANCE AT 1 NODES ON EDGE 4 : MAX XYZ DEVIATION 0.00687648 TOLERANCE 0.00131756 AT NODE 40 : INPUT EDGE COORDINATE T 0.996516 : INPUT X,Y,Z COORDINATES 4.08248, 7.07107, 0.123426 : EVALUATED X,Y,Z COORDINATES 4.08454, 7.07107, 0.129988 : XYZ DEVIATION > TOLERANCE AT 20 NODES ON EDGE 5 : MAX XYZ DEVIATION 0.00468154 TOLERANCE 0.00167181 AT NODE 20 : INPUT EDGE COORDINATE T 0.998768 : INPUT X,Y,Z COORDINATES 3.77001, -2.81137e-19, -0.00459131 : EVALUATED X,Y,Z COORDINATES 3.76537, -2.45219e-19, -0.00400473 : XYZ DEVIATION > TOLERANCE AT 39 NODES ON EDGE 7 : MAX XYZ DEVIATION 0.00692405 TOLERANCE 5.41787e-05 AT NODE 39 : INPUT EDGE COORDINATE T 0.996486 : INPUT X,Y,Z COORDINATES 5.90283, 7.07107, -0.368433 : EVALUATED X,Y,Z COORDINATES 5.8959, 7.07107, -0.368207 : XYZ DEVIATION > TOLERANCE AT 1 NODES ON EDGE 12 : MAX XYZ DEVIATION 0.00690409 TOLERANCE 0.00132091 AT NODE 40 : INPUT EDGE COORDINATE T 0.996502 : INPUT X,Y,Z COORDINATES 4.08248, -7.07107, 0.123426 : EVALUATED X,Y,Z COORDINATES 4.08455, -7.07107, 0.130014 : XYZ DEVIATION > TOLERANCE AT 39 NODES ON EDGE 14 : MAX XYZ DEVIATION 0.00690732 TOLERANCE 5.37685e-05 AT NODE 39 : INPUT EDGE COORDINATE T 0.996494 : INPUT X,Y,Z COORDINATES 5.90283, -7.07107, -0.368433 : EVALUATED X,Y,Z COORDINATES 5.89592, -7.07107, -0.368208 : XYZ DEVIATION > TOLERANCE AT 1 NODES ON EDGE 17 : MAX XYZ DEVIATION 0.0168917 TOLERANCE 0.00322032 AT NODE 5 : INPUT EDGE COORDINATE T 0.989329 : INPUT X,Y,Z COORDINATES 10, 0, 0 : EVALUATED X,Y,Z COORDINATES 9.99966, 1.03411e-18, 0.0168883 : XYZ DEVIATION > TOLERANCE AT 1 NODES ON EDGE 19 : MAX XYZ DEVIATION 0.0024621 TOLERANCE 0.000634929 AT NODE 39 : INPUT EDGE COORDINATE T 0.996882 : INPUT X,Y,Z COORDINATES 11.633, 2.82843, 0.0493704 : EVALUATED X,Y,Z COORDINATES 11.6337, 2.82843, 0.051723 : XYZ DEVIATION > TOLERANCE AT 5 NODES ON EDGE 20 : MAX XYZ DEVIATION 0.00842987 TOLERANCE 0.0028058 AT NODE 5 : INPUT EDGE COORDINATE T 0.994455 : INPUT X,Y,Z COORDINATES 11.508, -1.12455e-19, -0.00183653 : EVALUATED X,Y,Z COORDINATES 11.4996, -4.80733e-20, -0.000785096 : XYZ DEVIATION > TOLERANCE AT 38 NODES ON EDGE 22 : MAX XYZ DEVIATION 0.00240351 TOLERANCE 2.21881e-05 AT NODE 38 : INPUT EDGE COORDINATE T 0.99695 : INPUT X,Y,Z COORDINATES 12.3611, 2.82843, -0.147373 : EVALUATED X,Y,Z COORDINATES 12.3587, 2.82843, -0.147295 : XYZ DEVIATION > TOLERANCE AT 1 NODES ON EDGE 27 : MAX XYZ DEVIATION 0.00250778 TOLERANCE 0.000640121 AT NODE 39 : INPUT EDGE COORDINATE T 0.996824 : INPUT X,Y,Z COORDINATES 11.633, -2.82843, 0.0493704 : EVALUATED X,Y,Z COORDINATES 11.6337, -2.82843, 0.0517662 : XYZ DEVIATION > TOLERANCE AT 38 NODES ON EDGE 29 : MAX XYZ DEVIATION 0.00238522 TOLERANCE 2.20962e-05 AT NODE 38 : INPUT EDGE COORDINATE T 0.996974 : INPUT X,Y,Z COORDINATES 12.3611, -2.82843, -0.147373 : EVALUATED X,Y,Z COORDINATES 12.3587, -2.82843, -0.147296 : XYZ DEVIATION > TOLERANCE AT 6 NODES ON EDGE 32 : MAX XYZ DEVIATION 0.450685 TOLERANCE 0.231543 AT NODE 11 : INPUT EDGE COORDINATE T 1.56516 : INPUT X,Y,Z COORDINATES 4.89859e-15, -1.19981e-30, 80 : EVALUATED X,Y,Z COORDINATES -0.450683, 5.51928e-17, 79.9987 : XYZ DEVIATION > TOLERANCE AT 6 NODES ON EDGE 34 : MAX XYZ DEVIATION 0.450695 TOLERANCE 0.231783 AT