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Skipping 474 KB.. Full Log| 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| 9.8054e-02| 0.071067| 2.739763| 1.616077| 5.599701| 0.055267| | 0| 0| 1| 0.0000e+00| 0.0000e+00| 9.4128e-02| -0.447576| 2.193837| 1.571349| 5.070382| 0.046028| | 0| 0| 2| 0.0000e+00| 0.0000e+00| 9.2965e-02| -0.561159| 2.074597| 1.490746| 4.953698| 0.033910| | 0| 0| 3| 0.0000e+00| 0.0000e+00| 9.4134e-02| -0.723326| 1.921155| 1.390756| 4.790278| 0.049695| | 0| 0| 4| 0.0000e+00| 0.0000e+00| 9.3985e-02| -0.876572| 1.825653| 1.275093| 4.637161| 0.133976| | 0| 0| 5| 0.0000e+00| 0.0000e+00| 9.1936e-02| -1.029177| 1.759196| 1.156078| 4.482282| 0.368542| | 0| 0| 6| 0.0000e+00| 0.0000e+00| 9.0373e-02| -1.215334| 1.704909| 1.114966| 4.286060| 0.974759| | 0| 0| 7| 0.0000e+00| 0.0000e+00| 9.0997e-02| -1.329970| 1.644937| 1.145030| 4.116982| 2.716332| | 0| 0| 8| 0.0000e+00| 0.0000e+00| 8.9211e-02| -1.270672| 1.570739| 1.155400| 4.139480| 16.569216| | 0| 0| 9| 0.0000e+00| 0.0000e+00| 8.9655e-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 0m4.579s user 0m4.423s sys 0m0.998s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case su2_and_AFLR2_PyTest.py passed (as expected) ================================================= ================================================= + echo 'su2_and_AFLR4_AFLR3_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/CFD/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt 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/DARWIN64/ESP/DARWIN64/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 9.14.6 AFLR2 : Version Date 11/20/22 @ 09:21PM AFLR2 : Compile OS Darwin 22.3.0 arm64 AFLR2 : Compile Date 03/08/23 @ 05:14PM 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 11.4.5 AFLR4 : Version Date 04/20/23 @ 05:37PM AFLR4 : Compile OS Darwin 22.3.0 x86_64 AFLR4 : Compile Date 04/20/23 @ 11:55PM AFLR4 : Copyright 1994-2021, D.L. Marcum AFLR4 : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.23 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.23 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 39312 Number of elements = 226864 Number of triangles = 12446 Number of quadrilatarals = 0 Number of tetrahedrals = 214418 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. 39312 grid points. 214418 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). 214418 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.)| 17.1608| 84.739| | CV Face Area Aspect Ratio| 1.11815| 37015.5| | CV Sub-Volume Ratio| 1.04044| 455686| +--------------------------------------------------------------+ Setting the multigrid structure. +-------------------------------------------+ | MG Level| CVs|Aggl. Rate| CFL| +-------------------------------------------+ | 0| 39312| 1/1.00| 10| | 1| 6485| 1/6.06| 8.22658| | 2| 1015| 1/6.39| 6.65012| +-------------------------------------------+ 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| 1.4420e+00| -0.064586| 2.297676| 2.033300| 5.426310| 1.967108| | 0| 0| 1| 0.0000e+00| 0.0000e+00| 1.3603e+00| -0.028142| 2.443813| 2.177084| 5.469820| 2.669025| | 0| 0| 2| 0.0000e+00| 0.0000e+00| 1.3359e+00| 0.006388| 2.521945| 2.416533| 5.497519| 4.072698| | 0| 0| 3| 0.0000e+00| 0.0000e+00| 1.3439e+00| -0.032771| 2.543134| 2.541766| 5.444377| 5.959388| | 0| 0| 4| 0.0000e+00| 0.0000e+00| 1.3329e+00| -0.059484| 2.561671| 2.593774| 5.414288| 7.593451| | 0| 0| 5| 0.0000e+00| 0.0000e+00| 1.3156e+00| -0.076814| 2.565225| 2.615896| 5.407625| 8.782803| | 0| 0| 6| 0.0000e+00| 0.0000e+00| 1.3003e+00| -0.111978| 2.544207| 2.636258| 5.381265| 9.653546| | 0| 0| 7| 0.0000e+00| 0.0000e+00| 1.2869e+00| -0.156369| 2.495539| 2.651467| 5.333878| 10.185394| | 0| 0| 8| 0.0000e+00| 0.0000e+00| 1.2846e+00| -0.203072| 2.428150| 2.650114| 5.275471| 10.322264| | 0| 0| 9| 0.0000e+00| 0.0000e+00| 1.2818e+00| -0.251896| 2.375012| 2.624886| 5.221589| 10.161308| ----------------------------- Solver Exit ------------------------------- Maximum number of iterations reached (ITER = 10) before convergence. +-----------------------------------------------------------------------+ | Convergence Field | Value | Criterion | Converged | +-----------------------------------------------------------------------+ | rms[Rho]| -0.251896| < -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 = 0.796713 Cd = 0.078407 Cmx = 0.000211 Cmy = -0.204659 Cmz = 0.000288 Cx = 0.06449 Cy = 0.000454 Cz = 0.79796 Pressure Contribution Cl_p = 0.796713 Cd_p = 0.078407 Cmx_p = 0.000211 Cmy_p = -0.204659 Cmz_p = 0.000288 Cx_p = 0.06449 Cy_p = 0.000454 Cz_p = 0.79796 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 0m48.023s user 0m45.233s sys 0m1.297s + 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/DARWIN64/ESP/DARWIN64/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/DARWIN64/ESP/DARWIN64/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. 6320 grid points. 12346 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). 12346 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| 89.3051| | CV Face Area Aspect Ratio| 1.0235| 15.7138| | CV Sub-Volume Ratio| 1| 7.93643| +--------------------------------------------------------------+ Setting the multigrid structure. +-------------------------------------------+ | MG Level| CVs|Aggl. Rate| CFL| +-------------------------------------------+ | 0| 6320| 1/1.00| 10| | 1| 1790| 1/3.53| 7.98287| | 2| 504| 1/3.55| 6.35388| +-------------------------------------------+ 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| 7.9512e-02| -1.163171| 1.073770| 1.341444| 4.312165| 0.062120| | 0| 0| 1| 0.0000e+00| 0.0000e+00| 7.5323e-02| -1.561828| 0.808636| 0.967487| 3.922716| 0.139775| | 0| 0| 2| 0.0000e+00| 0.0000e+00| 7.8232e-02| -1.601698| 0.943793| 1.009036| 3.876382| 0.373708| | 0| 0| 3| 0.0000e+00| 0.0000e+00| 7.6317e-02| -1.659374| 1.008221| 1.015635| 3.799753| 0.952935| | 0| 0| 4| 0.0000e+00| 0.0000e+00| 7.6047e-02| -1.663585| 1.011627| 0.956487| 3.788246| 2.344781| | 0| 0| 5| 0.0000e+00| 0.0000e+00| 7.4759e-02| -1.633451| 0.991734| 0.872954| 3.829708| 6.259549| | 0| 0| 6| 0.0000e+00| 0.0000e+00| 7.4860e-02| -1.626398| 0.990123| 0.847075| 3.843511| 26.349556| | 0| 0| 7| 0.0000e+00| 0.0000e+00| 7.5868e-02| -1.643439| 1.009125| 0.895796| 3.825758| -56.104876| | 