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Skipping 676 KB.. Full Log| | 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. 39409 grid points. 214785 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). 214785 tetrahedra. Setting point connectivity. Renumbering points (Reverse Cuthill McKee Ordering). Recomputing point connectivity. Setting element connectivity. Checking the numerical grid orientation. All volume elements are correctly orientend. All surface elements are correctly orientend. Identifying edges and vertices. Setting the control volume structure. Volume of the computational grid: 2.08667e+06. Searching for the closest normal neighbors to the surfaces. Storing a mapping from global to local point index. Compute the surface curvature. Max K: 4873.1. Mean K: 61.8682. Standard deviation K: 266.942. Checking for periodicity. Computing mesh quality statistics for the dual control volumes. +--------------------------------------------------------------+ | Mesh Quality Metric| Minimum| Maximum| +--------------------------------------------------------------+ | Orthogonality Angle (deg.)| 22.9692| 86.4299| | CV Face Area Aspect Ratio| 1.17576| 35957.9| | CV Sub-Volume Ratio| 1.04269| 271441| +--------------------------------------------------------------+ Setting the multigrid structure. +-------------------------------------------+ | MG Level| CVs|Aggl. Rate| CFL| +-------------------------------------------+ | 0| 39409| 1/1.00| 10| | 1| 6497| 1/6.07| 8.2249| | 2| 993| 1/6.54| 6.5963| +-------------------------------------------+ 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| 1.0176e+00| -0.065121| 2.297141| 2.032765| 5.425774| 1.977037| | 0| 0| 1| 0.0000e+00| 0.0000e+00| 1.0418e+00| -0.010130| 2.475307| 2.169935| 5.491527| 2.684789| | 0| 0| 2| 0.0000e+00| 0.0000e+00| 1.0335e+00| 0.025684| 2.558562| 2.410348| 5.522363| 4.134053| | 0| 0| 3| 0.0000e+00| 0.0000e+00| 1.0234e+00| -0.018996| 2.592746| 2.554306| 5.465750| 6.097425| | 0| 0| 4| 0.0000e+00| 0.0000e+00| 1.0074e+00| -0.071521| 2.598267| 2.616947| 5.401400| 7.797273| | 0| 0| 5| 0.0000e+00| 0.0000e+00| 9.8812e-01| -0.081476| 2.598647| 2.631749| 5.400680| 9.018108| | 0| 0| 6| 0.0000e+00| 0.0000e+00| 9.7551e-01| -0.087135| 2.580354| 2.632473| 5.404256| 9.890141| | 0| 0| 7| 0.0000e+00| 0.0000e+00| 9.6627e-01| -0.119764| 2.522267| 2.630912| 5.367657| 10.368028| | 0| 0| 8| 0.0000e+00| 0.0000e+00| 9.6394e-01| -0.181348| 2.435900| 2.617551| 5.291778| 10.443409| | 0| 0| 9| 0.0000e+00| 0.0000e+00| 9.5933e-01| -0.243992| 2.372163| 2.582376| 5.218223| 10.207526| ----------------------------- Solver Exit ------------------------------- Maximum number of iterations reached (ITER = 10) before convergence. +-----------------------------------------------------------------------+ | Convergence Field | Value | Criterion | Converged | +-----------------------------------------------------------------------+ | rms[Rho]| -0.243992| < -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). +-----------------------------------------------------------------------+ --------------------------- Finalizing Solver --------------------------- 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 = 0.794284 Cd = 0.077814 Cmx = 0.000306 Cmy = -0.202551 Cmz = -5.6e-05 Cx = 0.06394 Cy = 8.7e-05 Cz = 0.795521 Pressure Contribution Cl_p = 0.794284 Cd_p = 0.077814 Cmx_p = 0.000306 Cmy_p = -0.202551 Cmz_p = -5.6e-05 Cx_p = 0.06394 Cy_p = 8.7e-05 Cz_p = 0.795521 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 0m29.035s user 0m26.270s sys 0m0.799s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case su2_and_AFLR4_AFLR3_PyTest.py passed (as expected) ================================================= ================================================= + echo 'su2_Morph_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.8/CAPS/CFD/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/pyCAPSlog.txt su2_Morph_PyTest.py test; + python -u su2_Morph_PyTest.py -outLevel=0 + tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.8/CAPS/CFD/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/pyCAPSlog.txt Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Wake, index = 3 Name = Farfield, index = 4 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 4 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Wake, index = 3 Name = Farfield, index = 4 AFLR4 : Proximity BG Surface Grid Generation Skipped AFLR4 : No Modifications Required Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Writing TECPLOT file: pyCAPS_AFLR4_AFLR3.dat .... Finished writing TECPLOT file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 4 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Wake, index = 3 Name = Farfield, index = 4 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Wake, index = 3 Name = Farfield, index = 4 Getting volume mesh AFLR2 : --------------------------------------- AFLR2 : AFLR2 LIBRARY AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR2 : TRIA/QUAD GRID GENERATOR AFLR2 : Version Number 9.14.7 AFLR2 : Version Date 07/16/23 @ 01:42PM AFLR2 : Compile OS Darwin 22.6.0 arm64 AFLR2 : Compile Date 08/01/23 @ 11:39PM AFLR2 : Copyright 1994-2021, D.L. Marcum AFLR2 : --------------------------------------- AFLR4 : --------------------------------------- AFLR4 : AFLR4 LIBRARY AFLR4 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR4 : TRIA/QUAD SURFACE GRID GENERATOR AFLR4 : Version Number 11.5.9 AFLR4 : Version Date 08/14/23 @ 12:27AM AFLR4 : Compile OS Darwin 22.6.0 arm64 AFLR4 : Compile Date 08/14/23 @ 12:31AM AFLR4 : Copyright 1994-2021, D.L. Marcum AFLR4 : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 55339 Number of elements = 320562 Number of triangles = 15872 Number of quadrilatarals = 0 Number of tetrahedrals = 304690 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing TECPLOT file: pyCAPS_AFLR4_AFLR3_VolMesh.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 Writing SU2 surface file Writing SU2 Motion File - su2AFLRTest_motion.dat Writing boundary flags - bcProps.surfaceProp[0].surfaceType = 3 - bcProps.surfaceProp[1].surfaceType = 15 - bcProps.surfaceProp[2].surfaceType = 1 - bcProps.surfaceProp[3].surfaceType = 1 Done boundary flags Warning: The su2 cfg file will be overwritten! Write SU2 configuration file for version "Harrier (8.0.0) " Running SU2...... ------------------------------------------------------------------------- | ___ _ _ ___ | | / __| | | |_ ) Release 8.0.0 "Harrier" | | \__ \ |_| |/ / | | |___/\___//___| 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_1 (0, 0, 0). - BC_2 (0, 0, 0) m. Surface(s) plotted in the output file: BC_1, BC_2. Surface(s) affected by the design variables: BC_1, BC_2. Input mesh file name: ../volumeMesh/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. 55339 grid points. 304690 volume elements. 4 surface markers. 9958 boundary elements in index 0 (Marker = BC_1). 5414 boundary elements in index 1 (Marker = BC_2). 80 boundary elements in index 2 (Marker = BC_3). 420 boundary elements in index 3 (Marker = BC_4). 304690 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: 5523.74. Mean K: 58.8178. Standard deviation K: 282.533. Checking for periodicity. Computing mesh quality statistics for the dual control volumes. +--------------------------------------------------------------+ | Mesh Quality Metric| Minimum| Maximum| +--------------------------------------------------------------+ | Orthogonality Angle (deg.)| 20.6872| 84.4759| | CV Face Area Aspect Ratio| 1.08526| 71557.9| | CV Sub-Volume Ratio| 1.03221| 362545| +--------------------------------------------------------------+ Setting the multigrid structure. +-------------------------------------------+ | MG Level| CVs|Aggl. Rate| CFL| +-------------------------------------------+ | 0| 55339| 1/1.00| 10| | 1| 9120| 1/6.07| 8.22392| | 2| 1399| 1/6.52| 6.60356| +-------------------------------------------+ Finding max control volume width. Semi-span length = 7.07107 m. Wetted area = 96.2324 m^2. Area projection in the x-plane = 7.65774 m^2, y-plane = 4.21853 m^2, z-plane = 45.5887 m^2. Max. coordinate in the x-direction = 12.3872 m, y-direction = 7.07107 m, z-direction = 0.521791 m. Min. coordinate in the x-direction = 0 m, y-direction = -7.07107 m, z-direction = -0.0650201 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| 1.2517e+00| -0.455051| 1.876098| 1.659528| 5.035844| 0.754635| | 0| 0| 1| 0.0000e+00| 0.0000e+00| 1.1838e+00| -0.459092| 2.018998| 1.735428| 5.036978| 1.425361| | 0| 0| 2| 0.0000e+00| 0.0000e+00| 1.1871e+00| -0.389675| 2.105963| 1.976831| 5.094947| 3.210144| | 0| 0| 3| 0.0000e+00| 0.0000e+00| 1.2258e+00| -0.376377| 2.152736| 2.119383| 5.095262| 6.903409| | 0| 0| 4| 0.0000e+00| 0.0000e+00| 1.2622e+00| -0.385182| 2.180271| 2.186668| 5.078359| 12.624695| | 0| 0| 5| 0.0000e+00| 0.0000e+00| 1.2870e+00| -0.404890| 2.191437| 2.212763| 5.060302| 19.899165| | 0| 0| 6| 0.0000e+00| 0.0000e+00| 1.2846e+00| -0.413885| 2.186175| 2.229463| 5.057016| 27.920723| | 0| 0| 7| 0.0000e+00| 0.0000e+00| 1.2748e+00| -0.407035| 2.160699| 2.243380| 5.064978| 32.872666| | 0| 0| 8| 0.0000e+00| 0.0000e+00| 1.2697e+00| -0.422830| 2.118245| 2.244734| 5.043053| 31.233087| | 0| 0| 9| 0.0000e+00| 0.0000e+00| 1.2749e+00| -0.467010| 2.062622| 2.225110| 4.990269| 26.191390| ----------------------------- Solver