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Started by upstream project "ESP_RegCaps" build number 649 originally caused by: Started by user galbramc Running as galbramc [EnvInject] - Loading node environment variables. Building remotely on viggen in workspace /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64 [WS-CLEANUP] Deleting project workspace... [WS-CLEANUP] Done Cleaning up /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/EGADS Deleting /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/EGADS/trunk/pyEGADS/pyEGADS/__pycache__ Deleting /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/EGADS/trunk/docs/EGADS_dot/src/circle1_dot Deleting /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/EGADS/trunk/docs/EGADS_dot/src/circle2_dot Deleting /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/EGADS/trunk/docs/EGADS_dot/src/naca_dot Deleting /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/EGADS/trunk/docs/EGADS_dot/src/ruled_naca_dot Deleting /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/EGADS/trunk/docs/UDP_UDF/data/tire Deleting /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/EGADS/trunk/docs/UDP_UDF/data/tire.o Deleting 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-0400' Using sole credentials 3614a4cf-01de-4393-97de-73734b7dd5a2 in realm ‘svn+ssh://acdl.mit.edu’ Using sole credentials 3614a4cf-01de-4393-97de-73734b7dd5a2 in realm ‘svn+ssh://acdl.mit.edu’ At revision 2495 Cleaning up /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/OpenCSM/trunk/data Updating svn+ssh://acdl.mit.edu/home/svnroot/OpenCSM/trunk/data at revision '2024-05-16T18:49:17.627 -0400' Using sole credentials 3614a4cf-01de-4393-97de-73734b7dd5a2 in realm ‘svn+ssh://acdl.mit.edu’ Using sole credentials 3614a4cf-01de-4393-97de-73734b7dd5a2 in realm ‘svn+ssh://acdl.mit.edu’ A Slugs A Slugs/verify_7.8.0 A Slugs/verify_7.8.0/blend12_1.vfy A Slugs/verify_7.8.0/blindeye_1.vfy A Slugs/verify_7.8.0/boxBall_1.vfy A Slugs/verify_7.8.0/boxHole_1.vfy A Slugs/verify_7.8.0/box_1.vfy A Slugs/verify_7.8.0/cylinderHole_1.vfy A Slugs/verify_7.8.0/cylinder_1.vfy A Slugs/verify_7.8.0/damaged_2.vfy A Slugs/verify_7.8.0/demo1_1.vfy A Slugs/verify_7.8.0/duct_1.vfy A 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Slugs/blindeye_0.jrnl A Slugs/blindeye_0.stl A Slugs/blindeye_1.csm A Slugs/box.plot A Slugs/boxBall_0.csm A Slugs/boxBall_1.csm A Slugs/boxHole.plot A Slugs/boxHole_0.csm A Slugs/boxHole_0.jrnl A Slugs/boxHole_0.stl A Slugs/box_0.csm A Slugs/box_0.jrnl A Slugs/box_0.stl A Slugs/cylinder.plot A Slugs/cylinderHole.plot A Slugs/cylinderHole_0.csm A Slugs/cylinderHole_0.jrnl A Slugs/cylinderHole_0.stl A Slugs/cylinder_0.csm A Slugs/cylinder_0.jrnl A Slugs/cylinder_0.stl A Slugs/damaged.plot A Slugs/damaged_0.csm A Slugs/damaged_0.stl A Slugs/damaged_1.jrnl A Slugs/demo1.plot A Slugs/demo1_0.csm A Slugs/demo1_0.jrnl A Slugs/demo1_0.stl A Slugs/duct.plot A Slugs/duct_0.csm A Slugs/duct_0.jrnl A Slugs/duct_0.stl A Slugs/eyeball.plot A Slugs/eyeball_0.csm A Slugs/eyeball_0.jrnl A Slugs/eyeball_0.stl A Slugs/myGlider.plot A Slugs/myGlider_0.cpc A Slugs/myGlider_0.stl A Slugs/pieslice.plot A Slugs/pieslice_0.csm A Slugs/pieslice_0.jrnl A Slugs/pieslice_0.stl A Slugs/sphere.plot A Slugs/sphere_0.csm A Slugs/sphere_0.jrnl A Slugs/torus.plot A Slugs/torus_0.csm A Slugs/torus_0.jrnl A Slugs/torus_0.stl A Slugs/tutorial1.jrnl A Slugs/tutorial1.plot A Slugs/tutorial1_setup.csm A Slugs/tutorial1_setup.stl A Slugs/wing.plot A Slugs/wingBody.plot A Slugs/wingBody_0.cpc A Slugs/wingBody_0.stl A Slugs/wing_0.csm A Slugs/wing_0.jrnl A Slugs/wing_0.stl A Slugs/blend12_1.csm A Slugs/boxHole_1.csm A Slugs/box_1.csm A Slugs/cylinderHole_1.csm A Slugs/cylinder_1.csm A Slugs/damaged_2.csm A Slugs/demo1_1.csm A Slugs/duct_1.csm A Slugs/myGlider_2.csm A Slugs/sphere_1.csm A Slugs/torus_1.csm A Slugs/tutorial1.csm A Slugs/wingBody_2.csm A Slugs/wing_1.csm A Slugs/testfiles A Slugs/testfiles/elbow.stl A Slugs/testfiles/elbow_NW.csm A Slugs/testfiles/elbow_NW.jrnl A Slugs/testfiles/elbow_NW.stl A Slugs/testfiles/nucleus1.csm A Slugs/testfiles/nucleus1.jrnl A Slugs/testfiles/nucleus1.stl A Slugs/testfiles/nucleus2.stl A Slugs/testfiles/nucleus3.stl AU Slugs/aneurysm_case1.iges AU Slugs/aneurysm_case1_slugs.stl A Slugs/eyeball_1.csm A Slugs/pieslice_1.csm A Slugs/myGlider_0.jrnl A Slugs/myGlider_1.jrnl A Slugs/damaged_0.jrnl A Slugs/wingBody_0.jrnl A Slugs/wingBody_1.jrnl A Slugs/tutorial1_setup.jrnl A Slugs/blend12_0.jrnl At revision 2495 Cleaning up /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/OpenCSM/trunk/pyOCSM Deleting /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/OpenCSM/trunk/pyOCSM/pyOCSM/__pycache__ Updating svn+ssh://acdl.mit.edu/home/svnroot/OpenCSM/trunk/pyOCSM at revision '2024-05-16T18:49:17.627 -0400' Using sole credentials 3614a4cf-01de-4393-97de-73734b7dd5a2 in realm ‘svn+ssh://acdl.mit.edu’ Using sole credentials 3614a4cf-01de-4393-97de-73734b7dd5a2 in realm ‘svn+ssh://acdl.mit.edu’ At revision 2495 No changes for svn+ssh://acdl.mit.edu/home/svnroot/EGADS since the previous build Using sole credentials 3614a4cf-01de-4393-97de-73734b7dd5a2 in realm ‘svn+ssh://acdl.mit.edu’ Using sole credentials 3614a4cf-01de-4393-97de-73734b7dd5a2 in realm ‘svn+ssh://acdl.mit.edu’ No changes for svn+ssh://acdl.mit.edu/home/svnroot/JenkinsESP since the previous build No changes for svn+ssh://acdl.mit.edu/home/svnroot/OpenCSM/trunk/src since the previous build No changes for svn+ssh://acdl.mit.edu/home/svnroot/OpenCSM/trunk/udc since the previous build No changes for svn+ssh://acdl.mit.edu/home/svnroot/OpenCSM/trunk/data since the previous build No changes for svn+ssh://acdl.mit.edu/home/svnroot/OpenCSM/trunk/pyOCSM since the previous build [GitCheckoutListener] SCM 'hudson.scm.SubversionSCM' is not of type GitSCM Run condition [Execution node ] enabling prebuild for step [Execute shell] Run condition [Execution node ] enabling prebuild for step [Execute Windows batch command] [Execution node] check if [viggen] is in [[macys, macys_VM, reynolds, viggen]] Run condition [Execution node ] enabling perform for step [Execute shell] [DARWIN_ARM64] $ /bin/bash -xe /var/folders/l7/7s0m18td3fxg_w_dxpkj1d600000gp/T/jenkins3819267782975803361.sh + rm -rf /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/CAPS/training/lectures + [[ CAPS/AEROELASTIC != *\S\l\u\g\s* ]] + rm -rf /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/OpenCSM/trunk/data/Slugs + [[ viggen == *\v\i\g\g\e\n* ]] + arch -arch arm64 /bin/bash -ex /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/JenkinsESP/ESP_Regression.sh + source /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/JenkinsESP/ESP_Env.sh ++ export OCCTREF=7.8 ++ OCCTREF=7.8 ++ AFLR_VERSION=11.5.14 ++ SU2_VERSION=8.0.0 ++ TETGEN_VERSION=1.6.0 ++ VSP_VERSION=3.38.0 ++ export PYTHON_VERSION=3.11.9 ++ PYTHON_VERSION=3.11.9 ++ export EFCOMP=gfortran ++ EFCOMP=gfortran ++ [[ viggen == \r\e\y\n\o\l\d\s ]] ++ [[ DARWIN_ARM64 == *\.\i\f\o\r\t ]] ++ '[' -f /opt/intel/oneapi/setvars.sh ']' ++ source /opt/intel/oneapi/setvars.sh ++ '[' -f /Users/jenkins/.bashrc ']' ++ export CAPS_OUTLEVEL=0 ++ CAPS_OUTLEVEL=0 ++ [[ DARWIN_ARM64 == \D\A\R\W\I\N\6\4\.\g\c\c ]] ++ export ESP_BLOC=/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64 ++ ESP_BLOC=/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64 ++ export ESP_ROOT=/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64 ++ ESP_ROOT=/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64 ++ export JULIA_DEPOT_PATH=/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/julia ++ JULIA_DEPOT_PATH=/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/julia ++ export AWAVE=awavemod.f ++ AWAVE=awavemod.f ++ export RLM_CONNECT_TIMEOUT=350 ++ RLM_CONNECT_TIMEOUT=350 ++ [[ 7.8 != '' ]] ++ [[ '' != '' ]] ++ [[ viggen == *\r\e\y\n\o\l\d\s* ]] ++ [[ viggen == *\m\a\c\y\s* ]] ++ [[ viggen == *\v\i\g\g\e\n* ]] ++ export EMPnumProc=2 ++ EMPnumProc=2 ++ export OMP_NUM_THREADS=2 ++ OMP_NUM_THREADS=2 ++ source /Users/jenkins/.bash_profile ++++ /opt/homebrew/bin/brew shellenv +++ eval 'export HOMEBREW_PREFIX="/opt/homebrew"; export HOMEBREW_CELLAR="/opt/homebrew/Cellar"; export HOMEBREW_REPOSITORY="/opt/homebrew"; export PATH="/opt/homebrew/bin:/opt/homebrew/sbin${PATH+:$PATH}"; export MANPATH="/opt/homebrew/share/man${MANPATH+:$MANPATH}:"; export INFOPATH="/opt/homebrew/share/info:${INFOPATH:-}";' ++++ export HOMEBREW_PREFIX=/opt/homebrew ++++ HOMEBREW_PREFIX=/opt/homebrew ++++ export HOMEBREW_CELLAR=/opt/homebrew/Cellar ++++ HOMEBREW_CELLAR=/opt/homebrew/Cellar ++++ export HOMEBREW_REPOSITORY=/opt/homebrew ++++ HOMEBREW_REPOSITORY=/opt/homebrew ++++ export PATH=/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin ++++ PATH=/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin ++++ export MANPATH=/opt/homebrew/share/man: ++++ MANPATH=/opt/homebrew/share/man: ++++ export INFOPATH=/opt/homebrew/share/info: ++++ INFOPATH=/opt/homebrew/share/info: +++ [[ -r /opt/homebrew/etc/profile.d/bash_completion.sh ]] +++ . /opt/homebrew/etc/profile.d/bash_completion.sh ++++ '[' -z '3.2.57(1)-release' -o -z '' -o -n '' ']' ++++ return +++ export NETCDF_PATH=/opt/homebrew +++ NETCDF_PATH=/opt/homebrew ++ [[ viggen == *\m\a\c\y\s* ]] ++ export PATH=/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/ ++ PATH=/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/ ++ [[ viggen == \m\a\c\y\s ]] ++ export CASARCH=. ++ CASARCH=. ++ '[' '!' -z '' ']' +++ ls -d /Users/jenkins/util/ESP/OpenCASCADE-7.7.0 ++ export CASROOT=/Users/jenkins/util/ESP/OpenCASCADE-7.7.0 ++ CASROOT=/Users/jenkins/util/ESP/OpenCASCADE-7.7.0 ++ export UDUNITS2_XML_PATH=/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/udunits/udunits2.xml ++ UDUNITS2_XML_PATH=/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/udunits/udunits2.xml ++ export ESP_EXTERN_LIBS=/Users/jenkins/util/ESP/ExternLibs ++ ESP_EXTERN_LIBS=/Users/jenkins/util/ESP/ExternLibs ++ export DYLD_LIBRARY_PATH=/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib:/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/lib:/opt/intel/oneapi/tbb/2021.5.0/env/../lib:/opt/intel/oneapi/mkl/2022.0.0/lib ++ DYLD_LIBRARY_PATH=/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib:/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/lib:/opt/intel/oneapi/tbb/2021.5.0/env/../lib:/opt/intel/oneapi/mkl/2022.0.0/lib ++ export AFLR=/Users/jenkins/util/AFLR/aflr_lib_11.5.14 ++ AFLR=/Users/jenkins/util/AFLR/aflr_lib_11.5.14 ++ [[ viggen == *\m\a\c\y\s* ]] ++ export AFLR_ARCH=MacOSX-arm64 ++ AFLR_ARCH=MacOSX-arm64 ++ export ASTROS_ROOT=/Users/jenkins/util/astros/Astros/Darwin-64bit ++ ASTROS_ROOT=/Users/jenkins/util/astros/Astros/Darwin-64bit ++ export PATH=/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/ ++ PATH=/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/ ++ export CART3D=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16 ++ CART3D=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16 ++ export CART3D_ARCH=OSX64_ICC ++ CART3D_ARCH=OSX64_ICC ++ export PATH=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/ ++ PATH=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/ ++ export PATH=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/ ++ PATH=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/ ++ export PATH=/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/ ++ PATH=/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/ ++ export VSP3_ROOT=/Users/jenkins/util/OpenVSP/OpenVSP-3.38.0-MacOS ++ VSP3_ROOT=/Users/jenkins/util/OpenVSP/OpenVSP-3.38.0-MacOS ++ export PATH=/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/ ++ PATH=/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/ ++ [[ viggen == \m\a\c\y\s ]] ++ [[ viggen == \v\i\g\g\e\n ]] ++ export SEACAS=/Users/jenkins/util/sandialabs/seacas ++ SEACAS=/Users/jenkins/util/sandialabs/seacas ++ [[ viggen == \v\i\g\g\e\n ]] ++ export NETCDFINC=/opt/homebrew/include ++ NETCDFINC=/opt/homebrew/include ++ export SU2_HOME=/Users/jenkins/util/SU2/SU2-v8.0.0 ++ SU2_HOME=/Users/jenkins/util/SU2/SU2-v8.0.0 ++ export SU2_RUN=/Users/jenkins/util/SU2/SU2-v8.0.0/bin ++ SU2_RUN=/Users/jenkins/util/SU2/SU2-v8.0.0/bin ++ export PATH=/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin ++ PATH=/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin ++ export PYTHONPATH=:/Users/jenkins/util/SU2/SU2-v8.0.0/bin ++ PYTHONPATH=:/Users/jenkins/util/SU2/SU2-v8.0.0/bin ++ export TETGEN=/Users/jenkins/util/tetgen/tetgen1.6.0 ++ TETGEN=/Users/jenkins/util/tetgen/tetgen1.6.0 ++ export PATH=/Users/jenkins/util/tsfoil:/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin ++ PATH=/Users/jenkins/util/tsfoil:/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin ++ '[' -d /Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16 ']' +++ perl -I/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl/lib/perl5 -Mlocal::lib=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl ++ eval 'PATH="/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl/bin${PATH:+:${PATH}}"; export PATH; PERL5LIB="/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl/lib/perl5${PERL5LIB:+:${PERL5LIB}}"; export PERL5LIB; PERL_LOCAL_LIB_ROOT="/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl${PERL_LOCAL_LIB_ROOT:+:${PERL_LOCAL_LIB_ROOT}}"; export PERL_LOCAL_LIB_ROOT; PERL_MB_OPT="--install_base \"/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl\""; export PERL_MB_OPT; PERL_MM_OPT="INSTALL_BASE=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl"; export PERL_MM_OPT;' +++ PATH=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl/bin:/Users/jenkins/util/tsfoil:/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin +++ export PATH +++ PERL5LIB=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl/lib/perl5 +++ export PERL5LIB +++ PERL_LOCAL_LIB_ROOT=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl +++ export PERL_LOCAL_LIB_ROOT +++ PERL_MB_OPT='--install_base "/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl"' +++ export PERL_MB_OPT +++ PERL_MM_OPT=INSTALL_BASE=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl +++ export PERL_MM_OPT ++ export PATH=/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl/bin:/Users/jenkins/util/tsfoil:/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin ++ PATH=/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl/bin:/Users/jenkins/util/tsfoil:/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin ++ export PATH=/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/test:/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl/bin:/Users/jenkins/util/tsfoil:/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin ++ PATH=/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/test:/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl/bin:/Users/jenkins/util/tsfoil:/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin ++ export PYTHONPATH=/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/EGADS/trunk/pyEGADS::/Users/jenkins/util/SU2/SU2-v8.0.0/bin ++ PYTHONPATH=/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/EGADS/trunk/pyEGADS::/Users/jenkins/util/SU2/SU2-v8.0.0/bin ++ export PYTHONPATH=/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/OpenCSM/trunk/pyOCSM:/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/EGADS/trunk/pyEGADS::/Users/jenkins/util/SU2/SU2-v8.0.0/bin ++ PYTHONPATH=/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/OpenCSM/trunk/pyOCSM:/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/EGADS/trunk/pyEGADS::/Users/jenkins/util/SU2/SU2-v8.0.0/bin ++ export PYTHONPATH=/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/CAPS/pyCAPS:/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/OpenCSM/trunk/pyOCSM:/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/EGADS/trunk/pyEGADS::/Users/jenkins/util/SU2/SU2-v8.0.0/bin ++ PYTHONPATH=/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/CAPS/pyCAPS:/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/OpenCSM/trunk/pyOCSM:/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/EGADS/trunk/pyEGADS::/Users/jenkins/util/SU2/SU2-v8.0.0/bin ++ [[ viggen == \m\a\c\y\s* ]] ++ [[ viggen == \v\i\g\g\e\n ]] ++ mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/bin ++ rm -f /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/bin/python ++ rm -f /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/bin/python-config ++ rm -f /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/bin/virtualenv ++ rm -f '/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/bin/analyze-*' ++ rm -f '/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/bin/intercept-*' ++ [[ viggen == \m\a\c\y\s ]] ++ [[ viggen == \v\i\g\g\e\n ]] ++ ln -s /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/python3 /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/bin/python ++ ln -s /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/python3-config /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/bin/python-config ++ ln -s /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/virtualenv /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/bin/virtualenv +++ ls /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/analyze-build /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/analyze-c++ /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/analyze-cc /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/intercept-build /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/intercept-c++ /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/intercept-cc ++ for i in '`ls /Users/jenkins/util/ESP/Python/ESP_Python-${PYTHON_VERSION}/bin/analyze-* /Users/jenkins/util/ESP/Python/ESP_Python-${PYTHON_VERSION}/bin/intercept-*`' +++ basename /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/analyze-build +++ basename /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/analyze-build ++ ln -s /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/analyze-build /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/bin/analyze-build ++ for i in '`ls /Users/jenkins/util/ESP/Python/ESP_Python-${PYTHON_VERSION}/bin/analyze-* /Users/jenkins/util/ESP/Python/ESP_Python-${PYTHON_VERSION}/bin/intercept-*`' +++ basename /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/analyze-c++ +++ basename /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/analyze-c++ ++ ln -s /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/analyze-c++ /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/bin/analyze-c++ ++ for i in '`ls /Users/jenkins/util/ESP/Python/ESP_Python-${PYTHON_VERSION}/bin/analyze-* /Users/jenkins/util/ESP/Python/ESP_Python-${PYTHON_VERSION}/bin/intercept-*`' +++ basename /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/analyze-cc +++ basename /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/analyze-cc ++ ln -s /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/analyze-cc /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/bin/analyze-cc ++ for i in '`ls /Users/jenkins/util/ESP/Python/ESP_Python-${PYTHON_VERSION}/bin/analyze-* /Users/jenkins/util/ESP/Python/ESP_Python-${PYTHON_VERSION}/bin/intercept-*`' +++ basename /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/intercept-build +++ basename /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/intercept-build ++ ln -s /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/intercept-build /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/bin/intercept-build ++ for i in '`ls /Users/jenkins/util/ESP/Python/ESP_Python-${PYTHON_VERSION}/bin/analyze-* /Users/jenkins/util/ESP/Python/ESP_Python-${PYTHON_VERSION}/bin/intercept-*`' +++ basename /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/intercept-c++ +++ basename /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/intercept-c++ ++ ln -s /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/intercept-c++ /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/bin/intercept-c++ ++ for i in '`ls /Users/jenkins/util/ESP/Python/ESP_Python-${PYTHON_VERSION}/bin/analyze-* /Users/jenkins/util/ESP/Python/ESP_Python-${PYTHON_VERSION}/bin/intercept-*`' +++ basename /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/intercept-cc +++ basename /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/intercept-cc ++ ln -s /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/intercept-cc /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/bin/intercept-cc +++ python-config --includes ++ export 'PYTHONINC=. -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11' ++ PYTHONINC='. -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11' +++ python-config --help ++ [[ Usage: /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/bin/python-config [--prefix|--exec-prefix|--includes|--libs|--cflags|--ldflags|--extension-suffix|--help|--abiflags|--configdir|--embed] == *\e\m\b\e\d* ]] +++ python-config --ldflags --embed ++ export 'PYTHONLIB=-L/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11 -ldl -framework CoreFoundation' ++ PYTHONLIB='-L/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11 -ldl -framework CoreFoundation' ++ [[ viggen == \m\a\c\y\s ]] ++ [[ viggen == \v\i\g\g\e\n ]] ++ export 'PYTHONLIB=-L/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11 -ldl -framework CoreFoundation -Wl,-w' ++ PYTHONLIB='-L/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11 -ldl -framework CoreFoundation -Wl,-w' ++ export PYTHONUNBUFFERED=true ++ PYTHONUNBUFFERED=true ++ export PYTHONFAULTHANDLER=true ++ PYTHONFAULTHANDLER=true ++ python --version Python 3.11.9 ++ [[ DARWIN_ARM64 == \D\A\R\W\I\N\6\4\.\g\c\c ]] ++ export CSMDATA=/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/OpenCSM/trunk/data ++ CSMDATA=/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/OpenCSM/trunk/data + source /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/JenkinsESP/ESPbfr.sh ++ cd /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ ++ tar -xvf /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/JenkinsESP/ESPbfr.tgz x ESP/ x ESP/CYGWIN64/ x ESP/CYGWIN64/bin/ x ESP/CYGWIN64/bin/mastros.exe x ESP/CYGWIN64/bin/ASTRO.D01 x ESP/CYGWIN64/bin/ASTRO.IDX x ESP/CYGWIN64/include/ x ESP/CYGWIN64/lib/ x ESP/CYGWIN64/lib/libquadmath-0.dll x ESP/CYGWIN64/lib/libwinpthread-1.dll x ESP/CYGWIN64/lib/libgcc_s_sjlj-1.dll x ESP/CYGWIN64/obj/ x ESP/CYGWIN64/test/ x ESP/DARWIN64/ x ESP/DARWIN64/bin/ x ESP/DARWIN64/bin/mastros.exe x ESP/DARWIN64/bin/ASTRO.D01 x ESP/DARWIN64/bin/mset x ESP/DARWIN64/bin/ASTRO.IDX x ESP/DARWIN64/bin/avl x ESP/DARWIN64/bin/xfoil x ESP/DARWIN64/bin/mses x ESP/DARWIN64/include/ x ESP/DARWIN64/include/nmb.h x ESP/DARWIN64/include/xddm/ x ESP/DARWIN64/include/xddm/xddmInternals.h x ESP/DARWIN64/include/xddm/xddm.h x ESP/DARWIN64/include/xddm/xddm.c x ESP/DARWIN64/include/converter.h x ESP/DARWIN64/include/libCart3D/ x ESP/DARWIN64/include/libCart3D/sensors.h x ESP/DARWIN64/include/libCart3D/SFC.h x ESP/DARWIN64/include/libCart3D/map.h x ESP/DARWIN64/include/libCart3D/MGinfo.h x ESP/DARWIN64/include/libCart3D/gridStructures.h x ESP/DARWIN64/include/libCart3D/timer.h x ESP/DARWIN64/include/libCart3D/ConvInfo.h x ESP/DARWIN64/include/libCart3D/dualtime.h x ESP/DARWIN64/include/libCart3D/stateVector.h x ESP/DARWIN64/include/libCart3D/cartCells.h x ESP/DARWIN64/include/libCart3D/encoding.h x ESP/DARWIN64/include/libCart3D/string_util.h x ESP/DARWIN64/include/libCart3D/int64.h x ESP/DARWIN64/include/libCart3D/bBox_stuff.h x ESP/DARWIN64/include/libCart3D/basicTypes.h x ESP/DARWIN64/include/libCart3D/utils_xml.h x ESP/DARWIN64/include/libCart3D/hex.h x ESP/DARWIN64/include/libCart3D/PostProcInfo.h x ESP/DARWIN64/include/libCart3D/SolverInfo.h x ESP/DARWIN64/include/libCart3D/earthBL_BC.h x ESP/DARWIN64/include/libCart3D/limiters.h x ESP/DARWIN64/include/libCart3D/geomStructures.h x ESP/DARWIN64/include/libCart3D/CaseInfo.h x ESP/DARWIN64/include/libCart3D/memory_util.h x ESP/DARWIN64/include/libCart3D/infoStructures.h x ESP/DARWIN64/include/libCart3D/geomTypes.h x ESP/DARWIN64/include/libCart3D/c3d_timeout.h x ESP/DARWIN64/include/libCart3D/myLList.h x ESP/DARWIN64/include/libCart3D/IOinfo.h x ESP/DARWIN64/include/libCart3D/GridInfo.h x ESP/DARWIN64/include/libCart3D/c3d_global.h x ESP/DARWIN64/include/libCart3D/vortexBC.h x ESP/DARWIN64/include/c3dio/ x ESP/DARWIN64/include/c3dio/c3dio_icemcfd.h x ESP/DARWIN64/include/c3dio/c3dio_lib.h x ESP/DARWIN64/include/udunits.h x ESP/DARWIN64/include/udunits2.h x ESP/DARWIN64/lib/ x ESP/DARWIN64/lib/libudunits2.dylib x ESP/DARWIN64/lib/libudunits2.0.dylib x ESP/DARWIN64/lib/libCart3D.a x ESP/DARWIN64/lib/libnmb.dylib x ESP/DARWIN64/lib/libc3dio.a x ESP/DARWIN64/obj/ x ESP/DARWIN64/test/ x ESP/DARWIN_ARM64/ x ESP/DARWIN_ARM64/bin/ x ESP/DARWIN_ARM64/bin/mastros.exe x ESP/DARWIN_ARM64/bin/ASTRO.D01 x ESP/DARWIN_ARM64/bin/mset x ESP/DARWIN_ARM64/bin/ASTRO.IDX x ESP/DARWIN_ARM64/bin/avl x ESP/DARWIN_ARM64/bin/xfoil x ESP/DARWIN_ARM64/bin/mses x ESP/DARWIN_ARM64/include/ x ESP/DARWIN_ARM64/include/nmb.h x ESP/DARWIN_ARM64/include/xddm/ x ESP/DARWIN_ARM64/include/xddm/xddmInternals.h x ESP/DARWIN_ARM64/include/xddm/xddm.h x ESP/DARWIN_ARM64/include/xddm/xddm.c x ESP/DARWIN_ARM64/include/converter.h x ESP/DARWIN_ARM64/include/libCart3D/ x ESP/DARWIN_ARM64/include/libCart3D/sensors.h x ESP/DARWIN_ARM64/include/libCart3D/SFC.h x ESP/DARWIN_ARM64/include/libCart3D/map.h x ESP/DARWIN_ARM64/include/libCart3D/MGinfo.h x ESP/DARWIN_ARM64/include/libCart3D/gridStructures.h x ESP/DARWIN_ARM64/include/libCart3D/timer.h x ESP/DARWIN_ARM64/include/libCart3D/ConvInfo.h x ESP/DARWIN_ARM64/include/libCart3D/dualtime.h x ESP/DARWIN_ARM64/include/libCart3D/stateVector.h x ESP/DARWIN_ARM64/include/libCart3D/cartCells.h x ESP/DARWIN_ARM64/include/libCart3D/encoding.h x ESP/DARWIN_ARM64/include/libCart3D/string_util.h x ESP/DARWIN_ARM64/include/libCart3D/int64.h x ESP/DARWIN_ARM64/include/libCart3D/bBox_stuff.h x ESP/DARWIN_ARM64/include/libCart3D/basicTypes.h x ESP/DARWIN_ARM64/include/libCart3D/utils_xml.h x ESP/DARWIN_ARM64/include/libCart3D/hex.h x ESP/DARWIN_ARM64/include/libCart3D/PostProcInfo.h x ESP/DARWIN_ARM64/include/libCart3D/SolverInfo.h x ESP/DARWIN_ARM64/include/libCart3D/earthBL_BC.h x ESP/DARWIN_ARM64/include/libCart3D/limiters.h x ESP/DARWIN_ARM64/include/libCart3D/geomStructures.h x ESP/DARWIN_ARM64/include/libCart3D/CaseInfo.h x ESP/DARWIN_ARM64/include/libCart3D/memory_util.h x ESP/DARWIN_ARM64/include/libCart3D/infoStructures.h x ESP/DARWIN_ARM64/include/libCart3D/geomTypes.h x ESP/DARWIN_ARM64/include/libCart3D/c3d_timeout.h x ESP/DARWIN_ARM64/include/libCart3D/myLList.h x ESP/DARWIN_ARM64/include/libCart3D/IOinfo.h x ESP/DARWIN_ARM64/include/libCart3D/GridInfo.h x ESP/DARWIN_ARM64/include/libCart3D/c3d_global.h x ESP/DARWIN_ARM64/include/libCart3D/vortexBC.h x ESP/DARWIN_ARM64/include/c3dio/ x ESP/DARWIN_ARM64/include/c3dio/c3dio_icemcfd.h x ESP/DARWIN_ARM64/include/c3dio/c3dio_lib.h x ESP/DARWIN_ARM64/include/udunits.h x ESP/DARWIN_ARM64/include/udunits2.h x ESP/DARWIN_ARM64/lib/ x ESP/DARWIN_ARM64/lib/libudunits2.dylib x ESP/DARWIN_ARM64/lib/libudunits2.0.dylib x ESP/DARWIN_ARM64/lib/libCart3D.a x ESP/DARWIN_ARM64/lib/libc3dio.a x ESP/DARWIN_ARM64/obj/ x ESP/DARWIN_ARM64/test/ x ESP/LINUX64/ x ESP/LINUX64/bin/ x ESP/LINUX64/bin/mastros.exe x ESP/LINUX64/bin/ASTRO.D01 x ESP/LINUX64/bin/mset x ESP/LINUX64/bin/ASTRO.IDX x ESP/LINUX64/bin/avl x ESP/LINUX64/bin/xfoil x ESP/LINUX64/bin/mses x ESP/LINUX64/include/ x ESP/LINUX64/include/nmb.h x ESP/LINUX64/include/xddm/ x ESP/LINUX64/include/xddm/xddmInternals.h x ESP/LINUX64/include/xddm/xddm.h x ESP/LINUX64/include/xddm/xddm.c x ESP/LINUX64/include/libCart3D/ x ESP/LINUX64/include/libCart3D/sensors.h x ESP/LINUX64/include/libCart3D/SFC.h x ESP/LINUX64/include/libCart3D/map.h x ESP/LINUX64/include/libCart3D/MGinfo.h x ESP/LINUX64/include/libCart3D/gridStructures.h x ESP/LINUX64/include/libCart3D/timer.h x ESP/LINUX64/include/libCart3D/ConvInfo.h x ESP/LINUX64/include/libCart3D/dualtime.h x ESP/LINUX64/include/libCart3D/stateVector.h x ESP/LINUX64/include/libCart3D/cartCells.h x ESP/LINUX64/include/libCart3D/encoding.h x ESP/LINUX64/include/libCart3D/string_util.h x ESP/LINUX64/include/libCart3D/int64.h x ESP/LINUX64/include/libCart3D/bBox_stuff.h x ESP/LINUX64/include/libCart3D/basicTypes.h x ESP/LINUX64/include/libCart3D/utils_xml.h x ESP/LINUX64/include/libCart3D/hex.h x ESP/LINUX64/include/libCart3D/PostProcInfo.h x ESP/LINUX64/include/libCart3D/SolverInfo.h x ESP/LINUX64/include/libCart3D/earthBL_BC.h x ESP/LINUX64/include/libCart3D/limiters.h x ESP/LINUX64/include/libCart3D/geomStructures.h x ESP/LINUX64/include/libCart3D/CaseInfo.h x ESP/LINUX64/include/libCart3D/memory_util.h x ESP/LINUX64/include/libCart3D/infoStructures.h x ESP/LINUX64/include/libCart3D/geomTypes.h x ESP/LINUX64/include/libCart3D/c3d_timeout.h x ESP/LINUX64/include/libCart3D/myLList.h x ESP/LINUX64/include/libCart3D/IOinfo.h x ESP/LINUX64/include/libCart3D/GridInfo.h x ESP/LINUX64/include/libCart3D/c3d_global.h x ESP/LINUX64/include/libCart3D/vortexBC.h x ESP/LINUX64/include/c3dio/ x ESP/LINUX64/include/c3dio/c3dio_icemcfd.h x ESP/LINUX64/include/c3dio/c3dio_lib.h x ESP/LINUX64/lib/ x ESP/LINUX64/lib/libnmb.so x ESP/LINUX64/lib/libCart3D.a x ESP/LINUX64/lib/libc3dio.a x ESP/LINUX64/obj/ x ESP/LINUX64/test/ x ESP/WIN64/ x ESP/WIN64/bin/ x ESP/WIN64/bin/mses.exe x ESP/WIN64/bin/avl.exe x ESP/WIN64/bin/mastros.exe x ESP/WIN64/bin/ASTRO.D01 x ESP/WIN64/bin/xfoil.exe x ESP/WIN64/bin/ASTRO.IDX x ESP/WIN64/bin/mset.exe x ESP/WIN64/include/ x ESP/WIN64/include/nmb.h x ESP/WIN64/include/winhelpers/ x ESP/WIN64/include/winhelpers/gettimeofday.h x ESP/WIN64/include/winhelpers/websock-w32.h x ESP/WIN64/include/winhelpers/netdb.h x ESP/WIN64/include/winhelpers/unistd.h x ESP/WIN64/include/winhelpers/strings.h x ESP/WIN64/include/winhelpers/sys/ x ESP/WIN64/include/winhelpers/sys/time.h x ESP/WIN64/include/converter.h x ESP/WIN64/include/udunits.h x ESP/WIN64/include/udunits2.h x ESP/WIN64/lib/ x ESP/WIN64/lib/libquadmath-0.dll x ESP/WIN64/lib/nmb.lib x ESP/WIN64/lib/libwinpthread-1.dll x ESP/WIN64/lib/udunits2.lib x ESP/WIN64/lib/libgcc_s_sjlj-1.dll x ESP/WIN64/lib/expat.dll x ESP/WIN64/lib/udunits2.dll x ESP/WIN64/lib/nmb.dll x ESP/WIN64/obj/ x ESP/WIN64/test/ x ESP/LINUX_AARCH64/ x ESP/LINUX_AARCH64/bin/ x ESP/LINUX_AARCH64/bin/mastros.exe x ESP/LINUX_AARCH64/bin/ASTRO.D01 x ESP/LINUX_AARCH64/bin/mset x ESP/LINUX_AARCH64/bin/ASTRO.IDX x ESP/LINUX_AARCH64/bin/avl x ESP/LINUX_AARCH64/bin/xfoil x ESP/LINUX_AARCH64/bin/mses x ESP/LINUX_AARCH64/include/ x ESP/LINUX_AARCH64/lib/ x ESP/LINUX_AARCH64/obj/ x ESP/LINUX_AARCH64/test/ x ESP/udunits/ x ESP/udunits/udunits2-accepted.xml x ESP/udunits/udunits2-base.xml x ESP/udunits/udunits2-common.xml x ESP/udunits/udunits2.xml x ESP/udunits/udunits2-derived.xml x ESP/udunits/udunits2-prefixes.xml ++ virtualenv /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/venv created virtual environment CPython3.11.9.final.0-64 in 461ms creator CPython3Posix(dest=/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/venv, clear=False, no_vcs_ignore=False, global=False) seeder FromAppData(download=False, pip=bundle, setuptools=bundle, wheel=bundle, via=copy, app_data_dir=/Users/jenkins/Library/Application Support/virtualenv) added seed packages: pip==24.0, setuptools==69.5.1, wheel==0.43.0 activators BashActivator,CShellActivator,FishActivator,NushellActivator,PowerShellActivator,PythonActivator ++ . /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/venv/bin/activate +++ '[' /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/venv/bin/activate = /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/JenkinsESP/ESP_Regression.sh ']' +++ deactivate nondestructive +++ unset -f pydoc +++ '[' -z '' ']' +++ '[' -z '' ']' +++ hash -r +++ '[' -z '' ']' +++ unset VIRTUAL_ENV +++ unset VIRTUAL_ENV_PROMPT +++ '[' '!' nondestructive = nondestructive ']' +++ VIRTUAL_ENV=/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/venv +++ '[' darwin23 = cygwin ']' +++ '[' darwin23 = msys ']' +++ export VIRTUAL_ENV +++ _OLD_VIRTUAL_PATH=/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/test:/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl/bin:/Users/jenkins/util/tsfoil:/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin +++ PATH=/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/venv/bin:/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/test:/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl/bin:/Users/jenkins/util/tsfoil:/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin +++ export PATH +++ '[' x '!=' x ']' ++++ basename /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/venv +++ VIRTUAL_ENV_PROMPT=venv +++ export VIRTUAL_ENV_PROMPT +++ '[' -z '' ']' +++ '[' -z '' ']' +++ _OLD_VIRTUAL_PS1= +++ PS1='(venv) ' +++ export PS1 +++ alias pydoc +++ true +++ hash -r ++ pip_install pip ++ /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/venv/bin/python -m pip install --only-binary all --upgrade pip Requirement already satisfied: pip in ./ESP/venv/lib/python3.11/site-packages (24.0) ++ pip_install f90nml ++ /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/venv/bin/python -m pip install --only-binary all --upgrade f90nml Collecting f90nml Using cached f90nml-1.4.4-py2.py3-none-any.whl.metadata (6.0 kB) Using cached f90nml-1.4.4-py2.py3-none-any.whl (32 kB) Installing collected packages: f90nml Successfully installed f90nml-1.4.4 ++ pip_install numpy ++ /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/venv/bin/python -m pip install --only-binary all --upgrade numpy Collecting numpy Using cached numpy-1.26.4-cp311-cp311-macosx_11_0_arm64.whl.metadata (114 kB) Using cached numpy-1.26.4-cp311-cp311-macosx_11_0_arm64.whl (14.0 MB) Installing collected packages: numpy Successfully installed numpy-1.26.4 ++ pip_install 'scipy!=1.9.2,!=1.9.3' ++ /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/venv/bin/python -m pip install --only-binary all --upgrade 'scipy!=1.9.2,!=1.9.3' Collecting scipy!=1.9.2,!=1.9.3 Using cached scipy-1.13.0-cp311-cp311-macosx_12_0_arm64.whl.metadata (60 kB) Requirement already satisfied: numpy<2.3,>=1.22.4 in ./ESP/venv/lib/python3.11/site-packages (from scipy!=1.9.2,!=1.9.3) (1.26.4) Using cached scipy-1.13.0-cp311-cp311-macosx_12_0_arm64.whl (30.3 MB) Installing collected packages: scipy Successfully installed scipy-1.13.0 ++ pip_install openmdao ++ /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/venv/bin/python -m pip install --only-binary all --upgrade openmdao Collecting openmdao Using cached openmdao-3.32.0-py3-none-any.whl Collecting networkx>=2.0 (from openmdao) Using cached networkx-3.3-py3-none-any.whl.metadata (5.1 kB) Requirement already satisfied: numpy<2 in ./ESP/venv/lib/python3.11/site-packages (from openmdao) (1.26.4) Collecting packaging (from openmdao) Using cached packaging-24.0-py3-none-any.whl.metadata (3.2 kB) Collecting requests (from openmdao) Using cached requests-2.31.0-py3-none-any.whl.metadata (4.6 kB) Requirement already satisfied: scipy in ./ESP/venv/lib/python3.11/site-packages (from openmdao) (1.13.0) Collecting charset-normalizer<4,>=2 (from requests->openmdao) Using cached charset_normalizer-3.3.2-cp311-cp311-macosx_11_0_arm64.whl.metadata (33 kB) Collecting idna<4,>=2.5 (from requests->openmdao) Using cached idna-3.7-py3-none-any.whl.metadata (9.9 kB) Collecting urllib3<3,>=1.21.1 (from requests->openmdao) Using cached urllib3-2.2.1-py3-none-any.whl.metadata (6.4 kB) Collecting certifi>=2017.4.17 (from requests->openmdao) Using cached certifi-2024.2.2-py3-none-any.whl.metadata (2.2 kB) Using cached networkx-3.3-py3-none-any.whl (1.7 MB) Using cached packaging-24.0-py3-none-any.whl (53 kB) Using cached requests-2.31.0-py3-none-any.whl (62 kB) Using cached certifi-2024.2.2-py3-none-any.whl (163 kB) Using cached charset_normalizer-3.3.2-cp311-cp311-macosx_11_0_arm64.whl (118 kB) Using cached idna-3.7-py3-none-any.whl (66 kB) Using cached urllib3-2.2.1-py3-none-any.whl (121 kB) Installing collected packages: urllib3, packaging, networkx, idna, charset-normalizer, certifi, requests, openmdao Successfully installed certifi-2024.2.2 charset-normalizer-3.3.2 idna-3.7 networkx-3.3 openmdao-3.32.0 packaging-24.0 requests-2.31.0 urllib3-2.2.1 ++ [[ viggen == *\v\i\g\g\e\n* ]] ++ export CVXOPT_BLAS_LIB_DIR=/Users/acdl/workspace/ESP/Python/lapack-3.10.1/build/lib ++ CVXOPT_BLAS_LIB_DIR=/Users/acdl/workspace/ESP/Python/lapack-3.10.1/build/lib ++ export CVXOPT_SUITESPARSE_SRC_DIR=/Users/acdl/workspace/ESP/Python/SuiteSparse-5.12.0 ++ CVXOPT_SUITESPARSE_SRC_DIR=/Users/acdl/workspace/ESP/Python/SuiteSparse-5.12.0 ++ GCC_MAJOR=12 ++ export 'CVXOPT_BLAS_EXTRA_LINK_ARGS=/opt/homebrew/opt/gcc/lib/gcc/current/libgfortran.a;/opt/homebrew/opt/gcc/lib/gcc/current/libquadmath.a;/opt/homebrew/opt/gcc/lib/gcc/current/gcc/aarch64-apple-darwin21/12/libgcc.a' ++ CVXOPT_BLAS_EXTRA_LINK_ARGS='/opt/homebrew/opt/gcc/lib/gcc/current/libgfortran.a;/opt/homebrew/opt/gcc/lib/gcc/current/libquadmath.a;/opt/homebrew/opt/gcc/lib/gcc/current/gcc/aarch64-apple-darwin21/12/libgcc.a' ++ pip_install cvxopt ++ /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/venv/bin/python -m pip install --only-binary all --upgrade cvxopt Collecting cvxopt Using cached cvxopt-1.3.2-cp311-cp311-macosx_11_0_arm64.whl.metadata (1.3 kB) Using cached cvxopt-1.3.2-cp311-cp311-macosx_11_0_arm64.whl (11.1 MB) Installing collected packages: cvxopt Successfully installed cvxopt-1.3.2 ++ pip_install dill ++ /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/venv/bin/python -m pip install --only-binary all --upgrade dill Collecting dill Using cached dill-0.3.8-py3-none-any.whl.metadata (10 kB) Using cached dill-0.3.8-py3-none-any.whl (116 kB) Installing collected packages: dill Successfully installed dill-0.3.8 ++ pip_install packaging ++ /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/venv/bin/python -m pip install --only-binary all --upgrade packaging Requirement already satisfied: packaging in ./ESP/venv/lib/python3.11/site-packages (24.0) ++ pip_install matplotlib ++ /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/venv/bin/python -m pip install --only-binary all --upgrade matplotlib Collecting matplotlib Using cached matplotlib-3.9.0-cp311-cp311-macosx_11_0_arm64.whl.metadata (11 kB) Collecting contourpy>=1.0.1 (from matplotlib) Using cached contourpy-1.2.1-cp311-cp311-macosx_11_0_arm64.whl.metadata (5.8 kB) Collecting cycler>=0.10 (from matplotlib) Using cached cycler-0.12.1-py3-none-any.whl.metadata (3.8 kB) Collecting fonttools>=4.22.0 (from matplotlib) Using cached fonttools-4.51.0-cp311-cp311-macosx_10_9_universal2.whl.metadata (159 kB) Collecting kiwisolver>=1.3.1 (from matplotlib) Using cached kiwisolver-1.4.5-cp311-cp311-macosx_11_0_arm64.whl.metadata (6.4 kB) Requirement already satisfied: numpy>=1.23 in ./ESP/venv/lib/python3.11/site-packages (from matplotlib) (1.26.4) Requirement already satisfied: packaging>=20.0 in ./ESP/venv/lib/python3.11/site-packages (from matplotlib) (24.0) Collecting pillow>=8 (from matplotlib) Using cached pillow-10.3.0-cp311-cp311-macosx_11_0_arm64.whl.metadata (9.2 kB) Collecting pyparsing>=2.3.1 (from matplotlib) Using cached pyparsing-3.1.2-py3-none-any.whl.metadata (5.1 kB) Collecting python-dateutil>=2.7 (from matplotlib) Using cached python_dateutil-2.9.0.post0-py2.py3-none-any.whl.metadata (8.4 kB) Collecting six>=1.5 (from python-dateutil>=2.7->matplotlib) Using cached six-1.16.0-py2.py3-none-any.whl.metadata (1.8 kB) Using cached matplotlib-3.9.0-cp311-cp311-macosx_11_0_arm64.whl (7.8 MB) Using cached contourpy-1.2.1-cp311-cp311-macosx_11_0_arm64.whl (245 kB) Using cached cycler-0.12.1-py3-none-any.whl (8.3 kB) Using cached fonttools-4.51.0-cp311-cp311-macosx_10_9_universal2.whl (2.8 MB) Using cached kiwisolver-1.4.5-cp311-cp311-macosx_11_0_arm64.whl (66 kB) Using cached pillow-10.3.0-cp311-cp311-macosx_11_0_arm64.whl (3.4 MB) Using cached pyparsing-3.1.2-py3-none-any.whl (103 kB) Using cached python_dateutil-2.9.0.post0-py2.py3-none-any.whl (229 kB) Using cached six-1.16.0-py2.py3-none-any.whl (11 kB) Installing collected packages: six, pyparsing, pillow, kiwisolver, fonttools, cycler, contourpy, python-dateutil, matplotlib Successfully installed contourpy-1.2.1 cycler-0.12.1 fonttools-4.51.0 kiwisolver-1.4.5 matplotlib-3.9.0 pillow-10.3.0 pyparsing-3.1.2 python-dateutil-2.9.0.post0 six-1.16.0 ++ [[ /Users/jenkins/util/ESP/ExternLibs == '' ]] ++ '[' -d /Users/jenkins/util/ESP/ExternLibs ']' ++ cp /Users/jenkins/util/ESP/ExternLibs/intersectWake.so /Users/jenkins/util/ESP/ExternLibs/markWakeEdges.so /Users/jenkins/util/ESP/ExternLibs/sansLIPAIM.