0| 0| 8| 0.0000e+00| 0.0000e+00| 7.6579e-02| -1.659565| 1.020774| 0.939260| 3.804303| -24.431167| | 0| 0| 9| 0.0000e+00| 0.0000e+00| 7.6873e-02| -1.676757| 1.012633| 0.938320| 3.783310| -21.456835| ----------------------------- Solver Exit ------------------------------- Maximum number of iterations reached (ITER = 10) before convergence. +-----------------------------------------------------------------------+ | Convergence Field | Value | Criterion | Converged | +-----------------------------------------------------------------------+ | rms[Rho]| -1.67676| < -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 = 0.805231 Cd = -0.037528 Cmz = 0.414714 Cx = -0.037528 Cy = 0.805231 Pressure Contribution Cl_p = 0.805231 Cd_p = -0.037528 Cmz_p = 0.414714 Cx_p = -0.037528 Cy_p = 0.805231 Viscous Contribution Cl_v = 0.0 Cd_v = 0.0 Cmz_v = 0.0 Cx_v = 0.0 Cy_v = 0.0 real 0m3.340s user 0m3.185s sys 0m0.959s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case su2_and_Delaundo_PyTest.py passed (as expected) ================================================= pointwise: /Applications/Pointwise/PointwiseV18.5R1/pointwise ================================================= + echo 'su2_and_pointwise_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/CFD/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt su2_and_pointwise_PyTest.py test; + python -u su2_and_pointwise_PyTest.py -outLevel=0 + tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/CFD/DARWIN64/ESP/DARWIN64/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 Writing global Glyph inputs... Writing egads file '/Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/CFD/DARWIN64/ESP/DARWIN64/examples/pyCAPS/SU2PointwiseAnalysisTest/Scratch/pointwise/caps.egads'.... Number of command line arguments = 2 Wed May 31 2023 2:45:30AM EDT Pointwise V18.5 Loading user defaults from capsUserDefaults.glf GeomToMesh: Defaults Connector level InitDim = 10 MaxDim = 15 MinDim = 3 TurnAngle = 0.000000 Deviation = 0.000000 SplitAngle = 0.000000 JoinCons = 0 ProxGrowthRate = 1.300000 SourceSpacing = 0 TurnAngleHard = 70.000000 EqualSpacing = 0 Domain level Algorithm = Delaunay FullLayers = 0 MaxLayers = 0 GrowthRate = 1.300000 IsoType = Triangle TRexType = Triangle TRexARLimit = 200.000000 TRexAngleBC = 0.000000 Decay = 0.500000 MinEdge = 0.000000 MaxEdge = 0.000000 Adapt = 0 WallSpacing = 0.000000 StrDomConvertARTrigger = 0.000000 Block level Algorithm = Delaunay VoxelLayers = 3 boundaryDecay = 0.500000 collisionBuffer = 0.500000 maxSkewAngle = 180.000000 TRexSkewDelay = 0 edgeMaxGrowthRate = 1.800000 fullLayers = 0 maxLayers = 0 growthRate = 1.300000 TRexType = TetPyramid volInitialize = 1 General SkipMeshing = 1 CAESolver = UGRID outerBoxScale = 0 sourceBoxLengthScale = 0.000000 sourceBoxDirection = 1.000000 0.000000 0.000000 sourceBoxAngle = 0.000000 sourceGrowthFactor = 10.000000 sourcePCDFile = ModelSize = 0 writeGMA = 2.0 assembleTolMult = 2.0 modelOrientIntMeshVolume = 1 Elevate On Export degree = Q1 costThreshold = 0.8 maxIncAngle = 175.0 relax = 0.05 smoothingPasses = 1000 WCNWeight = 0.5 WCNMode = Calculate writeVTU = false CADFile = caps.egads Determining model size from file. Info: Model Size adjusted to 100 Computing maximum DB edge tolerance. Quilt list has 19 entries. Quilt quilt-1: edge tolerance = 5e-07 Quilt quilt-2: edge tolerance = 6.19984e-05 Quilt quilt-3: edge tolerance = 6.19984e-05 Quilt quilt-4: edge tolerance = 6.19984e-05 Quilt quilt-5: edge tolerance = 6.19984e-05 Quilt quilt-6: edge tolerance = 6.19984e-05 Quilt quilt-7: edge tolerance = 6.19984e-05 Quilt quilt-8: edge tolerance = 6.19984e-05 Quilt quilt-9: edge tolerance = 6.19984e-05 Quilt quilt-10: edge tolerance = 8.32902e-05 Quilt quilt-11: edge tolerance = 8.32902e-05 Quilt quilt-12: edge tolerance = 8.32902e-05 Quilt quilt-13: edge tolerance = 8.32902e-05 Quilt quilt-14: edge tolerance = 8.32902e-05 Quilt quilt-15: edge tolerance = 8.32902e-05 Quilt quilt-16: edge tolerance = 8.32902e-05 Quilt quilt-17: edge tolerance = 8.32902e-05 Quilt quilt-18: edge tolerance = 6.19601e-06 Quilt quilt-19: edge tolerance = 6.19601e-06 Maximum DB edge tolerance = 8.32902e-05 Performing model assembly pass on geometry entities. domParams(MinEdge) defined as 1.665804e-04 due to model assembly tolerance Looking for quilt names in geometry. Quilt list has 19 entries. Quilt list has 19 entries. Original connector list has 36 entries. Minimum connector length = 0.00316783 Tolerance = 8.32902e-05 Performing merge on connectors with equal dimensions and common end points. After regular merge, connector list has 36 entries. Updating conData Min Edge Tol: 5.000e-07 on con-1 Max Edge Tol: 8.329e-05 on con-27 Adjusting connector dimensions based on average spacings. Checking dimension for connector 1/36, name = con-1 Checking dimension for connector 2/36, name = con-2 Changing dimension for connector 2/36 from 10 to 3 Checking dimension for connector 3/36, name = con-3 Checking dimension for connector 4/36, name = con-4 Changing dimension for connector 4/36 from 10 to 3 Checking dimension for connector 5/36, name = con-5 Changing dimension for connector 5/36 from 10 to 4 Checking dimension for connector 6/36, name = con-6 Checking dimension for connector 7/36, name = con-7 Changing dimension for connector 7/36 from 10 to 3 Checking dimension for connector 8/36, name = con-8 Checking dimension for connector 9/36, name = con-9 Changing dimension for connector 9/36 from 10 to 3 Checking dimension for connector 10/36, name = con-10 Changing dimension for connector 10/36 from 10 to 3 Checking dimension for connector 11/36, name = con-11 Changing dimension for connector 11/36 from 10 to 3 Checking dimension for connector 12/36, name = con-12 Checking dimension for connector 13/36, name = con-13 Changing dimension for connector 13/36 from 10 to 4 Checking dimension for connector 14/36, name = con-14 Checking dimension for connector 15/36, name = con-16 Changing dimension for connector 15/36 from 10 to 3 Checking dimension for connector 16/36, name = con-17 Checking dimension for connector 17/36, name = con-20 Changing dimension for connector 17/36 from 10 to 3 Checking dimension for connector 18/36, name = con-21 Checking dimension for connector 