Exit ------------------------------- Maximum number of iterations reached (ITER = 10) before convergence. +-----------------------------------------------------------------------+ | Convergence Field | Value | Criterion | Converged | +-----------------------------------------------------------------------+ | rms[Rho]| -0.46701| < -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). +-----------------------------------------------------------------------+ --------------------------- Finalizing Solver --------------------------- 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 = 0.523978 Cd = 0.020006 Projecting tessellation 1 (of 4) on to new body Projecting tessellation 2 (of 4) on to new body Projecting tessellation 3 (of 4) on to new body Projecting tessellation 4 (of 4) on to new body 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 Writing SU2 surface file Writing SU2 Motion File - su2AFLRTest_motion.dat Writing boundary flags - bcProps.surfaceProp[0].surfaceType = 3 - bcProps.surfaceProp[1].surfaceType = 15 - bcProps.surfaceProp[2].surfaceType = 1 - bcProps.surfaceProp[3].surfaceType = 1 Done boundary flags Warning: The su2 cfg file will be overwritten! Write SU2 configuration file for version "Harrier (8.0.0) " Mesh Morphing...... ------------------------------------------------------------------------- | ___ _ _ ___ | | / __| | | |_ ) Release 8.0.0 "Harrier" | | \__ \ |_| |/ / | | |___/\___//___| Suite (Mesh Deformation 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/>. | ------------------------------------------------------------------------- ----------------- Physical Case Definition ( Zone 0 ) ------------------- Input mesh file name: aflr3_0.su2 ---------------- Grid deformation parameters ( Zone 0 ) ---------------- Grid deformation using a linear elasticity method. -------------------- Output Information ( Zone 0 ) ---------------------- Output mesh file name: aflr3_0.su2. Cell stiffness scaled by distance to nearest solid surface. ------------- Config File Boundary Information ( Zone 0 ) --------------- +-----------------------------------------------------------------------+ | Marker Type| Marker Name| +-----------------------------------------------------------------------+ | Euler wall| BC_1| | | BC_2| +-----------------------------------------------------------------------+ | Far-field| BC_4| +-----------------------------------------------------------------------+ | Internal boundary| BC_3| +-----------------------------------------------------------------------+ Three dimensional problem. 55339 grid points. 304690 volume elements. 4 surface markers. 9958 boundary elements in index 0 (Marker = BC_1). 5414 boundary elements in index 1 (Marker = BC_2). 80 boundary elements in index 2 (Marker = BC_3). 420 boundary elements in index 3 (Marker = BC_4). 304690 tetrahedra. ----------------------- Preprocessing computations ---------------------- Setting local point connectivity. Checking the numerical grid orientation of the interior elements. All volume elements are correctly orientend. All surface elements are correctly orientend. Identify edges and vertices. Setting the bound control volume structure. Volume of the computational grid: 2.08667e+06. Info: Ignoring the following volume output fields/groups: SOLUTION Volume output fields: COORDINATES Info: Ignoring the following screen output fields: RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_ENERGY, EFFICIENCY Screen output fields: TIME_ITER, OUTER_ITER, INNER_ITER, CUR_TIME, TIME_STEP, WALL_TIME Info: Ignoring the following history output groups: RMS_RES, AERO_COEFF History output group(s): ITER, TIME_DOMAIN, WALL_TIME Ignoring Convergence Field(s): RMS_DENSITY Warning: No (valid) fields chosen for convergence monitoring. Convergence monitoring inactive. Warning: No (valid) fields chosen for time convergence monitoring. Time convergence monitoring inactive. --------------------- Surface grid deformation (ZONE 0) ----------------- Performing the deformation of the surface grid. Updating the surface coordinates from the input file. ------------------- Volumetric grid deformation (ZONE 0) ---------------- Performing the deformation of the volumetric grid. WARNING: Convexity is not checked for 3D elements (issue #1171). Completed in 5.699449 seconds on 1 core. ----------------------- Write deformed grid files ----------------------- |SU2 mesh |aflr3_0.su2 | |CSV file |surface_deformed.csv | |Paraview |volume_deformed.vtu | |Paraview surface |surface_deformed.vtu | Adding any FFD information to the SU2 file. ------------------------- Finalize Solver ------------------------- Deleted CNumerics container. Deleted CSolver container. Deleted CGeometry container. Deleted CSurfaceMovement class. Deleted CVolumetricMovement class. Deleted CConfig container. Deleted COutput class. ------------------------- Exit Success (SU2_DEF) ------------------------ Running SU2...... ------------------------------------------------------------------------- | ___ _ _ ___ | | / __| | | |_ ) Release 8.0.0 "Harrier" | | \__ \ |_| |/ / | | |___/\___//___| 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_1 (0, 0, 0). - BC_2 (0, 0, 0) m. Surface(s) plotted in the output file: BC_1, BC_2. Surface(s) affected by the design variables: BC_1, BC_2. Input mesh file name: 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. 55339 grid points. 304690 volume elements. 4 surface markers. 9958 boundary elements in index 0 (Marker = BC_1). 5414 boundary elements in index 1 (Marker = BC_2). 80 boundary elements in index 2 (Marker = BC_3). 420 boundary elements in index 3 (Marker = BC_4). 304690 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: 5523.56. Mean K: 58.7619. Standard deviation K: 282.437. Checking for periodicity. Computing mesh quality statistics for the dual control volumes. +--------------------------------------------------------------+ | Mesh Quality Metric| Minimum| Maximum| +--------------------------------------------------------------+ | Orthogonality Angle (deg.)| 18.6106| 84.6825| | CV Face Area Aspect Ratio| 1.04175| 73238.9| | CV Sub-Volume Ratio| 1.03565| 371551| +--------------------------------------------------------------+ Setting the multigrid structure. +-------------------------------------------+ | MG Level| CVs|Aggl. Rate| CFL| +-------------------------------------------+ | 0| 55339| 1/1.00| 10| | 1| 9120| 1/6.07| 8.22392| | 2| 1399| 1/6.52| 6.60356| +-------------------------------------------+ Finding max control volume width. Semi-span length = 7.07107 m. Wetted area = 95.6308 m^2. Area projection in the x-plane = 9.17945 m^2, y-plane = 4.04295 m^2, z-plane = 44.962 m^2. Max. coordinate in the x-direction = 12.3585 m, y-direction = 7.07107 m, z-direction = 0.521791 m. Min. coordinate in the x-direction = 0 m, y-direction = -7.07107 m, z-direction = -0.400127 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| 1.3616e+00| -0.394530| 1.981694| 1.648304| 5.096365| 1.917310| | 0| 0| 1| 0.0000e+00| 0.0000e+00| 1.3541e+00| -0.233914| 2.265234| 1.972344| 5.271880| 2.559203| | 0| 0| 2| 0.0000e+00| 0.0000e+00| 1.3154e+00| -0.175594| 2.341597| 2.237610| 5.318756| 3.926676| | 0| 0| 3| 0.0000e+00| 0.0000e+00| 1.2922e+00| -0.195281| 2.361848| 2.380415| 5.279705| 5.890418| | 0| 0| 4| 0.0000e+00| 0.0000e+00| 1.2834e+00| -0.242018| 2.375879| 2.436912| 5.221573| 7.786067| | 0| 0| 5| 0.0000e+00| 0.0000e+00| 1.2901e+00| -0.278221| 2.382542| 2.449435| 5.195620| 9.295306| | 0| 0| 6| 0.0000e+00| 0.0000e+00| 1.3025e+00| -0.293027| 2.379169| 2.451095| 5.196642| 10.499209| | 0| 0| 7| 0.0000e+00| 0.0000e+00| 1.2925e+00| -0.310323| 2.355118| 2.455861| 5.182868| 11.365989| | 0| 0| 8| 0.0000e+00| 0.0000e+00| 1.2784e+00| -0.337789| 2.304092| 2.453168| 5.146175| 11.815273| | 0| 0| 9| 0.0000e+00| 0.0000e+00| 1.2628e+00| -0.380565| 2.240236| 2.431020| 5.091006| 11.872402| ----------------------------- Solver Exit ------------------------------- Maximum number of iterations reached (ITER = 10) before convergence. +-----------------------------------------------------------------------+ | Convergence Field | Value | Criterion | Converged | +-----------------------------------------------------------------------+ | rms[Rho]| -0.380565| < -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). +-----------------------------------------------------------------------+ --------------------------- Finalizing Solver --------------------------- 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 = 0.888168 Cd = 0.074809 real 1m7.025s user 0m57.381s sys 0m2.012s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case su2_Morph_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/7.8/CAPS/CFD/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/pyCAPSlog.txt su2_and_Delaundo_PyTest.py test; + python -u su2_and_Delaundo_PyTest.py -outLevel=0 + tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.8/CAPS/CFD/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/pyCAPSlog.txt /Library/Developer/CommandLineTools/SDKs/MacOSX.sdk/usr/include/c++/v1/__iterator/reverse_iterator.h:145:64: runtime error: reference binding to misaligned address 0x000127027454 for type 'IntWalk_WalkingData', which requires 8 byte alignment 0x000127027454: note: pointer points here ff ff ff ff 4f da 08 41 