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/ ++ cd /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/EGADS/trunk/src ++ make touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include/DARWIN_ARM64 rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include/DARWIN_ARM64 cp -p ../include/DARWIN_ARM64 /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include/DARWIN_ARM64 touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include/STANALYZER.make rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include/STANALYZER.make cp -p ../include/STANALYZER.make /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include/STANALYZER.make touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include/egads.h rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include/egads.h cp -p ../include/egads.h /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include/egads.h touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include/egads_dot.h rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include/egads_dot.h cp -p ../include/egads_dot.h /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include/egads_dot.h touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include/egads.inc rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include/egads.inc cp -p ../include/egads.inc /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include/egads.inc touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include/egadsErrors.h rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include/egadsErrors.h cp -p ../include/egadsErrors.h /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include/egadsErrors.h touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include/egadsTypes.h rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include/egadsTypes.h cp -p ../include/egadsTypes.h /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include/egadsTypes.h touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include/emp.h rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include/emp.h cp -p ../include/emp.h /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include/emp.h touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include/prm.h rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include/prm.h cp -p ../include/prm.h /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include/prm.h touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include/wsserver.h rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include/wsserver.h cp -p ../include/wsserver.h /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include/wsserver.h touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include/wsserver.inc rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include/wsserver.inc cp -p ../include/wsserver.inc /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include/wsserver.inc touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include/wsss.h rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include/wsss.h cp -p ../include/wsss.h /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include/wsss.h touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include/egadsTris.h rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include/egadsTris.h cp -p egadsTris.h /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include/egadsTris.h touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include/egadsSplineFit.h rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include/egadsSplineFit.h cp -p egadsSplineFit.h /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include/egadsSplineFit.h touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include/egadsSplineVels.h rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include/egadsSplineVels.h cp -p egadsSplineVels.h /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include/egadsSplineVels.h touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include/egadsf90.inc rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include/egadsf90.inc cp -p ../include/egadsf90.inc /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include/egadsf90.inc mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include/Surreal cp Surreal/SurrealD.h /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include/Surreal/SurrealD.h mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include/Surreal cp Surreal/SurrealD_Lazy.h /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include/Surreal/SurrealD_Lazy.h mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include/Surreal cp Surreal/SurrealD_Trad.h /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include/Surreal/SurrealD_Trad.h mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include/Surreal cp Surreal/SurrealS.h /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include/Surreal/SurrealS.h mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include/Surreal cp Surreal/SurrealS_Lazy.h /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include/Surreal/SurrealS_Lazy.h mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include/Surreal cp Surreal/SurrealS_Trad.h /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include/Surreal/SurrealS_Trad.h mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include/Surreal cp Surreal/always_inline.h /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include/Surreal/always_inline.h clang++ -g -target arm64-apple-darwin -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -ffp-model=strict -DREVISION=7.7 -IOCC -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0 -I../include \ -I. egadsGeom.cpp -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egadsGeom.o clang++ -g -target arm64-apple-darwin -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -ffp-model=strict -DREVISION=7.7 -IOCC -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0 -I../include \ -I. egadsHLevel.cpp -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egadsHLevel.o clang++ -g -target arm64-apple-darwin -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -ffp-model=strict -DREVISION=7.7 -IOCC -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0 -I../include \ -I. egadsTopo.cpp -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egadsTopo.o clang++ -g -target arm64-apple-darwin -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -ffp-model=strict -DREVISION=7.7 -IOCC -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0 -I../include \ -I. egadsCopy.cpp -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egadsCopy.o clang++ -g -target arm64-apple-darwin -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -ffp-model=strict -DREVISION=7.7 -IOCC -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0 -I../include \ -I. egadsSpline.cpp -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egadsSpline.o clang++ -g -target arm64-apple-darwin -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -ffp-model=strict -DREVISION=7.7 -IOCC -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0 -I../include \ -I. egadsIO.cpp -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egadsIO.o clang++ -g -target arm64-apple-darwin -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -ffp-model=strict -DREVISION=7.7 -IOCC -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0 -I../include \ -I. egadsSplineFit.cpp -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egadsSplineFit.o clang++ -g -target arm64-apple-darwin -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -ffp-model=strict -DREVISION=7.7 -IOCC -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0 -I../include \ -I. egadsSkinning.cpp -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egadsSkinning.o clang++ -g -target arm64-apple-darwin -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -ffp-model=strict -DREVISION=7.7 -IOCC -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0 -I../include \ -I. egadsTessSens.cpp -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egadsTessSens.o clang++ -g -target arm64-apple-darwin -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -ffp-model=strict -DREVISION=7.7 -IOCC -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0 OCC/BRepLib_FuseEdges.cpp -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/BRepLib_FuseEdges.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I../util \ -I../util/uvmap egadsBase.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egadsBase.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I../util \ -I../util/uvmap egadsMemory.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egadsMemory.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I../util \ -I../util/uvmap egadsAttrs.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egadsAttrs.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I../util \ -I../util/uvmap egadsTess.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egadsTess.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I../util \ -I../util/uvmap egadsTessInp.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egadsTessInp.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I../util \ -I../util/uvmap egadsTris.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egadsTris.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I../util \ -I../util/uvmap egadsQuads.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egadsQuads.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I../util \ -I../util/uvmap egadsFit.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egadsFit.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I../util \ -I../util/uvmap egadsRobust.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egadsRobust.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I../util \ -I../util/uvmap egadsSBO.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egadsSBO.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I../util \ -I../util/uvmap prmCfit.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/prmCfit.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I../util \ -I../util/uvmap prmGrid.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/prmGrid.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I../util \ -I../util/uvmap prmUV.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/prmUV.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I../util \ -I../util/uvmap egadsExport.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egadsExport.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I../util \ -I../util/uvmap egadsEffect.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egadsEffect.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I../util \ -I../util/uvmap egadsSolids.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egadsSolids.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include ../util/emp.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/emp.o clang++ -g -target arm64-apple-darwin -x c++ -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -ffp-model=strict -DREVISION=7.7 -IOCC -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0 -I. -I../include \ ../util/evaluate.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/evaluate.o clang++ -g -target arm64-apple-darwin -x c++ -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -ffp-model=strict -DREVISION=7.7 -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0 -I. -I../include \ ../util/rational.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/rational.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0 -I../include -I../util \ ../util/regQuads.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/regQuads.o clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/SurrealD1 -O -std=c++11 -I. ../util/SurrealD1_btest.cpp /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/SurrealD1 SurrealD1_test_suite Complete! clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/SurrealD4 -O -std=c++11 -I. ../util/SurrealD4_btest.cpp /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/SurrealD4 SurrealD4_test_suite Complete! clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/SurrealS1 -O -std=c++11 -I. ../util/SurrealS1_btest.cpp /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/SurrealS1 SurrealS1_test_suite Complete! clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/SurrealS4 -O -std=c++11 -I. ../util/SurrealS4_btest.cpp /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/SurrealS4 SurrealS4_test_suite Complete! /Library/Developer/CommandLineTools/usr/bin/make -C ../util clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 uvmap/main/uvmap.c -Iuvmap \ -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/uvmap.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/EG_uvmapFindUV.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/EG_uvmapFindUV.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/EG_uvmapGen.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/EG_uvmapGen.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/EG_uvmapStructFree.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/EG_uvmapStructFree.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/EG_uvmapTest.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/EG_uvmapTest.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/EG_uvmap_Read.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/EG_uvmap_Read.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/EG_uvmap_Write.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/EG_uvmap_Write.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_add.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/uvmap_add.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_bnd_adj.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/uvmap_bnd_adj.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_chk_area_uv.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/uvmap_chk_area_uv.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_chk_edge_ratio.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/uvmap_chk_edge_ratio.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_cpu_message.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/uvmap_cpu_message.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_find_uv.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/uvmap_find_uv.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_from_egads.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/uvmap_from_egads.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_gen.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/uvmap_gen.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_gen_uv.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/uvmap_gen_uv.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_ibeibe.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/uvmap_ibeibe.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_ibfibf.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/uvmap_ibfibf.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_ibfin.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/uvmap_ibfin.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_iccibe.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/uvmap_iccibe.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_iccin.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/uvmap_iccin.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_idibe.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/uvmap_idibe.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_inibe.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/uvmap_inibe.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_inl_uv_bnd.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/uvmap_inl_uv_bnd.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_malloc.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/uvmap_malloc.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_mben_disc.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/uvmap_mben_disc.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_message.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/uvmap_message.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_norm_uv.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/uvmap_norm_uv.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_read.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/uvmap_read.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_solve.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/uvmap_solve.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_struct_tasks.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/uvmap_struct_tasks.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_test.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/uvmap_test.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_to_egads.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/uvmap_to_egads.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_version.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/uvmap_version.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_write.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/uvmap_write.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 egadsUVmap.c -Iuvmap \ -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egadsUVmap.o touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libuvmap.a rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libuvmap.a (cd /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj; ar rs /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libuvmap.a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egadsUVmap.o EG_uvmapFindUV.o EG_uvmapGen.o EG_uvmapStructFree.o EG_uvmapTest.o EG_uvmap_Read.o EG_uvmap_Write.o uvmap_add.o uvmap_bnd_adj.o uvmap_chk_area_uv.o uvmap_chk_edge_ratio.o uvmap_cpu_message.o uvmap_find_uv.o uvmap_from_egads.o uvmap_gen.o uvmap_gen_uv.o uvmap_ibeibe.o uvmap_ibfibf.o uvmap_ibfin.o uvmap_iccibe.o uvmap_iccin.o uvmap_idibe.o uvmap_inibe.o uvmap_inl_uv_bnd.o uvmap_malloc.o uvmap_mben_disc.o uvmap_message.o uvmap_norm_uv.o uvmap_read.o uvmap_solve.o uvmap_struct_tasks.o uvmap_test.o uvmap_to_egads.o uvmap_version.o uvmap_write.o; ) ar: creating archive /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libuvmap.a clang -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/test/uvmap.exe /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/uvmap.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -luvmap -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libegads.dylib rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libegads.dylib (cd /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj; clang -g -target arm64-apple-darwin -dynamiclib -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libegads.dylib egadsGeom.o egadsHLevel.o egadsTopo.o egadsCopy.o egadsSpline.o egadsIO.o egadsSplineFit.o egadsSkinning.o egadsTessSens.o BRepLib_FuseEdges.o \ egadsBase.o egadsMemory.o egadsAttrs.o egadsTess.o egadsTessInp.o egadsTris.o egadsQuads.o egadsFit.o egadsRobust.o egadsSBO.o prmCfit.o prmGrid.o prmUV.o egadsExport.o egadsEffect.o egadsSolids.o emp.o evaluate.o rational.o regQuads.o \ -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -L/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -luvmap -lTKBool -lTKernel -lTKFeat -lTKBO -lTKGeomAlgo -lTKMath -lTKOffset -lTKPrim -lTKTopAlgo -lTKBRep -lTKG2d -lTKG3d -lTKGeomBase -lTKShHealing -lTKSTEP -lTKSTEP209 -lTKSTEPBase -lTKSTEPAttr -lTKXSBase -lTKIGES -lTKFillet -lc++ \ -install_name '@rpath/libegads.dylib' \ -compatibility_version 7.7 \ -current_version 1.0.25 ) touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libegadstatic.a rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libegadstatic.a cp /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libuvmap.a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libegadstatic.a (cd /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj; \ ar rs /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libegadstatic.a egadsBase.o egadsMemory.o egadsAttrs.o egadsTess.o egadsTessInp.o egadsTris.o egadsQuads.o egadsFit.o egadsRobust.o egadsSBO.o prmCfit.o prmGrid.o prmUV.o egadsExport.o egadsEffect.o egadsSolids.o egadsGeom.o egadsHLevel.o egadsTopo.o egadsCopy.o egadsSpline.o egadsIO.o egadsSplineFit.o egadsSkinning.o egadsTessSens.o BRepLib_FuseEdges.o emp.o \ evaluate.o rational.o regQuads.o; ) clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include fgadsBase.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/fgadsBase.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include fgadsMemory.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/fgadsMemory.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include fgadsAttrs.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/fgadsAttrs.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include fgadsTess.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/fgadsTess.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include fgadsHLevel.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/fgadsHLevel.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include fgadsGeom.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/fgadsGeom.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include fgadsTopo.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/fgadsTopo.o touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libfgads.a rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libfgads.a (cd /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj; ar rs /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libfgads.a fgadsBase.o fgadsMemory.o fgadsAttrs.o fgadsTess.o fgadsHLevel.o fgadsGeom.o fgadsTopo.o; ) ar: creating archive /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libfgads.a touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libemp.a rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libemp.a (cd /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj; ar rs /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libemp.a emp.o; ) ar: creating archive /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libemp.a *** EGADS Build Complete! *** ++ cd /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/EGADS/trunk/wvServer ++ make clang++ -g -target arm64-apple-darwin -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -ffp-model=strict map.cpp -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/map.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include base64-decode.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/base64-decode.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include handshake.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/handshake.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include client-handshake.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/client-handshake.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include libwebsockets.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/libwebsockets.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include extension-deflate-stream.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/extension-deflate-stream.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include md5.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/md5.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include extension-x-google-mux.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/extension-x-google-mux.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include parsers.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/parsers.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include extension.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/extension.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include sha-1.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/sha-1.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include server.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/server.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include wv.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/wv.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include browserMessage.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/browserMessage.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include fwv.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/fwv.o touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libwsserver.a rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libwsserver.a (cd /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj; ar rs /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libwsserver.a map.o base64-decode.o handshake.o client-handshake.o libwebsockets.o extension-deflate-stream.o md5.o extension-x-google-mux.o parsers.o extension.o sha-1.o server.o wv.o browserMessage.o \ /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/fwv.o; ) ar: creating archive /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libwsserver.a clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -DSTANDALONE server.c \ -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/servertest.o clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/test/server /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/servertest.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libwsserver.a \ -lpthread -lz -lm touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libwsserver.dylib rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libwsserver.dylib (cd /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj; clang++ -g -target arm64-apple-darwin -dynamiclib -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libwsserver.dylib \ base64-decode.o handshake.o client-handshake.o libwebsockets.o extension-deflate-stream.o md5.o extension-x-google-mux.o parsers.o extension.o sha-1.o server.o wv.o browserMessage.o map.o -lz \ -install_name '@rpath/libwsserver.dylib' \ -compatibility_version 7.7 \ -current_version 1.0.25 ) ++ cd /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/EGADS/trunk/lite ++ make clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I. -I../src -I../util/uvmap \ liteBase.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/liteBase.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I. -I../src -I../util/uvmap \ liteMemory.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/liteMemory.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I. -I../src -I../util/uvmap \ liteGeom.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/liteGeom.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I. -I../src -I../util/uvmap \ liteTopo.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/liteTopo.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I. -I../src -I../util/uvmap \ liteAttrs.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/liteAttrs.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I. -I../src -I../util/uvmap \ liteImport.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/liteImport.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I. -I../src -I../util/uvmap \ liteString.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/liteString.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -DLITE -I../include -I. -I../src \ ../src/egadsTess.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/liteTess.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -DLITE -I../include -I. -I../src \ ../src/egadsTris.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/liteTris.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I. -I../src \ ../src/egadsQuads.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/liteQuads.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -DLITE -I../include -I. -I../src \ -I../util ../src/egadsTessInp.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/liteTessInp.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -DLITE -I../include -I. -I../src \ ../util/evaluate.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/evaLite.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -DLITE ../util/rational.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/ratLite.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -DLITE -I../include -I../util \ ../util/regQuads.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/liteRegQuads.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -DLITE -I../include -I. -I../src \ ../src/egadsEffect.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/liteEffect.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -DLITE -I../include -I. -I../src \ -I../util/uvmap liteUVmap.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/liteUVmap.o touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libegadslite.dylib rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libegadslite.dylib (cd /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj; clang -g -target arm64-apple-darwin -dynamiclib -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libegadslite.dylib \ liteBase.o liteMemory.o liteGeom.o liteTopo.o liteAttrs.o liteImport.o liteString.o liteTess.o liteTris.o liteQuads.o liteTessInp.o \ egadsRobust.o emp.o evaLite.o ratLite.o liteRegQuads.o \ liteEffect.o liteUVmap.o \ -install_name '@rpath/libegadslite.dylib' \ -current_version 1.0.25 ) touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libegadslitestatic.a rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libegadslitestatic.a (cd /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj; ar rs /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libegadslitestatic.a liteBase.o liteMemory.o liteGeom.o liteTopo.o liteAttrs.o liteImport.o liteString.o \ liteTess.o liteTris.o liteQuads.o liteTessInp.o egadsRobust.o \ emp.o evaLite.o ratLite.o liteRegQuads.o liteEffect.o \ liteUVmap.o ; ) ar: creating archive /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libegadslitestatic.a ++ cd /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/EGADS/trunk/test +++ ls BSplineIGES.make CSys.make GBO.make SBO.make addKnots.make agglom.make approx.make blend.make chamfer.make closure.make edge2WB.make edges.make effective.make egads2cart.make egads2ply.make egadsGeom_dot.make egadsHLevel_dot.make egadsSpline_dot.make egadsTopo_dot.make exportLite.make extrot.make fillet.make fit.make fitTri.make fullAttr.make fuseSheets.make globalTess.make hollow.make hollowFace.make intersect.make makeCone.make makeFace3D.make makeLoop.make mapTess.make mofb.make mssb.make multiContext.make offset.make rebuild.make refObj.make replace.make revolve.make ruled.make saveTess.make scribe.make sew.make simplePer.make smallEdges.make step.make sweep.make test.make tolerance.make union.make vAttr.make vCurvature.make vEffect.make vEto.make vFrame.make vGeom.make vQuad.make vTess.make vTessInp.make xform.make ++ for file in '`ls *.make`' ++ make -f BSplineIGES.make clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include BSplineIGES.c -o \ /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/BSplineIGES.o clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/test/BSplineIGES /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/BSplineIGES.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads \ -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f CSys.make clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include CSys.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/CSys.o clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/test/CSys /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/CSys.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f GBO.make clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include GBO.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/GBO.o clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/test/GBO /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/GBO.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f SBO.make clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include SBO.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/SBO.o clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/test/SBO /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/SBO.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f addKnots.make clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include addKnots.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/addKnots.o clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/test/addKnots /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/addKnots.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads \ -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f agglom.make clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include agglom.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/agglom.o clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/test/agglom /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/agglom.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -legads -lm ++ for file in '`ls *.make`' ++ make -f approx.make gfortran -g -c -O -frecursive -fcray-pointer -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include approx.f -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/approx.o gfortran -g -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/test/approx /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/approx.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lfgads \ -legads -Wl,-rpath,/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -Wl,-rpath,@loader_path/ -Wl,-rpath,/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lc++ -static-libgfortran -static-libgcc -Wl,-w ++ for file in '`ls *.make`' ++ make -f blend.make clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include blend.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/blend.o clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/test/blend /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/blend.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f chamfer.make clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include chamfer.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/chamfer.o clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/test/chamfer /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/chamfer.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads \ -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f closure.make gfortran -g -c -O -frecursive -fcray-pointer -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include closure.f -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/closure.o gfortran -g -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/test/closure /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/closure.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lfgads \ -legads -Wl,-rpath,/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -Wl,-rpath,@loader_path/ -Wl,-rpath,/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lc++ -static-libgfortran -static-libgcc -Wl,-w ++ for file in '`ls *.make`' ++ make -f edge2WB.make clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include edge2WB.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/edge2WB.o clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/test/edge2WB /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/edge2WB.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads \ -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f edges.make clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include edges.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/edges.o clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/test/edges /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/edges.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f effective.make clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include effective.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/effective.o clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/test/effective /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/effective.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads \ -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f egads2cart.make clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include egads2cart.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads2cart.o clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/test/egads2cart /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads2cart.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads \ -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f egads2ply.make clang++ -g -target arm64-apple-darwin -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -ffp-model=strict -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. egads2ply.cpp -std=c++11 \ -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads2ply.o clang++ -g -target arm64-apple-darwin -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -ffp-model=strict -DREVISION=7.7 -I. tinyply.cpp -std=c++11 -w \ -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/tinyply.o clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/test/egads2ply /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads2ply.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/tinyply.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f egadsGeom_dot.make clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include egadsGeom_dot.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egadsGeom_dot.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include egadsTools_dot.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egadsTools_dot.o clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/test/egadsGeom_dot /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egadsGeom_dot.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egadsTools_dot.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads \ -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f egadsHLevel_dot.make clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include egadsHLevel_dot.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egadsHLevel_dot.o clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/test/egadsHLevel_dot /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egadsHLevel_dot.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egadsTools_dot.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads \ -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f egadsSpline_dot.make clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include egadsSpline_dot.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egadsSpline_dot.o clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/test/egadsSpline_dot /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egadsSpline_dot.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egadsTools_dot.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads \ -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f egadsTopo_dot.make clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include egadsTopo_dot.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egadsTopo_dot.o clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/test/egadsTopo_dot /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egadsTopo_dot.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egadsTools_dot.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads \ -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f exportLite.make clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../util/uvmap \ ../src/egadsExport.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/exportLite.o -DSTANDALONE clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/test/exportLite /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/exportLite.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f extrot.make clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include extrot.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/extrot.o clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/test/extrot /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/extrot.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f fillet.make clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include fillet.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/fillet.o clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/test/fillet /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/fillet.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f fit.make clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include fit.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/fit.o clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/test/fit /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/fit.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f fitTri.make clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include fitTri.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/fitTri.o clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/test/fitTri /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/fitTri.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f fullAttr.make clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include fullAttr.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/fullAttr.o clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/test/fullAttr /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/fullAttr.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads \ -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f fuseSheets.make clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include fuseSheets.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/fuseSheets.o clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/test/fuseSheets /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/fuseSheets.