19/36, name = con-24 Changing dimension for connector 19/36 from 10 to 3 Checking dimension for connector 20/36, name = con-25 Changing dimension for connector 20/36 from 10 to 4 Checking dimension for connector 21/36, name = con-26 Checking dimension for connector 22/36, name = con-27 Changing dimension for connector 22/36 from 10 to 3 Checking dimension for connector 23/36, name = con-28 Checking dimension for connector 24/36, name = con-29 Changing dimension for connector 24/36 from 10 to 3 Checking dimension for connector 25/36, name = con-30 Changing dimension for connector 25/36 from 10 to 3 Checking dimension for connector 26/36, name = con-31 Changing dimension for connector 26/36 from 10 to 3 Checking dimension for connector 27/36, name = con-32 Checking dimension for connector 28/36, name = con-33 Changing dimension for connector 28/36 from 10 to 4 Checking dimension for connector 29/36, name = con-34 Checking dimension for connector 30/36, name = con-36 Changing dimension for connector 30/36 from 10 to 3 Checking dimension for connector 31/36, name = con-37 Checking dimension for connector 32/36, name = con-40 Changing dimension for connector 32/36 from 10 to 3 Checking dimension for connector 33/36, name = con-41 Checking dimension for connector 34/36, name = con-44 Changing dimension for connector 34/36 from 10 to 3 Checking dimension for connector 35/36, name = con-45 Checking dimension for connector 36/36, name = con-46 Processing spacing values for connector 1/36, name = con-1 Processing spacing values for connector 2/36, name = con-2 Processing spacing values for connector 3/36, name = con-3 Processing spacing values for connector 4/36, name = con-4 Processing spacing values for connector 5/36, name = con-5 Processing spacing values for connector 6/36, name = con-6 Processing spacing values for connector 7/36, name = con-7 Processing spacing values for connector 8/36, name = con-8 Processing spacing values for connector 9/36, name = con-9 Processing spacing values for connector 10/36, name = con-10 Processing spacing values for connector 11/36, name = con-11 Processing spacing values for connector 12/36, name = con-12 Processing spacing values for connector 13/36, name = con-13 Processing spacing values for connector 14/36, name = con-14 Processing spacing values for connector 15/36, name = con-16 Processing spacing values for connector 16/36, name = con-17 Processing spacing values for connector 17/36, name = con-20 Processing spacing values for connector 18/36, name = con-21 Processing spacing values for connector 19/36, name = con-24 Processing spacing values for connector 20/36, name = con-25 Processing spacing values for connector 21/36, name = con-26 Processing spacing values for connector 22/36, name = con-27 Processing spacing values for connector 23/36, name = con-28 Processing spacing values for connector 24/36, name = con-29 Processing spacing values for connector 25/36, name = con-30 Processing spacing values for connector 26/36, name = con-31 Processing spacing values for connector 27/36, name = con-32 Processing spacing values for connector 28/36, name = con-33 Processing spacing values for connector 29/36, name = con-34 Processing spacing values for connector 30/36, name = con-36 Processing spacing values for connector 31/36, name = con-37 Processing spacing values for connector 32/36, name = con-40 Processing spacing values for connector 33/36, name = con-41 Processing spacing values for connector 34/36, name = con-44 Processing spacing values for connector 35/36, name = con-45 Processing spacing values for connector 36/36, name = con-46 Number of unique endpoints = 24 Checking for baffle intersections. Performing Local Proximity Refinement Adjusting connector dimensions based on proximity to other connectors. Proximity test for connector 1/36, con-1. Connector dimension changed from 10 to 15, avg. spacing changed from 1.57135 to 1.01015 Proximity test for connector 2/36, con-2. Connector dimension changed from 3 to 9, avg. spacing changed from 2.5 to 0.625 Proximity test for connector 3/36, con-3. Connector dimension changed from 10 to 15, avg. spacing changed from 1.57135 to 1.01015 Proximity test for connector 4/36, con-4. Connector dimension changed from 3 to 9, avg. spacing changed from 2.5 to 0.625 Proximity test for connector 5/36, con-5. Connector dimension changed from 4 to 15, avg. spacing changed from 1.33869 to 0.286862 Proximity test for connector 6/36, con-6. Connector dimension changed from 10 to 15, avg. spacing changed from 0.821627 to 0.528189 Proximity test for connector 7/36, con-7. Connector dimension changed from 3 to 15, avg. spacing changed from 0.985229 to 0.140747 Proximity test for connector 8/36, con-8. Connector dimension changed from 10 to 15, avg. spacing changed from 0.907322 to 0.583278 Proximity test for connector 9/36, con-9. Connector dimension changed from 3 to 15, avg. spacing changed from 0.985232 to 0.140747 Proximity test for connector 10/36, con-10. Connector dimension changed from 3 to 15, avg. spacing changed from 0.985232 to 0.140747 Proximity test for connector 11/36, con-11. Proximity test for connector 12/36, con-12. Connector dimension changed from 10 to 15, avg. spacing changed from 0.907322 to 0.583278 Proximity test for connector 13/36, con-13. Connector dimension changed from 4 to 15, avg. spacing changed from 1.26705 to 0.271511 Proximity test for connector 14/36, con-14. Connector dimension changed from 10 to 15, avg. spacing changed from 0.821631 to 0.528191 Proximity test for connector 15/36, con-16. Proximity test for connector 16/36, con-17. Connector dimension changed from 10 to 15, avg. spacing changed from 0.821627 to 0.528189 Proximity test for connector 17/36, con-20. Connector dimension changed from 3 to 15, avg. spacing changed from 0.985229 to 0.140747 Proximity test for connector 18/36, con-21. Connector dimension changed from 10 to 15, avg. spacing changed from 0.821631 to 0.528191 Proximity test for connector 19/36, con-24. Proximity test for connector 20/36, con-25. Connector dimension changed from 4 to 15, avg. spacing changed from 0.535476 to 0.114745 Proximity test for connector 21/36, con-26. Connector dimension changed from 10 to 15, avg. spacing