44 4a 4f 49 4e 54 5f da 10 52 45 53 54 41 52 54 5f 46 49 4c 45 4e 41 4d ^ SUMMARY: UndefinedBehaviorSanitizer: undefined-behavior /Library/Developer/CommandLineTools/SDKs/MacOSX.sdk/usr/include/c++/v1/__iterator/reverse_iterator.h:145:64 in /Library/Developer/CommandLineTools/SDKs/MacOSX.sdk/usr/include/c++/v1/vector:1460:12: runtime error: reference binding to misaligned address 0x00014304caa4 for type 'value_type' (aka 'IntWalk_WalkingData'), which requires 8 byte alignment 0x00014304caa4: note: pointer points here 00 00 00 00 a0 6f 3f 93 17 70 e0 3f 00 00 00 00 00 00 f0 bf 0c 00 00 00 00 00 00 80 00 00 00 00 ^ SUMMARY: UndefinedBehaviorSanitizer: undefined-behavior /Library/Developer/CommandLineTools/SDKs/MacOSX.sdk/usr/include/c++/v1/vector:1460:12 in /Library/Developer/CommandLineTools/SDKs/MacOSX.sdk/usr/include/c++/v1/vector:1470:12: runtime error: reference binding to misaligned address 0x000143868ca4 for type 'const value_type' (aka 'const IntWalk_WalkingData'), which requires 8 byte alignment 0x000143868ca4: note: pointer points here 00 00 00 00 a0 6f 3f 93 17 70 e0 3f 00 00 00 00 00 00 00 c0 f4 ff ff ff 00 00 00 80 00 00 00 00 ^ SUMMARY: UndefinedBehaviorSanitizer: undefined-behavior /Library/Developer/CommandLineTools/SDKs/MacOSX.sdk/usr/include/c++/v1/vector:1470:12 in /Users/jenkins/util/ESP/opencascade-7.8/trunk/src/NCollection/NCollection_OccAllocator.hxx:153:25: runtime error: constructor call on misaligned address 0x0001131bbe6c for type 'IntWalk_WalkingData', which requires 8 byte alignment 0x0001131bbe6c: note: pointer points here 01 00 00 00 00 00 00 00 00 00 00 00 00 00 00 00 00 00 00 00 00 00 00 00 00 00 00 00 ff ff ff ff ^ SUMMARY: UndefinedBehaviorSanitizer: undefined-behavior /Users/jenkins/util/ESP/opencascade-7.8/trunk/src/NCollection/NCollection_OccAllocator.hxx:153:25 in 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 "Harrier (8.0.0) " Running SU2...... ------------------------------------------------------------------------- | ___ _ _ ___ | | / __| | | |_ ) Release 8.0.0 "Harrier" | | \__ \ |_| |/ / | | |___/\___//___| Suite (Computational Fluid Dynamics Code) | | | ------------------------------------------------------------------------- | SU2 Project Website: https://su2code.github.io | | | | The SU2 Project is maintained by the SU2 Foundation | | (http://su2foundation.org) | ------------------------------------------------------------------------- | Copyright 2012-2023, SU2 Contributors | | | | SU2 is free software; you can redistribute it and/or | | modify it under the terms of the GNU Lesser General Public | | License as published by the Free Software Foundation; either | | version 2.1 of the License, or (at your option) any later version. | | | | SU2 is distributed in the hope that it will be useful, | | but WITHOUT ANY WARRANTY; without even the implied warranty of | | MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU | | Lesser General Public License for more details. | | | | You should have received a copy of the GNU Lesser General Public | | License along with SU2. If not, see <http://www.gnu.org/licenses/>. | ------------------------------------------------------------------------- Parsing config file for zone 0 ----------------- Physical Case Definition ( Zone 0 ) ------------------- Compressible Euler equations. Mach number: 0.4. Angle of attack (AoA): 0 deg, and angle of sideslip (AoS): 0 deg. No restart solution, use the values at infinity (freestream). Dimensional simulation. The reference area is 1 m^2. The semi-span will be computed using the max y(3D) value. The reference length is 1 m. Reference origin for moment evaluation is (0, 0, 0). Surface(s) where the force coefficients are evaluated: BC_5. Surface(s) plotted in the output file: BC_5, BC_2. Input mesh file name: ../delaundo/delaundoMesh.su2 --------------- Space Numerical Integration ( Zone 0 ) ------------------ Roe (with entropy fix = 0.001) solver for the flow inviscid terms. Standard Roe without low-dissipation function. Second order integration in space, with slope limiter. Venkatakrishnan slope-limiting method, with constant: 0.05. The reference element size is: 1. Gradient for upwind reconstruction: inverse-distance weighted Least-Squares. Gradient for viscous and source terms: inverse-distance weighted Least-Squares. --------------- Time Numerical Integration ( Zone 0 ) ------------------ Local time stepping (steady state simulation). Euler implicit method for the flow equations. FGMRES is used for solving the linear system. Using a ILU(0) preconditioning. Convergence criteria of the linear solver: 1e-06. Max number of linear iterations: 10. V Multigrid Cycle, with 2 multigrid levels. Damping factor for the residual restriction: 0.75. Damping factor for the correction prolongation: 0.75. No CFL adaptation. +-------------------------------------------+ | MG Level| Presmooth|PostSmooth|CorrectSmo| +-------------------------------------------+ | 0| 1| 0| 0| | 1| 2| 0| 0| | 2| 3| 0| 0| +-------------------------------------------+ Courant-Friedrichs-Lewy number: 10 ------------------ Convergence Criteria ( Zone 0 ) --------------------- Maximum number of solver subiterations: 10. Begin convergence monitoring at iteration 5. Residual minimum value: 1e-14. Cauchy series min. value: 1e-10. Number of Cauchy elements: 100. Begin windowed time average at iteration 0. -------------------- Output Information ( Zone 0 ) ---------------------- File writing frequency: +------------------------------------+ | File| Frequency| +------------------------------------+ | RESTART| 250| | SURFACE_CSV| 250| | TECPLOT| 250| | SURFACE_TECPLOT| 250| +------------------------------------+ Writing the convergence history file every 1 inner iterations. Writing the screen convergence history every 1 inner iterations. The tabular file format is CSV (.csv). Convergence history file name: history. Forces breakdown file name: forces_breakdown_delaundoMesh.dat. Surface file name: surface_flow_delaundoMesh. Volume file name: flow_delaundoMesh. Restart file name: restart_flow_delaundoMesh.dat. ------------- Config File Boundary Information ( Zone 0 ) --------------- +-----------------------------------------------------------------------+ | Marker Type| Marker Name| +-----------------------------------------------------------------------+ | Euler wall| BC_5| | | BC_2| +-----------------------------------------------------------------------+ | Inlet boundary| BC_4| +-----------------------------------------------------------------------+ | Outlet boundary| BC_3| +-----------------------------------------------------------------------+ -------------------- Output Preprocessing ( Zone 0 ) -------------------- WARNING: SURFACE_PRESSURE_DROP can only be computed for at least 2 surfaces (outlet, inlet, ...) Screen output fields: TIME_ITER, OUTER_ITER, INNER_ITER, CUR_TIME, TIME_STEP, WALL_TIME, RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_ENERGY, EFFICIENCY History output group(s): ITER, TIME_DOMAIN, WALL_TIME, RMS_RES, AERO_COEFF Convergence field(s): RMS_DENSITY Warning: No (valid) fields chosen for time convergence monitoring. Time convergence monitoring inactive. Volume output fields: COORDINATES, SOLUTION, PRIMITIVE ------------------- Geometry Preprocessing ( Zone 0 ) ------------------- Two dimensional problem. 6317 grid points. 12340 volume elements. 5 surface markers. 24 boundary elements in index 0 (Marker = BC_2). 24 boundary elements in index 1 (Marker = BC_3). 24 boundary elements in index 2 (Marker = BC_2). 24 boundary elements in index 3 (Marker = BC_4). 198 boundary elements in index 4 (Marker = BC_5). 12340 triangles. Setting point connectivity. Renumbering points (Reverse Cuthill McKee Ordering). Recomputing point connectivity. Setting element connectivity. Checking the numerical grid orientation. All volume elements are correctly orientend. There has been a re-orientation of 294 LINE surface elements. Identifying edges and vertices. Setting the control volume structure. Area of the computational grid: 999.917. Searching for the closest normal neighbors to the surfaces. Storing a mapping from global to local point index. Compute the surface curvature. Max K: 1792.95. Mean K: 10.8142. Standard deviation K: 104.33. Checking for periodicity. Computing mesh quality statistics for the dual control volumes. +--------------------------------------------------------------+ | Mesh Quality Metric| Minimum| Maximum| +--------------------------------------------------------------+ | Orthogonality Angle (deg.)