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f globalTess.make clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include globalTess.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/globalTess.o clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/test/globalTess /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/globalTess.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads \ -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f hollow.make clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include hollow.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/hollow.o clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/test/hollow /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/hollow.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f hollowFace.make clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include hollowFace.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/hollowFace.o clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/test/hollowFace /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/hollowFace.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f intersect.make clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include intersect.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/intersect.o clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/test/intersect /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/intersect.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads \ -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f makeCone.make clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include makeCone.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/makeCone.o clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/test/makeCone /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/makeCone.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads \ -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f makeFace3D.make clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include makeFace3D.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/makeFace3D.o clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/test/makeFace3D /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/makeFace3D.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads \ -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f makeLoop.make clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include makeLoop.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/makeLoop.o clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/test/makeLoop /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/makeLoop.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads \ -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f mapTess.make clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include mapTess.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/mapTess.o clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/test/mapTess /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/mapTess.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads \ -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f mofb.make clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include mofb.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/mofb.o clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/test/mofb /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/mofb.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f mssb.make clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include mssb.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/mssb.o clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/test/mssb /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/mssb.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f multiContext.make clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include multiContext.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/multiContext.o clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/test/multiContext /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/multiContext.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib \ -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f offset.make clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include offset.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/offset.o clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/test/offset /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/offset.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f rebuild.make clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include rebuild.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/rebuild.o clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/test/rebuild /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/rebuild.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads \ -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f refObj.make clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include refObj.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/refObj.o clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/test/refObj /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/refObj.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f replace.make clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include replace.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/replace.o clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/test/replace /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/replace.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads \ -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f revolve.make clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include revolve.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/revolve.o clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/test/revolve /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/revolve.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads \ -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f ruled.make clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include ruled.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/ruled.o clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/test/ruled /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/ruled.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f saveTess.make clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include saveTess.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/saveTess.o clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/test/saveTess /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/saveTess.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads \ -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f scribe.make clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include scribe.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/scribe.o clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/test/scribe /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/scribe.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f sew.make clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include sew.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/sew.o clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/test/sew /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/sew.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f simplePer.make clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include simplePer.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/simplePer.o clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/test/simplePer /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/simplePer.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads \ -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f smallEdges.make clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include smallEdges.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/smallEdges.o clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/test/smallEdges /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/smallEdges.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f step.make gfortran -g -c -O -frecursive -fcray-pointer -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include step.f -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/step.o gfortran -g -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/test/step /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/step.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lfgads -legads \ -Wl,-rpath,/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -Wl,-rpath,@loader_path/ -Wl,-rpath,/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lc++ -static-libgfortran -static-libgcc -Wl,-w ++ for file in '`ls *.make`' ++ make -f sweep.make clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include sweep.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/sweep.o clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/test/sweep /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/sweep.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f test.make clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include testc.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/testc.o clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/test/testc /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/testc.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm gfortran -g -c -O -frecursive -fcray-pointer -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include testf.f -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/testf.o gfortran -g -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/test/testf /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/testf.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lfgads -legads \ -Wl,-rpath,/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -Wl,-rpath,@loader_path/ -Wl,-rpath,/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lc++ -static-libgfortran -static-libgcc -Wl,-w clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include parsec.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/parsec.o clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/test/parsec /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/parsec.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm gfortran -g -c -O -frecursive -fcray-pointer -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include parsef.f -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/parsef.o gfortran -g -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/test/parsef /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/parsef.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lfgads -legads \ -Wl,-rpath,/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -Wl,-rpath,@loader_path/ -Wl,-rpath,/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lc++ -static-libgfortran -static-libgcc -Wl,-w ++ for file in '`ls *.make`' ++ make -f tolerance.make clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include tolerance.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/tolerance.o clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/test/tolerance /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/tolerance.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads \ -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f union.make gfortran -g -c -O -frecursive -fcray-pointer -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include union.f -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/union.o gfortran -g -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/test/union /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/union.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lfgads -legads \ -Wl,-rpath,/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -Wl,-rpath,@loader_path/ -Wl,-rpath,/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lc++ -static-libgfortran -static-libgcc -Wl,-w ++ for file in '`ls *.make`' ++ make -f vAttr.make clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include vAttr.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/vAttr.o clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/test/vAttr /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/vAttr.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lwsserver -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib ++ for file in '`ls *.make`' ++ make -f vCurvature.make clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include vCurvature.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/vCurvature.o clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/test/vCurvature /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/vCurvature.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lwsserver -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib ++ for file in '`ls *.make`' ++ make -f vEffect.make clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include vEffect.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/vEffect.o clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/test/vEffect /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/vEffect.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lwsserver -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib ++ for file in '`ls *.make`' ++ make -f vEto.make clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include vEto.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/vEto.o clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/test/vEto /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/vEto.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lwsserver -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib ++ for file in '`ls *.make`' ++ make -f vFrame.make clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include vFrame.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/vFrame.o clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/test/vFrame /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/vFrame.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lwsserver -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib ++ for file in '`ls *.make`' ++ make -f vGeom.make clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include vGeom.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/vGeom.o clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/test/vGeom /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/vGeom.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lwsserver -legads \ -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib ++ for file in '`ls *.make`' ++ make -f vQuad.make clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include vQuad.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/vQuad.o clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/test/vQuad /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/vQuad.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lwsserver \ -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib ++ for file in '`ls *.make`' ++ make -f vTess.make clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include vTess.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/vTess.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include ../util/retessFaces.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/retessFaces.o clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/test/vTesstatic /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/vTess.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/retessFaces.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lwsserver -legadstatic -L/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lTKBool -lTKernel -lTKFeat -lTKBO -lTKGeomAlgo -lTKMath -lTKOffset -lTKPrim -lTKTopAlgo -lTKBRep -lTKG2d -lTKG3d -lTKGeomBase -lTKShHealing -lTKSTEP -lTKSTEP209 -lTKSTEPBase -lTKSTEPAttr -lTKXSBase -lTKIGES -lTKFillet \ -lpthread -lz -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/test/vTess /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/vTess.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/retessFaces.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lwsserver -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib ++ for file in '`ls *.make`' ++ make -f vTessInp.make clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include vTessInp.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/vTessInp.o clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/test/vTessInp /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/vTessInp.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lwsserver -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib ++ for file in '`ls *.make`' ++ make -f xform.make clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include xform.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/xform.o clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/test/xform /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/xform.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm ++ cd /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/EGADS/trunk/docs/Tutorial ++ make -f tire.make clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include tire.c clang++ -g -target arm64-apple-darwin -o tire tire.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm ++ make -f egads2tri.make clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include egads2tri.c clang++ -g -target arm64-apple-darwin -o egads2tri egads2tri.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm ++ cd /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/EGADS/trunk/docs/EGADS_dot/src ++ make clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. circle1_dot.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/circle1_dot.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. pingBodies.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/pingBodies.o clang -g -target arm64-apple-darwin -o circle1_dot /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/circle1_dot.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/pingBodies.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads -lm -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. circle2_dot.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/circle2_dot.o clang -g -target arm64-apple-darwin -o circle2_dot /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/circle2_dot.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/pingBodies.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads -lm -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. naca_dot.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/naca_dot.o clang -g -target arm64-apple-darwin -o naca_dot /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/naca_dot.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/pingBodies.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads -lm -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. ruled_naca_dot.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/ruled_naca_dot.o clang -g -target arm64-apple-darwin -o ruled_naca_dot /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/ruled_naca_dot.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/pingBodies.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads -lm -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib ++ cd /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/OpenCSM/trunk/src ++ make clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. serveCSM.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/serveCSM.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. OpenCSM.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/OpenCSM.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udp.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udp.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. tim.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/tim.o touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libocsm.dylib rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libocsm.dylib clang -g -target arm64-apple-darwin -dynamiclib -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libocsm.dylib /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/OpenCSM.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udp.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/tim.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads -lwsserver -ldl -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -install_name '@rpath/libocsm.dylib' -compatibility_version 1.0.25 -current_version 1.0.25 clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/bin/serveCSM /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/serveCSM.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -lwsserver -legads -ldl -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. serveESP.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/serveESP.o clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/bin/serveESP /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/serveESP.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -lwsserver -legads -ldl -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. sensCSM.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/sensCSM.o clang -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/bin/sensCSM /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/sensCSM.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udpBezier.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpBezier.o touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/bezier.so rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/bezier.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/bezier.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpBezier.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udpBiconvex.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpBiconvex.o touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/biconvex.so rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/biconvex.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/biconvex.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpBiconvex.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udpBox.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpBox.o touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/box.so rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/box.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/box.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpBox.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udpBspline.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpBspline.o touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/bspline.so rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/bspline.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/bspline.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpBspline.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udfCatmull.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfCatmull.o touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/catmull.so rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/catmull.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/catmull.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfCatmull.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udfCompare.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfCompare.o touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/compare.so rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/compare.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/compare.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfCompare.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udfCreateBEM.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfCreateBEM.o touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/createBEM.so rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/createBEM.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/createBEM.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfCreateBEM.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udfCreatePoly.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfCreatePoly.o touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/createPoly.so rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/createPoly.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/createPoly.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfCreatePoly.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udpCsm.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpCsm.o touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/csm.so rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/csm.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/csm.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpCsm.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udfDeform.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfDeform.o touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/deform.so rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/deform.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/deform.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfDeform.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udfDroop.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfDroop.o touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/droop.so rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/droop.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/droop.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfDroop.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udfDumpPmtrs.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfDumpPmtrs.o touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/dumpPmtrs.so rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/dumpPmtrs.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/dumpPmtrs.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfDumpPmtrs.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udfEditAttr.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfEditAttr.o touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/editAttr.so rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/editAttr.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/editAttr.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfEditAttr.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udpEllipse.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpEllipse.o touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/ellipse.so rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/ellipse.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/ellipse.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpEllipse.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udpEqn2body.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpEqn2body.o touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/eqn2body.so rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/eqn2body.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/eqn2body.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpEqn2body.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udpFitcurve.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpFitcurve.o touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/fitcurve.so rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/fitcurve.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/fitcurve.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpFitcurve.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udfFlend.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfFlend.o touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/flend.so rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/flend.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/flend.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfFlend.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udpFreeform.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpFreeform.o touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/freeform.so rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/freeform.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/freeform.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpFreeform.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udfGanged.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfGanged.o touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/ganged.so rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/ganged.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/ganged.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfGanged.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udfGuide.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfGuide.o touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/guide.so rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/guide.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/guide.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfGuide.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udpHex.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpHex.o touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/hex.so rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/hex.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/hex.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpHex.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udpImport.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpImport.o touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/import.so rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/import.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/import.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpImport.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udpKulfan.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpKulfan.o touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/kulfan.so rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/kulfan.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/kulfan.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpKulfan.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udfLinalg.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfLinalg.o touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/linalg.so rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/linalg.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/linalg.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfLinalg.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udfMatchBodys.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfMatchBodys.o touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/matchBodys.so rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/matchBodys.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/matchBodys.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfMatchBodys.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udfMechanism.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfMechanism.o touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/mechanism.so rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/mechanism.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/mechanism.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfMechanism.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udpNaca.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpNaca.o touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/naca.so rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/naca.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/naca.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpNaca.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udfNaca6mc.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfNaca6mc.o touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/naca6mc.so rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/naca6mc.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/naca6mc.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfNaca6mc.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udfNacelle.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfNacelle.o touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/nacelle.so rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/nacelle.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/nacelle.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfNacelle.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udpNurbbody.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpNurbbody.o touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/nurbbody.so rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/nurbbody.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/nurbbody.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpNurbbody.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udfNuscale.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfNuscale.o touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/nuscale.so rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/nuscale.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/nuscale.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfNuscale.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udfOffset.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfOffset.o touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/offset.so rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/offset.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/offset.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfOffset.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udpParabaloid.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpParabaloid.o touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/parabaloid.so rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/parabaloid.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/parabaloid.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpParabaloid.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm clang++ -g -target arm64-apple-darwin -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -ffp-model=strict -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udpParsec.cpp -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpParsec.o touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/parsec.so rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/parsec.so clang++ -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/parsec.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpParsec.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udpPod.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpPod.o touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/pod.so rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/pod.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/pod.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpPod.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udpPoly.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpPoly.o touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/poly.so rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/poly.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/poly.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpPoly.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udfPrintBbox.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfPrintBbox.o touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/printBbox.so rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/printBbox.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/printBbox.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfPrintBbox.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udfPrintBrep.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfPrintBrep.o touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/printBrep.so rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/printBrep.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/printBrep.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfPrintBrep.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udfPrintEgo.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfPrintEgo.o touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/printEgo.so rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/printEgo.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/printEgo.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfPrintEgo.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udpProp.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpProp.o touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/prop.so rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/prop.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/prop.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpProp.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udpRadwaf.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpRadwaf.o touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/radwaf.so rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/radwaf.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/radwaf.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpRadwaf.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udpSample.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpSample.o touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/sample.so rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/sample.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/sample.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpSample.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udpSew.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpSew.o touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/sew.so rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/sew.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/sew.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpSew.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udfShadow.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfShadow.o touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/shadow.so rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/shadow.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/shadow.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfShadow.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udfSlices.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfSlices.o touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/slices.so rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/slices.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/slices.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfSlices.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udpStag.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpStag.o touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/stag.so rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/stag.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/stag.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpStag.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udfStiffener.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfStiffener.o touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/stiffener.so rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/stiffener.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/stiffener.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfStiffener.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udpSupell.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpSupell.o touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/supell.so rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/supell.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/supell.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpSupell.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udfTester1.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfTester1.o touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/tester1.so rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/tester1.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/tester1.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfTester1.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udpTester2.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpTester2.o touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/tester2.so rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/tester2.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/tester2.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpTester2.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udpVsp3.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpVsp3.o touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/vsp3.so rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/vsp3.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/vsp3.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpVsp3.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udpWaffle.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpWaffle.o touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/waffle.so rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/waffle.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/waffle.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpWaffle.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udpWarp.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpWarp.o touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/warp.so rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/warp.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/warp.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpWarp.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. eggPDT2.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/eggPDT2.o touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/PDT2.so rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/PDT2.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/PDT2.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/eggPDT2.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udpNaca456.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpNaca456.o gfortran -g -c -O -frecursive -fcray-pointer naca456.f90 -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/naca456.o -J /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/naca456.so rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/naca456.so gfortran -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/naca456.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpNaca456.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/naca456.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm -static-libgfortran -static-libgcc -Wl,-w clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. timEreped.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/timEreped.o touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/ereped.so rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/ereped.so clang++ -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/ereped.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/timEreped.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -lwsserver -legads -ldl -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. timMitten.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/timMitten.o touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/mitten.so rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/mitten.so clang++ -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/mitten.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/timMitten.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -lwsserver -legads -ldl -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. timPlotter.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/timPlotter.o touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/plotter.so rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/plotter.so clang++ -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/plotter.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/timPlotter.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -lwsserver -legads -ldl -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. timPlugs.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/timPlugs.o touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/plugs.so rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/plugs.so clang++ -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/plugs.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/timPlugs.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -lwsserver -legads -ldl -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. timSlugs.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/timSlugs.o touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/slugs.so rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/slugs.so clang++ -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/slugs.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/timSlugs.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -lwsserver -legads -ldl -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. timVspSetup.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/timVspSetup.o touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/vspSetup.so rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/vspSetup.so clang++ -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/vspSetup.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/timVspSetup.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -lwsserver -legads -ldl -lm touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include/OpenCSM.h rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include/OpenCSM.h cp -p OpenCSM.h /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include/OpenCSM.h touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include/common.h rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include/common.h cp -p common.h /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include/common.h touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include/udp.h rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include/udp.h cp -p udp.h /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include/udp.h touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include/esp.h rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include/esp.h cp -p esp.h /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include/esp.h touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include/tim.h rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include/tim.h cp -p tim.h /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include/tim.h touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include/egg.h rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include/egg.h cp -p egg.h /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include/egg.h touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include/udpUtilities.h rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include/udpUtilities.h cp -p udpUtilities.h /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include/udpUtilities.h touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include/udpUtilities.c rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include/udpUtilities.c cp -p udpUtilities.c /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include/udpUtilities.c ++ cd /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/EGADS/trunk/docs/UDP_UDF/data ++ make clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include udpTire.c -o tire.o clang -g -target arm64-apple-darwin -o tire tire.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads -lm -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -DUDP -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include udpTire.c touch tire.so rm tire.so clang -g -target arm64-apple-darwin -bundle -o tire.so udpTire.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads -lm -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib ++ [[ '' == '' ]] ++ cd /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/CAPS ++ make (cd src; make) touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include/caps.h rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include/caps.h cp -p ../include/caps.h /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include/caps.h touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include/capsErrors.h rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include/capsErrors.h cp -p ../include/capsErrors.h /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include/capsErrors.h touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include/capsTypes.h rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include/capsTypes.h cp -p ../include/capsTypes.h /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include/capsTypes.h touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include/aimUtil.h rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include/aimUtil.h cp -p ../include/aimUtil.h /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include/aimUtil.h touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include/aimMesh.h rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include/aimMesh.h cp -p ../include/aimMesh.h /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include/aimMesh.h clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../include \ -I/usr/include/udunits2 aimUtil.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/aimUtil.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include \ -I/usr/include/udunits2 aimTransferUtil.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/aimTransferUtil.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../include \ aimMesh.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/aimMesh.o touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libaimUtil.a rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libaimUtil.a ar -rs /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libaimUtil.a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/aimUtil.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/aimMesh.o \ /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/aimTransferUtil.o ar: creating archive /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libaimUtil.a clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. \ -I/usr/include/udunits2 capsBase.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/capsBase.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. \ -I/usr/include/udunits2 capsAnalysis.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/capsAnalysis.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. \ -I/usr/include/udunits2 capsApprox.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/capsApprox.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. \ -I/usr/include/udunits2 capsAttr.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/capsAttr.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. \ -I/usr/include/udunits2 capsAIM.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/capsAIM.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. \ -I/usr/include/udunits2 capsBound.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/capsBound.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. \ -I/usr/include/udunits2 capsProblem.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/capsProblem.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. \ -I/usr/include/udunits2 capsValue.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/capsValue.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. \ -I/usr/include/udunits2 capsUnits.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/capsUnits.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. \ -I/usr/include/udunits2 conjGrad.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/conjGrad.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. \ -I/usr/include/udunits2 capsFunIDs.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/capsFunIDs.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. \ -I/usr/include/udunits2 capsChkInpt.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/capsChkInpt.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. \ -I/usr/include/udunits2 printObject.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/printObject.o touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libcaps.dylib rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libcaps.dylib (cd /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj; clang -g -target arm64-apple-darwin -dynamiclib -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libcaps.dylib capsBase.o capsAnalysis.o capsApprox.o capsAttr.o capsAIM.o capsBound.o capsProblem.o capsValue.o capsUnits.o conjGrad.o capsFunIDs.o capsChkInpt.o printObject.o \ -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -ludunits2 -locsm -legads -ldl \ -install_name '@rpath/libcaps.dylib' \ -compatibility_version 1.0.25 \ -current_version 1.0.25 ) touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libcapsstatic.a rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libcapsstatic.a (cd /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj; ar -rs /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libcapsstatic.a capsBase.o capsAnalysis.o capsApprox.o capsAttr.o capsAIM.o capsBound.o capsProblem.o capsValue.o capsUnits.o conjGrad.o capsFunIDs.o capsChkInpt.o printObject.o ) ar: creating archive /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libcapsstatic.a clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include testingAIM.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/testingAIM.o rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/testingAIM.so rm: /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/testingAIM.so: No such file or directory make[1]: [/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/testingAIM.so] Error 1 (ignored) clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/testingAIM.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/testingAIM.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -laimUtil -legads -locsm -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include testingWriter.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/testingWriter.o rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/testingWriter.so rm: /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/testingWriter.so: No such file or directory make[1]: [/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/testingWriter.so] Error 1 (ignored) clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/testingWriter.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/testingWriter.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -laimUtil -ldl -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include phaseUtil.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/phaseUtil.o clang -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/bin/phaseUtil /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/phaseUtil.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lcaps -ludunits2 -locsm -legads -ldl -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm (cd aim; make) /Library/Developer/CommandLineTools/usr/bin/make -C utils clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. -DHAVE_PYTHON -I. -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython attrUtils.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/attrUtils.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. -DHAVE_PYTHON -I. -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython meshUtils.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/meshUtils.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. -DHAVE_PYTHON -I. -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython cfdUtils.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/cfdUtils.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. -DHAVE_PYTHON -I. -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython miscUtils.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/miscUtils.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. -DHAVE_PYTHON -I. -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython feaUtils.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/feaUtils.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. -DHAVE_PYTHON -I. -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython vlmUtils.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/vlmUtils.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. -DHAVE_PYTHON -I. -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython nastranUtils.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/nastranUtils.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. -DHAVE_PYTHON -I. -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython tecplotUtils.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/tecplotUtils.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. -DHAVE_PYTHON -I. -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython arrayUtils.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/arrayUtils.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. -DHAVE_PYTHON -I. -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython deprecateUtils.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/deprecateUtils.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. -DHAVE_PYTHON -I. -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython cardUtils.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/cardUtils.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. -DHAVE_PYTHON -I. -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython nastranCards.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/nastranCards.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. -DHAVE_PYTHON -I. -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython jsonUtils.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/jsonUtils.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. -DHAVE_PYTHON -I. -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython cython/nastranOP2Reader.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/nastranOP2Reader.o clang++ -g -target arm64-apple-darwin -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -ffp-model=strict -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. vlmSpanSpace.cpp -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/vlmSpanSpace.o touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libutils.a rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libutils.a (cd /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj; ar -rs /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libutils.a attrUtils.o meshUtils.o cfdUtils.o miscUtils.o feaUtils.o vlmUtils.o nastranUtils.o tecplotUtils.o arrayUtils.o deprecateUtils.o cardUtils.o nastranCards.o jsonUtils.o nastranOP2Reader.o vlmSpanSpace.o ) ar: creating archive /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libutils.a mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include/aim/utils cp -p -f arrayUtils.h /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include/aim/utils/arrayUtils.h cp -p -f attrTypes.h /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include/aim/utils/attrTypes.h cp -p -f attrUtils.h /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include/aim/utils/attrUtils.h cp -p -f cardTypes.h /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include/aim/utils/cardTypes.h cp -p -f cardUtils.h /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include/aim/utils/cardUtils.h cp -p -f cfdTypes.h /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include/aim/utils/cfdTypes.h cp -p -f cfdUtils.h /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include/aim/utils/cfdUtils.h cp -p -f deprecateUtils.h /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include/aim/utils/deprecateUtils.h cp -p -f feaTypes.h /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include/aim/utils/feaTypes.h cp -p -f feaUtils.h /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include/aim/utils/feaUtils.h cp -p -f jsonUtils.h /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include/aim/utils/jsonUtils.h cp -p -f meshTypes.h /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include/aim/utils/meshTypes.h cp -p -f meshUtils.h /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include/aim/utils/meshUtils.h cp -p -f miscTypes.h /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include/aim/utils/miscTypes.h cp -p -f miscUtils.h /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include/aim/utils/miscUtils.h cp -p -f nastranCards.h /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include/aim/utils/nastranCards.h cp -p -f nastranUtils.h /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include/aim/utils/nastranUtils.h cp -p -f tecplotUtils.h /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include/aim/utils/tecplotUtils.h cp -p -f vlmSpanSpace.h /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include/aim/utils/vlmSpanSpace.h cp -p -f vlmTypes.h /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include/aim/utils/vlmTypes.h cp -p -f vlmUtils.h /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include/aim/utils/vlmUtils.h /Library/Developer/CommandLineTools/usr/bin/make -C abaqus clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../utils \ abaqusAIM.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/abaqusAIM.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -DHAVE_PYTHON -I. -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../utils \ abaqusUtils.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/abaqusUtils.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../utils \ -I. -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 cython/abaqusFILReader.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/abaqusFILReader.o echo "Building Abaqus with Python" Building Abaqus with Python clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/abaqusAIM.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/abaqusAIM.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/abaqusUtils.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/abaqusFILReader.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lutils -laimUtil -locsm -legads -ludunits2 -L/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11 -ldl -framework CoreFoundation -Wl,-w -lm -ldl -Wl,-rpath /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib /Library/Developer/CommandLineTools/usr/bin/make -C aflr2 clang -g -target arm64-apple-darwin -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.14/src aflr2_version.c \ -L/Users/jenkins/util/AFLR/aflr_lib_11.5.14/MacOSX-arm64/lib -laflr2c -lm \ -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/aflr2_version /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/aflr2_version clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.14/src \ -I../utils aflr2AIM.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/aflr2AIM.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.14/src \ -I../utils aflr2_Interface.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/aflr2_Interface.o touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/aflr2AIM.so rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/aflr2AIM.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/aflr2AIM.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/aflr2AIM.o \ /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/aflr2_Interface.o -L/Users/jenkins/util/AFLR/aflr_lib_11.5.14/MacOSX-arm64/lib \ -laflr2c -legen -lrec2 -ldftr2 -ldftr3 -ldgeom -lotb -lqtb -lug_io -lug_cpp -lice2 -lug3 -lug2 -lug_gq -lug -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lutils \ -laimUtil -locsm -legads -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lc++ -lm /Library/Developer/CommandLineTools/usr/bin/make -C aflr3 clang -g -target arm64-apple-darwin -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.14/src aflr3_version.c \ -L/Users/jenkins/util/AFLR/aflr_lib_11.5.14/MacOSX-arm64/lib -laflr3 \ -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/aflr3_version /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/aflr3_version 16.32.50 clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../utils -I/Users/jenkins/util/AFLR/aflr_lib_11.5.14/src \ aflr3AIM.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/aflr3AIM.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../utils -I/Users/jenkins/util/AFLR/aflr_lib_11.5.14/src \ aflr3_Interface.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/aflr3_Interface.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.14/src /Users/jenkins/util/AFLR/aflr_lib_11.5.14/src/egads_aflr4/EG_getEffBodyTopos.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/EG_getEffBodyTopos.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.14/src /Users/jenkins/util/AFLR/aflr_lib_11.5.14/src/egads_aflr4/egads_aflr4_check_tess_coord.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_aflr4_check_tess_coord.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.14/src /Users/jenkins/util/AFLR/aflr_lib_11.5.14/src/egads_aflr4/egads_aflr4_check_tess_ordering.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_aflr4_check_tess_ordering.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.14/src /Users/jenkins/util/AFLR/aflr_lib_11.5.14/src/egads_aflr4/egads_aflr4_get_bedge_coord.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_aflr4_get_bedge_coord.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.14/src /Users/jenkins/util/AFLR/aflr_lib_11.5.14/src/egads_aflr4/egads_aflr4_get_edge_spacing.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_aflr4_get_edge_spacing.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.14/src /Users/jenkins/util/AFLR/aflr_lib_11.5.14/src/egads_aflr4/egads_aflr4_get_faceOrder.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_aflr4_get_faceOrder.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.14/src /Users/jenkins/util/AFLR/aflr_lib_11.5.14/src/egads_aflr4/egads_aflr4_get_face_spacing.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_aflr4_get_face_spacing.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.14/src /Users/jenkins/util/AFLR/aflr_lib_11.5.14/src/egads_aflr4/egads_aflr4_get_surf_grid.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_aflr4_get_surf_grid.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.14/src /Users/jenkins/util/AFLR/aflr_lib_11.5.14/src/egads_aflr4/egads_aflr4_create_tess.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_aflr4_create_tess.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.14/src /Users/jenkins/util/AFLR/aflr_lib_11.5.14/src/egads_aflr4/egads_aflr4_tess_to_dgeom.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_aflr4_tess_to_dgeom.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.14/src /Users/jenkins/util/AFLR/aflr_lib_11.5.14/src/egads_aflr4/egads_aflr4_version.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_aflr4_version.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.14/src /Users/jenkins/util/AFLR/aflr_lib_11.5.14/src/egads_aflr4/egads_auto_cad_geom_setup.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_auto_cad_geom_setup.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.14/src /Users/jenkins/util/AFLR/aflr_lib_11.5.14/src/egads_aflr4/egads_cad_geom_add_attr.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_add_attr.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.14/src /Users/jenkins/util/AFLR/aflr_lib_11.5.14/src/egads_aflr4/egads_cad_geom_add_ff.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_add_ff.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.14/src /Users/jenkins/util/AFLR/aflr_lib_11.5.14/src/egads_aflr4/egads_cad_geom_add_ret_attr.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_add_ret_attr.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.14/src /Users/jenkins/util/AFLR/aflr_lib_11.5.14/src/egads_aflr4/egads_cad_geom_bodyFlag.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_bodyFlag.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.14/src /Users/jenkins/util/AFLR/aflr_lib_11.5.14/src/egads_aflr4/egads_cad_geom_check_bc.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_check_bc.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.14/src /Users/jenkins/util/AFLR/aflr_lib_11.5.14/src/egads_aflr4/egads_cad_geom_data_cleanup.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_data_cleanup.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.14/src /Users/jenkins/util/AFLR/aflr_lib_11.5.14/src/egads_aflr4/egads_cad_geom_edgeData.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_edgeData.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.14/src /Users/jenkins/util/AFLR/aflr_lib_11.5.14/src/egads_aflr4/egads_cad_geom_edgeFace.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_edgeFace.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.14/src /Users/jenkins/util/AFLR/aflr_lib_11.5.14/src/egads_aflr4/egads_cad_geom_edit.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_edit.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.14/src /Users/jenkins/util/AFLR/aflr_lib_11.5.14/src/egads_aflr4/egads_cad_geom_faceEdge.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_faceEdge.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.14/src /Users/jenkins/util/AFLR/aflr_lib_11.5.14/src/egads_aflr4/egads_cad_geom_faceFace.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_faceFace.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.14/src /Users/jenkins/util/AFLR/aflr_lib_11.5.14/src/egads_aflr4/egads_cad_geom_faceFlag.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_faceFlag.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.14/src /Users/jenkins/util/AFLR/aflr_lib_11.5.14/src/egads_aflr4/egads_cad_geom_faceLoop.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_faceLoop.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.14/src /Users/jenkins/util/AFLR/aflr_lib_11.5.14/src/egads_aflr4/egads_cad_geom_file_read.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_file_read.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.14/src /Users/jenkins/util/AFLR/aflr_lib_11.5.14/src/egads_aflr4/egads_cad_geom_file_write.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_file_write.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.14/src /Users/jenkins/util/AFLR/aflr_lib_11.5.14/src/egads_aflr4/egads_cad_geom_idef2idef.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_idef2idef.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.14/src /Users/jenkins/util/AFLR/aflr_lib_11.5.14/src/egads_aflr4/egads_cad_geom_loopEdge.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_loopEdge.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.14/src /Users/jenkins/util/AFLR/aflr_lib_11.5.14/src/egads_aflr4/egads_cad_geom_nodeData.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_nodeData.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.14/src /Users/jenkins/util/AFLR/aflr_lib_11.5.14/src/egads_aflr4/egads_cad_geom_reset_attr.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_reset_attr.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.14/src /Users/jenkins/util/AFLR/aflr_lib_11.5.14/src/egads_aflr4/egads_cad_geom_setup.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_setup.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.14/src /Users/jenkins/util/AFLR/aflr_lib_11.5.14/src/egads_aflr4/egads_cad_geom_write_topo_data.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_write_topo_data.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.14/src /Users/jenkins/util/AFLR/aflr_lib_11.5.14/src/egads_aflr4/egads_eval_curv_at_uv.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_eval_curv_at_uv.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.14/src /Users/jenkins/util/AFLR/aflr_lib_11.5.14/src/egads_aflr4/egads_eval_edge_arclen.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_eval_edge_arclen.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.14/src /Users/jenkins/util/AFLR/aflr_lib_11.5.14/src/egads_aflr4/egads_eval_norm_at_uv.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_eval_norm_at_uv.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.14/src /Users/jenkins/util/AFLR/aflr_lib_11.5.14/src/egads_aflr4/egads_eval_uv_at_t.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_eval_uv_at_t.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.14/src /Users/jenkins/util/AFLR/aflr_lib_11.5.14/src/egads_aflr4/egads_eval_uv_at_xyz.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_eval_uv_at_xyz.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.14/src /Users/jenkins/util/AFLR/aflr_lib_11.5.14/src/egads_aflr4/egads_eval_uv_bounds.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_eval_uv_bounds.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.14/src /Users/jenkins/util/AFLR/aflr_lib_11.5.14/src/egads_aflr4/egads_eval_xyz_at_u.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_eval_xyz_at_u.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.14/src /Users/jenkins/util/AFLR/aflr_lib_11.5.14/src/egads_aflr4/egads_eval_xyz_at_uv.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_eval_xyz_at_uv.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.14/src /Users/jenkins/util/AFLR/aflr_lib_11.5.14/src/egads_aflr4/egads_face_node_map.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_face_node_map.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.14/src /Users/jenkins/util/AFLR/aflr_lib_11.5.14/src/egads_aflr4/egads_cad_geom_faceMatch.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_faceMatch.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.14/src /Users/jenkins/util/AFLR/aflr_lib_11.5.14/src/egads_aflr4/egads_data.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_data.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.14/src /Users/jenkins/util/AFLR/aflr_lib_11.5.14/src/egads_aflr4/egads_mzone.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_mzone.o touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/aflr3AIM.so rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/aflr3AIM.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/aflr3AIM.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/aflr3AIM.o \ /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/aflr3_Interface.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/EG_getEffBodyTopos.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_aflr4_check_tess_coord.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_aflr4_check_tess_ordering.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_aflr4_get_bedge_coord.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_aflr4_get_edge_spacing.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_aflr4_get_faceOrder.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_aflr4_get_face_spacing.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_aflr4_get_surf_grid.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_aflr4_create_tess.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_aflr4_tess_to_dgeom.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_aflr4_version.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_auto_cad_geom_setup.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_add_attr.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_add_ff.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_add_ret_attr.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_bodyFlag.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_check_bc.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_data_cleanup.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_edgeData.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_edgeFace.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_edit.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_faceEdge.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_faceFace.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_faceFlag.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_faceLoop.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_file_read.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_file_write.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_idef2idef.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_loopEdge.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_nodeData.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_reset_attr.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_setup.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_write_topo_data.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_eval_curv_at_uv.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_eval_edge_arclen.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_eval_norm_at_uv.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_eval_uv_at_t.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_eval_uv_at_xyz.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_eval_uv_bounds.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_eval_xyz_at_u.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_eval_xyz_at_uv.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_face_node_map.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_faceMatch.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_data.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_mzone.o -L/Users/jenkins/util/AFLR/aflr_lib_11.5.14/MacOSX-arm64/lib \ -laflr3 -laflr43 -laflr4 -lsurf_auto_cpp -lsurf_auto -lrec3 -lug_mp -lanbl3 -laflr2c -lrec2 -lbl1 -lotb -legen -lice2 -lice3 -ldftr2 -ldftr3 -ldgeom -lug_io -lug_gq -lug_cpp -lcgns -lqtb -lug3 -lug -lug2 -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lutils \ -laimUtil -locsm -legads -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lc++ -lm /Library/Developer/CommandLineTools/usr/bin/make -C aflr4 clang -g -target arm64-apple-darwin -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.14/src aflr4_version.c \ -L/Users/jenkins/util/AFLR/aflr_lib_11.5.14/MacOSX-arm64/lib -laflr4 -lm \ -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/aflr4_version /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/aflr4_version clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.14/src -I../utils aflr4AIM.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/aflr4AIM.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.14/src \ -I../utils aflr4_Interface.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/aflr4_Interface.o touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/aflr4AIM.so rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/aflr4AIM.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/aflr4AIM.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/aflr4AIM.o \ /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/aflr4_Interface.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/EG_getEffBodyTopos.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_aflr4_check_tess_coord.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_aflr4_check_tess_ordering.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_aflr4_get_bedge_coord.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_aflr4_get_edge_spacing.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_aflr4_get_faceOrder.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_aflr4_get_face_spacing.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_aflr4_get_surf_grid.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_aflr4_create_tess.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_aflr4_tess_to_dgeom.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_aflr4_version.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_auto_cad_geom_setup.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_add_attr.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_add_ff.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_add_ret_attr.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_bodyFlag.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_check_bc.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_data_cleanup.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_edgeData.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_edgeFace.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_edit.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_faceEdge.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_faceFace.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_faceFlag.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_faceLoop.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_file_read.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_file_write.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_idef2idef.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_loopEdge.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_nodeData.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_reset_attr.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_setup.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_write_topo_data.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_eval_curv_at_uv.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_eval_edge_arclen.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_eval_norm_at_uv.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_eval_uv_at_t.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_eval_uv_at_xyz.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_eval_uv_bounds.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_eval_xyz_at_u.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_eval_xyz_at_uv.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_face_node_map.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_faceMatch.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_data.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_mzone.o -L/Users/jenkins/util/AFLR/aflr_lib_11.5.14/MacOSX-arm64/lib \ -laflr4 -laflr2c -lsurf_auto -lsurf_auto_cpp -laflr3 -legen -lrec2 -lrec3 -ldftr3 -ldftr2 -ldgeom -lotb -lqtb -lice2 -lice3 -lug3 -lug2 -lug -lug_mp -lug_gq -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lutils \ -laimUtil -locsm -legads -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lc++ -lm /Library/Developer/CommandLineTools/usr/bin/make -C astros clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../utils astrosAIM.