changed from 0.328651 to 0.211275 Proximity test for connector 22/36, con-27. Connector dimension changed from 3 to 15, avg. spacing changed from 0.394092 to 0.0562988 Proximity test for connector 23/36, con-28. Connector dimension changed from 10 to 15, avg. spacing changed from 0.362929 to 0.233311 Proximity test for connector 24/36, con-29. Connector dimension changed from 3 to 15, avg. spacing changed from 0.394096 to 0.0562994 Proximity test for connector 25/36, con-30. Connector dimension changed from 3 to 15, avg. spacing changed from 0.394096 to 0.0562994 Proximity test for connector 26/36, con-31. Proximity test for connector 27/36, con-32. Connector dimension changed from 10 to 15, avg. spacing changed from 0.362929 to 0.233311 Proximity test for connector 28/36, con-33. Connector dimension changed from 4 to 15, avg. spacing changed from 0.506821 to 0.108604 Proximity test for connector 29/36, con-34. Connector dimension changed from 10 to 15, avg. spacing changed from 0.328652 to 0.211277 Proximity test for connector 30/36, con-36. Proximity test for connector 31/36, con-37. Connector dimension changed from 10 to 15, avg. spacing changed from 0.328651 to 0.211275 Proximity test for connector 32/36, con-40. Connector dimension changed from 3 to 15, avg. spacing changed from 0.394092 to 0.0562988 Proximity test for connector 33/36, con-41. Connector dimension changed from 10 to 15, avg. spacing changed from 0.328652 to 0.211277 Proximity test for connector 34/36, con-44. Proximity test for connector 35/36, con-45. Connector dimension changed from 10 to 15, avg. spacing changed from 27.9253 to 17.952 Proximity test for connector 36/36, con-46. Connector dimension changed from 10 to 15, avg. spacing changed from 27.9253 to 17.952 Adjusting node spacing from geometry Adjusting connector dimensions based on end spacings. Connector con-1 current dim = 15 Connector con-2 current dim = 9 Connector con-3 current dim = 15 Connector con-4 current dim = 9 Connector con-5 current dim = 15 Connector con-6 current dim = 15 Connector con-7 current dim = 15 Connector con-8 current dim = 15 Connector con-9 current dim = 15 Connector con-10 current dim = 15 Connector con-11 current dim = 3 Connector con-12 current dim = 15 Connector con-13 current dim = 15 Connector con-14 current dim = 15 Connector con-16 current dim = 3 Connector con-17 current dim = 15 Connector con-20 current dim = 15 Connector con-21 current dim = 15 Connector con-24 current dim = 3 Connector con-25 current dim = 15 Connector con-26 current dim = 15 Connector con-27 current dim = 15 Connector con-28 current dim = 15 Connector con-29 current dim = 15 Connector con-30 current dim = 15 Connector con-31 current dim = 3 Connector con-32 current dim = 15 Connector con-33 current dim = 15 Connector con-34 current dim = 15 Connector con-36 current dim = 3 Connector con-37 current dim = 15 Connector con-40 current dim = 15 Connector con-41 current dim = 15 Connector con-44 current dim = 3 Connector con-45 current dim = 15 Connector con-46 current dim = 15 Domain list has 19 entries. Looking for periodic domain attributes from geometry. Tolerance = 8.32902e-05 Number of periodic target domains = 0 Unstructured domain 1 of 19: boundary name = Wake. Unstructured domain 2 of 19: boundary name = Wing1. Creating boundary name Wing1 Unstructured domain 3 of 19: boundary name = Wing1. Wing1 already in boundary name list. Unstructured domain 4 of 19: boundary name = Wing1. Wing1 already in boundary name list. Unstructured domain 5 of 19: boundary name = Wing1. Wing1 already in boundary name list. Unstructured domain 6 of 19: boundary name = Wing1. Wing1 already in boundary name list. Unstructured domain 7 of 19: boundary name = Wing1. Wing1 already in boundary name list. Unstructured domain 8 of 19: boundary name = Wing1. Wing1 already in boundary name list. Unstructured domain 9 of 19: boundary name = Wing1. Wing1 already in boundary name list. Unstructured domain 10 of 19: boundary name = Wing2. Creating boundary name Wing2 Unstructured domain 11 of 19: boundary name = Wing2. Wing2 already in boundary name list. Unstructured domain 12 of 19: boundary name = Wing2. Wing2 already in boundary name list. Unstructured domain 13 of 19: boundary name = Wing2. Wing2 already in boundary name list. Unstructured domain 14 of 19: boundary name = Wing2. Wing2 already in boundary name list. Unstructured domain 15 of 19: boundary name = Wing2. Wing2 already in boundary name list. Unstructured domain 16 of 19: boundary name = Wing2. Wing2 already in boundary name list. Unstructured domain 17 of 19: boundary name = Wing2. Wing2 already in boundary name list. Unstructured domain 18 of 19: boundary name = Farfield. Creating boundary name Farfield Unstructured domain 19 of 19: boundary name = Farfield. Farfield already in boundary name list. Checking for blunt flag attribute on geometry faces. Number of baffles = 1 Adjusting connector dimensions and distributions for wake treatment. Number of exit connectors = 0 Number of wake edge connectors = 4 Number of TE connectors = 0 Number of exit nodes = 0 Number of TE nodes = 0 New minimum spacing for Wake treatment = 1.0e20 WARNING: T-Rex wall boundary con-1 not found! WARNING: T-Rex wall boundary con-2 not found! WARNING: T-Rex wall boundary con-3 not found! WARNING: T-Rex wall boundary con-4 not found! Adding Edge connector con-1 to redimension list. Adding Edge connector con-2 to redimension list. Adding Edge connector con-3 to redimension list. Adding Edge connector con-4 to redimension list. Checking connector con-1 Checking connector con-2 Checking connector con-3 Checking connector con-4 Performing initialization pass on all unstructured domains. Unstructured domain list for assembly has 19 entries. Baffle domain dom-1 Number of baffles = 1 Structured domain list for assembly has 0 entries. Periodic target domain list for assembly has 0 entries. Creating unstructured block from 18 domains. Block = auto-blk Setting up unstructured block. Retrieving block attributes from geometry. Initializing unstructured block. CAE Solver set to UGRID GeomToMesh finished! Wed May 31 2023 2:45:34AM EDT Run Time: 00 Hours 00 Minutes 04 Seconds Pointwise save filename = caps.GeomToMesh.pw