| 45.3524| 89.2595| | CV Face Area Aspect Ratio| 1.03245| 15.7138| | CV Sub-Volume Ratio| 1| 7.93643| +--------------------------------------------------------------+ Setting the multigrid structure. +-------------------------------------------+ | MG Level| CVs|Aggl. Rate| CFL| +-------------------------------------------+ | 0| 6317| 1/1.00| 10| | 1| 1792| 1/3.53| 7.98923| | 2| 509| 1/3.52| 6.38684| +-------------------------------------------+ Finding max control volume width. Wetted area = 2.07206 m. Area projection in the x-plane = 0.179342 m, y-plane = 1.00053 m. Max. coordinate in the x-direction = 1 m, y-direction = 0.138492 m. Min. coordinate in the x-direction = -0.00104578 m, y-direction = -0.0151891 m. Checking if Euler & Symmetry markers are straight/plane: Boundary marker BC_5 is NOT a single straight. Boundary marker BC_2 is a single straight. Computing wall distances. -------------------- Solver Preprocessing ( Zone 0 ) -------------------- Inviscid flow: Computing density based on free-stream temperature and pressure using the ideal gas law. Force coefficients computed using free-stream values. -- Models: +------------------------------------------------------------------------------+ | Viscosity Model| Conductivity Model| Fluid Model| +------------------------------------------------------------------------------+ | -| -| STANDARD_AIR| +------------------------------------------------------------------------------+ -- Fluid properties: +------------------------------------------------------------------------------+ | Name| Dim. value| Ref. value| Unit|Non-dim. value| +------------------------------------------------------------------------------+ | Gas Constant| 287.058| 1| N.m/kg.K| 287.058| | Spec. Heat Ratio| -| -| -| 1.4| +------------------------------------------------------------------------------+ -- Initial and free-stream conditions: +------------------------------------------------------------------------------+ | Name| Dim. value| Ref. value| Unit|Non-dim. value| +------------------------------------------------------------------------------+ | Static Pressure| 101325| 1| Pa| 101325| | Density| 1.22498| 1| kg/m^3| 1.22498| | Temperature| 288.15| 1| K| 288.15| | Total Energy| 216054| 1| m^2/s^2| 216054| | Velocity-X| 136.119| 1| m/s| 136.119| | Velocity-Y| 0| 1| m/s| 0| | Velocity Magnitude| 136.119| 1| m/s| 136.119| +------------------------------------------------------------------------------+ | Mach Number| -| -| -| 0.4| +------------------------------------------------------------------------------+ Initialize Jacobian structure (Euler). MG level: 0. Initialize Jacobian structure (Euler). MG level: 1. Initialize Jacobian structure (Euler). MG level: 2. ------------------- Numerics Preprocessing ( Zone 0 ) ------------------- ----------------- Integration Preprocessing ( Zone 0 ) ------------------ ------------------- Iteration Preprocessing ( Zone 0 ) ------------------ Euler/Navier-Stokes/RANS fluid iteration. ------------------------------ Begin Solver ----------------------------- Simulation Run using the Single-zone Driver WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better, see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better, see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better, see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations +----------------------------------------------------------------------------------------------------------------------------------------------+ | Time_Iter| Outer_Iter| Inner_Iter| Cur_Time| Time_Step| Time(sec)| rms[Rho]| rms[RhoU]| rms[RhoV]| rms[RhoE]| CEff| +----------------------------------------------------------------------------------------------------------------------------------------------+ | 0| 0| 0| 0.0000e+00| 0.0000e+00| 6.1466e-02| -1.163068| 1.073873| 1.341547| 4.312268| 0.062082| | 0| 0| 1| 0.0000e+00| 0.0000e+00| 5.9716e-02| -1.558471| 0.813117| 0.969484| 3.926501| 0.143132| | 0| 0| 2| 0.0000e+00| 0.0000e+00| 5.7680e-02| -1.599269| 0.950037| 1.012154| 3.879885| 0.386300| | 0| 0| 3| 0.0000e+00| 0.0000e+00| 5.3863e-02| -1.661284| 1.005970| 1.023067| 3.797319| 0.981260| | 0| 0| 4| 0.0000e+00| 0.0000e+00| 5.2837e-02| -1.658421| 1.009907| 0.965279| 3.792658| 2.399755| | 0| 0| 5| 0.0000e+00| 0.0000e+00| 5.1856e-02| -1.630602| 0.996801| 0.859556| 3.833204| 6.390579| | 0| 0| 6| 0.0000e+00| 0.0000e+00| 5.2086e-02| -1.628009| 1.002770| 0.822847| 3.846297| 27.872536| | 0| 0| 7| 0.0000e+00| 0.0000e+00| 5.2300e-02| -1.646113| 1.024424| 0.882502| 3.830202| -48.293527| | 0| 0| 8| 0.0000e+00| 0.0000e+00| 5.2599e-02| -1.672152| 1.033657| 0.939200| 3.797228| -22.113788| | 0| 0| 9| 0.0000e+00| 0.0000e+00| 5.1638e-02| -1.695131| 1.018255| 0.944150| 3.765919| -19.281368| ----------------------------- Solver Exit ------------------------------- Maximum number of iterations reached (ITER = 10) before convergence. +-----------------------------------------------------------------------+ | Convergence Field | Value | Criterion | Converged | +-----------------------------------------------------------------------+ | rms[Rho]| -1.69513| < -14| No| +-----------------------------------------------------------------------+ ------------------------------------------------------------------------- +-----------------------------------------------------------------------+ | File Writing Summary | Filename | +-----------------------------------------------------------------------+ |SU2 binary restart |restart_flow_delaundoMesh.dat | Writing the forces breakdown file (forces_breakdown_delaundoMesh.dat). |CSV file |surface_flow_delaundoMesh.csv | Writing the forces breakdown file (forces_breakdown_delaundoMesh.dat). |Tecplot binary |flow_delaundoMesh.szplt | Writing the forces breakdown file (forces_breakdown_delaundoMesh.dat). |Tecplot binary surface |surface_flow_delaundoMesh.szplt | Error in tecFileWriterClose: Not all node map values for zone 1 have been written. Currently need 492 more values.0: Error finishing Tecplot file output. Writing the forces breakdown file (forces_breakdown_delaundoMesh.dat). +-----------------------------------------------------------------------+ --------------------------- Finalizing Solver --------------------------- Deleted CNumerics container. Deleted CIntegration container. Deleted CSolver container. Deleted CIteration container. Deleted CInterface container. Deleted CGeometry container. Deleted CFreeFormDefBox class. Deleted CSurfaceMovement class. Deleted CVolumetricMovement class. Deleted CConfig container. Deleted nInst container. Deleted COutput class. ------------------------------------------------------------------------- ------------------------- Exit Success (SU2_CFD) ------------------------ Total Force - Pressure + Viscous Cl = 0.805707 Cd = -0.041787 Cmz = 0.408515 Cx = -0.041787 Cy = 0.805707 Pressure Contribution Cl_p = 0.805707 Cd_p = -0.041787 Cmz_p = 0.408515 Cx_p = -0.041787 Cy_p = 0.805707 Viscous Contribution Cl_v = 0.0 Cd_v = 0.0 Cmz_v = 0.0 Cx_v = 0.0 Cy_v = 0.0 real 0m2.252s user 0m2.197s sys 0m0.645s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case su2_and_Delaundo_PyTest.py passed (as expected) ================================================= ================================================= + echo 'su2_and_Tetgen_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.8/CAPS/CFD/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/pyCAPSlog.txt su2_and_Tetgen_PyTest.py test; + python -u su2_and_Tetgen_PyTest.py -outLevel=0 + tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.8/CAPS/CFD/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/pyCAPSlog.txt Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Getting surface mesh for body 1 (of 3) Getting surface mesh for body 2 (of 3) Getting surface mesh for body 3 (of 3) Body 1 (of 3) Number of nodes = 2236 Number of elements = 4468 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 4468 Number of quadrilateral elements = 0 Body 2 (of 3) Number of nodes = 636 Number of elements = 1268 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 1268 Number of quadrilateral elements = 0 Body 3 (of 3) Number of nodes = 258 Number of elements = 512 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 512 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 3130 Total number of elements = 6248 Writing TECPLOT file: egadsTessMesh_Surf_0.dat .... Finished writing TECPLOT file Writing TECPLOT file: egadsTessMesh_Surf_1.dat .... Finished writing TECPLOT file Writing TECPLOT file: egadsTessMesh_Surf_2.dat .... Finished writing TECPLOT file Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Number of surface: nodes - 3130, elements - 6248 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000T1.00e-16A Delaunizing vertices... Delaunay seconds: 0.048667 Creating surface mesh ... Surface mesh seconds: 0.009702 Recovering boundaries... Boundary recovery seconds: 0.119371 Removing exterior tetrahedra ... Spreading region attributes. Exterior tets removal seconds: 0.006948 Suppressing Steiner points ... Steiner suppression seconds: 7e-06 Recovering Delaunayness... Delaunay recovery seconds: 0.02477 Refining mesh... 4180 insertions, added 2142 points, 134947 tetrahedra in queue. 1391 insertions, added 431 points, 139550 tetrahedra in queue. 1855 insertions, added 477 points, 138154 tetrahedra in queue. 2472 insertions, added 613 points, 122807 tetrahedra in queue. 3296 insertions, added 507 points, 67228 tetrahedra in queue. 4393 insertions, added 431 points, 1310 tetrahedra in queue. Refinement seconds: 1.04753 Smoothing vertices... Mesh smoothing seconds: 0.783142 Improving mesh... Mesh improvement seconds: 0.036281 Jettisoning redundant points. Writing nodes. Writing elements. Writing faces. Writing edges. Output seconds: 0.002207 Total running seconds: 2.07908 Statistics: Input points: 3130 Input facets: 6248 Input segments: 9372 Input holes: 2 Input regions: 0 Mesh points: 8227 Mesh tetrahedra: 40661 Mesh faces: 84447 Mesh faces on exterior boundary: 6250 Mesh faces on input facets: 6250 Mesh edges on input segments: 9373 Steiner points on input segments: 1 Steiner points inside domain: 5096 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 "Harrier (8.0.0) " Running SU2...... ------------------------------------------------------------------------- | ___ _ _ ___ | | / __| | | |_ ) Release 8.0.0 "Harrier" | | \__ \ |_| |/ / | | |___/\___//___| 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. 