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/astrosAIM.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../utils astrosUtils.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/astrosUtils.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../utils astrosCards.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/astrosCards.o clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/astrosAIM.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/astrosAIM.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/astrosUtils.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/astrosCards.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm -L/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11 -ldl -framework CoreFoundation -Wl,-w /Library/Developer/CommandLineTools/usr/bin/make -C avl clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../utils avlAIM.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/avlAIM.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_BODY.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/avlRead_BODY.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_CNC.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/avlRead_CNC.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_CPOML.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/avlRead_CPOML.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_DERMATB.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/avlRead_DERMATB.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_DERMATM.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/avlRead_DERMATM.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_DERMATS.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/avlRead_DERMATS.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_ELE.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/avlRead_ELE.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_HINGE.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/avlRead_HINGE.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_STRP.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/avlRead_STRP.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_SURF.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/avlRead_SURF.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_TOT.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/avlRead_TOT.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_VM.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/avlRead_VM.o touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/avlAIM.so rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/avlAIM.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/avlAIM.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/avlAIM.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/avlRead_BODY.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/avlRead_CNC.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/avlRead_CPOML.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/avlRead_DERMATB.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/avlRead_DERMATM.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/avlRead_DERMATS.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/avlRead_ELE.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/avlRead_HINGE.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/avlRead_STRP.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/avlRead_SURF.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/avlRead_TOT.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/avlRead_VM.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -laimUtil -lutils -locsm -legads -ludunits2 -ldl \ -lc++ -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm /Library/Developer/CommandLineTools/usr/bin/make -C awave clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../utils awaveAIM.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/awaveAIM.o clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/awaveAIM.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/awaveAIM.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm gfortran -g -c -O -frecursive -fcray-pointer -std=legacy awavemod.f -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/awave.o gfortran -g -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/test/awave /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/awave.o -static-libgfortran -static-libgcc -Wl,-w /Library/Developer/CommandLineTools/usr/bin/make -C cart3d clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -DCAPS_MESHUTILS -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../utils -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include/libCart3D -I./xddm \ cart3dAIM.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/cart3dAIM.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include/c3dio \ -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include/libCart3D -I./xddm \ writeTrix.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/writeTrix.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include/c3dio \ -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include/libCart3D \ surfTrix.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/surfTrix.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -pedantic -I./xddm -I. \ `xml2-config --cflags` ./xddm/xddm.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/xddm.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include bodyTess.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/bodyTess.o clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/cart3dAIM.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/cart3dAIM.o \ /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/writeTrix.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/surfTrix.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/xddm.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/bodyTess.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lutils \ -laimUtil -locsm -legads -ludunits2 -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include/ \ -lc3dio -lCart3D -ldl -L/Library/Developer/CommandLineTools/SDKs/MacOSX.sdk/usr/lib -lxml2 -lz -licucore -Wl,-no_compact_unwind -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include cart3dTest.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/cart3dTest.o clang -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/test/cart3dTest /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/cart3dTest.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lcaps -locsm -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm -ldl clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I./xddm \ -I. `xml2-config --cflags` ESPxddm.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/ESPxddm.o clang -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/bin/ESPxddm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/ESPxddm.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/writeTrix.o \ /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/surfTrix.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/xddm.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/bodyTess.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads \ -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include/ -lc3dio -lCart3D \ -lpthread -ldl -Wl,-rpath,/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -Wl,-rpath,@loader_path/ -Wl,-rpath,/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -L/Library/Developer/CommandLineTools/SDKs/MacOSX.sdk/usr/lib -lxml2 -lz -licucore -Wl,-no_compact_unwind -lm /Library/Developer/CommandLineTools/usr/bin/make -C cbaero clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../utils -I../meshWriter/fastWriter cbaeroAIM.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/cbaeroAIM.o clang -g -target arm64-apple-darwin -bundle /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/cbaeroAIM.o -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/cbaeroAIM.so -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lutils -laimUtil -locsm -legads -ludunits2 -lm -ldl /Library/Developer/CommandLineTools/usr/bin/make -C cgt clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include egads2cgt.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads2cgt.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include aflr4egads.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/aflr4egads.o clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/test/egads2cgt /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads2cgt.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/aflr4egads.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads -lcaps -locsm -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm -ldl /Library/Developer/CommandLineTools/usr/bin/make -C custom make[2]: Nothing to be done for `default'. /Library/Developer/CommandLineTools/usr/bin/make -C delaundo clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../utils delaundoAIM.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/delaundoAIM.o touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/delaundoAIM.so rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/delaundoAIM.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/delaundoAIM.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/delaundoAIM.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl \ -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm /Library/Developer/CommandLineTools/usr/bin/make -C egadsTess clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../utils egadsTessAIM.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egadsTessAIM.o touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/egadsTessAIM.so rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/egadsTessAIM.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/egadsTessAIM.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egadsTessAIM.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl \ -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm /Library/Developer/CommandLineTools/usr/bin/make -C friction clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -Wno-format -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../utils frictionAIM.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/frictionAIM.o clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/frictionAIM.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/frictionAIM.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm gfortran -g -c -O -frecursive -fcray-pointer friction_eja_mod.f -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/friction.o gfortran -g -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/test/friction /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/friction.o -static-libgfortran -static-libgcc -Wl,-w /Library/Developer/CommandLineTools/usr/bin/make -C fun3d clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -DHAVE_PYTHON -DCYTHON_PEP489_MULTI_PHASE_INIT=0 \ -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../utils -I../meshWriter/ugridWriter \ -I. -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython fun3dAIM.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/fun3dAIM.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../utils -I../meshWriter/ugridWriter \ fun3dUtils.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/fun3dUtils.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -DCYTHON_PEP489_MULTI_PHASE_INIT=0 \ -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../utils \ -I. -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 cython/fun3dNamelist.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/fun3dNamelist.o Building FUN3D with Python clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/fun3dAIM.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/fun3dAIM.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/fun3dUtils.o \ /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/fun3dNamelist.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lutils -laimUtil -locsm \ -legads -ludunits2 -ldl -L/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11 -ldl -framework CoreFoundation -Wl,-w -lm -Wl,-rpath /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib /Library/Developer/CommandLineTools/usr/bin/make -C hsm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../utils hsmAIM.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/hsmAIM.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../utils hsmUtils.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/hsmUtils.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../utils hsmAdj.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/hsmAdj.o clang++ -g -target arm64-apple-darwin -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -ffp-model=strict -Wno-comment rcm/rcm.cpp -DREVISION=7.7 \ -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/rcm.o clang++ -g -target arm64-apple-darwin -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -ffp-model=strict rcm/genrcmi.cpp -DREVISION=7.7 \ -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/genrcmi.o /Library/Developer/CommandLineTools/usr/bin/make -C src atanc.o gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero atanc.f -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/atanc.o /Library/Developer/CommandLineTools/usr/bin/make -C src bmdump.o gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero bmdump.f -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/bmdump.o /Library/Developer/CommandLineTools/usr/bin/make -C src cross.o gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero cross.f -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/cross.o /Library/Developer/CommandLineTools/usr/bin/make -C src hsmabd.o gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmabd.f -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/hsmabd.o /Library/Developer/CommandLineTools/usr/bin/make -C src hsmbb2.o gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmbb2.f -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/hsmbb2.o /Library/Developer/CommandLineTools/usr/bin/make -C src hsmbc.o gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmbc.f -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/hsmbc.o /Library/Developer/CommandLineTools/usr/bin/make -C src hsmdep.o gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmdep.f -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/hsmdep.o /Library/Developer/CommandLineTools/usr/bin/make -C src hsmeqn.o gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmeqn.f -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/hsmeqn.o /Library/Developer/CommandLineTools/usr/bin/make -C src hsmgeo.o gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmgeo.f -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/hsmgeo.o /Library/Developer/CommandLineTools/usr/bin/make -C src hsmglr.o gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmglr.f -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/hsmglr.o /Library/Developer/CommandLineTools/usr/bin/make -C src hsmout.o gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmout.f -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/hsmout.o /Library/Developer/CommandLineTools/usr/bin/make -C src hsmprj.o gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmprj.f -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/hsmprj.o /Library/Developer/CommandLineTools/usr/bin/make -C src hsmre1.o gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmre1.f -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/hsmre1.o /Library/Developer/CommandLineTools/usr/bin/make -C src hsmren.o gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmren.f -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/hsmren.o /Library/Developer/CommandLineTools/usr/bin/make -C src hsmrfm.o gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmrfm.f -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/hsmrfm.o /Library/Developer/CommandLineTools/usr/bin/make -C src hsmrun.o gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero -fno-recursive hsmrun.f -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/hsmrun.o /Library/Developer/CommandLineTools/usr/bin/make -C src hsmsol.o gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmsol.f -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/hsmsol.o /Library/Developer/CommandLineTools/usr/bin/make -C src ludcmp.o gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero ludcmp.f -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/ludcmp.o /Library/Developer/CommandLineTools/usr/bin/make -C src sbsolve.o gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero sbsolve.f -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/sbsolve.o /Library/Developer/CommandLineTools/usr/bin/make -C src /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libhsm.a touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libhsm.a rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libhsm.a (cd /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj; ar -rs /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libhsm.a hsmsol.o hsmdep.o hsmout.o hsmgeo.o hsmabd.o hsmeqn.o hsmbc.o hsmprj.o hsmren.o hsmre1.o hsmrfm.o hsmbb2.o hsmglr.o ludcmp.o sbsolve.o atanc.o bmdump.o cross.o ) ar: creating archive /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libhsm.a touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/hsmAIM.so rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/hsmAIM.so gfortran -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/hsmAIM.so \ /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/hsmAIM.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/hsmUtils.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/hsmAdj.o \ /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/rcm.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/genrcmi.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lutils -laimUtil -locsm \ -legads -ludunits2 -lhsm -ldl -Wl,-rpath,/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -Wl,-rpath,@loader_path/ -Wl,-rpath,/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lc++ -static-libgfortran -static-libgcc -Wl,-w /Library/Developer/CommandLineTools/usr/bin/make -C interference clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include interferenceAIM.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/interferenceAIM.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. cloudFns.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/cloudFns.o touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/interferenceAIM.so rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/interferenceAIM.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/interferenceAIM.so \ /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/interferenceAIM.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/cloudFns.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib \ -laimUtil -locsm -legads -ludunits2 -ldl -lc++ -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm /Library/Developer/CommandLineTools/usr/bin/make -C jfd3 clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../utils jfd3AIM.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/jfd3AIM.o clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/jfd3AIM.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/jfd3AIM.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm /Library/Developer/CommandLineTools/usr/bin/make -C masstran clang++ -g -target arm64-apple-darwin -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -ffp-model=strict -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../utils masstranAIM.cpp \ -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/masstranAIM.o clang++ -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/masstranAIM.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/masstranAIM.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm /Library/Developer/CommandLineTools/usr/bin/make -C meshWriter /Library/Developer/CommandLineTools/usr/bin/make -C bstlWriter clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include bstlWriter.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/bstlWriter.o clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/bstlWriter.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/bstlWriter.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -laimUtil -legads -locsm -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm /Library/Developer/CommandLineTools/usr/bin/make -C bvtkWriter clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include bvtkWriter.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/bvtkWriter.o clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/bvtkWriter.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/bvtkWriter.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -laimUtil -legads -locsm -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm /Library/Developer/CommandLineTools/usr/bin/make -C exodusWriter clang++ -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -std=c++11 -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I/Users/jenkins/util/sandialabs/seacas/include -I/opt/homebrew/include exodusWriter.cpp \ -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/exodusWriter.o clang++ -g -target arm64-apple-darwin -bundle -std=c++11 -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/exodusWriter.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/exodusWriter.o \ -L/Users/jenkins/util/sandialabs/seacas/lib -lexodus -Wl,-rpath /Users/jenkins/util/sandialabs/seacas/lib -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -laimUtil -legads -locsm -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm /Library/Developer/CommandLineTools/usr/bin/make -C fastWriter clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include fastWriter.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/fastWriter.o clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/fastWriter.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/fastWriter.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -laimUtil -legads -locsm -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm /Library/Developer/CommandLineTools/usr/bin/make -C libmeshbWriter clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include libmeshbWriter.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/libmeshbWriter.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -IlibMeshb/sources -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include libMeshb/sources/libmeshb7.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/libmeshb7.o clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libmeshbWriter.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/libmeshbWriter.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/libmeshb7.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -laimUtil -legads -locsm -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm /Library/Developer/CommandLineTools/usr/bin/make -C stlWriter clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include stlWriter.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/stlWriter.o clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/stlWriter.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/stlWriter.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -laimUtil -legads -locsm -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm /Library/Developer/CommandLineTools/usr/bin/make -C su2Writer clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include su2Writer.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/su2Writer.o clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/su2Writer.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/su2Writer.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -laimUtil -legads -locsm -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm /Library/Developer/CommandLineTools/usr/bin/make -C tecplotWriter clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include tecplotWriter.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/tecplotWriter.o clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/tecplotWriter.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/tecplotWriter.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -laimUtil -legads -locsm -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm /Library/Developer/CommandLineTools/usr/bin/make -C ugridWriter clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include ugridWriter.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/ugridWriter.o clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/ugridWriter.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/ugridWriter.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -laimUtil -legads -locsm -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm /Library/Developer/CommandLineTools/usr/bin/make -C vtkWriter clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include vtkWriter.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/vtkWriter.o clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/vtkWriter.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/vtkWriter.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -laimUtil -legads -locsm -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm /Library/Developer/CommandLineTools/usr/bin/make -C mses clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../utils msesAIM.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/msesAIM.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../utils msesUtils.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/msesUtils.o clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/msesAIM.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/msesAIM.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/msesUtils.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm /Library/Developer/CommandLineTools/usr/bin/make -C mystran clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../utils mystranAIM.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/mystranAIM.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../utils mystranUtils.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/mystranUtils.o clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/mystranAIM.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/mystranAIM.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/mystranUtils.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm -L/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11 -ldl -framework CoreFoundation -Wl,-w /Library/Developer/CommandLineTools/usr/bin/make -C nastran clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../utils nastranAIM.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/nastranAIM.o clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/nastranAIM.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/nastranAIM.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm -L/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11 -ldl -framework CoreFoundation -Wl,-w /Library/Developer/CommandLineTools/usr/bin/make -C plato clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../meshWriter/exodusWriter -I../utils -I/Users/jenkins/util/sandialabs/seacas/include -I/opt/homebrew/include platoAIM.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/platoAIM.o clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/platoAIM.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/platoAIM.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib \ -L/Users/jenkins/util/sandialabs/seacas/lib -lexodus -Wl,-rpath /Users/jenkins/util/sandialabs/seacas/lib \ -laimUtil -locsm -legads -ludunits2 -ldl -lm /Library/Developer/CommandLineTools/usr/bin/make -C pointwise clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../utils pointwiseAIM.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/pointwiseAIM.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../utils hashElement.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/hashElement.o touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/pointwiseAIM.so rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/pointwiseAIM.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/pointwiseAIM.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/pointwiseAIM.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/hashElement.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl \ -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm -lpthread /Library/Developer/CommandLineTools/usr/bin/make -C refine clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../utils -I../meshWriter/libmeshbWriter refineAIM.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/refineAIM.o touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/refineAIM.so rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/refineAIM.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/refineAIM.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/refineAIM.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/libmeshb7.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl \ -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm /Library/Developer/CommandLineTools/usr/bin/make -C sierraSD clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../meshWriter/exodusWriter -I../utils -I/Users/jenkins/util/sandialabs/seacas/include -I/opt/homebrew/include sierraSDAIM.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/sierraSDAIM.o clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/sierraSDAIM.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/sierraSDAIM.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib \ -L/Users/jenkins/util/sandialabs/seacas/lib -lexodus -Wl,-rpath /Users/jenkins/util/sandialabs/seacas/lib \ -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm /Library/Developer/CommandLineTools/usr/bin/make -C sierraSM clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../meshWriter/exodusWriter -I../utils -I/Users/jenkins/util/sandialabs/seacas/include -I/opt/homebrew/include sierraSMAIM.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/sierraSMAIM.o clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/sierraSMAIM.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/sierraSMAIM.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib \ -L/Users/jenkins/util/sandialabs/seacas/lib -lexodus -Wl,-rpath /Users/jenkins/util/sandialabs/seacas/lib \ -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm /Library/Developer/CommandLineTools/usr/bin/make -C skeleton clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../utils skeletonAIM.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/skeletonAIM.o clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/skeletonAIM.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/skeletonAIM.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm /Library/Developer/CommandLineTools/usr/bin/make -C spinnaker clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include \ -I../meshWriter/exodusWriter \ -I../meshWriter/libmeshbWriter \ -I../utils -I/Users/jenkins/util/sandialabs/seacas/include \ -I/opt/homebrew/include \ spinnakerAIM.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/spinnakerAIM.o clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/spinnakerAIM.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/spinnakerAIM.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/libmeshb7.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib \ -L/Users/jenkins/util/sandialabs/seacas/lib -lexodus -Wl,-rpath /Users/jenkins/util/sandialabs/seacas/lib \ -laimUtil -locsm -legads -ludunits2 -ldl -lm /Library/Developer/CommandLineTools/usr/bin/make -C su2 clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../meshWriter/su2Writer -I../utils su2AIM.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/su2AIM.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../utils su2Utils.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/su2Utils.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../utils su2_4_Cardinal.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/su2_4_Cardinal.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../utils su2_5_Raven.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/su2_5_Raven.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../utils su2_6_Falcon.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/su2_6_Falcon.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../utils su2_7_Blackbird.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/su2_7_Blackbird.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../utils su2_801_Harrier.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/su2_801_Harrier.o clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/su2AIM.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/su2AIM.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/su2Utils.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/su2_4_Cardinal.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/su2_5_Raven.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/su2_6_Falcon.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/su2_7_Blackbird.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/su2_801_Harrier.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm /Library/Developer/CommandLineTools/usr/bin/make -C tacs clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../utils tacsAIM.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/tacsAIM.o clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/tacsAIM.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/tacsAIM.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm -L/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11 -ldl -framework CoreFoundation -Wl,-w /Library/Developer/CommandLineTools/usr/bin/make -C tetgen clang++ -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../utils tetgenAIM.cpp \ -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/tetgenAIM.o clang++ -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I/Users/jenkins/util/tetgen/tetgen1.6.0 -I../utils \ -DTETLIBRARY tetgen_Interface.cpp -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/tetgen_Interface.o clang++ -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DTETLIBRARY -w /Users/jenkins/util/tetgen/tetgen1.6.0/tetgen.cxx -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/tetgen.o clang++ -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -O0 -w /Users/jenkins/util/tetgen/tetgen1.6.0/predicates.cxx -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/predicates.o clang++ -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/tetgenAIM.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/tetgenAIM.o \ /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/tetgen_Interface.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/tetgen.o \ /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/predicates.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lutils -laimUtil -locsm \ -legads -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm /Library/Developer/CommandLineTools/usr/bin/make -C tsfoil clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../utils \ tsfoilAIM.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/tsfoilAIM.o clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/tsfoilAIM.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/tsfoilAIM.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm /Library/Developer/CommandLineTools/usr/bin/make -C unitTest mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/aimUnitTest mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/aimUnitTest/pyCAPS cp -p -f pyCAPS/Mesh_Formats.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/aimUnitTest/pyCAPS/Mesh_Formats.py cp -p -f pyCAPS/test_aflr2.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/aimUnitTest/pyCAPS/test_aflr2.py cp -p -f pyCAPS/test_aflr3.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/aimUnitTest/pyCAPS/test_aflr3.py cp -p -f pyCAPS/test_aflr4.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/aimUnitTest/pyCAPS/test_aflr4.py cp -p -f pyCAPS/test_astros.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/aimUnitTest/pyCAPS/test_astros.py cp -p -f pyCAPS/test_avl.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/aimUnitTest/pyCAPS/test_avl.py cp -p -f pyCAPS/test_cart3d.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/aimUnitTest/pyCAPS/test_cart3d.py cp -p -f pyCAPS/test_cbaero.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/aimUnitTest/pyCAPS/test_cbaero.py cp -p -f pyCAPS/test_egadsTess.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/aimUnitTest/pyCAPS/test_egadsTess.py cp -p -f pyCAPS/test_fun3d.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/aimUnitTest/pyCAPS/test_fun3d.py cp -p -f pyCAPS/test_masstran.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/aimUnitTest/pyCAPS/test_masstran.py cp -p -f pyCAPS/test_mses.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/aimUnitTest/pyCAPS/test_mses.py cp -p -f pyCAPS/test_pointwise.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/aimUnitTest/pyCAPS/test_pointwise.py cp -p -f pyCAPS/test_refine.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/aimUnitTest/pyCAPS/test_refine.py cp -p -f pyCAPS/test_su2.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/aimUnitTest/pyCAPS/test_su2.py cp -p -f pyCAPS/test_tacs.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/aimUnitTest/pyCAPS/test_tacs.py cp -p -f pyCAPS/test_tetgen.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/aimUnitTest/pyCAPS/test_tetgen.py cp -p -f pyCAPS/test_xfoil.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/aimUnitTest/pyCAPS/test_xfoil.py cp -p -f pyCAPS/test_zaero.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/aimUnitTest/pyCAPS/test_zaero.py cp -p -f pyCAPS/Makefile /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/aimUnitTest/pyCAPS/Makefile mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/aimUnitTest/csmData cp -p -f csmData/airfoilSection.csm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/aimUnitTest/csmData/airfoilSection.csm cp -p -f csmData/avlSections.csm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/aimUnitTest/csmData/avlSections.csm cp -p -f csmData/cfd2D.csm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/aimUnitTest/csmData/cfd2D.csm cp -p -f csmData/cfdMultiBody.csm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/aimUnitTest/csmData/cfdMultiBody.csm cp -p -f csmData/cfdSingleBody.csm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/aimUnitTest/csmData/cfdSingleBody.csm cp -p -f csmData/cornerGeom.csm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/aimUnitTest/csmData/cornerGeom.csm cp -p -f csmData/feaSimplePlate.csm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/aimUnitTest/csmData/feaSimplePlate.csm cp -p -f csmData/feaWingBEMAero.csm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/aimUnitTest/csmData/feaWingBEMAero.csm cp -p -f csmData/feaWingOMLAero.csm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/aimUnitTest/csmData/feaWingOMLAero.csm cp -p -f csmData/kulfanSection.csm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/aimUnitTest/csmData/kulfanSection.csm cp -p -f csmData/kulfanSymmetricSection.csm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/aimUnitTest/csmData/kulfanSymmetricSection.csm cp -p -f csmData/masstran.csm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/aimUnitTest/csmData/masstran.csm cp -p -f csmData/multiRegions.csm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/aimUnitTest/csmData/multiRegions.csm mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/aimUnitTest/cCAPS /Library/Developer/CommandLineTools/usr/bin/make -C xfoil clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../utils \ xfoilAIM.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/xfoilAIM.o clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/xfoilAIM.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/xfoilAIM.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm /Library/Developer/CommandLineTools/usr/bin/make -C zaero clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../utils zaeroAIM.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/zaeroAIM.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../utils zaeroUtils.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/zaeroUtils.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../utils zaeroLinearFlutter.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/zaeroLinearFlutter.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../utils zaeroTrim.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/zaeroTrim.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../utils zaeroTypes.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/zaeroTypes.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../utils zaeroCards.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/zaeroCards.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../utils zaeroGeneral.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/zaeroGeneral.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../utils zaeroGraphical.