Wed May 31 2023 2:45:34AM EDT Exporting in UGRID format to file basename = caps.GeomToMesh Mapped 104 / 104 curves to EGADS originals GMA contains 36 edge groups GMA contains 19 face groups Wrote geometry-mesh associativity to caps.GeomToMesh.gma GeomToMesh I/O finished! Wed May 31 2023 2:45:37AM EDT Export Time: 00 Hours 00 Minutes 03 Seconds Volume mesh: Number of nodes = 16870 Number of elements = 98731 Number of triangles = 2982 Number of quadrilatarals = 0 Number of tetrahedrals = 98731 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Body = 1 Number of nodes = 548 Number of elements = 1092 Number of tris = 1092 Number of quad = 0 Body = 2 Number of nodes = 550 Number of elements = 1096 Number of tris = 1096 Number of quad = 0 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 Body = 3 Number of nodes = 147 Number of elements = 248 Number of tris = 248 Number of quad = 0 Body = 4 Number of nodes = 399 Number of elements = 794 Number of tris = 794 Number of quad = 0 No project name ("Proj_Name") provided - A volume mesh will not be written out 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 40 m^2. The semi-span will be computed using the max y(3D) value. The reference length is 14.1421 m. Surface(s) where the force coefficients are evaluated and their reference origin for moment computation: - BC_2 (0, 0, 0). - BC_3 (0, 0, 0) m. Surface(s) plotted in the output file: BC_2, BC_3. Input mesh file name: ../pointwise/caps.GeomToMesh.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| | 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_Pointwise.dat. Surface file name: surface_flow_pyCAPS_SU2_Pointwise. Volume file name: flow_pyCAPS_SU2_Pointwise. Restart file name: restart_flow_pyCAPS_SU2_Pointwise.dat. ------------- Config File Boundary Information ( Zone 0 ) --------------- +-----------------------------------------------------------------------+ | Marker Type| Marker Name| +-----------------------------------------------------------------------+ | Euler wall| BC_2| | | BC_3| +-----------------------------------------------------------------------+ | Far-field| BC_1| +-----------------------------------------------------------------------+ -------------------- 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. 16870 grid points. 98731 volume elements. 3 surface markers. 794 boundary elements in index 0 (Marker = BC_1). 1092 boundary elements in index 1 (Marker = BC_2). 1096 boundary elements in index 2 (Marker = BC_3). 98731 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: 2.11323e+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: 6570.86. Mean K: 103.119. Standard deviation K: 509.62. Checking for periodicity. Computing mesh quality statistics for the dual control volumes. +--------------------------------------------------------------+ | Mesh Quality Metric| Minimum| Maximum| +--------------------------------------------------------------+ | Orthogonality Angle (deg.)| 40.8168| 82.866| | CV Face Area Aspect Ratio| 1.30324| 81.5706| | CV Sub-Volume Ratio| 1.14956| 3053.46| +--------------------------------------------------------------+ Setting the multigrid structure. +-------------------------------------------+ | MG Level| CVs|Aggl. Rate| CFL| +-------------------------------------------+ | 0| 16870| 1/1.00| 10| | 1| 2644| 1/6.38| 8.08736| | 2| 377| 1/7.01| 6.3376| +-------------------------------------------+ Finding max control volume width. Semi-span length = 7.07107 m. Wetted area = 90.1734 m^2. Area projection in the x-plane = 8.28864 m^2, y-plane = 3.67857 m^2, z-plane = 42.4935 m^2. Max. coordinate in the x-direction = 12.3619 m, y-direction = 7.07107 m, z-direction = 0.510646 m. Min. coordinate in the x-direction = 0 m, y-direction = -7.07107 m, z-direction = -0.368435 m. Checking if Euler & Symmetry markers are straight/plane: Boundary marker BC_2 is NOT a single plane. Boundary marker BC_3 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| 5.8054e-01| 0.430329| 2.847041| 2.393380| 5.921224| 2.215361| | 0| 0| 1| 0.0000e+00| 0.0000e+00| 5.9635e-01| 0.159133| 2.646991| 2.355222| 5.644667| 2.769337| | 0| 0| 2| 0.0000e+00| 0.0000e+00| 5.9244e-01| 0.129573| 2.637903| 2.496115| 5.602137| 3.729143| | 0| 0| 3| 0.0000e+00| 0.0000e+00| 5.7768e-01| 0.062336| 2.612837| 2.562238| 5.530319| 4.783075| | 0| 0| 4| 0.0000e+00| 0.0000e+00| 5.7104e-01| -0.003418| 2.606253| 2.575619| 5.473177| 5.540540| ----------------------------- Solver Exit ------------------------------- Maximum number of iterations reached (ITER = 5) before convergence. +-----------------------------------------------------------------------+ | Convergence Field | Value | Criterion | Converged | +-----------------------------------------------------------------------+ | rms[Rho]| -0.00341772| < -14| No| +-----------------------------------------------------------------------+ ------------------------------------------------------------------------- +-----------------------------------------------------------------------+ | File Writing Summary | Filename | +-----------------------------------------------------------------------+ |SU2 binary restart |restart_flow_pyCAPS_SU2_Pointwise.dat| Writing the forces breakdown file (forces_breakdown_pyCAPS_SU2_Pointwise.dat). |CSV file |surface_flow_pyCAPS_SU2_Pointwise.csv| Writing the forces breakdown file (forces_breakdown_pyCAPS_SU2_Pointwise.dat). |Tecplot binary |flow_pyCAPS_SU2_Pointwise.szplt | Writing the forces breakdown file (forces_breakdown_pyCAPS_SU2_Pointwise.dat). |Tecplot binary surface |surface_flow_pyCAPS_SU2_Pointwise.szplt| Writing the forces breakdown file (forces_breakdown_pyCAPS_SU2_Pointwise.