8227 grid points. 40661 volume elements. 3 surface markers. 4468 boundary elements in index 0 (Marker = BC_1). 1270 boundary elements in index 1 (Marker = BC_2). 512 boundary elements in index 2 (Marker = BC_3). 40661 tetrahedra. Setting point connectivity. Renumbering points (Reverse Cuthill McKee Ordering). Recomputing point connectivity. Setting element connectivity. Checking the numerical grid orientation. All volume elements are correctly orientend. All surface elements are correctly orientend. Identifying edges and vertices. Setting the control volume structure. Volume of the computational grid: 2.08741e+06. Searching for the closest normal neighbors to the surfaces. Storing a mapping from global to local point index. Compute the surface curvature. Max K: 414.134. Mean K: 30.6158. Standard deviation K: 37.5195. Checking for periodicity. Computing mesh quality statistics for the dual control volumes. +--------------------------------------------------------------+ | Mesh Quality Metric| Minimum| Maximum| +--------------------------------------------------------------+ | Orthogonality Angle (deg.)| 2.25569| 83.562| | CV Face Area Aspect Ratio| 1.40614| 7154.17| | CV Sub-Volume Ratio| 1.02596| 261709| +--------------------------------------------------------------+ Setting the multigrid structure. +-------------------------------------------+ | MG Level| CVs|Aggl. Rate| CFL| +-------------------------------------------+ | 0| 8227| 1/1.00| 10| | 1| 1360| 1/6.05| 8.23235| | 2| 235| 1/5.79| 6.87793| +-------------------------------------------+ Finding max control volume width. Semi-span length = 7.90569 m. Wetted area = 120.046 m^2. Area projection in the x-plane = 10.7914 m^2, y-plane = 4.5843 m^2, z-plane = 57.287 m^2. Max. coordinate in the x-direction = 12.6407 m, y-direction = 7.90569 m, z-direction = 0.557773 m. Min. coordinate in the x-direction = -0.00409054 m, y-direction = -7.90569 m, z-direction = -0.41192 m. Checking if Euler & Symmetry markers are straight/plane: Boundary marker BC_1 is NOT a single plane. Boundary marker BC_2 is NOT a single plane. Computing wall distances. -------------------- Solver Preprocessing ( Zone 0 ) -------------------- Inviscid flow: Computing density based on free-stream temperature and pressure using the ideal gas law. Force coefficients computed using free-stream values. -- Models: +------------------------------------------------------------------------------+ | Viscosity Model| Conductivity Model| Fluid Model| +------------------------------------------------------------------------------+ | -| -| STANDARD_AIR| +------------------------------------------------------------------------------+ -- Fluid properties: +------------------------------------------------------------------------------+ | Name| Dim. value| Ref. value| Unit|Non-dim. value| +------------------------------------------------------------------------------+ | Gas Constant| 287.058| 1| N.m/kg.K| 287.058| | Spec. Heat Ratio| -| -| -| 1.4| +------------------------------------------------------------------------------+ -- Initial and free-stream conditions: +------------------------------------------------------------------------------+ | Name| Dim. value| Ref. value| Unit|Non-dim. value| +------------------------------------------------------------------------------+ | Static Pressure| 101325| 1| Pa| 101325| | Density| 1.22498| 1| kg/m^3| 1.22498| | Temperature| 288.15| 1| K| 288.15| | Total Energy| 226952| 1| m^2/s^2| 226952| | Velocity-X| 200.779| 1| m/s| 200.779| | Velocity-Y| 0| 1| m/s| 0| | Velocity-Z| 3.50461| 1| m/s| 3.50461| | Velocity Magnitude| 200.809| 1| m/s| 200.809| +------------------------------------------------------------------------------+ | Mach Number| -| -| -| 0.5901| +------------------------------------------------------------------------------+ Initialize Jacobian structure (Euler). MG level: 0. Initialize Jacobian structure (Euler). MG level: 1. Initialize Jacobian structure (Euler). MG level: 2. ------------------- Numerics Preprocessing ( Zone 0 ) ------------------- ----------------- Integration Preprocessing ( Zone 0 ) ------------------ ------------------- Iteration Preprocessing ( Zone 0 ) ------------------ Euler/Navier-Stokes/RANS fluid iteration. ------------------------------ Begin Solver ----------------------------- Simulation Run using the Single-zone Driver WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better, see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better, see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better, see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations +----------------------------------------------------------------------------------------------------------------------------------------------+ | Time_Iter| Outer_Iter| Inner_Iter| Cur_Time| Time_Step| Time(sec)| rms[Rho]| rms[RhoU]| rms[RhoV]| rms[RhoE]| CEff| +----------------------------------------------------------------------------------------------------------------------------------------------+ | 0| 0| 0| 0.0000e+00| 0.0000e+00| 1.6474e-01| 0.614349| 3.046325| 2.089422| 6.105244| 1.831854| | 0| 0| 1| 0.0000e+00| 0.0000e+00| 1.6338e-01| 0.764583| 3.258604| 2.974732| 6.265552| 2.165840| | 0| 0| 2| 0.0000e+00| 0.0000e+00| 1.6106e-01| 0.642409| 3.278261| 3.214494| 6.139447| 3.169947| | 0| 0| 3| 0.0000e+00| 0.0000e+00| 1.5809e-01| 0.541917| 3.250446| 3.272037| 6.028748| 4.533401| | 0| 0| 4| 0.0000e+00| 0.0000e+00| 1.5616e-01| 0.535101| 3.187480| 3.218588| 6.011712| 5.728616| ----------------------------- Solver Exit ------------------------------- Maximum number of iterations reached (ITER = 5) before convergence. +-----------------------------------------------------------------------+ | Convergence Field | Value | Criterion | Converged | +-----------------------------------------------------------------------+ | rms[Rho]| 0.535101| < -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). +-----------------------------------------------------------------------+ --------------------------- Finalizing Solver --------------------------- 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 = 0.763097 Cd = 0.133208 Cmx = -0.004493 Cmy = -0.215511 Cmz = 0.000816 Cx = 0.11987 Cy = 0.0005 Cz = 0.765306 real 0m7.206s user 0m7.076s sys 0m0.445s + 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/7.8/CAPS/CFD/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/pyCAPSlog.txt su2_X43a_PyTest.py test; + python -u su2_X43a_PyTest.py -outLevel=0 + tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.8/CAPS/CFD/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/pyCAPSlog.txt /Library/Developer/CommandLineTools/SDKs/MacOSX.sdk/usr/include/c++/v1/__iterator/reverse_iterator.h:145:64: runtime error: reference binding to misaligned address 0x00013104c054 for type 'IntWalk_WalkingData', which requires 8 byte alignment 0x00013104c054: note: pointer points here ff ff ff ff ff ff ff ff ff ff ff ff ff ff ff ff ff ff ff ff ff ff ff ff ff ff ff ff ff ff ff ff ^ SUMMARY: UndefinedBehaviorSanitizer: undefined-behavior /Library/Developer/CommandLineTools/SDKs/MacOSX.sdk/usr/include/c++/v1/__iterator/reverse_iterator.h:145:64 in /Library/Developer/CommandLineTools/SDKs/MacOSX.sdk/usr/include/c++/v1/vector:1460:12: runtime error: reference binding to misaligned address 0x00013104c0a4 for type 'value_type' (aka 'IntWalk_WalkingData'), which requires 8 byte alignment 0x00013104c0a4: note: pointer points here 01 00 00 00 00 00 00 00 00 00 f0 3f 2a a1 9a e8 57 b5 e6 3f 0c 00 00 00 20 58 21 40 00 00 00 00 ^ SUMMARY: UndefinedBehaviorSanitizer: undefined-behavior /Library/Developer/CommandLineTools/SDKs/MacOSX.sdk/usr/include/c++/v1/vector:1460:12 in /Users/jenkins/util/ESP/opencascade-7.8/trunk/src/NCollection/NCollection_OccAllocator.hxx:153:25: runtime error: constructor call on misaligned address 0x00013106006c for type 'IntWalk_WalkingData', which requires 8 byte alignment 0x00013106006c: note: pointer points here 01 00 00 00 63 44 fc 3f 30 f1 e6 93 f4 17 fe 3f 68 eb 9b 37 eb a4 ff 3f a0 01 32 90 ff ff ff ff ^ SUMMARY: UndefinedBehaviorSanitizer: undefined-behavior /Users/jenkins/util/ESP/opencascade-7.8/trunk/src/NCollection/NCollection_OccAllocator.hxx:153:25 in /Library/Developer/CommandLineTools/SDKs/MacOSX.sdk/usr/include/c++/v1/vector:1470:12: runtime error: reference binding to misaligned address 0x00013104c0a4 for type 'const value_type' (aka 'const IntWalk_WalkingData'), which requires 8 byte alignment 0x00013104c0a4: note: pointer points here 01 00 00 00 00 00 00 00 00 00 f0 3f 2a a1 9a e8 57 b5 e6 3f f4 ff ff ff 20 58 21 40 00 00 00 00 ^ SUMMARY: UndefinedBehaviorSanitizer: undefined-behavior /Library/Developer/CommandLineTools/SDKs/MacOSX.sdk/usr/include/c++/v1/vector:1470:12 in 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 = 5678 Number of elements = 11352 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 