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/zaeroGraphical.o clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/zaeroAIM.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/zaeroAIM.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/zaeroUtils.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/zaeroLinearFlutter.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/zaeroTrim.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/zaeroTypes.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/zaeroCards.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/zaeroGeneral.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/zaeroGraphical.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lutils -laimUtil -locsm -legads -ludunits2 -lm -ldl (cd Slugs/src; make) clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. Slugs.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/Slugs.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. Fitter.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/Fitter.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. RedBlackTree.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/RedBlackTree.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. Tessellate.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/Tessellate.o clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/bin/Slugs /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/Slugs.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/Fitter.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/RedBlackTree.o \ /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/Tessellate.o -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lwsserver -legads \ -lpthread -lz -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. TestFit.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/TestFit.o clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/bin/TestFit /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/TestFit.o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/Fitter.o -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads \ -lpthread -lz -lm (cd test; make -f aim.make) clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include aim.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/aim.o clang -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/test/aim /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/aim.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lcaps -locsm -legads \ -lwsserver -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib cp -p -f testingAIM.csm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/test/testingAIM.csm (cd test; make -f autoExec.make) clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include autoExec.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/autoExec.o clang -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/test/autoExec /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/autoExec.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lcaps -locsm \ -legads -lwsserver -lpthread -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lz -lm -ldl (cd test; make -f newPhase.make) clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include newPhase.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/newPhase.o clang -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/test/newPhase /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/newPhase.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib \ -lcaps -locsm -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm -ldl (cd test; make -f basic.make) clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include basic.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/basic.o clang -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/test/basic /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/basic.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lcaps -locsm -legads\ -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm -ldl (cd test; make -f geomIn.make) clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include geomIn.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/geomIn.o clang -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/test/geomIn /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/geomIn.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lcaps -locsm -legads\ -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm -ldl (cd test; make -f utilsTest.make) clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include aimTransferUtilTest.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/aimTransferUtilTest.o clang -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/test/aimTransferUtilTest /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/aimTransferUtilTest.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lcaps -laimUtil -locsm -legads \ -lpthread -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -ludunits2 -lm -ldl clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../aim/utils miscUtilsTest.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/miscUtilsTest.o clang -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/test/miscUtilsTest /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/miscUtilsTest.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -laimUtil -locsm -legads \ -lpthread -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -ludunits2 -lm -ldl clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../aim/utils vlmUtilsTest.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/vlmUtilsTest.o clang -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/test/vlmUtilsTest /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/vlmUtilsTest.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lutils -laimUtil -locsm -legads \ -lpthread -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -ludunits2 -lm -ldl (cd test; make -f vVS.make) clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include vVS.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/vVS.o clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/test/vVS /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/vVS.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lwsserver -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib (cd examples; make) mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/analysisData mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/csmData mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/cCAPS mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/corsairlite cp -p -f pyCAPS/abaqus_AGARD445_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/abaqus_AGARD445_PyTest.py cp -p -f pyCAPS/abaqus_SingleLoadCase_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/abaqus_SingleLoadCase_PyTest.py cp -p -f pyCAPS/aeroelasticModal_Fun3D_and_Astros.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/aeroelasticModal_Fun3D_and_Astros.py cp -p -f pyCAPS/aeroelasticModal_Fun3D_and_Mystran.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/aeroelasticModal_Fun3D_and_Mystran.py cp -p -f pyCAPS/aeroelasticModal_Fun3D_and_Nastran.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/aeroelasticModal_Fun3D_and_Nastran.py cp -p -f pyCAPS/aeroelasticSimple_Displacement_Fun3D_and_Mystran.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/aeroelasticSimple_Displacement_Fun3D_and_Mystran.py cp -p -f pyCAPS/aeroelasticSimple_Displacement_SU2_and_Astros.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/aeroelasticSimple_Displacement_SU2_and_Astros.py cp -p -f pyCAPS/aeroelasticSimple_Displacement_SU2_and_Mystran.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/aeroelasticSimple_Displacement_SU2_and_Mystran.py cp -p -f pyCAPS/aeroelasticSimple_Iterative_Cart3D_and_Mystran.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/aeroelasticSimple_Iterative_Cart3D_and_Mystran.py cp -p -f pyCAPS/aeroelasticSimple_Iterative_Fun3D_and_Mystran.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/aeroelasticSimple_Iterative_Fun3D_and_Mystran.py cp -p -f pyCAPS/aeroelasticSimple_Iterative_SU2_and_Astros.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/aeroelasticSimple_Iterative_SU2_and_Astros.py cp -p -f pyCAPS/aeroelasticSimple_Iterative_SU2_and_Mystran.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/aeroelasticSimple_Iterative_SU2_and_Mystran.py cp -p -f pyCAPS/aeroelasticSimple_Pressure_Fun3D_and_Mystran.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/aeroelasticSimple_Pressure_Fun3D_and_Mystran.py cp -p -f pyCAPS/aeroelasticSimple_Pressure_SU2_and_Astros.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/aeroelasticSimple_Pressure_SU2_and_Astros.py cp -p -f pyCAPS/aeroelasticSimple_Pressure_SU2_and_Mystran.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/aeroelasticSimple_Pressure_SU2_and_Mystran.py cp -p -f pyCAPS/aeroelasticSimple_Temperature_SU2_and_TACS.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/aeroelasticSimple_Temperature_SU2_and_TACS.py cp -p -f pyCAPS/aeroelastic_Iterative_Fun3D_and_Mystran.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/aeroelastic_Iterative_Fun3D_and_Mystran.py cp -p -f pyCAPS/aeroelastic_Iterative_SU2_and_Astros.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/aeroelastic_Iterative_SU2_and_Astros.py cp -p -f pyCAPS/aeroelastic_Iterative_SU2_and_Mystran.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/aeroelastic_Iterative_SU2_and_Mystran.py cp -p -f pyCAPS/aflr2_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/aflr2_PyTest.py cp -p -f pyCAPS/aflr4_Generic_Missile.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/aflr4_Generic_Missile.py cp -p -f pyCAPS/aflr4_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/aflr4_PyTest.py cp -p -f pyCAPS/aflr4_QuadMesh_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/aflr4_QuadMesh_PyTest.py cp -p -f pyCAPS/aflr4_Symmetry_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/aflr4_Symmetry_PyTest.py cp -p -f pyCAPS/aflr4_TipTreat_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/aflr4_TipTreat_PyTest.py cp -p -f pyCAPS/aflr4_and_Tetgen_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/aflr4_and_Tetgen_PyTest.py cp -p -f pyCAPS/aflr4_and_aflr3_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/aflr4_and_aflr3_PyTest.py cp -p -f pyCAPS/aflr4_and_aflr3_Symmetry_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/aflr4_and_aflr3_Symmetry_PyTest.py cp -p -f pyCAPS/aflr4_tetgen_Regions_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/aflr4_tetgen_Regions_PyTest.py cp -p -f pyCAPS/astros_AGARD445_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/astros_AGARD445_PyTest.py cp -p -f pyCAPS/astros_Aeroelastic_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/astros_Aeroelastic_PyTest.py cp -p -f pyCAPS/astros_CompositeWingFreq_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/astros_CompositeWingFreq_PyTest.py cp -p -f pyCAPS/astros_Composite_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/astros_Composite_PyTest.py cp -p -f pyCAPS/astros_Flutter_15degree.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/astros_Flutter_15degree.py cp -p -f pyCAPS/astros_MultipleLoadCase_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/astros_MultipleLoadCase_PyTest.py cp -p -f pyCAPS/astros_OptControl_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/astros_OptControl_PyTest.py cp -p -f pyCAPS/astros_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/astros_PyTest.py cp -p -f pyCAPS/astros_SingleLoadCase_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/astros_SingleLoadCase_PyTest.py cp -p -f pyCAPS/astros_ThreeBarFreq_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/astros_ThreeBarFreq_PyTest.py cp -p -f pyCAPS/astros_ThreeBarLinkDesign_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/astros_ThreeBarLinkDesign_PyTest.py cp -p -f pyCAPS/astros_ThreeBarMultiLoad_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/astros_ThreeBarMultiLoad_PyTest.py cp -p -f pyCAPS/astros_ThreeBar_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/astros_ThreeBar_PyTest.py cp -p -f pyCAPS/astros_Trim_15degree.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/astros_Trim_15degree.py cp -p -f pyCAPS/autoLink_Pytest.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/autoLink_Pytest.py cp -p -f pyCAPS/avl_AutoSpan_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/avl_AutoSpan_PyTest.py cp -p -f pyCAPS/avl_ControlSurf_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/avl_ControlSurf_PyTest.py cp -p -f pyCAPS/avl_DesignSweep_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/avl_DesignSweep_PyTest.py cp -p -f pyCAPS/avl_EigenValue_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/avl_EigenValue_PyTest.py cp -p -f pyCAPS/avl_OpenMDAO_3_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/avl_OpenMDAO_3_PyTest.py cp -p -f pyCAPS/avl_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/avl_PyTest.py cp -p -f pyCAPS/awave_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/awave_PyTest.py cp -p -f pyCAPS/cart3d_OpenMDAO_3_alpha_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/cart3d_OpenMDAO_3_alpha_PyTest.py cp -p -f pyCAPS/cart3d_OpenMDAO_3_twist_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/cart3d_OpenMDAO_3_twist_PyTest.py cp -p -f pyCAPS/cart3d_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/cart3d_PyTest.py cp -p -f 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/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/egadsTess_Spheres_Quad_PyTest.py cp -p -f pyCAPS/friction_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/friction_PyTest.py cp -p -f pyCAPS/fun3d_Morph_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/fun3d_Morph_PyTest.py cp -p -f pyCAPS/fun3d_OpenMDAO_3_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/fun3d_OpenMDAO_3_PyTest.py cp -p -f pyCAPS/fun3d_and_AFLR2_NodeDist_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/fun3d_and_AFLR2_NodeDist_PyTest.py cp -p -f pyCAPS/fun3d_and_AFLR2_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/fun3d_and_AFLR2_PyTest.py cp -p 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/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/csmData/feaJoinedPlate.csm cp -p -f csmData/feaSimplePlate.csm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/csmData/feaSimplePlate.csm cp -p -f csmData/feaThreeBar.csm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/csmData/feaThreeBar.csm cp -p -f csmData/feaWingBEM.csm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/csmData/feaWingBEM.csm cp -p -f csmData/feaWingBEMAero.csm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/csmData/feaWingBEMAero.csm cp -p -f csmData/frictionWingTailFuselage.csm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/csmData/frictionWingTailFuselage.csm cp -p -f csmData/generic_missile.csm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/csmData/generic_missile.csm cp -p -f csmData/interference.csm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/csmData/interference.csm cp -p -f csmData/linearAero.csm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/csmData/linearAero.csm cp -p -f csmData/nosecone1.csm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/csmData/nosecone1.csm cp -p -f csmData/regions.csm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/csmData/regions.csm cp -p -f csmData/simpleWingBox.csm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/csmData/simpleWingBox.csm cp -p -f csmData/spheres.csm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/csmData/spheres.csm cp -p -f csmData/table.csm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/csmData/table.csm cp -p -f csmData/tiptreat.csm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/csmData/tiptreat.csm cp -p -f csmData/avlWing.udc /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/csmData/avlWing.udc mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/analysisData/nastran cp -p -f analysisData/nastran/NastranAeroWingBEM.f06 /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/analysisData/nastran/NastranAeroWingBEM.f06 cp -p -f analysisData/nastran/NastranCompositePlate.f06 /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/analysisData/nastran/NastranCompositePlate.f06 cp -p -f analysisData/nastran/NastranCompositeWing_Design.f06 /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/analysisData/nastran/NastranCompositeWing_Design.f06 cp -p -f analysisData/nastran/NastranCompositeWing_Freq.f06 /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/analysisData/nastran/NastranCompositeWing_Freq.f06 cp -p -f analysisData/nastran/NastranFlutter15Deg.f06 /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/analysisData/nastran/NastranFlutter15Deg.f06 cp -p -f analysisData/nastran/NastranMiscLoadPlate.f06 /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/analysisData/nastran/NastranMiscLoadPlate.f06 cp -p -f analysisData/nastran/NastranModalAGARD445.f06 /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/analysisData/nastran/NastranModalAGARD445.f06 cp -p -f analysisData/nastran/NastranMultiLoadPlate.f06 /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/analysisData/nastran/NastranMultiLoadPlate.f06 cp -p -f analysisData/nastran/NastranOptMultiLoadPlate.f06 /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/analysisData/nastran/NastranOptMultiLoadPlate.f06 cp -p -f analysisData/nastran/NastranSingleLoadPlate.f06 /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/analysisData/nastran/NastranSingleLoadPlate.f06 cp -p -f analysisData/nastran/NastranThreeBar.f06 /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/analysisData/nastran/NastranThreeBar.f06 cp -p -f analysisData/nastran/NastranThreeBarDesign.f06 /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/analysisData/nastran/NastranThreeBarDesign.f06 cp -p -f analysisData/nastran/NastranThreeBarFreq.f06 /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/analysisData/nastran/NastranThreeBarFreq.f06 cp -p -f analysisData/nastran/NastranThreeBarLinkDesign.f06 /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/analysisData/nastran/NastranThreeBarLinkDesign.f06 cp -p -f analysisData/nastran/NastranThreeBarMultiLoad.f06 /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/analysisData/nastran/NastranThreeBarMultiLoad.f06 cp -p -f analysisData/nastran/NastranTrim15Deg.f06 /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/analysisData/nastran/NastranTrim15Deg.f06 cp -p -f analysisData/nastran/NastranWingBEM.f06 /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/analysisData/nastran/NastranWingBEM.f06 mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/corsairlite/capsPhase/csm mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/corsairlite/capsPhase/pyCAPS mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/corsairlite/multifidelity/csm mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/corsairlite/multifidelity/pyCAPS cp -p -f corsairlite/boydBox.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/corsairlite/boydBox.py cp -p -f corsairlite/gp.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/corsairlite/gp.py cp -p -f corsairlite/hoburg_blackbox.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/corsairlite/hoburg_blackbox.py cp -p -f corsairlite/hoburg_gp.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/corsairlite/hoburg_gp.py cp -p -f corsairlite/qp.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/corsairlite/qp.py cp -p -f corsairlite/sp.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/corsairlite/sp.py cp -p -f corsairlite/capsPhase/csm/wing1.csm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/corsairlite/capsPhase/csm/wing1.csm cp -p -f corsairlite/capsPhase/csm/wing2.csm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/corsairlite/capsPhase/csm/wing2.csm cp -p -f corsairlite/capsPhase/pyCAPS/optTaperAvl.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/corsairlite/capsPhase/pyCAPS/optTaperAvl.py cp -p -f corsairlite/capsPhase/pyCAPS/optWingAvl.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/corsairlite/capsPhase/pyCAPS/optWingAvl.py cp -p -f corsairlite/capsPhase/pyCAPS/sizeWing.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/corsairlite/capsPhase/pyCAPS/sizeWing.py cp -p -f corsairlite/multifidelity/csm/naca.csm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/corsairlite/multifidelity/csm/naca.csm cp -p -f corsairlite/multifidelity/pyCAPS/CMConstraint.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/corsairlite/multifidelity/pyCAPS/CMConstraint.py cp -p -f corsairlite/multifidelity/pyCAPS/Camber.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/corsairlite/multifidelity/pyCAPS/Camber.py cp -p -f corsairlite/multifidelity/pyCAPS/FlowTrip.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/corsairlite/multifidelity/pyCAPS/FlowTrip.py cp -p -f corsairlite/multifidelity/pyCAPS/GPSize.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/corsairlite/multifidelity/pyCAPS/GPSize.py cp -p -f corsairlite/multifidelity/pyCAPS/Kulfan2.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/corsairlite/multifidelity/pyCAPS/Kulfan2.py cp -p -f corsairlite/multifidelity/pyCAPS/Kulfan4.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/corsairlite/multifidelity/pyCAPS/Kulfan4.py cp -p -f corsairlite/multifidelity/pyCAPS/MSES.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/corsairlite/multifidelity/pyCAPS/MSES.py cp -p -f corsairlite/multifidelity/pyCAPS/fullModelKulfan.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/corsairlite/multifidelity/pyCAPS/fullModelKulfan.py cp -p -f corsairlite/multifidelity/pyCAPS/fullModelNACA.py /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/corsairlite/multifidelity/pyCAPS/fullModelNACA.py cp -p -f regressionTest/execute_CTestRegression.sh /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/execute_CTestRegression.sh cp -p -f regressionTest/execute_PyTestRegression.sh /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/execute_PyTestRegression.sh (make -C cCAPS -f aeroelastic_SU2.make) clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include aeroelasticSimple_Iterative_SU2_and_MystranTest.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/aeroelasticSimple_Iterative_SU2_and_MystranTest.o clang -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/cCAPS/aeroelasticSimple_Iterative_SU2_and_MystranTest /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/aeroelasticSimple_Iterative_SU2_and_MystranTest.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lcaps -locsm -legads \ -ludunits2 -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm -ldl (make -C cCAPS -f avlTest.make) clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include avlTest.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/avlTest.o clang -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/cCAPS/avlTest /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/avlTest.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lcaps -legads -locsm \ -ludunits2 -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm -ldl (make -C cCAPS -f awaveTest.make) clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include awaveTest.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/awaveTest.o clang -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/cCAPS/awaveTest /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/awaveTest.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lcaps -legads -locsm \ -ludunits2 -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm -ldl (make -C cCAPS -f frictionTest.make) clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include frictionTest.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/frictionTest.o clang -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/cCAPS/frictionTest /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/frictionTest.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lcaps -locsm -legads \ -ludunits2 -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm -ldl (make -C cCAPS -f fun3d.make) clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include fun3dAFLR2Test.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/fun3dAFLR2Test.o clang -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/cCAPS/fun3dAFLR2Test /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/fun3dAFLR2Test.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm -ldl clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include fun3dTetgenTest.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/fun3dTetgenTest.o clang -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/cCAPS/fun3dTetgenTest /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/fun3dTetgenTest.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm -ldl clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include aeroelasticTest.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/aeroelasticTest.o clang -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/cCAPS/aeroelasticTest /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/aeroelasticTest.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm -ldl (make -C cCAPS -f hsm.make) clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include hsmTest.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/hsmTest.o clang -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/cCAPS/hsmTest /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/hsmTest.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm -ldl clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include hsmSimplePlateTest.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/hsmSimplePlateTest.o clang -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/cCAPS/hsmSimplePlateTest /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/hsmSimplePlateTest.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm -ldl clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include hsmCantileverPlateTest.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/hsmCantileverPlateTest.o clang -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/cCAPS/hsmCantileverPlateTest /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/hsmCantileverPlateTest.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm -ldl clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include hsmJoinedPlateTest.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/hsmJoinedPlateTest.o clang -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/cCAPS/hsmJoinedPlateTest /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/hsmJoinedPlateTest.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm -ldl (make -C cCAPS -f interferenceTest.make) clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include interferenceTest.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/interferenceTest.o clang -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/cCAPS/interferenceTest /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/interferenceTest.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm -ldl (make -C cCAPS -f msesTest.make) clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include msesTest.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/msesTest.o clang -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/cCAPS/msesTest /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/msesTest.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lcaps -legads -locsm \ -ludunits2 -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm -ldl (make -C cCAPS -f mystran.make) clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include mystranTest.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/mystranTest.o clang -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/cCAPS/mystranTest /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/mystranTest.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm -ldl (make -C cCAPS -f pointwiseTest.make) clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include pointwiseTest.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/pointwiseTest.o clang -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/cCAPS/pointwiseTest /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/pointwiseTest.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lcaps -locsm -legads \ -ludunits2 -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm -ldl +++ find /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/CAPS/training/ -name Makefile ++ for i in '`find $WORKSPACE/CAPS/training/ -name Makefile`' ++ [[ /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/CAPS/training//2023/lectures/Makefile == *\l\e\c\t\u\r\e\s* ]] ++ continue ++ for i in '`find $WORKSPACE/CAPS/training/ -name Makefile`' ++ [[ /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/CAPS/training//2023/data/session01/Makefile == *\l\e\c\t\u\r\e\s* ]] +++ dirname /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/CAPS/training//2023/data/session01/Makefile ++ cd /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/CAPS/training//2023/data/session01 ++ make clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include template_avl.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/template_avl.o clang -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/test/template_avl /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/template_avl.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lcaps -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm -ldl ++ for i in '`find $WORKSPACE/CAPS/training/ -name Makefile`' ++ [[ /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/CAPS/training//data/session01/Makefile == *\l\e\c\t\u\r\e\s* ]] +++ dirname /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/CAPS/training//data/session01/Makefile ++ cd /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/CAPS/training//data/session01 ++ make make: Nothing to be done for `default'. ++ cd /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/OpenCSM/trunk/src ++ make -f serveESP.make clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. timCapsMode.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/timCapsMode.o touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/capsMode.so rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/capsMode.so clang++ -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/capsMode.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/timCapsMode.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lcaps -locsm -lwsserver -legads -ldl -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. timFlowchart.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/timFlowchart.o touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/flowchart.so rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/flowchart.so clang++ -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/flowchart.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/timFlowchart.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lcaps -locsm -lwsserver -legads -ldl -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. timViewer.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/timViewer.o touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/viewer.so rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/viewer.so clang++ -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/viewer.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/timViewer.o -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lcaps -locsm -lwsserver -legads -ldl -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. -I. -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 timPyscript.c -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/timPyscript.o touch /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/pyscript.so rm /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/pyscript.so clang++ -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/pyscript.so /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/timPyscript.o -L/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11 -ldl -framework CoreFoundation -Wl,-w -L/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lcaps -locsm -lwsserver -legads -ldl -rpath /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -Wl,-rpath /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib ++ ln -f -s /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/OpenCSM/trunk/udc /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64 +++ find /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/OpenCSM/trunk/data/training/ -name Makefile + mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/test + cd /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/test + source /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/JenkinsESP/RunRegression.sh ++ [[ 0 == 1 ]] ++ [[ 0 == 2 ]] ++ [[ /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64 == '' ]] ++ [[ CAPS/AEROELASTIC == '' ]] ++ [[ 7.7 == '' ]] ++ [[ ! -d /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/JenkinsESP ]] ++ rm -f csmFiles.txt ++ [[ CAPS/AEROELASTIC =~ [0-9]+.[0-9]+ ]] ++ export ESPTEST=CAPS/AEROELASTIC ++ ESPTEST=CAPS/AEROELASTIC ++ [[ CAPS/AEROELASTIC == \C\A\P\S* ]] ++ [[ ! -d /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/CAPS ]] ++ export CAPSTARGET=AEROELASTIC ++ CAPSTARGET=AEROELASTIC ++ [[ AEROELASTIC == \u\n\i\t ]] ++ [[ AEROELASTIC == \t\r\a\i\n\i\n\g\2\0\1\8 ]] ++ [[ AEROELASTIC == \t\r\a\i\n\i\n\g ]] ++ [[ AEROELASTIC == *\_\o\f\f ]] ++ cd /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/CAPS/examples/ ++ make test TYPE=AEROELASTIC (make -C cCAPS -f aeroelastic_SU2.make) make[1]: `/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/cCAPS/aeroelasticSimple_Iterative_SU2_and_MystranTest' is up to date. (make -C cCAPS -f avlTest.make) make[1]: `/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/cCAPS/avlTest' is up to date. (make -C cCAPS -f awaveTest.make) make[1]: `/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/cCAPS/awaveTest' is up to date. (make -C cCAPS -f frictionTest.make) make[1]: `/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/cCAPS/frictionTest' is up to date. (make -C cCAPS -f fun3d.make) make[1]: Nothing to be done for `fun3d'. (make -C cCAPS -f hsm.make) make[1]: `hsm' is up to date. (make -C cCAPS -f interferenceTest.make) make[1]: `/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/cCAPS/interferenceTest' is up to date. (make -C cCAPS -f msesTest.make) make[1]: `/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/cCAPS/msesTest' is up to date. (make -C cCAPS -f mystran.make) make[1]: `/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/cCAPS/mystranTest' is up to date. (make -C cCAPS -f pointwiseTest.make) make[1]: `/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/cCAPS/pointwiseTest' is up to date. (cd /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest; ./execute_CTestRegression.sh AEROELASTIC) Running.... AEROELASTIC c-Tests All tests pass! ================================================= ================================================= (cd /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest; ./execute_PyTestRegression.sh AEROELASTIC) ================================================= Using python : /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/venv/bin/python ================================================= Running.... AEROELASTIC PyTests ================================================= + echo 'aeroelasticSimple_Pressure_SU2_and_Astros.py test;' + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/pyCAPSlog.txt aeroelasticSimple_Pressure_SU2_and_Astros.py test; + python -u aeroelasticSimple_Pressure_SU2_and_Astros.py -outLevel=0 -noPlotData + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/pyCAPSlog.txt Running PreAnalysis ...... su2 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Farfield, index = 1 Name = SymmPlane, index = 2 Name = Skin, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 AFLR2 : --------------------------------------- AFLR2 : AFLR2 LIBRARY AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR2 : TRIA/QUAD GRID GENERATOR AFLR2 : Version Number 9.17.15 AFLR2 : Version Date 04/23/24 @ 12:51AM AFLR2 : Compile OS Darwin 23.4.0 arm64 AFLR2 : Compile Date 04/23/24 @ 12:51AM 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 11.5.14 AFLR4 : Version Date 04/18/24 @ 12:45PM AFLR4 : Compile OS Darwin 23.4.0 arm64 AFLR4 : Compile Date 04/18/24 @ 03:04PM AFLR4 : Copyright 1994-2021, D.L. Marcum AFLR4 : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : EGADS CAD Geometry Setup EGADS : Model has 1 Active Bodies EGADS : Body 0 is a SolidBody EGADS : Body 0 has 1 Shells EGADS : Body 0 has 9 Faces EGADS : Body 0 has 18 Edges EGADS : Body 0 has 10 Loops EGADS : Body 0 has 12 Nodes EGADS : Check Grid BCs EGADS : Grid BCs are OK EGADS : Face Neighbor-Faces Information EGADS : QC = Face Quad Combination Flag EGADS : IER = Face Isolated Edge Refinement Flag EGADS : ER = Face Edge Refinement Factor EGADS : Not applicable for Faces with a FarField Grid BC. EGADS : SF = Face Scale Factor EGADS : Not applicable for Faces with a FarField Grid BC. EGADS : Face Body QC IER ER Scale Neighbor EGADS : ID Active ID Flag Flag Weight Factor Faces EGADS : 1 Yes 0 0 1 0 1 2 3 4 5 EGADS : 2 Yes 0 0 1 0 1 1 3 5 6 EGADS : 3 Yes 0 0 1 0 1 1 2 4 6 7 8 EGADS : 4 Yes 0 0 1 0 1 1 3 5 6 EGADS : 5 Yes 0 0 1 0 1 1 2 4 6 EGADS : 6 Yes 0 0 1 0 1 2 3 4 5 EGADS : 7 Yes 0 0 1 0 1 3 8 9 EGADS : 8 Yes 0 0 1 0 1 3 7 9 EGADS : 9 Yes 0 0 1 0 1 7 8 EGADS : Face Edges Information EGADS : Face Edges EGADS : 1 1 2 -3 -4 EGADS : 2 5 6 -7 -1 EGADS : 3 -2 7 9 -8 -10 -11 EGADS : 4 -12 3 8 -13 EGADS : 5 4 12 -14 -5 EGADS : 6 -6 14 13 -9 EGADS : 7 15 10 -17 -16 EGADS : 8 17 11 -15 -18 EGADS : 9 16 18 EGADS : Face Loops Information EGADS : Face Loops EGADS : 1 1 EGADS : 2 2 EGADS : 3 3 4 EGADS : 4 5 EGADS : 5 6 EGADS : 6 7 EGADS : 7 8 EGADS : 8 9 EGADS : 9 10 EGADS : Loop Edges Information EGADS : Loop Active Edges EGADS : 1 Yes 1 2 -3 -4 EGADS : 2 Yes 5 6 -7 -1 EGADS : 3 Yes -2 7 9 -8 EGADS : 4 Yes -10 -11 EGADS : 5 Yes -12 3 8 -13 EGADS : 6 Yes 4 12 -14 -5 EGADS : 7 Yes -6 14 13 -9 EGADS : 8 Yes 15 10 -17 -16 EGADS : 9 Yes 17 11 -15 -18 EGADS : 10 Yes 16 18 EGADS : Edge Node, Scale Factor, and Neighbor-Faces Information EGADS : ESF = Edge Scale Factor EGADS : Not applicable for DEGENERATE Edges or Edges with a FarField EGADS : Grid BC Neighbor Face. EGADS : Neighbor EGADS : Edge Body Active Node1 Node2 ESF Faces EGADS : 1 0 Yes 2 1 1 1 2 EGADS : 2 0 Yes 1 3 1 1 3 EGADS : 3 0 Yes 4 3 1 1 4 EGADS : 4 0 Yes 2 4 1 1 5 EGADS : 5 0 Yes 2 5 1 2 5 EGADS : 6 0 Yes 5 6 1 2 6 EGADS : 7 0 Yes 1 6 1 2 3 EGADS : 8 0 Yes 3 7 1 3 4 EGADS : 9 0 Yes 6 7 1 3 6 EGADS : 10 0 Yes 8 9 1 3 7 EGADS : 11 0 Yes 9 8 1 3 8 EGADS : 12 0 Yes 4 10 1 4 5 EGADS : 13 0 Yes 10 7 1 4 6 EGADS : 14 0 Yes 5 10 1 5 6 EGADS : 15 0 Yes 11 8 1 7 8 EGADS : 16 0 Yes 11 12 1 7 9 EGADS : 17 0 Yes 12 9 1 7 8 EGADS : 18 0 Yes 12 11 1 8 9 EGADS : Node Information EGADS : Node Active Coordinates EGADS : 1 Yes 0 0 0 EGADS : 2 Yes 0 40 0 EGADS : 3 Yes 0 0 20 EGADS : 4 Yes 0 40 20 EGADS : 5 Yes 20 40 0 EGADS : 6 Yes 20 0 0 EGADS : 7 Yes 20 0 20 EGADS : 8 Yes 1.61374306 0 0 EGADS : 9 Yes 0 0 0 EGADS : 10 Yes 20 40 20 EGADS : 11 Yes 2.53650745 3.87298335 0.334116517 EGADS : 12 Yes 1.57194608 3.87298335 0.249728332 EGADS : Face and Edge Match Information EGADS : No Face Matches Found AFLR4 : Surface Mesh Spacing Setup AFLR4 : Max Bounding Box Length = 40 AFLR4 : Min Bounding Box Length = 40 AFLR4 : Max Ref Bounding Box Length = 40 AFLR4 : Min Ref Bounding Box Length = 40 AFLR4 : Reference Length = 1.61374 AFLR4 : BL Thickness = 0 AFLR4 : Abs Min Surf Spacing = 0.00403436 AFLR4 : Min Surf Spacing = 0.161374 AFLR4 : Max Surf Spacing = 1.21031 AFLR4 : Global Scale Factor = 1 AFLR4 : Geometry Definition Information AFLR4 : Definition Definition Composite Grid BC AFLR4 : ID Type ID Type AFLR4 : 0 glue-only composite - - AFLR4 : 1 CAD geometry 0 STD w/BL AFLR4 : 2 CAD geometry 0 STD w/BL AFLR4 : 3 CAD geometry 0 STD w/BL AFLR4 : 4 CAD geometry 0 STD w/BL AFLR4 : 5 CAD geometry 0 STD w/BL AFLR4 : 6 CAD geometry 0 STD w/BL AFLR4 : 7 CAD geometry 0 STD w/BL AFLR4 : 8 CAD geometry 0 STD w/BL AFLR4 : 9 CAD geometry 0 STD w/BL AFLR4 : Define CAD surface definition 1 AFLR4 : Define CAD surface definition 2 AFLR4 : Define CAD surface definition 3 AFLR4 : Define CAD surface definition 4 AFLR4 : Define CAD surface definition 5 AFLR4 : Define CAD surface definition 6 AFLR4 : Define CAD surface definition 7 AFLR4 : Define CAD surface definition 8 AFLR4 : Define CAD surface definition 9 AFLR4 : Surface Grid Generation AFLR4 : Generate optimal mesh on surface definition 1 AFLR2 : Nodes, Trias,Quads= 1318 2502 0 AFLR4 : Nodes, Trias,Quads= 1293 2452 0 AFLR4 : Generate optimal mesh on surface definition 2 AFLR2 : Nodes, Trias,Quads= 1318 2502 0 AFLR4 : Nodes, Trias,Quads= 1298 2462 0 AFLR4 : Generate optimal mesh on surface definition 3 AFLR2 : Nodes, Trias,Quads= 3418 6687 0 AFLR4 : Nodes, Trias,Quads= 3008 5867 0 AFLR4 : Generate optimal mesh on surface definition 4 AFLR2 : Nodes, Trias,Quads= 1316 2498 0 AFLR4 : Nodes, Trias,Quads= 1297 2460 0 AFLR4 : Generate optimal mesh on surface definition 5 AFLR2 : Nodes, Trias,Quads= 1318 2502 0 AFLR4 : Nodes, Trias,Quads= 1297 2460 0 AFLR4 : Generate optimal mesh on surface definition 6 AFLR2 : Nodes, Trias,Quads= 1319 2504 0 AFLR4 : Nodes, Trias,Quads= 1294 2454 0 AFLR4 : Generate optimal mesh on surface definition 7 AFLR2 : Nodes, Trias,Quads= 200 344 0 AFLR4 : Nodes, Trias,Quads= 160 264 0 AFLR4 : Generate optimal mesh on surface definition 8 AFLR2 : Nodes, Trias,Quads= 193 330 0 AFLR4 : Nodes, Trias,Quads= 155 254 0 AFLR4 : Generate optimal mesh on surface definition 9 AFLR2 : Nodes, Trias,Quads= 17 21 0 AFLR4 : Nodes, Trias,Quads= 11 9 0 DGEOM : Add surface definitions to composite definition 0 DGEOM : Glue composite surface definition 0 DGEOM : Nodes,Faces,BEdges= 9343 18682 928 AFLR4 : Auto Mode Turned OFF OVERALL : CPU Time = 0.143 seconds Body 1 (of 1) Number of nodes = 9343 Number of elements = 18682 Number of triangle elements = 18682 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 9343 Total number of elements = 18682 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Farfield, index = 1 Name = SymmPlane, index = 2 Name = Skin, index = 3 Getting volume mesh AFLR2 : --------------------------------------- AFLR2 : AFLR2 LIBRARY AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR2 : TRIA/QUAD GRID GENERATOR AFLR2 : Version Number 9.17.15 AFLR2 : Version Date 04/23/24 @ 12:51AM AFLR2 : Compile OS Darwin 23.4.0 arm64 AFLR2 : Compile Date 04/23/24 @ 12:51AM 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 11.5.14 AFLR4 : Version Date 04/18/24 @ 12:45PM AFLR4 : Compile OS Darwin 23.4.0 arm64 AFLR4 : Compile Date 04/18/24 @ 03:04PM AFLR4 : Copyright 1994-2021, D.L. Marcum AFLR4 : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 57531 Number of elements = 331031 Number of triangles = 18682 Number of quadrilatarals = 0 Number of tetrahedrals = 312349 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing SU2 file .... Finished writing SU2 file Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Skin Boundary condition name - SymmPlane Done getting CFD boundary conditions Info: No recognized data transfer names found. Warning: The su2 cfg file will be overwritten! Write SU2 configuration file for version "Harrier (8.0.1)" 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: 0.294118. 