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 = 0.661032 Cd = 0.119308 Cmx = -0.002417 Cmy = -0.196145 Cmz = 0.000635 Cx = 0.107753 Cy = -0.000326 Cz = 0.663014 real 0m16.661s user 0m14.932s sys 0m2.319s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case su2_and_pointwise_PyTest.py passed (as expected) ================================================= ================================================= + echo 'su2_and_Tetgen_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/CFD/DARWIN64/ESP/DARWIN64/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/DARWIN64/ESP/DARWIN64/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 = 265 Number of elements = 526 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 526 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 3137 Total number of elements = 6262 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 - 3137, elements - 6262 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000T1.00e-16A Delaunizing vertices... Delaunay seconds: 0.079146 Creating surface mesh ... Surface mesh seconds: 0.015898 Recovering boundaries... Boundary recovery seconds: 0.176002 Removing exterior tetrahedra ... Spreading region attributes. Exterior tets removal seconds: 0.018273 Suppressing Steiner points ... Steiner suppression seconds: 1.4e-05 Recovering Delaunayness... Delaunay recovery seconds: 0.024754 Refining mesh... 4186 insertions, added 2132 points, 130189 tetrahedra in queue. 1393 insertions, added 396 points, 133609 tetrahedra in queue. 1857 insertions, added 413 points, 131356 tetrahedra in queue. 2476 insertions, added 454 points, 112928 tetrahedra in queue. 3300 insertions, added 466 points, 67068 tetrahedra in queue. 4399 insertions, added 435 points, 292 tetrahedra in queue. 5864 insertions, added 590 points, 479 tetrahedra in queue. Refinement seconds: 2.19878 Smoothing vertices... Mesh smoothing seconds: 1.47107 Improving mesh... Mesh improvement seconds: 0.079183 Jettisoning redundant points. Writing nodes. Writing elements. Writing faces. Writing edges. Output seconds: 0.008675 Total running seconds: 4.07241 Statistics: Input points: 3137 Input facets: 6262 Input segments: 9393 Input holes: 2 Input regions: 0 Mesh points: 8091 Mesh tetrahedra: 39789 Mesh faces: 82710 Mesh faces on exterior boundary: 6264 Mesh faces on input facets: 6264 Mesh edges on input segments: 9394 Steiner points on input segments: 1 Steiner points inside domain: 4953 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. 8091 grid points. 39789 volume elements. 3 surface markers. 4468 boundary elements in index 0 (Marker = BC_1). 1270 boundary elements in index 1 (Marker = BC_2). 526 boundary elements in index 2 (Marker = BC_3). 39789 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: 2.08926e+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: 30.5804. Standard deviation K: 37.5377. Checking for periodicity. Computing mesh quality statistics for the dual control volumes. +--------------------------------------------------------------+ | Mesh Quality Metric| Minimum| Maximum| +--------------------------------------------------------------+ | Orthogonality Angle (deg.)| 1.66644| 84.3027| | CV Face Area Aspect Ratio| 1.51408| 6441.7| | CV Sub-Volume Ratio| 1.03202| 58553.9| +--------------------------------------------------------------+ Setting the multigrid structure. +-------------------------------------------+ | MG Level| CVs|Aggl. Rate| CFL| +-------------------------------------------+ | 0| 8091| 1/1.00| 10| | 1| 1351| 1/5.99| 8.25992| | 2| 223| 1/6.06| 6.79647| +-------------------------------------------+ 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 = 4.58502 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| 2.3198e-01| 0.617984| 3.049944| 2.093190| 6.108879| 1.810742| | 0| 0| 1| 0.0000e+00| 0.0000e+00| 2.2999e-01| 0.748911| 3.251769| 2.987153| 6.248586| 2.155825| | 0| 0| 2| 0.0000e+00| 0.0000e+00| 2.2688e-01| 0.688623| 3.311837| 3.249508| 6.186781| 3.173369| | 0| 0| 3| 0.0000e+00| 0.0000e+00| 2.2280e-01| 0.587426| 3.265724| 3.310895| 6.060983| 4.532123| | 0| 0| 4| 0.0000e+00| 0.0000e+00| 2.2266e-01| 0.563655| 3.196458| 3.256149| 6.028232| 5.638253| ----------------------------- Solver Exit ------------------------------- Maximum number of iterations reached (ITER = 5) before convergence. +-----------------------------------------------------------------------+ | Convergence Field | Value | Criterion | Converged | +-----------------------------------------------------------------------+ | rms[Rho]| 0.563655| < -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 = 0.751804 Cd = 0.13334 Cmx = -0.004647 Cmy = -0.210652 Cmz = 0.001238 Cx = 0.120199 Cy = 0.000192 Cz = 0.754017 real 1m9.732s user 1m8.483s sys 0m0.962s + 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/DARWIN64/ESP/DARWIN64/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/DARWIN64/ESP/DARWIN64/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 = 3808 Number of elements = 7616 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 7616 Number of quadrilateral elements = 0 Body 2 (of 2) Number of nodes = 5654 Number of elements = 11304 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 11304 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 9462 Total number of elements = 18920 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 - 9462, elements - 18920 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000T1.00e-16A Delaunizing vertices... Delaunay seconds: 0.135161 Creating surface mesh ... Surface mesh seconds: 0.047679 Recovering boundaries... Warning: 6 segments are not recovered. Boundary recovery seconds: 0.390494 Removing exterior tetrahedra ... Spreading region attributes. Exterior tets removal seconds: 0.037929 Suppressing Steiner points ... Steiner suppression seconds: 1.5e-05 Recovering Delaunayness... Delaunay recovery seconds: 0.051248 Refining mesh... 12618 insertions, added 5274 points, 8959 tetrahedra in queue. Refinement seconds: 1.73638 Smoothing vertices... Mesh smoothing seconds: 1.50192 Improving mesh... Mesh improvement seconds: 0.099178 Jettisoning redundant points. Writing nodes. Writing elements. Writing faces. Writing edges. Output seconds: 0.015949 Total running seconds: 4.03123 Statistics: Input points: 9462 Input facets: 18920 Input segments: 28380 Input holes: 1 Input regions: 0 Mesh points: 14879 Mesh tetrahedra: 61475 Mesh faces: 132413 Mesh faces on exterior boundary: 18926 Mesh faces on input facets: 18926 Mesh edges on input segments: 28383 Steiner points on input segments: 3 Steiner points inside domain: 5414 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 - 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. 14879 grid points. 61475 volume elements. 2 surface markers. 7622 boundary elements in index 0 (Marker = BC_1). 