11352 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 9486 Total number of elements = 18968 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 - 9486, elements - 18968 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000T1.00e-16A Delaunizing vertices... Delaunay seconds: 0.130952 Creating surface mesh ... Surface mesh seconds: 0.023791 Recovering boundaries... Warning: 2 segments are not recovered. Boundary recovery seconds: 0.324838 Removing exterior tetrahedra ... Spreading region attributes. Exterior tets removal seconds: 0.019342 Suppressing Steiner points ... Steiner suppression seconds: 2.2e-05 Recovering Delaunayness... Delaunay recovery seconds: 0.03967 Refining mesh... 12647 insertions, added 5257 points, 11940 tetrahedra in queue. Refinement seconds: 1.12192 Smoothing vertices... Mesh smoothing seconds: 0.94673 Improving mesh... Mesh improvement seconds: 0.048501 Jettisoning redundant points. Writing nodes. Writing elements. Writing faces. Writing edges. Output seconds: 0.007579 Total running seconds: 2.66416 Statistics: Input points: 9486 Input facets: 18968 Input segments: 28452 Input holes: 1 Input regions: 0 Mesh points: 14929 Mesh tetrahedra: 61505 Mesh faces: 132494 Mesh faces on exterior boundary: 18968 Mesh faces on input facets: 18968 Mesh edges on input segments: 28452 Steiner points inside domain: 5443 Done meshing using TetGen! Writing SU2 file .... Finished writing SU2 file Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - x43A Done getting CFD boundary conditions Writing boundary flags - bcProps.surfaceProp[0].surfaceType = 3 - bcProps.surfaceProp[1].surfaceType = 1 Done boundary flags Warning: The su2 cfg file will be overwritten! Write SU2 configuration file for version "Harrier (8.0.0) " Running SU2...... ------------------------------------------------------------------------- | ___ _ _ ___ | | / __| | | |_ ) Release 8.0.0 "Harrier" | | \__ \ |_| |/ / | | |___/\___//___| 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. 14929 grid points. 61505 volume elements. 2 surface markers. 7616 boundary elements in index 0 (Marker = BC_1). 11352 boundary elements in index 1 (Marker = BC_2). 61505 tetrahedra. Setting point connectivity. Renumbering points (Reverse Cuthill McKee Ordering). Recomputing point connectivity. Setting element connectivity. Checking the numerical grid orientation. All volume elements are correctly orientend. All surface elements are correctly orientend. Identifying edges and vertices. Setting the control volume structure. Volume of the computational grid: 2.67745e+08. Searching for the closest normal neighbors to the surfaces. Storing a mapping from global to local point index. Compute the surface curvature. Max K: 95.6599. Mean K: 0.523696. Standard deviation K: 2.57688. Checking for periodicity. Computing mesh quality statistics for the dual control volumes. +--------------------------------------------------------------+ | Mesh Quality Metric| Minimum| Maximum| +--------------------------------------------------------------+ | Orthogonality Angle (deg.)| 2.01085| 85.2046| | CV Face Area Aspect Ratio| 1.41431| 3475.64| | CV Sub-Volume Ratio| 1| 768690| +--------------------------------------------------------------+ Setting the multigrid structure. +-------------------------------------------+ | MG Level| CVs|Aggl. Rate| CFL| +-------------------------------------------+ | 0| 14929| 1/1.00| 10| | 1| 2715| 1/5.5| 8.49841| | 2| 490| 1/5.54| 7.20395| +-------------------------------------------+ Finding max control volume width. Semi-span length = 30 m. Wetted area = 13596.3 m^2. Area projection in the x-plane = 761.676 m^2, y-plane = 2062.27 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| 2.6229e-01| 2.730238| 5.664282| 4.727966| 8.729713| -0.338259| | 0| 0| 1| 0.0000e+00| 0.0000e+00| 2.7874e-01| 3.172855| 6.235351| 5.708733| 9.163474| -0.117122| | 0| 0| 2| 0.0000e+00| 0.0000e+00| 2.8540e-01| 3.313832| 6.405575| 5.809826| 9.273948| -0.036095| | 0| 0| 3| 0.0000e+00| 0.0000e+00| 2.8517e-01| 3.301504| 6.396712| 5.682129| 9.288613| -0.015822| | 0| 0| 4| 0.0000e+00| 0.0000e+00| 2.8450e-01| 3.134853| 6.203812| 5.540269| 9.119715| -0.030764| ----------------------------- Solver Exit ------------------------------- Maximum number of iterations reached (ITER = 5) before convergence. +-----------------------------------------------------------------------+ | Convergence Field | Value | Criterion | Converged | +-----------------------------------------------------------------------+ | rms[Rho]| 3.13485| < -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: 58 reconstructed states for upwinding are non-physical. --------------------------- Finalizing Solver --------------------------- 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 = -3.688941 Cd = 119.911192 Cmx = 35.034239 Cmy = 8986.683762 Cmz = 192.445678 Cx = 119.939922 Cy = 1.734147 Cz = 2.591782 real 0m17.242s user 0m25.593s sys 0m0.733s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case su2_X43a_PyTest.py passed (as expected) ================================================= ./execute_PyTestRegression.sh: line 413: 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 ================================================= + tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.8/CAPS/CFD/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/pyCAPSlog.txt + echo 'cart3d_PyTest.py test;' cart3d_PyTest.py test; + python -u cart3d_PyTest.py -outLevel=0 + tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.8/CAPS/CFD/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/pyCAPSlog.txt Loading AIM Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = Wing, index = 1 Body size = 3.796888 Tessellating body 1 with MaxEdge = 0.094922 Sag = 0.003797 Angle = 15.000000 Executing: autoInputs -r 30.000000 -nDiv 6 -maxR 9 > autoInputs.out Executing: ./aero.csh > aero.out C_A 0.023693377 C_Y -0.0012129282 C_N 0.065395002 C_D 0.025961197 C_S -0.0012129282 C_L 0.064528278 C_l 0.0510971 C_m 0.000248187 C_n -0.017525 C_M_x 0.0504544 C_M_y 0.000248187 C_M_z -0.0192976 real 0m28.824s user 0m35.101s sys 0m1.231s + 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/7.8/CAPS/CFD/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/pyCAPSlog.txt cart3d_OpenMDAO_3_alpha_PyTest.py test; + python -u cart3d_OpenMDAO_3_alpha_PyTest.py -outLevel=0 + tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.8/CAPS/CFD/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/pyCAPSlog.txt ---------------------------------------- >>> alpha [2.] Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = Wing, index = 1 Getting CFD design variables....... Number of design variables - 1 Design Variable name - alpha Done getting CFD design variables Getting CFD functional....... Number of design variables - 1 Objective name - CL2 Done getting CFD functional Body size = 3.625615 Tessellating body 1 with MaxEdge = 0.090640 Sag = 0.003626 Angle = 15.000000 Executing: autoInputs -r 30.000000 -nDiv 5 -maxR 7 -mesh2d > autoInputs.out o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (11:15:41) Running aero.csh on 2 core(s) in M0.5901A2B0_DP1 (11:15:44) 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 (11:15:45) Running aero.csh on 2 core(s) in M0.5901A2B0_DP1 (11:15:50) 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 (11:15:51) Linearizing cut-cells (11:15:51) ... done o Number of simultaneous xsensit jobs: 1 (11:15:51) Computing gradients (11:15:55) ... 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 (11:15:56) Running aero.csh on 2 core(s) in M0.5901A1.98427B0_DP1 (11:16:00) 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 (11:16:01) Running aero.csh on 2 core(s) in M0.5901A1.98427B0_DP1 (11:16:07) 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 (11:16:07) Linearizing cut-cells (11:16:07) ... done o Number of simultaneous xsensit jobs: 1 (11:16:07) Computing gradients (11:16:11) ... 