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_3. Surface(s) plotted in the output file: BC_3. Surface(s) affected by the design variables: BC_3. Input mesh file name: ../aflr3/aflr3_CAPS.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: 3. 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_aeroelasticSimple_Pressure_SA.dat. Surface file name: surface_flow_aeroelasticSimple_Pressure_SA. Volume file name: flow_aeroelasticSimple_Pressure_SA. Restart file name: restart_flow_aeroelasticSimple_Pressure_SA.dat. ------------- Config File Boundary Information ( Zone 0 ) --------------- +-----------------------------------------------------------------------+ | Marker Type| Marker Name| +-----------------------------------------------------------------------+ | Euler wall| BC_3| +-----------------------------------------------------------------------+ | Far-field| BC_1| +-----------------------------------------------------------------------+ | Symmetry plane| 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. 57531 grid points. 312349 volume elements. 3 surface markers. 12288 boundary elements in index 0 (Marker = BC_1). 5867 boundary elements in index 1 (Marker = BC_2). 527 boundary elements in index 2 (Marker = BC_3). 312349 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: 63999.5. Searching for the closest normal neighbors to the surfaces. Storing a mapping from global to local point index. Compute the surface curvature. Max K: 102.753. Mean K: 0.74689. Standard deviation K: 4.38956. Checking for periodicity. Computing mesh quality statistics for the dual control volumes. +--------------------------------------------------------------+ | Mesh Quality Metric| Minimum| Maximum| +--------------------------------------------------------------+ | Orthogonality Angle (deg.)| 48.3512| 86.0919| | CV Face Area Aspect Ratio| 1.11561| 35.2066| | CV Sub-Volume Ratio| 1| 18.8559| +--------------------------------------------------------------+ Setting the multigrid structure. +-------------------------------------------+ | MG Level| CVs|Aggl. Rate| CFL| +-------------------------------------------+ | 0| 57531| 1/1.00| 10| | 1| 9779| 1/5.88| 8.30913| | 2| 1716| 1/5.7| 6.97784| +-------------------------------------------+ Finding max control volume width. Semi-span length = 3.87298 m. Wetted area = 9.04169 m^2. Area projection in the x-plane = 0.644461 m^2, y-plane = 0.295795 m^2, z-plane = 4.29819 m^2. Max. coordinate in the x-direction = 2.53651 m, y-direction = 3.87298 m, z-direction = 0.379751 m. Min. coordinate in the x-direction = 0 m, y-direction = -2.86125e-18 m, z-direction = -0.0467278 m. Checking if Euler & Symmetry markers are straight/plane: Boundary marker BC_3 is NOT a single plane. Boundary marker BC_2 is 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| 211798| 1| m^2/s^2| 211798| | Velocity-X| 100.087| 1| m/s| 100.087| | Velocity-Y| 0| 1| m/s| 0| | Velocity-Z| 0| 1| m/s| 0| | Velocity Magnitude| 100.087| 1| m/s| 100.087| +------------------------------------------------------------------------------+ | Mach Number| -| -| -| 0.294118| +------------------------------------------------------------------------------+ 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| 1.6493e+00| -1.299765| 0.996854| 0.627451| 4.169341| -0.962501| | 0| 0| 1| 0.0000e+00| 0.0000e+00| 1.6406e+00| -1.689451| 0.841935| 0.460737| 3.766643| -0.517631| | 0| 0| 2| 0.0000e+00| 0.0000e+00| 1.6334e+00| -1.703013| 0.658675| 0.298032| 3.753378| 1.611420| ----------------------------- Solver Exit ------------------------------- Maximum number of iterations reached (ITER = 3) before convergence. +-----------------------------------------------------------------------+ | Convergence Field | Value | Criterion | Converged | +-----------------------------------------------------------------------+ | rms[Rho]| -1.70301| < -14| No| +-----------------------------------------------------------------------+ ------------------------------------------------------------------------- +-----------------------------------------------------------------------+ | File Writing Summary | Filename | +-----------------------------------------------------------------------+ |SU2 binary restart |restart_flow_aeroelasticSimple_Pressure_SA.dat| Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Pressure_SA.dat). |CSV file |surface_flow_aeroelasticSimple_Pressure_SA.csv| Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Pressure_SA.dat). |Tecplot binary |flow_aeroelasticSimple_Pressure_SA.szplt| Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Pressure_SA.dat). |Tecplot binary surface |surface_flow_aeroelasticSimple_Pressure_SA.szplt| Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Pressure_SA.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) ------------------------ Running PostAnalysis ...... su2 Running ...... astros Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = Rib_Root, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = Skin, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 3 Name = Skin_Top, index = 1 Name = Skin_Bottom, index = 2 Name = Skin_Tip, index = 3 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Skin, index = 1 Name = Rib_Root, index = 2 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 180 Number of elements = 194 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 32 Elemental Quad4 = 162 Aero_Reference value is NULL - No aero reference parameters set Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 2 Property name - Rib_Root Property name - Skin Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - pressureAero No "groupName" specified for Load tuple pressureAero, going to use load name Done getting FEA loads Optimization Control tuple is NULL - Default optimization control is used Getting FEA optimization control....... Done getting FEA Optimization Control Design_Variable tuple is NULL - No design variables applied Design_Constraint tuple is NULL - No design constraints applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Reading SU2 AeroLoad File - surface_flow_aeroelasticSimple_Pressure_SA.csv Number of variables = 16 Number of data points = 273 CAPS Info: Bound 'Skin_Top' Normalized Integrated 'Pressure' Rank 0: src = 3.100922e+09, tgt = 3.100922e+09, diff = 1.828803e+02 Reading SU2 AeroLoad File - surface_flow_aeroelasticSimple_Pressure_SA.csv Number of variables = 16 Number of data points = 273 CAPS Info: Bound 'Skin_Bottom' Normalized Integrated 'Pressure' Rank 0: src = 3.018738e+09, tgt = 3.018738e+09, diff = 2.203347e+02 Reading SU2 AeroLoad File - surface_flow_aeroelasticSimple_Pressure_SA.csv Number of variables = 16 Number of data points = 273 CAPS Info: Bound 'Skin_Tip' Normalized Integrated 'Pressure' Rank 0: src = 4.338994e+07, tgt = 4.338994e+07, diff = 3.559001e-03 Extracting external pressure loads from data transfer.... TransferName = Skin_Top Number of Elements = 81 (total = 81) Extracting external pressure loads from data transfer.... TransferName = Skin_Bottom Number of Elements = 81 (total = 162) Extracting external pressure loads from data transfer.... TransferName = Skin_Tip Number of Elements = 16 (total = 178) Writing Astros grid and connectivity file (in free field format) .... Finished writing Astros grid file Writing subElement types (if any) - appending mesh file Writing Astros instruction file.... Writing analysis cards Writing load ADD cards Writing constraint cards--each subcase individually Writing load cards Writing material cards Writing property cards Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG real 0m23.183s user 0m17.565s sys 0m1.410s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case aeroelasticSimple_Pressure_SU2_and_Astros.py passed (as expected) ================================================= ================================================= + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/pyCAPSlog.txt + echo 'aeroelasticSimple_Displacement_SU2_and_Astros.py test;' aeroelasticSimple_Displacement_SU2_and_Astros.py test; + python -u aeroelasticSimple_Displacement_SU2_and_Astros.py -outLevel=0 -noPlotData + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/pyCAPSlog.txt Running PreAnalysis ...... astros Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = Rib_Root, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = Skin, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 3 Name = Skin_Top, index = 1 Name = Skin_Bottom, index = 2 Name = Skin_Tip, index = 3 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Skin, index = 1 Name = Rib_Root, index = 2 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 180 Number of elements = 194 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 32 Elemental Quad4 = 162 Aero_Reference value is NULL - No aero reference parameters set Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 2 Property name - Rib_Root Property name - Skin Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - pressureInternal Done getting FEA loads Optimization Control tuple is NULL - Default optimization control is used Getting FEA optimization control....... Done getting FEA Optimization Control Design_Variable tuple is NULL - No design variables applied Design_Constraint tuple is NULL - No design constraints applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Astros grid and connectivity file (in free field format) .... Finished writing Astros grid file Writing subElement types (if any) - appending mesh file Writing Astros instruction file.... Writing analysis cards Writing load ADD cards Writing constraint cards--each subcase individually Writing load cards Writing material cards Writing property cards Running Astros...... Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG Running PostAnalysis ...... astros Running PreAnalysis ...... su2 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Farfield, index = 1 Name = SymmPlane, index = 2 Name = Skin, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 AFLR2 : --------------------------------------- AFLR2 : AFLR2 LIBRARY AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR2 : TRIA/QUAD GRID GENERATOR AFLR2 : Version Number 9.17.15 AFLR2 : Version Date 04/23/24 @ 12:51AM AFLR2 : Compile OS Darwin 23.4.0 arm64 AFLR2 : Compile Date 04/23/24 @ 12:51AM 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 11.5.14 AFLR4 : Version Date 04/18/24 @ 12:45PM AFLR4 : Compile OS Darwin 23.4.0 arm64 AFLR4 : Compile Date 04/18/24 @ 03:04PM AFLR4 : Copyright 1994-2021, D.L. Marcum AFLR4 : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : EGADS CAD Geometry Setup EGADS : Model has 1 Active Bodies EGADS : Body 0 is a SolidBody EGADS : Body 0 has 1 Shells EGADS : Body 0 has 9 Faces EGADS : Body 0 has 18 Edges EGADS : Body 0 has 10 Loops EGADS : Body 0 has 12 Nodes EGADS : Check Grid BCs EGADS : Grid BCs are OK EGADS : Face Neighbor-Faces Information EGADS : QC = Face Quad Combination Flag EGADS : IER = Face Isolated Edge Refinement Flag EGADS : ER = Face Edge Refinement Factor EGADS : Not applicable for Faces with a FarField Grid BC. EGADS : SF = Face Scale Factor EGADS : Not applicable for Faces with a FarField Grid BC. EGADS : Face Body QC IER ER Scale Neighbor EGADS : ID Active ID Flag Flag Weight Factor Faces EGADS : 1 Yes 0 0 1 0 1 2 3 4 5 EGADS : 2 Yes 0 0 1 0 1 1 3 5 6 EGADS : 3 Yes 0 0 1 0 1 1 2 4 6 7 8 EGADS : 4 Yes 0 0 1 0 1 1 3 5 6 EGADS : 5 Yes 0 0 1 0 1 1 2 4 6 EGADS : 6 Yes 0 0 1 0 1 2 3 4 5 EGADS : 7 Yes 0 0 1 0 1 3 8 9 EGADS : 8 Yes 0 0 1 0 1 3 7 9 EGADS : 9 Yes 0 0 1 0 1 7 8 EGADS : Face Edges Information EGADS : Face Edges EGADS : 1 1 2 -3 -4 EGADS : 2 5 6 -7 -1 EGADS : 3 -2 7 9 -8 -10 -11 EGADS : 4 -12 3 8 -13 EGADS : 5 4 12 -14 -5 EGADS : 6 -6 14 13 -9 EGADS : 7 15 10 -17 -16 EGADS : 8 17 11 -15 -18 EGADS : 9 16 18 EGADS : Face Loops Information EGADS : Face Loops EGADS : 1 1 EGADS : 2 2 EGADS : 3 3 4 EGADS : 4 5 EGADS : 5 6 EGADS : 6 7 EGADS : 7 8 EGADS : 8 9 EGADS : 9 10 EGADS : Loop Edges Information EGADS : Loop Active Edges EGADS : 1 Yes 1 2 -3 -4 EGADS : 2 Yes 5 6 -7 -1 EGADS : 3 Yes -2 7 9 -8 EGADS : 4 Yes -10 -11 EGADS : 5 Yes -12 3 8 -13 EGADS : 6 Yes 4 12 -14 -5 EGADS : 7 Yes -6 14 13 -9 EGADS : 8 Yes 15 10 -17 -16 EGADS : 9 Yes 17 11 -15 -18 EGADS : 10 Yes 16 18 EGADS : Edge Node, Scale Factor, and Neighbor-Faces Information EGADS : ESF = Edge Scale Factor EGADS : Not applicable for DEGENERATE Edges or Edges with a FarField EGADS : Grid BC Neighbor Face. EGADS : Neighbor EGADS : Edge Body Active Node1 Node2 ESF Faces EGADS : 1 0 Yes 2 1 1 1 2 EGADS : 2 0 Yes 1 3 1 1 3 EGADS : 3 0 Yes 4 3 1 1 4 EGADS : 4 0 Yes 2 4 1 1 5 EGADS : 5 0 Yes 2 5 1 2 5 EGADS : 6 0 Yes 5 6 1 2 6 EGADS : 7 0 Yes 1 6 1 2 3 EGADS : 8 0 Yes 3 7 1 3 4 EGADS : 9 0 Yes 6 7 1 3 6 EGADS : 10 0 Yes 8 9 1 3 7 EGADS : 11 0 Yes 9 8 1 3 8 EGADS : 12 0 Yes 4 10 1 4 5 EGADS : 13 0 Yes 10 7 1 4 6 EGADS : 14 0 Yes 5 10 1 5 6 EGADS : 15 0 Yes 11 8 1 7 8 EGADS : 16 0 Yes 11 12 1 7 9 EGADS : 17 0 Yes 12 9 1 7 8 EGADS : 18 0 Yes 12 11 1 8 9 EGADS : Node Information EGADS : Node Active Coordinates EGADS : 1 Yes 0 0 0 EGADS : 2 Yes 0 40 0 EGADS : 3 Yes 0 0 20 EGADS : 4 Yes 0 40 20 EGADS : 5 Yes 20 40 0 EGADS : 6 Yes 20 0 0 EGADS : 7 Yes 20 0 20 EGADS : 8 Yes 1.61374306 0 0 EGADS : 9 Yes 0 0 0 EGADS : 10 Yes 20 40 20 EGADS : 11 Yes 2.53650745 3.87298335 0.334116517 EGADS : 12 Yes 1.57194608 3.87298335 0.249728332 EGADS : Face and Edge Match Information EGADS : No Face Matches Found AFLR4 : Surface Mesh Spacing Setup AFLR4 : Max Bounding Box Length = 40 AFLR4 : Min Bounding Box Length = 40 AFLR4 : Max Ref Bounding Box Length = 40 AFLR4 : Min Ref Bounding Box Length = 40 AFLR4 : Reference Length = 1.61374 AFLR4 : BL Thickness = 0 AFLR4 : Abs Min Surf Spacing = 0.00403436 AFLR4 : Min Surf Spacing = 0.161374 AFLR4 : Max Surf Spacing = 1.21031 AFLR4 : Global Scale Factor = 1 AFLR4 : Geometry Definition Information AFLR4 : Definition Definition Composite Grid BC AFLR4 : ID Type ID Type AFLR4 : 0 glue-only composite - - AFLR4 : 1 CAD geometry 0 STD w/BL AFLR4 : 2 CAD geometry 0 STD w/BL AFLR4 : 3 CAD geometry 0 STD w/BL AFLR4 : 4 CAD geometry 0 STD w/BL AFLR4 : 5 CAD geometry 0 STD w/BL AFLR4 : 6 CAD geometry 0 STD w/BL AFLR4 : 7 CAD geometry 0 STD w/BL AFLR4 : 8 CAD geometry 0 STD w/BL AFLR4 : 9 CAD geometry 0 STD w/BL AFLR4 : Define CAD surface definition 1 AFLR4 : Define CAD surface definition 2 AFLR4 : Define CAD surface definition 3 AFLR4 : Define CAD surface definition 4 AFLR4 : Define CAD surface definition 5 AFLR4 : Define CAD surface definition 6 AFLR4 : Define CAD surface definition 7 AFLR4 : Define CAD surface definition 8 AFLR4 : Define CAD surface definition 9 AFLR4 : Surface Grid Generation AFLR4 : Generate optimal mesh on surface definition 1 AFLR2 : Nodes, Trias,Quads= 1318 2502 0 AFLR4 : Nodes, Trias,Quads= 1293 2452 0 AFLR4 : Generate optimal mesh on surface definition 2 AFLR2 : Nodes, Trias,Quads= 1318 2502 0 AFLR4 : Nodes, Trias,Quads= 1298 2462 0 AFLR4 : Generate optimal mesh on surface definition 3 AFLR2 : Nodes, Trias,Quads= 3418 6687 0 AFLR4 : Nodes, Trias,Quads= 3008 5867 0 AFLR4 : Generate optimal mesh on surface definition 4 AFLR2 : Nodes, Trias,Quads= 1316 2498 0 AFLR4 : Nodes, Trias,Quads= 1297 2460 0 AFLR4 : Generate optimal mesh on surface definition 5 AFLR2 : Nodes, Trias,Quads= 1318 2502 0 AFLR4 : Nodes, Trias,Quads= 1297 2460 0 AFLR4 : Generate optimal mesh on surface definition 6 AFLR2 : Nodes, Trias,Quads= 1319 2504 0 AFLR4 : Nodes, Trias,Quads= 1294 2454 0 AFLR4 : Generate optimal mesh on surface definition 7 AFLR2 : Nodes, Trias,Quads= 200 344 0 AFLR4 : Nodes, Trias,Quads= 160 264 0 AFLR4 : Generate optimal mesh on surface definition 8 AFLR2 : Nodes, Trias,Quads= 193 330 0 AFLR4 : Nodes, Trias,Quads= 155 254 0 AFLR4 : Generate optimal mesh on surface definition 9 AFLR2 : Nodes, Trias,Quads= 17 21 0 AFLR4 : Nodes, Trias,Quads= 11 9 0 DGEOM : Add surface definitions to composite definition 0 DGEOM : Glue composite surface definition 0 DGEOM : Nodes,Faces,BEdges= 9343 18682 928 AFLR4 : Auto Mode Turned OFF OVERALL : CPU Time = 0.136 seconds Body 1 (of 1) Number of nodes = 9343 Number of elements = 18682 Number of triangle elements = 18682 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 9343 Total number of elements = 18682 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Farfield, index = 1 Name = SymmPlane, index = 2 Name = Skin, index = 3 Getting volume mesh AFLR2 : --------------------------------------- AFLR2 : AFLR2 LIBRARY AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR2 : TRIA/QUAD GRID GENERATOR AFLR2 : Version Number 9.17.15 AFLR2 : Version Date 04/23/24 @ 12:51AM AFLR2 : Compile OS Darwin 23.4.0 arm64 AFLR2 : Compile Date 04/23/24 @ 12:51AM 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 11.5.14 AFLR4 : Version Date 04/18/24 @ 12:45PM AFLR4 : Compile OS Darwin 23.4.0 arm64 AFLR4 : Compile Date 04/18/24 @ 03:04PM AFLR4 : Copyright 1994-2021, D.L. Marcum AFLR4 : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 57531 Number of elements = 331031 Number of triangles = 18682 Number of quadrilatarals = 0 Number of tetrahedrals = 312349 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing SU2 file .... Finished writing SU2 file Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Skin Boundary condition name - SymmPlane Done getting CFD boundary conditions Writing SU2 data transfer files Writing SU2 Motion File - aeroelasticSimple_Displacement_SA_motion.dat Warning: The su2 cfg file will be overwritten! Write SU2 configuration file for version "Harrier (8.0.1)" Running SU2...... ------------------------------------------------------------------------- | ___ _ _ ___ | | / __| | | |_ ) 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/aflr3_CAPS.su2 ---------------- Grid deformation parameters ( Zone 0 ) ---------------- Grid deformation using a linear elasticity method. -------------------- Output Information ( Zone 0 ) ---------------------- Output mesh file name: ../aflr3/aflr3_CAPS.su2. Cell stiffness scaled by distance to nearest solid surface. ------------- Config File Boundary Information ( Zone 0 ) --------------- +-----------------------------------------------------------------------+ | Marker Type| Marker Name| +-----------------------------------------------------------------------+ | Euler wall| BC_3| +-----------------------------------------------------------------------+ | Far-field| BC_1| +-----------------------------------------------------------------------+ | Symmetry plane| BC_2| +-----------------------------------------------------------------------+ Three dimensional problem. 57531 grid points. 312349 volume elements. 3 surface markers. 12288 boundary elements in index 0 (Marker = BC_1). 5867 boundary elements in index 1 (Marker = BC_2). 527 boundary elements in index 2 (Marker = BC_3). 312349 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: 63999.5. 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 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 14.473226 seconds on 1 core. ----------------------- Write deformed grid files ----------------------- |SU2 mesh |../aflr3/aflr3_CAPS.su2 | |CSV file |surface_deformed.csv | |Tecplot binary |volume_deformed.szplt | |Tecplot binary surface |surface_deformed.szplt | 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) ------------------------ ------------------------------------------------------------------------- | ___ _ _ ___ | | / __| | | |_ ) 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: 0.294118. 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_3. Surface(s) plotted in the output file: BC_3. Surface(s) affected by the design variables: BC_3. Input mesh file name: ../aflr3/aflr3_CAPS.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: 3. 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_aeroelasticSimple_Displacement_SA.dat. Surface file name: surface_flow_aeroelasticSimple_Displacement_SA. Volume file name: flow_aeroelasticSimple_Displacement_SA. Restart file name: restart_flow_aeroelasticSimple_Displacement_SA.dat. ------------- Config File Boundary Information ( Zone 0 ) --------------- +-----------------------------------------------------------------------+ | Marker Type| Marker Name| +-----------------------------------------------------------------------+ | Euler wall| BC_3| +-----------------------------------------------------------------------+ | Far-field| BC_1| +-----------------------------------------------------------------------+ | Symmetry plane| 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. 57531 grid points. 312349 volume elements. 3 surface markers. 12288 boundary elements in index 0 (Marker = BC_1). 5867 boundary elements in index 1 (Marker = BC_2). 527 boundary elements in index 2 (Marker = BC_3). 312349 tetrahedra. Setting point connectivity. Renumbering points (Reverse Cuthill McKee Ordering). Recomputing point connectivity. Setting element connectivity. Checking the numerical grid orientation. There has been a re-orientation of 1 TETRAHEDRON volume elements. All surface elements are correctly orientend. Identifying edges and vertices. Setting the control volume structure. Volume of the computational grid: 63997.8. Searching for the closest normal neighbors to the surfaces. Storing a mapping from global to local point index. Compute the surface curvature. Max K: 84.836. Mean K: 0.75089. Standard deviation K: 3.83533. Checking for periodicity. Computing mesh quality statistics for the dual control volumes. +--------------------------------------------------------------+ | Mesh Quality Metric| Minimum| Maximum| +--------------------------------------------------------------+ | Orthogonality Angle (deg.)| 41.5576| 86.1004| | CV Face Area Aspect Ratio| 1.11561| 33.3076| | CV Sub-Volume Ratio| 1| 68.3008| +--------------------------------------------------------------+ Setting the multigrid structure. +-------------------------------------------+ | MG Level| CVs|Aggl. Rate| CFL| +-------------------------------------------+ | 0| 57531| 1/1.00| 10| | 1| 9779| 1/5.88| 8.30913| | 2| 1716| 1/5.7| 6.97784| +-------------------------------------------+ Finding max control volume width. Semi-span length = 3.89964 m. Wetted area = 11.4382 m^2. Area projection in the x-plane = 2.82758 m^2, y-plane = 1.25436 m^2, z-plane = 4.17954 m^2. Max. coordinate in the x-direction = 2.53729 m, y-direction = 3.89964 m, z-direction = 0.526515 m. Min. coordinate in the x-direction = 0.000170858 m, y-direction = -2.86125e-18 m, z-direction = -0.705261 m. Checking if Euler & Symmetry markers are straight/plane: Boundary marker BC_3 is NOT a single plane. Boundary marker BC_2 is 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| 211798| 1| m^2/s^2| 211798| | Velocity-X| 100.087| 1| m/s| 100.087| | Velocity-Y| 0| 1| m/s| 0| | Velocity-Z| 0| 1| m/s| 0| | Velocity Magnitude| 100.087| 1| m/s| 100.087| +------------------------------------------------------------------------------+ | Mach Number| -| -| -| 0.294118| +------------------------------------------------------------------------------+ 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| 1.5102e+00| -0.622071| 1.813033| 1.305623| 4.847034| 0.070229| | 0| 0| 1| 0.0000e+00| 0.0000e+00| 1.5060e+00| -1.089888| 1.515924| 1.156988| 4.382145| 0.058664| | 0| 0| 2| 0.0000e+00| 0.0000e+00| 1.5120e+00| -1.096792| 1.282257| 0.955302| 4.370060| 0.133547| ----------------------------- Solver Exit ------------------------------- Maximum number of iterations reached (ITER = 3) before convergence. +-----------------------------------------------------------------------+ | Convergence Field | Value | Criterion | Converged | +-----------------------------------------------------------------------+ | rms[Rho]| -1.09679| < -14| No| +-----------------------------------------------------------------------+ ------------------------------------------------------------------------- +-----------------------------------------------------------------------+ | File Writing Summary | Filename | +-----------------------------------------------------------------------+ |SU2 binary restart |restart_flow_aeroelasticSimple_Displacement_SA.dat| Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Displacement_SA.dat). |CSV file |surface_flow_aeroelasticSimple_Displacement_SA.csv| Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Displacement_SA.dat). |Tecplot binary |flow_aeroelasticSimple_Displacement_SA.szplt| Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Displacement_SA.dat). |Tecplot binary surface |surface_flow_aeroelasticSimple_Displacement_SA.szplt| Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Displacement_SA.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) ------------------------ Running PostAnalysis ...... su2 real 0m48.778s user 0m36.346s sys 0m2.390s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case aeroelasticSimple_Displacement_SU2_and_Astros.py passed (as expected) ================================================= ================================================= + echo 'aeroelasticSimple_Iterative_SU2_and_Astros.py test;' + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/pyCAPSlog.txt aeroelasticSimple_Iterative_SU2_and_Astros.py test; + python -u aeroelasticSimple_Iterative_SU2_and_Astros.py -outLevel=0 + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/pyCAPSlog.txt Running PreAnalysis ...... su2 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Farfield, index = 1 Name = SymmPlane, index = 2 Name = Skin, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 AFLR2 : --------------------------------------- AFLR2 : AFLR2 LIBRARY AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR2 : TRIA/QUAD GRID GENERATOR AFLR2 : Version Number 9.17.15 AFLR2 : Version Date 04/23/24 @ 12:51AM AFLR2 : Compile OS Darwin 23.4.0 arm64 AFLR2 : Compile Date 04/23/24 @ 12:51AM 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 11.5.14 AFLR4 : Version Date 04/18/24 @ 12:45PM AFLR4 : Compile OS Darwin 23.4.0 arm64 AFLR4 : Compile Date 04/18/24 @ 03:04PM AFLR4 : Copyright 1994-2021, D.L. Marcum AFLR4 : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : EGADS CAD Geometry Setup EGADS : Model has 1 Active Bodies EGADS : Body 0 is a SolidBody EGADS : Body 0 has 1 Shells EGADS : Body 0 has 9 Faces EGADS : Body 0 has 18 Edges EGADS : Body 0 has 10 Loops EGADS : Body 0 has 12 Nodes EGADS : Check Grid BCs EGADS : Grid BCs are OK EGADS : Face Neighbor-Faces Information EGADS : QC = Face Quad Combination Flag EGADS : IER = Face Isolated Edge Refinement Flag EGADS : ER = Face Edge Refinement Factor EGADS : Not applicable for Faces with a FarField Grid BC. EGADS : SF = Face Scale Factor EGADS : Not applicable for Faces with a FarField Grid BC. EGADS : Face Body QC IER ER Scale Neighbor EGADS : ID Active ID Flag Flag Weight Factor Faces EGADS : 1 Yes 0 0 1 0 1 2 3 4 5 EGADS : 2 Yes 0 0 1 0 1 1 3 5 6 EGADS : 3 Yes 0 0 1 0 1 1 2 4 6 7 8 EGADS : 4 Yes 0 0 1 0 1 1 3 5 6 EGADS : 5 Yes 0 0 1 0 1 1 2 4 6 EGADS : 6 Yes 0 0 1 0 1 2 3 4 5 EGADS : 7 Yes 0 0 1 0 1 3 8 9 EGADS : 8 Yes 0 0 1 0 1 3 7 9 EGADS : 9 Yes 0 0 1 0 1 7 8 EGADS : Face Edges Information EGADS : Face Edges EGADS : 1 1 2 -3 -4 EGADS : 2 5 6 -7 -1 EGADS : 3 -2 7 9 -8 -10 -11 EGADS : 4 -12 3 8 -13 EGADS : 5 4 12 -14 -5 EGADS : 6 -6 14 13 -9 EGADS : 7 15 10 -17 -16 EGADS : 8 17 11 -15 -18 EGADS : 9 16 18 EGADS : Face Loops Information EGADS : Face Loops EGADS : 1 1 EGADS : 2 2 EGADS : 3 3 4 EGADS : 4 5 EGADS : 5 6 EGADS : 6 7 EGADS : 7 8 EGADS : 8 9 EGADS : 9 10 EGADS : Loop Edges Information EGADS : Loop Active Edges EGADS : 1 Yes 1 2 -3 -4 EGADS : 2 Yes 5 6 -7 -1 EGADS : 3 Yes -2 7 9 -8 EGADS : 4 Yes -10 -11 EGADS : 5 Yes -12 3 8 -13 EGADS : 6 Yes 4 12 -14 -5 EGADS : 7 Yes -6 14 13 -9 EGADS : 8 Yes 15 10 -17 -16 EGADS : 9 Yes 17 11 -15 -18 EGADS : 10 Yes 16 18 EGADS : Edge Node, Scale Factor, and Neighbor-Faces Information EGADS : ESF = Edge Scale Factor EGADS : Not applicable for DEGENERATE Edges or Edges with a FarField EGADS : Grid BC Neighbor Face. EGADS : Neighbor EGADS : Edge Body Active Node1 Node2 ESF Faces EGADS : 1 0 Yes 2 1 1 1 2 EGADS : 2 0 Yes 1 3 1 1 3 EGADS : 3 0 Yes 4 3 1 1 4 EGADS : 4 0 Yes 2 4 1 1 5 EGADS : 5 0 Yes 2 5 1 2 5 EGADS : 6 0 Yes 5 6 1 2 6 EGADS : 7 0 Yes 1 6 1 2 3 EGADS : 8 0 Yes 3 7 1 3 4 EGADS : 9 0 Yes 6 7 1 3 6 EGADS : 10 0 Yes 8 9 1 3 7 EGADS : 11 0 Yes 9 8 1 3 8 EGADS : 12 0 Yes 4 10 1 4 5 EGADS : 13 0 Yes 10 7 1 4 6 EGADS : 14 0 Yes 5 10 1 5 6 EGADS : 15 0 Yes 11 8 1 7 8 EGADS : 16 0 Yes 11 12 1 7 9 EGADS : 17 0 Yes 12 9 1 7 8 EGADS : 18 0 Yes 12 11 1 8 9 EGADS : Node Information EGADS : Node Active Coordinates EGADS : 1 Yes 0 0 0 EGADS : 2 Yes 0 40 0 EGADS : 3 Yes 0 0 20 EGADS : 4 Yes 0 40 20 EGADS : 5 Yes 20 40 0 EGADS : 6 Yes 20 0 0 EGADS : 7 Yes 20 0 20 EGADS : 8 Yes 1.61374306 0 0 EGADS : 9 Yes 0 0 0 EGADS : 10 Yes 20 40 20 EGADS : 11 Yes 2.53650745 3.87298335 0.334116517 EGADS : 12 Yes 1.57194608 3.87298335 0.249728332 EGADS : Face and Edge Match Information EGADS : No Face Matches Found AFLR4 : Surface Mesh Spacing Setup AFLR4 : Max Bounding Box Length = 40 AFLR4 : Min Bounding Box Length = 40 AFLR4 : Max Ref Bounding Box Length = 40 AFLR4 : Min Ref Bounding Box Length = 40 AFLR4 : Reference Length = 1.61374 AFLR4 : BL Thickness = 0 AFLR4 : Abs Min Surf Spacing = 0.00403436 AFLR4 : Min Surf Spacing = 0.161374 AFLR4 : Max Surf Spacing = 1.21031 AFLR4 : Global Scale Factor = 2 AFLR4 : Geometry Definition Information AFLR4 : Definition Definition Composite Grid BC AFLR4 : ID Type ID Type AFLR4 : 0 glue-only composite - - AFLR4 : 1 CAD geometry 0 STD w/BL AFLR4 : 2 CAD geometry 0 STD w/BL AFLR4 : 3 CAD geometry 0 STD w/BL AFLR4 : 4 CAD geometry 0 STD w/BL AFLR4 : 5 CAD geometry 0 STD w/BL AFLR4 : 6 CAD geometry 0 STD w/BL AFLR4 : 7 CAD geometry 0 STD w/BL AFLR4 : 8 CAD geometry 0 STD w/BL AFLR4 : 9 CAD geometry 0 STD w/BL AFLR4 : Define CAD surface definition 1 AFLR4 : Define CAD surface definition 2 AFLR4 : Define CAD surface definition 3 AFLR4 : Define CAD surface definition 4 AFLR4 : Define CAD surface definition 5 AFLR4 : Define CAD surface definition 6 AFLR4 : Define CAD surface definition 7 AFLR4 : Define CAD surface definition 8 AFLR4 : Define CAD surface definition 9 AFLR4 : Surface Grid Generation AFLR4 : Generate optimal mesh on surface definition 1 AFLR2 : Nodes, Trias,Quads= 376 682 0 AFLR4 : Nodes, Trias,Quads= 381 692 0 AFLR4 : Generate optimal mesh on surface definition 2 AFLR2 : Nodes, Trias,Quads= 374 678 0 AFLR4 : Nodes, Trias,Quads= 380 690 0 AFLR4 : Generate optimal mesh on surface definition 3 AFLR2 : Nodes, Trias,Quads= 927 1777 0 AFLR4 : Nodes, Trias,Quads= 821 1565 0 AFLR4 : Generate optimal mesh on surface definition 4 AFLR2 : Nodes, Trias,Quads= 376 682 0 AFLR4 : Nodes, Trias,Quads= 380 690 0 AFLR4 : Generate optimal mesh on surface definition 5 AFLR2 : Nodes, Trias,Quads= 374 678 0 AFLR4 : Nodes, Trias,Quads= 380 690 0 AFLR4 : Generate optimal mesh on surface definition 6 AFLR2 : Nodes, Trias,Quads= 376 682 0 AFLR4 : Nodes, Trias,Quads= 378 686 0 AFLR4 : Generate optimal mesh on surface definition 7 AFLR2 : Nodes, Trias,Quads= 63 96 0 AFLR4 : Nodes, Trias,Quads= 55 80 0 AFLR4 : Generate optimal mesh on surface definition 8 AFLR2 : Nodes, Trias,Quads= 64 96 0 AFLR4 : Nodes, Trias,Quads= 57 82 0 AFLR4 : Generate optimal mesh on surface definition 9 AFLR2 : Nodes, Trias,Quads= 11 13 0 AFLR4 : Nodes, Trias,Quads= 7 5 0 DGEOM : Add surface definitions to composite definition 0 DGEOM : Glue composite surface definition 0 DGEOM : Nodes,Faces,BEdges= 2592 5180 482 AFLR4 : Auto Mode Turned OFF OVERALL : CPU Time = 0.075 seconds Body 1 (of 1) Number of nodes = 2592 Number of elements = 5180 Number of triangle elements = 5180 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 2592 Total number of elements = 5180 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Farfield, index = 1 Name = SymmPlane, index = 2 Name = Skin, index = 3 Getting volume mesh AFLR2 : --------------------------------------- AFLR2 : AFLR2 LIBRARY AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR2 : TRIA/QUAD GRID GENERATOR AFLR2 : Version Number 9.17.15 AFLR2 : Version Date 04/23/24 @ 12:51AM AFLR2 : Compile OS Darwin 23.4.0 arm64 AFLR2 : Compile Date 04/23/24 @ 12:51AM 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 11.5.14 AFLR4 : Version Date 04/18/24 @ 12:45PM AFLR4 : Compile OS Darwin 23.4.0 arm64 AFLR4 : Compile Date 04/18/24 @ 03:04PM AFLR4 : Copyright 1994-2021, D.L. Marcum AFLR4 : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 10490 Number of elements = 59345 Number of triangles = 5180 Number of quadrilatarals = 0 Number of tetrahedrals = 54165 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing SU2 file .... Finished writing SU2 file Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Skin Boundary condition name - SymmPlane Done getting CFD boundary conditions Writing SU2 data transfer files Writing SU2 Motion File - aeroelasticSimple_Iterative_motion.dat Warning: The su2 cfg file will be overwritten! Write SU2 configuration file for version "Harrier (8.0.1)" 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: 0.294118. 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_3. Surface(s) plotted in the output file: BC_3. Surface(s) affected by the design variables: BC_3. Input mesh file name: ../aflr3/aflr3_CAPS.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: 3. 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_aeroelasticSimple_Iterative.dat. Surface file name: surface_flow_aeroelasticSimple_Iterative. Volume file name: flow_aeroelasticSimple_Iterative. Restart file name: restart_flow_aeroelasticSimple_Iterative.dat. ------------- Config File Boundary Information ( Zone 0 ) --------------- +-----------------------------------------------------------------------+ | Marker Type| Marker Name| +-----------------------------------------------------------------------+ | Euler wall| BC_3| +-----------------------------------------------------------------------+ | Far-field| BC_1| +-----------------------------------------------------------------------+ | Symmetry plane| 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. 10490 grid points. 54165 volume elements. 3 surface markers. 3448 boundary elements in index 0 (Marker = BC_1). 1565 boundary elements in index 1 (Marker = BC_2). 167 boundary elements in index 2 (Marker = BC_3). 54165 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: 63999.5. Searching for the closest normal neighbors to the surfaces. Storing a mapping from global to local point index. Compute the surface curvature. Max K: 51.6883. Mean K: 0.709733. Standard deviation K: 3.22588. Checking for periodicity. Computing mesh quality statistics for the dual control volumes. +--------------------------------------------------------------+ | Mesh Quality Metric| Minimum| Maximum| +--------------------------------------------------------------+ | Orthogonality Angle (deg.)| 44.3316| 85.098| | CV Face Area Aspect Ratio| 1.16221| 27.4272| | CV Sub-Volume Ratio| 1| 81.5516| +--------------------------------------------------------------+ Setting the multigrid structure. +-------------------------------------------+ | MG Level| CVs|Aggl. Rate| CFL| +-------------------------------------------+ | 0| 10490| 1/1.00| 10| | 1| 1870| 1/5.61| 8.44202| | 2| 389| 1/4.81| 7.5031| +-------------------------------------------+ Finding max control volume width. Semi-span length = 3.87298 m. Wetted area = 7.82006 m^2. Area projection in the x-plane = 0.576038 m^2, y-plane = 0.250011 m^2, z-plane = 3.65657 m^2. Max. coordinate in the x-direction = 2.53651 m, y-direction = 3.87298 m, z-direction = 0.37624 m. Min. coordinate in the x-direction = 0 m, y-direction = -2.47212e-18 m, z-direction = -0.0403729 m. Checking if Euler & Symmetry markers are straight/plane: Boundary marker BC_3 is NOT a single plane. Boundary marker BC_2 is 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| 211798| 1| m^2/s^2| 211798| | Velocity-X| 100.087| 1| m/s| 100.087| | Velocity-Y| 0| 1| m/s| 0| | Velocity-Z| 0| 1| m/s| 0| | Velocity Magnitude| 100.087| 1| m/s| 100.087| +------------------------------------------------------------------------------+ | Mach Number| -| -| -| 0.294118| +------------------------------------------------------------------------------+ 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| 2.5335e-01| -0.750102| 1.605585| 1.225778| 4.719004| -1.220061| | 0| 0| 1| 0.0000e+00| 0.0000e+00| 2.6327e-01| -1.054063| 1.501703| 1.099411| 4.403235| -0.967223| | 0| 0| 2| 0.0000e+00| 0.0000e+00| 2.6159e-01| -1.154784| 1.382975| 0.974644| 4.298316| -0.248219| ----------------------------- Solver Exit ------------------------------- Maximum number of iterations reached (ITER = 3) before convergence. +-----------------------------------------------------------------------+ | Convergence Field | Value | Criterion | Converged | +-----------------------------------------------------------------------+ | rms[Rho]| -1.15478| < -14| No| +-----------------------------------------------------------------------+ ------------------------------------------------------------------------- +-----------------------------------------------------------------------+ | File Writing Summary | Filename | +-----------------------------------------------------------------------+ |SU2 binary restart |restart_flow_aeroelasticSimple_Iterative.dat| Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Iterative.dat). |CSV file |surface_flow_aeroelasticSimple_Iterative.csv| Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Iterative.dat). |Tecplot binary |flow_aeroelasticSimple_Iterative.szplt| Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Iterative.dat). |Tecplot binary surface |surface_flow_aeroelasticSimple_Iterative.szplt| Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Iterative.