11304 boundary elements in index 1 (Marker = BC_2). 61475 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: 2.67744e+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: 0.525129. Standard deviation K: 2.57985. Checking for periodicity. Computing mesh quality statistics for the dual control volumes. +--------------------------------------------------------------+ | Mesh Quality Metric| Minimum| Maximum| +--------------------------------------------------------------+ | Orthogonality Angle (deg.)| 1.97178| 85.1584| | CV Face Area Aspect Ratio| 1.89387| 2232.84| | CV Sub-Volume Ratio| 1| 662807| +--------------------------------------------------------------+ Setting the multigrid structure. +-------------------------------------------+ | MG Level| CVs|Aggl. Rate| CFL| +-------------------------------------------+ | 0| 14879| 1/1.00| 10| | 1| 2664| 1/5.59| 8.45431| | 2| 482| 1/5.53| 7.17255| +-------------------------------------------+ Finding max control volume width. Semi-span length = 30 m. Wetted area = 13596.7 m^2. Area projection in the x-plane = 761.676 m^2, y-plane = 2062.48 m^2, z-plane = 5463.61 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| 4.5331e-01| 2.730957| 5.664998| 4.728682| 8.730433| -0.398804| | 0| 0| 1| 0.0000e+00| 0.0000e+00| 4.6400e-01| 3.137446| 6.177776| 5.665282| 9.126833| -0.137986| | 0| 0| 2| 0.0000e+00| 0.0000e+00| 4.4879e-01| 3.221739| 6.293564| 5.717532| 9.173826| -0.037061| | 0| 0| 3| 0.0000e+00| 0.0000e+00| 4.3442e-01| 3.189146| 6.230574| 5.640455| 9.149183| -0.012053| | 0| 0| 4| 0.0000e+00| 0.0000e+00| 4.2376e-01| 3.223156| 6.256981| 5.536034| 9.185450| -0.028725| ----------------------------- Solver Exit ------------------------------- Maximum number of iterations reached (ITER = 5) before convergence. +-----------------------------------------------------------------------+ | Convergence Field | Value | Criterion | Converged | +-----------------------------------------------------------------------+ | rms[Rho]| 3.22316| < -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 124 non-physical points in the solution. Warning: 85 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 = -3.497481 Cd = 121.75903 Cmx = -17.512377 Cmy = 9356.955958 Cmz = 278.947628 Cx = 121.775208 Cy = 2.435697 Cz = 2.879687 real 0m26.567s user 0m42.554s sys 0m1.407s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case su2_X43a_PyTest.py passed (as expected) ================================================= ./execute_PyTestRegression.sh: line 404: 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/DARWIN64/ESP/DARWIN64/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/DARWIN64/ESP/DARWIN64/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 0m23.660s user 0m39.431s sys 0m1.068s + 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/DARWIN64/ESP/DARWIN64/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/DARWIN64/ESP/DARWIN64/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 (02:48:07) Running aero.csh on 2 core(s) in M0.5901A2B0_DP1 (02:48:10) 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 (02:48:11) Running aero.csh on 2 core(s) in M0.5901A2B0_DP1 (02:48:14) 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 (02:48:15) Linearizing cut-cells (02:48:15) ... done o Number of simultaneous xsensit jobs: 1 (02:48:15) Computing gradients (02:48:19) ... 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 (02:48:21) Running aero.csh on 2 core(s) in M0.5901A1.98427B0_DP1 (02:48:24) 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 (02:48:26) Running aero.csh on 2 core(s) in M0.5901A1.98427B0_DP1 (02:48:29) 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 (02:48:30) Linearizing cut-cells (02:48:30) ... done o Number of simultaneous xsensit jobs: 1 (02:48:30) Computing gradients (02:48:34) ... 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 (02:48:35) Running aero.csh on 2 core(s) in M0.5901A-0.0109918B0_DP1 (02:48:38) aero.csh done o case M0.5901A-0.0109918B0_DP1, averaging data over 1 cycle(s) >>> CL2 [6.05653687e-06] CL 0.00246101 ---------------------------------------- ======================================== o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (02:48:39) Running aero.csh on 2 core(s) in M0.5901A-0.0109918B0_DP1 (02:48:42) 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 (02:48:43) Linearizing cut-cells (02:48:43) ... done o Number of simultaneous xsensit jobs: 1 (02:48:43) Computing gradients (02:48:47) ... done o case M0.5901A-0.0109918B0_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 (02:48:48) Running aero.csh on 2 core(s) in M0.5901A-0.0514929B0_DP1 (02:48:52) aero.csh done o case M0.5901A-0.0514929B0_DP1, averaging data over 1 cycle(s) >>> CL2 [2.59817201e-10] CL 1.612e-05 ---------------------------------------- ======================================== o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (02:48:53) Running aero.csh on 2 core(s) in M0.5901A-0.0514929B0_DP1 (02:48:57) 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 (02:48:57) Linearizing cut-cells (02:48:57) ... done o Number of simultaneous xsensit jobs: 1 (02:48:58) Computing gradients (02:49:02) ... done o case M0.5901A-0.0514929B0_DP1, averaging data over 1 cycle(s) >>> CL2_alpha [[2.03612486e-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 (02:49:03) Running aero.csh on 2 core(s) in M0.5901A-0.0517603B0_DP1 (02:49:06) aero.csh done o case M0.5901A-0.0517603B0_DP1, averaging data over 1 cycle(s) >>> CL2 [9.26120217e-15] CL 1e-07 ---------------------------------------- ======================================== o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (02:49:08) Running aero.csh on 2 core(s) in M0.5901A-0.0517603B0_DP1 (02:49:11) 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 (02:49:12) Linearizing cut-cells (02:49:12) ... done o Number of simultaneous xsensit jobs: 1 (02:49:12) Computing gradients (02:49:16) ... done o case M0.5901A-0.0517603B0_DP1, averaging data over 1 cycle(s) >>> CL2_alpha [[1.21394333e-08]] ======================================== At iterate 4 f= 9.26120D-15 |proj g|= 1.21394D-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 9.261D-15 F = 9.2612021713000013E-015 CONVERGENCE: NORM_OF_PROJECTED_GRADIENT_<=_PGTOL Optimization Complete ----------------------------------- Optimized value: [-0.05176027] real 1m32.982s user 1m1.630s sys 0m11.724s + 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/DARWIN64/ESP/DARWIN64/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/DARWIN64/ESP/DARWIN64/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 (02:49:25) Running aero.csh on 2 core(s) in M0.5901A0B0_DP1 (02:49:42) 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 (02:49:45) Running aero.csh on 2 core(s) in M0.5901A0B0_DP1 (02:50:12) 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 (02:50:12) Linearizing cut-cells (02:50:14) ... done o Number of simultaneous xsensit jobs: 1 (02:50:14) Computing gradients (02:50:18) ... 