NODE 11 : INPUT EDGE COORDINATE T 7.84835 : INPUT X,Y,Z COORDINATES 4.89859e-15, -1.19981e-30, 80 : EVALUATED X,Y,Z COORDINATES 0.450694, -1.10388e-16, 79.9987 *** NON-FATAL EGADS ERROR 3299 *** *** COORDINATES FOUND THAT DEVIATE FROM EGADS GEOMETRY *** Volume mesh: Number of nodes = 85215 Number of elements = 497264 Number of triangles = 15680 Number of quadrilatarals = 0 Number of tetrahedrals = 481584 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing TECPLOT file: pyCAPS_AFLR4_AFLR3_VolMesh.dat .... Finished writing TECPLOT file Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - Wing2 Done getting CFD boundary conditions Getting CFD design variables....... Number of design variables - 2 Design Variable name - Alpha Design Variable name - twist Done getting CFD design variables Getting CFD functional....... Number of design variables - 2 Objective name - Cd2 Objective name - Const Done getting CFD functional Python library was linked, but will not be used! Creating FUN3D directory tree DesignVariable = Alpha DesignVariable = twist Writing sensitivity file for body 1, File - Rubberize/model.tec.1.sd1 Writing sensitivity file for body 2, File - Rubberize/model.tec.2.sd1 Writing sensitivity file for body 3, File - Rubberize/model.tec.3.sd1 Writing rubber.data Writing surface file for 1 (of 3) in body 1 File - Flow/fun3dAFLRTest_body1.dat Writing surface file for 1 (of 3) in body 1 File - Flow/fun3dAFLRTest_body1.dat Writing surface file for 1 (of 3) in body 1 File - Flow/fun3dAFLRTest_body1.dat Writing MAPBC file .... Finished writing MAPBC file Warning: The fun3d.nml file will be overwritten! Writing fun3d.nml Info: No recognized data transfer names found. Reading rubber.data Projecting tessellation 1 (of 3) on to new body Projecting tessellation 2 (of 3) on to new body Projecting tessellation 3 (of 3) on to new body Python library was linked, but will not be used! Creating FUN3D directory tree DesignVariable = Alpha DesignVariable = twist Writing sensitivity file for body 1, File - Rubberize/model.tec.1.sd1 Writing sensitivity file for body 2, File - Rubberize/model.tec.2.sd1 Writing sensitivity file for body 3, File - Rubberize/model.tec.3.sd1 Writing surface file for 1 (of 3) in body 1 File - Flow/fun3dAFLRTest_body1.dat Writing surface file for 1 (of 3) in body 1 File - Flow/fun3dAFLRTest_body1.dat Writing surface file for 1 (of 3) in body 1 File - Flow/fun3dAFLRTest_body1.dat Writing MAPBC file .... Finished writing MAPBC file Warning: The fun3d.nml file will be overwritten! Writing fun3d.nml Info: No recognized data transfer names found. Reading rubber.data real 0m14.391s user 0m13.321s sys 0m0.623s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case fun3d_Morph_PyTest.py passed (as expected) ================================================= ************************************************* ************************************************* ================================================= Did not run examples for: Fun3D ================================================= All tests pass! ================================================= ================================================= [GNU C Compiler (gcc)] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/CFD/DARWIN_ARM64') [GNU C Compiler (gcc)] Successfully parsed console log [GNU C Compiler (gcc)] -> found 0 issues (skipped 0 duplicates) [GNU C Compiler (gcc)] Skipping post processing [GNU C Compiler (gcc)] No filter has been set, publishing all 0 issues [GNU C Compiler (gcc)] Repository miner is not configured, skipping repository mining [Clang] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/CFD/DARWIN_ARM64') [Clang] -> found 0 issues (skipped 0 duplicates) [Clang] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/CFD/DARWIN_ARM64') [Clang] -> found 0 issues (skipped 0 duplicates) [Clang] Successfully parsed console log [Clang] -> found 0 issues (skipped 0 duplicates) [Clang] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/CFD/DARWIN_ARM64') [Clang] Skipping post processing [Clang] No filter has been set, publishing all 0 issues [Clang] Repository miner is not configured, skipping repository mining [Static Analysis] Successfully parsed console log [Static Analysis] -> found 0 issues (skipped 0 duplicates) [Static Analysis] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/CFD/DARWIN_ARM64') [Static Analysis] Successfully parsed console log [Static Analysis] -> found 0 issues (skipped 0 duplicates) [Static Analysis] Skipping post processing [Static Analysis] No filter has been set, publishing all 0 issues [Static Analysis] Repository miner is not configured, skipping repository mining [Static Analysis] Successfully parsed console log [Static Analysis] -> found 0 issues (skipped 0 duplicates) [Static Analysis] Successfully parsed console log [Static Analysis] -> found 0 issues (skipped 0 duplicates) [Static Analysis] Successfully parsed console log [Static Analysis] -> found 0 issues (skipped 0 duplicates) [Static Analysis] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/CFD/DARWIN_ARM64') [Static Analysis] Skipping post processing [Static Analysis] No filter has been set, publishing all 0 issues [Static Analysis] Repository miner is not configured, skipping repository mining [Static Analysis] Reference build recorder is not configured [Static Analysis] Obtaining reference build from same job (7.7,CAPS/CFD,DARWIN_ARM64,viggen) [Static Analysis] Using reference build 'ESP_UndefinedCaps/CASREV=7.7,ESPTEST=CAPS/CFD,ESP_ARCH=DARWIN_ARM64,buildnode=viggen #183' to compute new, fixed, and outstanding issues [Static Analysis] Issues delta (vs. reference build): outstanding: 0, new: 0, fixed: 0 [Static Analysis] Evaluating quality gates [Static Analysis] -> PASSED - Total (any severity): 0 - Quality Gate: 1 [Static Analysis] -> All quality gates have been passed [Static Analysis] Health report is disabled - skipping [Static Analysis] Created analysis result for 0 issues (found 0 new issues, fixed 0 issues) [Static Analysis] Attaching ResultAction with ID 'analysis' to build 'ESP_UndefinedCaps/CASREV=7.7,ESPTEST=CAPS/CFD,ESP_ARCH=DARWIN_ARM64,buildnode=viggen #185'. [Checks API] No suitable checks publisher found. [PostBuildScript] - [INFO] Executing post build scripts. [PostBuildScript] - [INFO] build step #0 should only be executed on MATRIX [WS-CLEANUP] Deleting project workspace... [WS-CLEANUP] done Finished: SUCCESS