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 (11:16:12) Running aero.csh on 2 core(s) in M0.5901A-0.0109917B0_DP1 (11:16:16) aero.csh done o case M0.5901A-0.0109917B0_DP1, averaging data over 1 cycle(s) >>> CL2 [6.05653711e-06] CL 0.00246101 ---------------------------------------- ======================================== o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (11:16:17) Running aero.csh on 2 core(s) in M0.5901A-0.0109917B0_DP1 (11:16:24) 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 (11:16:24) Linearizing cut-cells (11:16:24) ... done o Number of simultaneous xsensit jobs: 1 (11:16:24) Computing gradients (11:16:28) ... done o case M0.5901A-0.0109917B0_DP1, averaging data over 1 cycle(s) >>> CL2_alpha [[0.00031042]] ======================================== At iterate 2 f= 6.05654D-06 |proj g|= 3.10424D-04 ---------------------------------------- >>> alpha [-0.05149286] o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (11:16:29) Running aero.csh on 2 core(s) in M0.5901A-0.0514929B0_DP1 (11:16:33) aero.csh done o case M0.5901A-0.0514929B0_DP1, averaging data over 1 cycle(s) >>> CL2 [2.59817062e-10] CL 1.612e-05 ---------------------------------------- ======================================== o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (11:16:34) Running aero.csh on 2 core(s) in M0.5901A-0.0514929B0_DP1 (11:16:40) 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 (11:16:40) Linearizing cut-cells (11:16:40) ... done o Number of simultaneous xsensit jobs: 1 (11:16:40) Computing gradients (11:16:44) ... done o case M0.5901A-0.0514929B0_DP1, averaging data over 1 cycle(s) >>> CL2_alpha [[2.03612433e-06]] ======================================== At iterate 3 f= 2.59817D-10 |proj g|= 2.03612D-06 ---------------------------------------- >>> alpha [-0.05176027] o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (11:16:46) Running aero.csh on 2 core(s) in M0.5901A-0.0517603B0_DP1 (11:16:50) aero.csh done o case M0.5901A-0.0517603B0_DP1, averaging data over 1 cycle(s) >>> CL2 [9.25766089e-15] CL 1e-07 ---------------------------------------- ======================================== o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (11:16:51) Running aero.csh on 2 core(s) in M0.5901A-0.0517603B0_DP1 (11:16:56) 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 (11:16:56) Linearizing cut-cells (11:16:56) ... done o Number of simultaneous xsensit jobs: 1 (11:16:56) Computing gradients (11:17:00) ... done o case M0.5901A-0.0517603B0_DP1, averaging data over 1 cycle(s) >>> CL2_alpha [[1.21372408e-08]] ======================================== At iterate 4 f= 9.25766D-15 |proj g|= 1.21372D-08 * * * Tit = total number of iterations Tnf = total number of function evaluations Tnint = total number of segments explored during Cauchy searches Skip = number of BFGS updates skipped Nact = number of active bounds at final generalized Cauchy point Projg = norm of the final projected gradient F = final function value * * * N Tit Tnf Tnint Skip Nact Projg F 1 4 5 4 0 0 1.214D-08 9.258D-15 F = 9.2576608860000000E-015 CONVERGENCE: NORM_OF_PROJECTED_GRADIENT_<=_PGTOL Optimization Complete ----------------------------------- Optimized value: [-0.05176027] real 1m28.160s user 0m56.817s sys 0m10.013s + 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/7.8/CAPS/CFD/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/pyCAPSlog.txt cart3d_OpenMDAO_3_twist_PyTest.py test; + python -u cart3d_OpenMDAO_3_twist_PyTest.py -outLevel=0 + tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.8/CAPS/CFD/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/pyCAPSlog.txt ---------------------------------------- >>> twist [4.] Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = Wing, index = 1 Getting CFD design variables....... Number of design variables - 1 Design Variable name - twist Done getting CFD design variables Getting CFD functional....... Number of design variables - 1 Objective name - CL2 Done getting CFD functional Body size = 3.630958 Tessellating body 1 with MaxEdge = 0.018155 Sag = 0.000908 Angle = 10.000000 Executing: autoInputs -r 5.123450 -nDiv 5 -maxR 7 -symmY -halfBody > autoInputs.out o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (11:17:06) Running aero.csh on 2 core(s) in M0.5901A0B0_DP1 (11:17:29) 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 (11:17:31) Running aero.csh on 2 core(s) in M0.5901A0B0_DP1 (11:18:07) 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 (11:18:07) Linearizing cut-cells (11:18:09) ... done o Number of simultaneous xsensit jobs: 1 (11:18:09) Computing gradients (11:18:13) ... done o case M0.5901A0B0_DP1, averaging data over 1 cycle(s) >>> CL2_twist [[0.00210056]] ======================================== 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|= 2.10056D-03 ---------------------------------------- >>> twist [3.99789944] 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 (11:18:19) Running aero.csh on 2 core(s) in M0.5901A0B0_DP1 (11:18:40) aero.csh done o case M0.5901A0B0_DP1, averaging data over 1 cycle(s) >>> CL2 [0.0041123] CL 0.0641197 ---------------------------------------- ======================================== o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (11:18:41) Running aero.csh on 2 core(s) in M0.5901A0B0_DP1 (11:19:11) 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 (11:19:11) Linearizing cut-cells (11:19:13) ... done o Number of simultaneous xsensit jobs: 1 (11:19:13) Computing gradients (11:19:17) ... done o case M0.5901A0B0_DP1, averaging data over 1 cycle(s) >>> CL2_twist [[0.00210014]] ======================================== At iterate 1 f= 4.11230D-03 |proj g|= 2.10014D-03 ---------------------------------------- >>> twist [-6.51746276] Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = Wing, index = 1 Body size = 3.635732 Tessellating body 1 with MaxEdge = 0.018179 Sag = 0.000909 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 (11:19:21) Running aero.csh on 2 core(s) in M0.5901A0B0_DP1 (11:19:50) aero.csh done o case M0.5901A0B0_DP1, averaging data over 1 cycle(s) >>> CL2 [0.00998113] CL -0.0999038 ---------------------------------------- ======================================== o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (11:19:52) Running aero.csh on 2 core(s) in M0.5901A0B0_DP1 (11:20:27) aero.csh done Max memory allowed: 32 GB Flow hexes: 37089 Estimated cutter memory: 0.003709 GB / DV Estimated xsensit memory: 0.070469 GB / DV Available threads: 2 # DVs: 1 o Number of simultaneous cutter jobs: 1 (11:20:27) Linearizing cut-cells (11:20:29) ... done o Number of simultaneous xsensit jobs: 1 (11:20:30) Computing gradients (11:20:34) ... done o case M0.5901A0B0_DP1, averaging data over 1 cycle(s) >>> CL2_twist [[-0.00319688]] ======================================== ---------------------------------------- >>> twist [-0.14346253] Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = Wing, index = 1 Body size = 3.625762 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 (11:20:38) Running aero.csh on 2 core(s) in M0.5901A0B0_DP1 (11:21:09) aero.csh done o case M0.5901A0B0_DP1, averaging data over 1 cycle(s) >>> CL2 [4.79399981e-08] CL -0.00022338 ---------------------------------------- ======================================== o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (11:21:10) Running aero.csh on 2 core(s) in M0.5901A0B0_DP1 (11:21:45) 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 (11:21:46) Linearizing cut-cells (11:21:48) ... done o Number of simultaneous xsensit jobs: 1 (11:21:48) Computing gradients (11:21:52) ... done o case M0.5901A0B0_DP1, averaging data over 1 cycle(s) >>> CL2_twist [[-7.24744796e-06]] ======================================== At iterate 2 f= 4.79400D-08 |proj g|= 7.24745D-06 ---------------------------------------- >>> twist [-0.12922012] Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = Wing, index = 1 Body size = 3.625747 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 (11:21:57) Running aero.csh on 2 core(s) in M0.5901A0B0_DP1 (11:22:21) aero.csh done o case M0.5901A0B0_DP1, averaging data over 1 cycle(s) >>> CL2 [2.18171454e-08] CL 0.00015117 ---------------------------------------- ======================================== o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (11:22:22) Running aero.csh on 2 core(s) in M0.5901A0B0_DP1 (11:22:51) 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 (11:22:51) Linearizing cut-cells (11:22:53) ... done o Number of simultaneous xsensit jobs: 1 (11:22:53) Computing gradients (11:22:57) ... done o case M0.5901A0B0_DP1, averaging data over 1 cycle(s) >>> CL2_twist [[4.89192855e-06]] ======================================== At iterate 3 f= 2.18171D-08 |proj g|= 4.89193D-06 * * * 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 3 5 3 0 0 4.892D-06 2.182D-08 F = 2.1817145410999999E-008 CONVERGENCE: REL_REDUCTION_OF_F_<=_FACTR*EPSMCH Optimization Complete ----------------------------------- Optimized values: [-0.12922012] real 5m56.468s user 6m14.442s sys 0m15.712s + 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/7.8/CAPS/CFD/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/pyCAPSlog.txt fun3d_Morph_PyTest.py test; + python -u fun3d_Morph_PyTest.py -outLevel=0 -noAnalysis + tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.8/CAPS/CFD/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/pyCAPSlog.txt Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 AFLR4 : Proximity BG Surface Grid Generation Skipped AFLR4 : No Modifications Required Writing TECPLOT file: pyCAPS_AFLR4_AFLR3.dat .... Finished writing TECPLOT file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Getting volume mesh AFLR2 : --------------------------------------- AFLR2 : AFLR2 LIBRARY AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR2 : TRIA/QUAD GRID GENERATOR AFLR2 : Version Number 9.14.7 AFLR2 : Version Date 07/16/23 @ 01:42PM AFLR2 : Compile OS Darwin 22.6.0 arm64 AFLR2 : Compile Date 08/01/23 @ 11:39PM AFLR2 : Copyright 1994-2021, D.L. Marcum AFLR2 : --------------------------------------- AFLR4 : --------------------------------------- AFLR4 : AFLR4 LIBRARY AFLR4 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR4 : TRIA/QUAD SURFACE GRID GENERATOR AFLR4 : Version Number 11.5.9 AFLR4 : Version Date 08/14/23 @ 12:27AM AFLR4 : Compile OS Darwin 22.6.0 arm64 AFLR4 : Compile Date 08/14/23 @ 12:31AM AFLR4 : Copyright 1994-2021, D.L. Marcum AFLR4 : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 81588 Number of elements = 475862 Number of triangles = 15680 Number of quadrilatarals = 0 Number of tetrahedrals = 460182 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 