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 (02:50:24) Running aero.csh on 2 core(s) in M0.5901A0B0_DP1 (02:50:43) 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 (02:50:45) Running aero.csh on 2 core(s) in M0.5901A0B0_DP1 (02:51:12) 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 (02:51:13) Linearizing cut-cells (02:51:15) ... done o Number of simultaneous xsensit jobs: 1 (02:51:15) Computing gradients (02:51:19) ... 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 [-1.80638251] Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = Wing, index = 1 Body size = 3.627700 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 (02:51:24) Running aero.csh on 2 core(s) in M0.5901A0B0_DP1 (02:51:43) aero.csh done o case M0.5901A0B0_DP1, averaging data over 1 cycle(s) >>> CL2 [0.00077495] CL -0.027841 ---------------------------------------- ======================================== o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (02:51:46) Running aero.csh on 2 core(s) in M0.5901A0B0_DP1 (02:52:12) aero.csh done Max memory allowed: 32 GB Flow hexes: 37739 Estimated cutter memory: 0.003774 GB / DV Estimated xsensit memory: 0.071704 GB / DV Available threads: 2 # DVs: 1 o Number of simultaneous cutter jobs: 1 (02:52:12) Linearizing cut-cells (02:52:14) ... done o Number of simultaneous xsensit jobs: 1 (02:52:15) Computing gradients (02:52:19) ... done o case M0.5901A0B0_DP1, averaging data over 1 cycle(s) >>> CL2_twist [[-0.00093632]] ======================================== At iterate 2 f= 7.74952D-04 |proj g|= 9.36323D-04 ---------------------------------------- >>> twist [-0.01621197] Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = Wing, index = 1 Body size = 3.625631 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 (02:52:24) Running aero.csh on 2 core(s) in M0.5901A0B0_DP1 (02:52:42) aero.csh done o case M0.5901A0B0_DP1, averaging data over 1 cycle(s) >>> CL2 [1.56317765e-06] CL 0.00125932 ---------------------------------------- ======================================== o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (02:52:45) Running aero.csh on 2 core(s) in M0.5901A0B0_DP1 (02:53:12) 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 (02:53:12) Linearizing cut-cells (02:53:14) ... done o Number of simultaneous xsensit jobs: 1 (02:53:14) Computing gradients (02:53:19) ... done o case M0.5901A0B0_DP1, averaging data over 1 cycle(s) >>> CL2_twist [[4.17557755e-05]] ======================================== At iterate 3 f= 1.56318D-06 |proj g|= 4.17558D-05 ---------------------------------------- >>> twist [-0.09263728] Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = Wing, index = 1 Body size = 3.625709 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 (02:53:25) Running aero.csh on 2 core(s) in M0.5901A0B0_DP1 (02:53:43) aero.csh done o case M0.5901A0B0_DP1, averaging data over 1 cycle(s) >>> CL2 [6.54574809e-07] CL 0.00081002 ---------------------------------------- ======================================== o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (02:53:46) Running aero.csh on 2 core(s) in M0.5901A0B0_DP1 (02:54:12) 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 (02:54:12) Linearizing cut-cells (02:54:14) ... done o Number of simultaneous xsensit jobs: 1 (02:54:15) Computing gradients (02:54:19) ... done o case M0.5901A0B0_DP1, averaging data over 1 cycle(s) >>> CL2_twist [[2.67924268e-05]] ======================================== At iterate 4 f= 6.54575D-07 |proj g|= 2.67924D-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 2.679D-05 6.546D-07 F = 6.5457480904999998E-007 CONVERGENCE: REL_REDUCTION_OF_F_<=_FACTR*EPSMCH Optimization Complete ----------------------------------- Optimized values: [-0.09263728] real 5m2.910s user 7m35.002s sys 0m13.675s + 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/DARWIN64/ESP/DARWIN64/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/DARWIN64/ESP/DARWIN64/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 9.14.6 AFLR2 : Version Date 11/20/22 @ 09:21PM AFLR2 : Compile OS Darwin 22.3.0 arm64 AFLR2 : Compile Date 03/08/23 @ 05:14PM 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 11.4.5 AFLR4 : Version Date 04/20/23 @ 05:37PM AFLR4 : Compile OS Darwin 22.3.0 x86_64 AFLR4 : Compile Date 04/20/23 @ 11:55PM AFLR4 : Copyright 1994-2021, D.L. Marcum AFLR4 : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.23 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.23 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 79623 Number of elements = 464233 Number of triangles = 15680 Number of quadrilatarals = 0 Number of tetrahedrals = 448553 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 0m19.960s user 0m18.403s sys 0m1.131s + 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/DARWIN64') [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/DARWIN64') [Clang] -> found 0 issues (skipped 0 duplicates) [Clang] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/CFD/DARWIN64') [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/DARWIN64') [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/DARWIN64') [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/DARWIN64') [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,DARWIN64,macys) [Static Analysis] Using reference build 'ESP_UndefinedCaps/CASREV=7.7,ESPTEST=CAPS/CFD,ESP_ARCH=DARWIN64,buildnode=macys #180' 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=DARWIN64,buildnode=macys #182'. [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