0m12.136s user 0m10.581s sys 0m0.471s + 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/7.8/CAPS/CFD/DARWIN_ARM64') [GNU C Compiler (gcc)] Successfully parsed console log [GNU C Compiler (gcc)] -> found 20 issues (skipped 0 duplicates) [GNU C Compiler (gcc)] Post processing issues on 'viggen' with source code encoding 'UTF-8' [GNU C Compiler (gcc)] Creating SCM blamer to obtain author and commit information for affected files [GNU C Compiler (gcc)] SCM 'hudson.scm.SubversionSCM' is not of type GitSCM [GNU C Compiler (gcc)] -> Git blamer could not be created for SCM 'hudson.scm.SubversionSCM@30d23cc1' in working tree '/Users/jenkins/workspace/ESP_UndefinedCaps/7.8/CAPS/CFD/DARWIN_ARM64' [GNU C Compiler (gcc)] -> No suitable blamer found. [GNU C Compiler (gcc)] Resolving file names for all issues in workspace '/Users/jenkins/workspace/ESP_UndefinedCaps/7.8/CAPS/CFD/DARWIN_ARM64' [GNU C Compiler (gcc)] -> resolved paths in source directory (3 found, 0 not found) [GNU C Compiler (gcc)] Resolving module names from module definitions (build.xml, pom.xml, or Manifest.mf files) [GNU C Compiler (gcc)] -> resolved module names for 20 issues [GNU C Compiler (gcc)] Resolving package names (or namespaces) by parsing the affected files [GNU C Compiler (gcc)] -> resolved package names of 3 affected files [GNU C Compiler (gcc)] No filter has been set, publishing all 20 issues [GNU C Compiler (gcc)] Creating fingerprints for all affected code blocks to track issues over different builds [GNU C Compiler (gcc)] -> created fingerprints for 20 issues (skipped 0 issues) [GNU C Compiler (gcc)] Copying affected files to Jenkins' build folder '/var/lib/jenkins/jobs/ESP_UndefinedCaps/configurations/axis-CASREV/7.8/axis-ESPTEST/CAPS%2FCFD/axis-ESP_ARCH/DARWIN_ARM64/axis-buildnode/viggen/builds/198/files-with-issues' [GNU C Compiler (gcc)] -> 0 copied, 20 not in workspace, 0 not-found, 0 with I/O error [GNU C Compiler (gcc)] Skipping cleaning of source code files in old builds [GNU C Compiler (gcc)] Repository miner is not configured, skipping repository mining [Clang] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_UndefinedCaps/7.8/CAPS/CFD/DARWIN_ARM64') [Clang] -> found 20 issues (skipped 0 duplicates) [Clang] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_UndefinedCaps/7.8/CAPS/CFD/DARWIN_ARM64') [Clang] -> found 20 issues (skipped 0 duplicates) [Clang] Successfully parsed console log [Clang] -> found 20 issues (skipped 0 duplicates) [Clang] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_UndefinedCaps/7.8/CAPS/CFD/DARWIN_ARM64') [Clang] Post processing issues on 'viggen' with source code encoding 'UTF-8' [Clang] Creating SCM blamer to obtain author and commit information for affected files [Clang] SCM 'hudson.scm.SubversionSCM' is not of type GitSCM [Clang] -> Git blamer could not be created for SCM 'hudson.scm.SubversionSCM@30d23cc1' in working tree '/Users/jenkins/workspace/ESP_UndefinedCaps/7.8/CAPS/CFD/DARWIN_ARM64' [Clang] -> No suitable blamer found. [Clang] Resolving file names for all issues in workspace '/Users/jenkins/workspace/ESP_UndefinedCaps/7.8/CAPS/CFD/DARWIN_ARM64' [Clang] -> resolved paths in source directory (3 found, 0 not found) [Clang] Resolving module names from module definitions (build.xml, pom.xml, or Manifest.mf files) [Clang] -> resolved module names for 20 issues [Clang] Resolving package names (or namespaces) by parsing the affected files [Clang] -> resolved package names of 3 affected files [Clang] No filter has been set, publishing all 20 issues [Clang] Creating fingerprints for all affected code blocks to track issues over different builds [Clang] -> created fingerprints for 20 issues (skipped 0 issues) [Clang] Copying affected files to Jenkins' build folder '/var/lib/jenkins/jobs/ESP_UndefinedCaps/configurations/axis-CASREV/7.8/axis-ESPTEST/CAPS%2FCFD/axis-ESP_ARCH/DARWIN_ARM64/axis-buildnode/viggen/builds/198/files-with-issues' [Clang] -> 0 copied, 20 not in workspace, 0 not-found, 0 with I/O error [Clang] Skipping cleaning of source code files in old builds [Clang] Repository miner is not configured, skipping repository mining [Static Analysis] Successfully parsed console log [Static Analysis] -> found 20 issues (skipped 0 duplicates) [Static Analysis] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_UndefinedCaps/7.8/CAPS/CFD/DARWIN_ARM64') [Static Analysis] Successfully parsed console log [Static Analysis] -> found 20 issues (skipped 0 duplicates) [Static Analysis] Post processing issues on 'viggen' with source code encoding 'UTF-8' [Static Analysis] Creating SCM blamer to obtain author and commit information for affected files [Static Analysis] SCM 'hudson.scm.SubversionSCM' is not of type GitSCM [Static Analysis] -> Git blamer could not be created for SCM 'hudson.scm.SubversionSCM@30d23cc1' in working tree '/Users/jenkins/workspace/ESP_UndefinedCaps/7.8/CAPS/CFD/DARWIN_ARM64' [Static Analysis] -> No suitable blamer found. [Static Analysis] Resolving file names for all issues in workspace '/Users/jenkins/workspace/ESP_UndefinedCaps/7.8/CAPS/CFD/DARWIN_ARM64' [Static Analysis] -> resolved paths in source directory (3 found, 0 not found) [Static Analysis] Resolving module names from module definitions (build.xml, pom.xml, or Manifest.mf files) [Static Analysis] -> resolved module names for 20 issues [Static Analysis] Resolving package names (or namespaces) by parsing the affected files [Static Analysis] -> resolved package names of 3 affected files [Static Analysis] No filter has been set, publishing all 20 issues [Static Analysis] Creating fingerprints for all affected code blocks to track issues over different builds [Static Analysis] -> created fingerprints for 20 issues (skipped 0 issues) [Static Analysis] Copying affected files to Jenkins' build folder '/var/lib/jenkins/jobs/ESP_UndefinedCaps/configurations/axis-CASREV/7.8/axis-ESPTEST/CAPS%2FCFD/axis-ESP_ARCH/DARWIN_ARM64/axis-buildnode/viggen/builds/198/files-with-issues' [Static Analysis] -> 0 copied, 20 not in workspace, 0 not-found, 0 with I/O error [Static Analysis] Skipping cleaning of source code files in old builds [Static Analysis] Repository miner is not configured, skipping repository mining [Static Analysis] Successfully parsed console log [Static Analysis] -> found 20 issues (skipped 0 duplicates) [Static Analysis] Successfully parsed console log [Static Analysis] -> found 20 issues (skipped 0 duplicates) [Static Analysis] Successfully parsed console log [Static Analysis] -> found 20 issues (skipped 0 duplicates) [Static Analysis] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_UndefinedCaps/7.8/CAPS/CFD/DARWIN_ARM64') [Static Analysis] Post processing issues on 'viggen' with source code encoding 'UTF-8' [Static Analysis] Creating SCM blamer to obtain author and commit information for affected files [Static Analysis] SCM 'hudson.scm.SubversionSCM' is not of type GitSCM [Static Analysis] -> Git blamer could not be created for SCM 'hudson.scm.SubversionSCM@30d23cc1' in working tree '/Users/jenkins/workspace/ESP_UndefinedCaps/7.8/CAPS/CFD/DARWIN_ARM64' [Static Analysis] -> No suitable blamer found. [Static Analysis] Resolving file names for all issues in workspace '/Users/jenkins/workspace/ESP_UndefinedCaps/7.8/CAPS/CFD/DARWIN_ARM64' [Static Analysis] -> resolved paths in source directory (3 found, 0 not found) [Static Analysis] Resolving module names from module definitions (build.xml, pom.xml, or Manifest.mf files) [Static Analysis] -> resolved module names for 20 issues [Static Analysis] Resolving package names (or namespaces) by parsing the affected files [Static Analysis] -> resolved package names of 3 affected files [Static Analysis] No filter has been set, publishing all 20 issues [Static Analysis] Creating fingerprints for all affected code blocks to track issues over different builds [Static Analysis] -> created fingerprints for 20 issues (skipped 0 issues) [Static Analysis] Copying affected files to Jenkins' build folder '/var/lib/jenkins/jobs/ESP_UndefinedCaps/configurations/axis-CASREV/7.8/axis-ESPTEST/CAPS%2FCFD/axis-ESP_ARCH/DARWIN_ARM64/axis-buildnode/viggen/builds/198/files-with-issues' [Static Analysis] -> 0 copied, 20 not in workspace, 0 not-found, 0 with I/O error [Static Analysis] Skipping cleaning of source code files in old builds [Static Analysis] Repository miner is not configured, skipping repository mining [Static Analysis] Reference build recorder is not configured [Static Analysis] No valid reference build found [Static Analysis] All reported issues will be considered outstanding [Static Analysis] No quality gates have been set - skipping [Static Analysis] Health report is disabled - skipping [Static Analysis] Created analysis result for 40 issues (found 0 new issues, fixed 0 issues) [Static Analysis] Attaching ResultAction with ID 'analysis' to build 'ESP_UndefinedCaps/CASREV=7.8,ESPTEST=CAPS/CFD,ESP_ARCH=DARWIN_ARM64,buildnode=viggen #198'. [Checks API] No suitable checks publisher found. Build step 'Console output (build log) parsing' changed build result to FAILURE [PostBuildScript] - [INFO] Executing post build scripts. [PostBuildScript] - [INFO] build step #0 should only be executed on MATRIX [WS-CLEANUP] Deleting project workspace... [WS-CLEANUP] Skipped based on build state FAILURE Finished: FAILURE