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) ------------------------ Running PostAnalysis ...... su2 Running PreAnalysis ...... su2 Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = Rib_Root, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = Skin, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 3 Name = Skin_Top, index = 1 Name = Skin_Bottom, index = 2 Name = Skin_Tip, index = 3 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Skin, index = 1 Name = Rib_Root, index = 2 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 180 Number of elements = 194 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 32 Elemental Quad4 = 162 Aero_Reference value is NULL - No aero reference parameters set Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 2 Property name - Rib_Root Property name - Skin Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - pressureAero No "groupName" specified for Load tuple pressureAero, going to use load name Done getting FEA loads Optimization Control tuple is NULL - Default optimization control is used Getting FEA optimization control....... Done getting FEA Optimization Control Design_Variable tuple is NULL - No design variables applied Design_Constraint tuple is NULL - No design constraints applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Reading SU2 AeroLoad File - surface_flow_aeroelasticSimple_Iterative.csv Number of variables = 16 Number of data points = 89 CAPS Info: Bound 'Skin_Top' Normalized Integrated 'Pressure' Rank 0: src = 3.095732e+09, tgt = 3.095732e+09, diff = 1.167212e+02 Reading SU2 AeroLoad File - surface_flow_aeroelasticSimple_Iterative.csv Number of variables = 16 Number of data points = 89 CAPS Info: Bound 'Skin_Bottom' Normalized Integrated 'Pressure' Rank 0: src = 3.014252e+09, tgt = 3.014252e+09, diff = 2.113069e+02 Reading SU2 AeroLoad File - surface_flow_aeroelasticSimple_Iterative.csv Number of variables = 16 Number of data points = 89 CAPS Info: Bound 'Skin_Tip' Normalized Integrated 'Pressure' Rank 0: src = 3.928484e+07, tgt = 3.928484e+07, diff = 7.997701e-02 Extracting external pressure loads from data transfer.... TransferName = Skin_Top Number of Elements = 81 (total = 81) Extracting external pressure loads from data transfer.... TransferName = Skin_Bottom Number of Elements = 81 (total = 162) Extracting external pressure loads from data transfer.... TransferName = Skin_Tip Number of Elements = 16 (total = 178) Writing Astros grid and connectivity file (in free field format) .... Finished writing Astros grid file Writing subElement types (if any) - appending mesh file Writing Astros instruction file.... Writing analysis cards Writing load ADD cards Writing constraint cards--each subcase individually Writing load cards Writing material cards Writing property cards Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG Writing SU2 data transfer files Writing SU2 Motion File - aeroelasticSimple_Iterative_motion.dat Warning: The su2 cfg file will be overwritten! Write SU2 configuration file for version "Harrier (8.0.1)" Running SU2...... ------------------------------------------------------------------------- | ___ _ _ ___ | | / __| | | |_ ) 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/aflr3_CAPS.su2 ---------------- Grid deformation parameters ( Zone 0 ) ---------------- Grid deformation using a linear elasticity method. -------------------- Output Information ( Zone 0 ) ---------------------- Output mesh file name: ../aflr3/aflr3_CAPS.su2. Cell stiffness scaled by distance to nearest solid surface. ------------- Config File Boundary Information ( Zone 0 ) --------------- +-----------------------------------------------------------------------+ | Marker Type| Marker Name| +-----------------------------------------------------------------------+ | Euler wall| BC_3| +-----------------------------------------------------------------------+ | Far-field| BC_1| +-----------------------------------------------------------------------+ | Symmetry plane| BC_2| +-----------------------------------------------------------------------+ Three dimensional problem. 10490 grid points. 54165 volume elements. 3 surface markers. 3448 boundary elements in index 0 (Marker = BC_1). 1565 boundary elements in index 1 (Marker = BC_2). 167 boundary elements in index 2 (Marker = BC_3). 54165 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: 63999.5. 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 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 0.924554 seconds on 1 core. ----------------------- Write deformed grid files ----------------------- |SU2 mesh |../aflr3/aflr3_CAPS.su2 | |CSV file |surface_deformed.csv | |Tecplot binary |volume_deformed.szplt | |Tecplot binary surface |surface_deformed.szplt | 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) ------------------------ ------------------------------------------------------------------------- | ___ _ _ ___ | | / __| | | |_ ) 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: 0.294118. 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_3. Surface(s) plotted in the output file: BC_3. Surface(s) affected by the design variables: BC_3. Input mesh file name: ../aflr3/aflr3_CAPS.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: 3. 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_aeroelasticSimple_Iterative.dat. Surface file name: surface_flow_aeroelasticSimple_Iterative. Volume file name: flow_aeroelasticSimple_Iterative. Restart file name: restart_flow_aeroelasticSimple_Iterative.dat. ------------- Config File Boundary Information ( Zone 0 ) --------------- +-----------------------------------------------------------------------+ | Marker Type| Marker Name| +-----------------------------------------------------------------------+ | Euler wall| BC_3| +-----------------------------------------------------------------------+ | Far-field| BC_1| +-----------------------------------------------------------------------+ | Symmetry plane| 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. 10490 grid points. 54165 volume elements. 3 surface markers. 3448 boundary elements in index 0 (Marker = BC_1). 1565 boundary elements in index 1 (Marker = BC_2). 167 boundary elements in index 2 (Marker = BC_3). 54165 tetrahedra. Setting point connectivity. Renumbering points (Reverse Cuthill McKee Ordering). Recomputing point connectivity. Setting element connectivity. Checking the numerical grid orientation. There has been a re-orientation of 749 TETRAHEDRON volume elements. There has been a re-orientation of 26 TRIANGLE surface elements. Identifying edges and vertices. Setting the control volume structure. Volume of the computational grid: 64498.3. Searching for the closest normal neighbors to the surfaces. Storing a mapping from global to local point index. Compute the surface curvature. Max K: 22.0948. Mean K: 0.527216. Standard deviation K: 1.7157. Checking for periodicity. Computing mesh quality statistics for the dual control volumes. +--------------------------------------------------------------+ | Mesh Quality Metric| Minimum| Maximum| +--------------------------------------------------------------+ | Orthogonality Angle (deg.)| 7.2469| 85.7269| | CV Face Area Aspect Ratio| 1.16376| 323.111| | CV Sub-Volume Ratio| 1| 13009| +--------------------------------------------------------------+ Setting the multigrid structure. +-------------------------------------------+ | MG Level| CVs|Aggl. Rate| CFL| +-------------------------------------------+ | 0| 10490| 1/1.00| 10| | 1| 1870| 1/5.61| 8.44202| | 2| 389| 1/4.81| 7.5031| +-------------------------------------------+ Finding max control volume width. Semi-span length = 4.41037 m. Wetted area = 165.297 m^2. Area projection in the x-plane = 64.0735 m^2, y-plane = 33.8815 m^2, z-plane = 4.99829 m^2. Max. coordinate in the x-direction = 2.77394 m, y-direction = 4.41037 m, z-direction = 16.2689 m. Min. coordinate in the x-direction = -0.658365 m, y-direction = -0.0470459 m, z-direction = -19.3812 m. Checking if Euler & Symmetry markers are straight/plane: Boundary marker BC_3 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| 211798| 1| m^2/s^2| 211798| | Velocity-X| 100.087| 1| m/s| 100.087| | Velocity-Y| 0| 1| m/s| 0| | Velocity-Z| 0| 1| m/s| 0| | Velocity Magnitude| 100.087| 1| m/s| 100.087| +------------------------------------------------------------------------------+ | Mach Number| -| -| -| 0.294118| +------------------------------------------------------------------------------+ 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| 2.4578e-01| 1.816485| 4.769066| 4.879546| 7.285591| -0.019238| | 0| 0| 1| 0.0000e+00| 0.0000e+00| 2.4767e-01| 2.241333| 4.856618| 4.845215| 7.696248| -0.040086| | 0| 0| 2| 0.0000e+00| 0.0000e+00| 2.5016e-01| 2.384284| 4.932235| 4.860433| 7.812202| -0.053014| ----------------------------- Solver Exit ------------------------------- Maximum number of iterations reached (ITER = 3) before convergence. +-----------------------------------------------------------------------+ | Convergence Field | Value | Criterion | Converged | +-----------------------------------------------------------------------+ | rms[Rho]| 2.38428| < -14| No| +-----------------------------------------------------------------------+ ------------------------------------------------------------------------- +-----------------------------------------------------------------------+ | File Writing Summary | Filename | +-----------------------------------------------------------------------+ |SU2 binary restart |restart_flow_aeroelasticSimple_Iterative.dat| Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Iterative.dat). |CSV file |surface_flow_aeroelasticSimple_Iterative.csv| Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Iterative.dat). |Tecplot binary |flow_aeroelasticSimple_Iterative.szplt| Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Iterative.dat). |Tecplot binary surface |surface_flow_aeroelasticSimple_Iterative.szplt| Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Iterative.dat). +-----------------------------------------------------------------------+ Warning: there are 27 non-physical points in the solution. Warning: 2 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) ------------------------ Running PostAnalysis ...... su2 Running PreAnalysis ...... su2 Reading SU2 AeroLoad File - surface_flow_aeroelasticSimple_Iterative.csv Number of variables = 16 Number of data points = 89 CAPS Info: Bound 'Skin_Top' Normalized Integrated 'Pressure' Rank 0: src = 2.016562e+09, tgt = 2.016562e+09, diff = 3.305119e+02 Reading SU2 AeroLoad File - surface_flow_aeroelasticSimple_Iterative.csv Number of variables = 16 Number of data points = 89 CAPS Info: Bound 'Skin_Bottom' Normalized Integrated 'Pressure' Rank 0: src = 1.492384e+09, tgt = 1.492384e+09, diff = 4.421872e+02 Reading SU2 AeroLoad File - surface_flow_aeroelasticSimple_Iterative.csv Number of variables = 16 Number of data points = 89 CAPS Info: Bound 'Skin_Tip' Normalized Integrated 'Pressure' Rank 0: src = 2.354248e+07, tgt = 2.354248e+07, diff = 6.210823e-03 Extracting external pressure loads from data transfer.... TransferName = Skin_Top Number of Elements = 81 (total = 81) Extracting external pressure loads from data transfer.... TransferName = Skin_Bottom Number of Elements = 81 (total = 162) Extracting external pressure loads from data transfer.... TransferName = Skin_Tip Number of Elements = 16 (total = 178) Writing Astros grid and connectivity file (in free field format) .... Finished writing Astros grid file Writing subElement types (if any) - appending mesh file Writing Astros instruction file.... Writing analysis cards Writing load ADD cards Writing constraint cards--each subcase individually Writing load cards Writing material cards Writing property cards Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG Writing SU2 data transfer files Writing SU2 Motion File - aeroelasticSimple_Iterative_motion.dat Warning: The su2 cfg file will be overwritten! Write SU2 configuration file for version "Harrier (8.0.1)" Running SU2...... ------------------------------------------------------------------------- | ___ _ _ ___ | | / __| | | |_ ) 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/aflr3_CAPS.su2 ---------------- Grid deformation parameters ( Zone 0 ) ---------------- Grid deformation using a linear elasticity method. -------------------- Output Information ( Zone 0 ) ---------------------- Output mesh file name: ../aflr3/aflr3_CAPS.su2. Cell stiffness scaled by distance to nearest solid surface. ------------- Config File Boundary Information ( Zone 0 ) --------------- +-----------------------------------------------------------------------+ | Marker Type| Marker Name| +-----------------------------------------------------------------------+ | Euler wall| BC_3| +-----------------------------------------------------------------------+ | Far-field| BC_1| +-----------------------------------------------------------------------+ | Symmetry plane| BC_2| +-----------------------------------------------------------------------+ Three dimensional problem. 10490 grid points. 54165 volume elements. 3 surface markers. 3448 boundary elements in index 0 (Marker = BC_1). 1565 boundary elements in index 1 (Marker = BC_2). 167 boundary elements in index 2 (Marker = BC_3). 54165 tetrahedra. ----------------------- Preprocessing computations ---------------------- Setting local point connectivity. Checking the numerical grid orientation of the interior elements. There has been a re-orientation of 749 TETRAHEDRON volume elements. There has been a re-orientation of 26 TRIANGLE surface elements. Identify edges and vertices. Setting the bound control volume structure. Volume of the computational grid: 64498.3. 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 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 1.065473 seconds on 1 core. ----------------------- Write deformed grid files ----------------------- |SU2 mesh |../aflr3/aflr3_CAPS.su2 | |CSV file |surface_deformed.csv | |Tecplot binary |volume_deformed.szplt | |Tecplot binary surface |surface_deformed.szplt | 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) ------------------------ ------------------------------------------------------------------------- | ___ _ _ ___ | | / __| | | |_ ) 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: 0.294118. 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_3. Surface(s) plotted in the output file: BC_3. Surface(s) affected by the design variables: BC_3. Input mesh file name: ../aflr3/aflr3_CAPS.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: 3. 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_aeroelasticSimple_Iterative.dat. Surface file name: surface_flow_aeroelasticSimple_Iterative. Volume file name: flow_aeroelasticSimple_Iterative. Restart file name: restart_flow_aeroelasticSimple_Iterative.dat. ------------- Config File Boundary Information ( Zone 0 ) --------------- +-----------------------------------------------------------------------+ | Marker Type| Marker Name| +-----------------------------------------------------------------------+ | Euler wall| BC_3| +-----------------------------------------------------------------------+ | Far-field| BC_1| +-----------------------------------------------------------------------+ | Symmetry plane| 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. 10490 grid points. 54165 volume elements. 3 surface markers. 3448 boundary elements in index 0 (Marker = BC_1). 1565 boundary elements in index 1 (Marker = BC_2). 167 boundary elements in index 2 (Marker = BC_3). 54165 tetrahedra. Setting point connectivity. Renumbering points (Reverse Cuthill McKee Ordering). Recomputing point connectivity. Setting element connectivity. Checking the numerical grid orientation. There has been a re-orientation of 7226 TETRAHEDRON volume elements. There has been a re-orientation of 206 TRIANGLE surface elements. Identifying edges and vertices. Setting the control volume structure. Volume of the computational grid: 66889.1. Searching for the closest normal neighbors to the surfaces. Storing a mapping from global to local point index. Compute the surface curvature. Max K: 273.938. Mean K: 1.56756. Standard deviation K: 9.44503. Checking for periodicity. Computing mesh quality statistics for the dual control volumes. +--------------------------------------------------------------+ | Mesh Quality Metric| Minimum| Maximum| +--------------------------------------------------------------+ | Orthogonality Angle (deg.)| 0.764151| 84.0172| | CV Face Area Aspect Ratio| 1.22546| 165.439| | CV Sub-Volume Ratio| 1| 500673| +--------------------------------------------------------------+ Setting the multigrid structure. +-------------------------------------------+ | MG Level| CVs|Aggl. Rate| CFL| +-------------------------------------------+ | 0| 10490| 1/1.00| 10| | 1| 1874| 1/5.6| 8.44804| | 2| 394| 1/4.76| 7.53511| +-------------------------------------------+ Finding max control volume width. Semi-span length = 5.82231 m. Wetted area = 324.882 m^2. Area projection in the x-plane = 143.505 m^2, y-plane = 129.703 m^2, z-plane = 26.6043 m^2. Max. coordinate in the x-direction = 8.09968 m, y-direction = 5.82231 m, z-direction = 29.9711 m. Min. coordinate in the x-direction = 0.0260146 m, y-direction = -0.933278 m, z-direction = -41.6074 m. Checking if Euler & Symmetry markers are straight/plane: Boundary marker BC_3 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| 211798| 1| m^2/s^2| 211798| | Velocity-X| 100.087| 1| m/s| 100.087| | Velocity-Y| 0| 1| m/s| 0| | Velocity-Z| 0| 1| m/s| 0| | Velocity Magnitude| 100.087| 1| m/s| 100.087| +------------------------------------------------------------------------------+ | Mach Number| -| -| -| 0.294118| +------------------------------------------------------------------------------+ 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| 2.3183e-01| 2.533258| 5.487132| 5.285803| 8.002364| 0.610334| | 0| 0| 1| 0.0000e+00| 0.0000e+00| 2.6563e-01| 2.546660| 5.300889| 5.160160| 7.964705| 0.450573| | 0| 0| 2| 0.0000e+00| 0.0000e+00| 2.5638e-01| 2.637735| 5.231933| 5.225949| 8.013544| 0.420275| ----------------------------- Solver Exit ------------------------------- Maximum number of iterations reached (ITER = 3) before convergence. +-----------------------------------------------------------------------+ | Convergence Field | Value | Criterion | Converged | +-----------------------------------------------------------------------+ | rms[Rho]| 2.63773| < -14| No| +-----------------------------------------------------------------------+ ------------------------------------------------------------------------- +-----------------------------------------------------------------------+ | File Writing Summary | Filename | +-----------------------------------------------------------------------+ |SU2 binary restart |restart_flow_aeroelasticSimple_Iterative.dat| Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Iterative.dat). |CSV file |surface_flow_aeroelasticSimple_Iterative.csv| Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Iterative.dat). |Tecplot binary |flow_aeroelasticSimple_Iterative.szplt| Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Iterative.dat). |Tecplot binary surface |surface_flow_aeroelasticSimple_Iterative.szplt| Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Iterative.dat). +-----------------------------------------------------------------------+ Warning: there are 149 non-physical points in the solution. Warning: 13 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) ------------------------ Running PostAnalysis ...... su2 Running PreAnalysis ...... su2 Reading SU2 AeroLoad File - surface_flow_aeroelasticSimple_Iterative.csv Number of variables = 16 Number of data points = 89 CAPS Info: Bound 'Skin_Top' Normalized Integrated 'Pressure' Rank 0: src = 1.529337e+09, tgt = 1.529336e+09, diff = 3.412616e+01 Reading SU2 AeroLoad File - surface_flow_aeroelasticSimple_Iterative.csv Number of variables = 16 Number of data points = 89 CAPS Info: Bound 'Skin_Bottom' Normalized Integrated 'Pressure' Rank 0: src = 1.234296e+09, tgt = 1.234296e+09, diff = 1.286251e+02 Reading SU2 AeroLoad File - surface_flow_aeroelasticSimple_Iterative.csv Number of variables = 16 Number of data points = 89 CAPS Info: Bound 'Skin_Tip' Normalized Integrated 'Pressure' Rank 0: src = 5.628084e+06, tgt = 5.628084e+06, diff = 4.735513e-02 Extracting external pressure loads from data transfer.... TransferName = Skin_Top Number of Elements = 81 (total = 81) Extracting external pressure loads from data transfer.... TransferName = Skin_Bottom Number of Elements = 81 (total = 162) Extracting external pressure loads from data transfer.... TransferName = Skin_Tip Number of Elements = 16 (total = 178) Writing Astros grid and connectivity file (in free field format) .... Finished writing Astros grid file Writing subElement types (if any) - appending mesh file Writing Astros instruction file.... Writing analysis cards Writing load ADD cards Writing constraint cards--each subcase individually Writing load cards Writing material cards Writing property cards Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG Writing SU2 data transfer files Writing SU2 Motion File - aeroelasticSimple_Iterative_motion.dat Warning: The su2 cfg file will be overwritten! Write SU2 configuration file for version "Harrier (8.0.1)" Running SU2...... ------------------------------------------------------------------------- | ___ _ _ ___ | | / __| | | |_ ) 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/aflr3_CAPS.su2 ---------------- Grid deformation parameters ( Zone 0 ) ---------------- Grid deformation using a linear elasticity method. -------------------- Output Information ( Zone 0 ) ---------------------- Output mesh file name: ../aflr3/aflr3_CAPS.su2. Cell stiffness scaled by distance to nearest solid surface. ------------- Config File Boundary Information ( Zone 0 ) --------------- +-----------------------------------------------------------------------+ | Marker Type| Marker Name| +-----------------------------------------------------------------------+ | Euler wall| BC_3| +-----------------------------------------------------------------------+ | Far-field| BC_1| +-----------------------------------------------------------------------+ | Symmetry plane| BC_2| +-----------------------------------------------------------------------+ Three dimensional problem. 10490 grid points. 54165 volume elements. 3 surface markers. 3448 boundary elements in index 0 (Marker = BC_1). 1565 boundary elements in index 1 (Marker = BC_2). 167 boundary elements in index 2 (Marker = BC_3). 54165 tetrahedra. ----------------------- Preprocessing computations ---------------------- Setting local point connectivity. Checking the numerical grid orientation of the interior elements. There has been a re-orientation of 7226 TETRAHEDRON volume elements. There has been a re-orientation of 206 TRIANGLE surface elements. Identify edges and vertices. Setting the bound control volume structure. Volume of the computational grid: 66889.1. 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 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 30.067079 seconds on 1 core. ----------------------- Write deformed grid files ----------------------- |SU2 mesh |../aflr3/aflr3_CAPS.su2 | |CSV file |surface_deformed.csv | |Tecplot binary |volume_deformed.szplt | |Tecplot binary surface |surface_deformed.szplt | 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) ------------------------ ------------------------------------------------------------------------- | ___ _ _ ___ | | / __| | | |_ ) 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: 0.294118. 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_3. Surface(s) plotted in the output file: BC_3. Surface(s) affected by the design variables: BC_3. Input mesh file name: ../aflr3/aflr3_CAPS.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: 3. 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_aeroelasticSimple_Iterative.dat. Surface file name: surface_flow_aeroelasticSimple_Iterative. Volume file name: flow_aeroelasticSimple_Iterative. Restart file name: restart_flow_aeroelasticSimple_Iterative.dat. ------------- Config File Boundary Information ( Zone 0 ) --------------- +-----------------------------------------------------------------------+ | Marker Type| Marker Name| +-----------------------------------------------------------------------+ | Euler wall| BC_3| +-----------------------------------------------------------------------+ | Far-field| BC_1| +-----------------------------------------------------------------------+ | Symmetry plane| 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. 10490 grid points. 54165 volume elements. 3 surface markers. 3448 boundary elements in index 0 (Marker = BC_1). 1565 boundary elements in index 1 (Marker = BC_2). 167 boundary elements in index 2 (Marker = BC_3). 54165 tetrahedra. Setting point connectivity. Renumbering points (Reverse Cuthill McKee Ordering). Recomputing point connectivity. Setting element connectivity. Checking the numerical grid orientation. There has been a re-orientation of 21656 TETRAHEDRON volume elements. There has been a re-orientation of 781 TRIANGLE surface elements. Identifying edges and vertices. Setting the control volume structure. Volume of the computational grid: 9.57518e+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: 64.2172. Mean K: 1.24404. Standard deviation K: 4.50057. Checking for periodicity. Computing mesh quality statistics for the dual control volumes. +--------------------------------------------------------------+ | Mesh Quality Metric| Minimum| Maximum| +--------------------------------------------------------------+ | Orthogonality Angle (deg.)| 0.199724| 82.2754| | CV Face Area Aspect Ratio| 1.51901| 568.479| | CV Sub-Volume Ratio| 1| 363347| +--------------------------------------------------------------+ Setting the multigrid structure. +-------------------------------------------+ | MG Level| CVs|Aggl. Rate| CFL| +-------------------------------------------+ | 0| 10490| 1/1.00| 10| | 1| 1867| 1/5.62| 8.43751| | 2| 383| 1/4.87| 7.46432| +-------------------------------------------+ Finding max control volume width. Semi-span length = 1.89332 m. Wetted area = 3244.51 m^2. Area projection in the x-plane = 382.333 m^2, y-plane = 822.101 m^2, z-plane = 47.4578 m^2. Max. coordinate in the x-direction = 3.14656 m, y-direction = 1.89332 m, z-direction = 335.653 m. Min. coordinate in the x-direction = -0.577333 m, y-direction = -20.5655 m, z-direction = -2.52092 m. Checking if Euler & Symmetry markers are straight/plane: Boundary marker BC_3 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| 211798| 1| m^2/s^2| 211798| | Velocity-X| 100.087| 1| m/s| 100.087| | Velocity-Y| 0| 1| m/s| 0| | Velocity-Z| 0| 1| m/s| 0| | Velocity Magnitude| 100.087| 1| m/s| 100.087| +------------------------------------------------------------------------------+ | Mach Number| -| -| -| 0.294118| +------------------------------------------------------------------------------+ 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| 2.7743e-01| 4.230882| 7.196541| 7.171336| 9.699988| -0.009721| | 0| 0| 1| 0.0000e+00| 0.0000e+00| 3.2232e-01| 4.757294| 7.278987| 7.271916| 10.158721| -0.008032| | 0| 0| 2| 0.0000e+00| 0.0000e+00| 3.2504e-01| 4.810154| 7.321114| 7.265251| 10.179303| -0.008305| ----------------------------- Solver Exit ------------------------------- Maximum number of iterations reached (ITER = 3) before convergence. +-----------------------------------------------------------------------+ | Convergence Field | Value | Criterion | Converged | +-----------------------------------------------------------------------+ | rms[Rho]| 4.81015| < -14| No| +-----------------------------------------------------------------------+ ------------------------------------------------------------------------- +-----------------------------------------------------------------------+ | File Writing Summary | Filename | +-----------------------------------------------------------------------+ |SU2 binary restart |restart_flow_aeroelasticSimple_Iterative.dat| Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Iterative.dat). |CSV file |surface_flow_aeroelasticSimple_Iterative.csv| Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Iterative.dat). |Tecplot binary |flow_aeroelasticSimple_Iterative.szplt| Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Iterative.dat). |Tecplot binary surface |surface_flow_aeroelasticSimple_Iterative.szplt| Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Iterative.dat). +-----------------------------------------------------------------------+ Warning: there are 430 non-physical points in the solution. Warning: 43 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) ------------------------ Running PostAnalysis ...... su2 Cl = -157.195727 Cd = 18928.839931 real 1m3.598s user 0m46.747s sys 0m2.710s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case aeroelasticSimple_Iterative_SU2_and_Astros.py passed (as expected) ================================================= ================================================= + echo 'aeroelastic_Iterative_SU2_and_Astros.py test;' + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/pyCAPSlog.txt aeroelastic_Iterative_SU2_and_Astros.py test; + python -u aeroelastic_Iterative_SU2_and_Astros.py -outLevel=0 + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/pyCAPSlog.txt Running PreAnalysis ...... su2 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Farfield, index = 1 Name = SymmPlane, index = 2 Name = Skin, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 AFLR2 : --------------------------------------- AFLR2 : AFLR2 LIBRARY AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR2 : TRIA/QUAD GRID GENERATOR AFLR2 : Version Number 9.17.15 AFLR2 : Version Date 04/23/24 @ 12:51AM AFLR2 : Compile OS Darwin 23.4.0 arm64 AFLR2 : Compile Date 04/23/24 @ 12:51AM 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 11.5.14 AFLR4 : Version Date 04/18/24 @ 12:45PM AFLR4 : Compile OS Darwin 23.4.0 arm64 AFLR4 : Compile Date 04/18/24 @ 03:04PM AFLR4 : Copyright 1994-2021, D.L. Marcum AFLR4 : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : EGADS CAD Geometry Setup EGADS : Model has 1 Active Bodies EGADS : Body 0 is a SolidBody EGADS : Body 0 has 1 Shells EGADS : Body 0 has 9 Faces EGADS : Body 0 has 18 Edges EGADS : Body 0 has 10 Loops EGADS : Body 0 has 12 Nodes EGADS : Check Grid BCs EGADS : Grid BCs are OK EGADS : Face Neighbor-Faces Information EGADS : QC = Face Quad Combination Flag EGADS : IER = Face Isolated Edge Refinement Flag EGADS : ER = Face Edge Refinement Factor EGADS : Not applicable for Faces with a FarField Grid BC. EGADS : SF = Face Scale Factor EGADS : Not applicable for Faces with a FarField Grid BC. EGADS : Face Body QC IER ER Scale Neighbor EGADS : ID Active ID Flag Flag Weight Factor Faces EGADS : 1 Yes 0 0 1 0 1 2 3 4 5 EGADS : 2 Yes 0 0 1 0 1 1 3 5 6 EGADS : 3 Yes 0 0 1 0 1 1 2 4 6 7 8 EGADS : 4 Yes 0 0 1 0 1 1 3 5 6 EGADS : 5 Yes 0 0 1 0 1 1 2 4 6 EGADS : 6 Yes 0 0 1 0 1 2 3 4 5 EGADS : 7 Yes 0 0 1 0 1 3 8 9 EGADS : 8 Yes 0 0 1 0 1 3 7 9 EGADS : 9 Yes 0 0 1 0 1 7 8 EGADS : Face Edges Information EGADS : Face Edges EGADS : 1 1 2 -3 -4 EGADS : 2 5 6 -7 -1 EGADS : 3 -2 7 9 -8 -10 -11 EGADS : 4 -12 3 8 -13 EGADS : 5 4 12 -14 -5 EGADS : 6 -6 14 13 -9 EGADS : 7 15 10 -17 -16 EGADS : 8 17 11 -15 -18 EGADS : 9 16 18 EGADS : Face Loops Information EGADS : Face Loops EGADS : 1 1 EGADS : 2 2 EGADS : 3 3 4 EGADS : 4 5 EGADS : 5 6 EGADS : 6 7 EGADS : 7 8 EGADS : 8 9 EGADS : 9 10 EGADS : Loop Edges Information EGADS : Loop Active Edges EGADS : 1 Yes 1 2 -3 -4 EGADS : 2 Yes 5 6 -7 -1 EGADS : 3 Yes -2 7 9 -8 EGADS : 4 Yes -10 -11 EGADS : 5 Yes -12 3 8 -13 EGADS : 6 Yes 4 12 -14 -5 EGADS : 7 Yes -6 14 13 -9 EGADS : 8 Yes 15 10 -17 -16 EGADS : 9 Yes 17 11 -15 -18 EGADS : 10 Yes 16 18 EGADS : Edge Node, Scale Factor, and Neighbor-Faces Information EGADS : ESF = Edge Scale Factor EGADS : Not applicable for DEGENERATE Edges or Edges with a FarField EGADS : Grid BC Neighbor Face. EGADS : Neighbor EGADS : Edge Body Active Node1 Node2 ESF Faces EGADS : 1 0 Yes 2 1 1 1 2 EGADS : 2 0 Yes 1 3 1 1 3 EGADS : 3 0 Yes 4 3 1 1 4 EGADS : 4 0 Yes 2 4 1 1 5 EGADS : 5 0 Yes 2 5 1 2 5 EGADS : 6 0 Yes 5 6 1 2 6 EGADS : 7 0 Yes 1 6 1 2 3 EGADS : 8 0 Yes 3 7 1 3 4 EGADS : 9 0 Yes 6 7 1 3 6 EGADS : 10 0 Yes 8 9 1 3 7 EGADS : 11 0 Yes 9 8 1 3 8 EGADS : 12 0 Yes 4 10 1 4 5 EGADS : 13 0 Yes 10 7 1 4 6 EGADS : 14 0 Yes 5 10 1 5 6 EGADS : 15 0 Yes 11 8 1 7 8 EGADS : 16 0 Yes 11 12 1 7 9 EGADS : 17 0 Yes 12 9 1 7 8 EGADS : 18 0 Yes 12 11 1 8 9 EGADS : Node Information EGADS : Node Active Coordinates EGADS : 1 Yes 0 0 0 EGADS : 2 Yes 0 40 0 EGADS : 3 Yes 0 0 20 EGADS : 4 Yes 0 40 20 EGADS : 5 Yes 20 40 0 EGADS : 6 Yes 20 0 0 EGADS : 7 Yes 20 0 20 EGADS : 8 Yes 1.61374306 0 0 EGADS : 9 Yes 0 0 0 EGADS : 10 Yes 20 40 20 EGADS : 11 Yes 2.53650745 3.87298335 0.334116517 EGADS : 12 Yes 1.57194608 3.87298335 0.249728332 EGADS : Face and Edge Match Information EGADS : No Face Matches Found AFLR4 : Surface Mesh Spacing Setup AFLR4 : Max Bounding Box Length = 40 AFLR4 : Min Bounding Box Length = 40 AFLR4 : Max Ref Bounding Box Length = 40 AFLR4 : Min Ref Bounding Box Length = 40 AFLR4 : Reference Length = 1.61374 AFLR4 : BL Thickness = 0 AFLR4 : Abs Min Surf Spacing = 0.00403436 AFLR4 : Min Surf Spacing = 0.161374 AFLR4 : Max Surf Spacing = 1.21031 AFLR4 : Global Scale Factor = 2 AFLR4 : Geometry Definition Information AFLR4 : Definition Definition Composite Grid BC AFLR4 : ID Type ID Type AFLR4 : 0 glue-only composite - - AFLR4 : 1 CAD geometry 0 STD w/BL AFLR4 : 2 CAD geometry 0 STD w/BL AFLR4 : 3 CAD geometry 0 STD w/BL AFLR4 : 4 CAD geometry 0 STD w/BL AFLR4 : 5 CAD geometry 0 STD w/BL AFLR4 : 6 CAD geometry 0 STD w/BL AFLR4 : 7 CAD geometry 0 STD w/BL AFLR4 : 8 CAD geometry 0 STD w/BL AFLR4 : 9 CAD geometry 0 STD w/BL AFLR4 : Define CAD surface definition 1 AFLR4 : Define CAD surface definition 2 AFLR4 : Define CAD surface definition 3 AFLR4 : Define CAD surface definition 4 AFLR4 : Define CAD surface definition 5 AFLR4 : Define CAD surface definition 6 AFLR4 : Define CAD surface definition 7 AFLR4 : Define CAD surface definition 8 AFLR4 : Define CAD surface definition 9 AFLR4 : Surface Grid Generation AFLR4 : Generate optimal mesh on surface definition 1 AFLR2 : Nodes, Trias,Quads= 376 682 0 AFLR4 : Nodes, Trias,Quads= 381 692 0 AFLR4 : Generate optimal mesh on surface definition 2 AFLR2 : Nodes, Trias,Quads= 374 678 0 AFLR4 : Nodes, Trias,Quads= 380 690 0 AFLR4 : Generate optimal mesh on surface definition 3 AFLR2 : Nodes, Trias,Quads= 927 1777 0 AFLR4 : Nodes, Trias,Quads= 821 1565 0 AFLR4 : Generate optimal mesh on surface definition 4 AFLR2 : Nodes, Trias,Quads= 376 682 0 AFLR4 : Nodes, Trias,Quads= 380 690 0 AFLR4 : Generate optimal mesh on surface definition 5 AFLR2 : Nodes, Trias,Quads= 374 678 0 AFLR4 : Nodes, Trias,Quads= 380 690 0 AFLR4 : Generate optimal mesh on surface definition 6 AFLR2 : Nodes, Trias,Quads= 376 682 0 AFLR4 : Nodes, Trias,Quads= 378 686 0 AFLR4 : Generate optimal mesh on surface definition 7 AFLR2 : Nodes, Trias,Quads= 63 96 0 AFLR4 : Nodes, Trias,Quads= 55 80 0 AFLR4 : Generate optimal mesh on surface definition 8 AFLR2 : Nodes, Trias,Quads= 64 96 0 AFLR4 : Nodes, Trias,Quads= 57 82 0 AFLR4 : Generate optimal mesh on surface definition 9 AFLR2 : Nodes, Trias,Quads= 11 13 0 AFLR4 : Nodes, Trias,Quads= 7 5 0 DGEOM : Add surface definitions to composite definition 0 DGEOM : Glue composite surface definition 0 DGEOM : Nodes,Faces,BEdges= 2592 5180 482 AFLR4 : Auto Mode Turned OFF OVERALL : CPU Time = 0.061 seconds Body 1 (of 1) Number of nodes = 2592 Number of elements = 5180 Number of triangle elements = 5180 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 2592 Total number of elements = 5180 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Farfield, index = 1 Name = SymmPlane, index = 2 Name = Skin, index = 3 Getting volume mesh AFLR2 : --------------------------------------- AFLR2 : AFLR2 LIBRARY AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR2 : TRIA/QUAD GRID GENERATOR AFLR2 : Version Number 9.17.15 AFLR2 : Version Date 04/23/24 @ 12:51AM AFLR2 : Compile OS Darwin 23.4.0 arm64 AFLR2 : Compile Date 04/23/24 @ 12:51AM 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 11.5.14 AFLR4 : Version Date 04/18/24 @ 12:45PM AFLR4 : Compile OS Darwin 23.4.0 arm64 AFLR4 : Compile Date 04/18/24 @ 03:04PM AFLR4 : Copyright 1994-2021, D.L. Marcum AFLR4 : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 10490 Number of elements = 59345 Number of triangles = 5180 Number of quadrilatarals = 0 Number of tetrahedrals = 54165 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing SU2 file .... Finished writing SU2 file Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Skin Boundary condition name - SymmPlane Done getting CFD boundary conditions Writing SU2 data transfer files Writing SU2 Motion File - aeroelastic_Iterative_motion.dat Warning: The su2 cfg file will be overwritten! Write SU2 configuration file for version "Harrier (8.0.1)" 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: 0.294118. 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_3. Surface(s) plotted in the output file: BC_3. Surface(s) affected by the design variables: BC_3. Input mesh file name: ../aflr3/aflr3_CAPS.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: 3. 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_aeroelastic_Iterative.dat. Surface file name: surface_flow_aeroelastic_Iterative. Volume file name: flow_aeroelastic_Iterative. Restart file name: restart_flow_aeroelastic_Iterative.dat. ------------- Config File Boundary Information ( Zone 0 ) --------------- +-----------------------------------------------------------------------+ | Marker Type| Marker Name| +-----------------------------------------------------------------------+ | Euler wall| BC_3| +-----------------------------------------------------------------------+ | Far-field| BC_1| +-----------------------------------------------------------------------+ | Symmetry plane| 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. 10490 grid points. 54165 volume elements. 3 surface markers. 3448 boundary elements in index 0 (Marker = BC_1). 1565 boundary elements in index 1 (Marker = BC_2). 167 boundary elements in index 2 (Marker = BC_3). 54165 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: 63999.5. Searching for the closest normal neighbors to the surfaces. Storing a mapping from global to local point index. Compute the surface curvature. Max K: 51.6883. Mean K: 0.709733. Standard deviation K: 3.22588. Checking for periodicity. Computing mesh quality statistics for the dual control volumes. +--------------------------------------------------------------+ | Mesh Quality Metric| Minimum| Maximum| +--------------------------------------------------------------+ | Orthogonality Angle (deg.)| 44.3316| 85.098| | CV Face Area Aspect Ratio| 1.16221| 27.4272| | CV Sub-Volume Ratio| 1| 81.5516| +--------------------------------------------------------------+ Setting the multigrid structure. +-------------------------------------------+ | MG Level| CVs|Aggl. Rate| CFL| +-------------------------------------------+ | 0| 10490| 1/1.00| 10| | 1| 1870| 1/5.61| 8.44202| | 2| 389| 1/4.81| 7.5031| +-------------------------------------------+ Finding max control volume width. Semi-span length = 3.87298 m. Wetted area = 7.82006 m^2. Area projection in the x-plane = 0.576038 m^2, y-plane = 0.250011 m^2, z-plane = 3.65657 m^2. Max. coordinate in the x-direction = 2.53651 m, y-direction = 3.87298 m, z-direction = 0.37624 m. Min. coordinate in the x-direction = 0 m, y-direction = -2.47212e-18 m, z-direction = -0.0403729 m. Checking if Euler & Symmetry markers are straight/plane: Boundary marker BC_3 is NOT a single plane. Boundary marker BC_2 is 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| 211798| 1| m^2/s^2| 211798| | Velocity-X| 100.087| 1| m/s| 100.087| | Velocity-Y| 0| 1| m/s| 0| | Velocity-Z| 0| 1| m/s| 0| | Velocity Magnitude| 100.087| 1| m/s| 100.087| +------------------------------------------------------------------------------+ | Mach Number| -| -| -| 0.294118| +------------------------------------------------------------------------------+ 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| 2.5857e-01| -0.750102| 1.605585| 1.225778| 4.719004| -1.220061| | 0| 0| 1| 0.0000e+00| 0.0000e+00| 2.5957e-01| -1.054063| 1.501703| 1.099411| 4.403235| -0.967223| | 0| 0| 2| 0.0000e+00| 0.0000e+00| 2.6339e-01| -1.154784| 1.382975| 0.974644| 4.298316| -0.248219| ----------------------------- Solver Exit ------------------------------- Maximum number of iterations reached (ITER = 3) before convergence. +-----------------------------------------------------------------------+ | Convergence Field | Value | Criterion | Converged | +-----------------------------------------------------------------------+ | rms[Rho]| -1.15478| < -14| No| +-----------------------------------------------------------------------+ ------------------------------------------------------------------------- +-----------------------------------------------------------------------+ | File Writing Summary | Filename | +-----------------------------------------------------------------------+ |SU2 binary restart |restart_flow_aeroelastic_Iterative.dat| Writing the forces breakdown file (forces_breakdown_aeroelastic_Iterative.dat). |CSV file |surface_flow_aeroelastic_Iterative.csv| Writing the forces breakdown file (forces_breakdown_aeroelastic_Iterative.dat). |Tecplot binary |flow_aeroelastic_Iterative.szplt | Writing the forces breakdown file (forces_breakdown_aeroelastic_Iterative.dat). |Tecplot binary surface |surface_flow_aeroelastic_Iterative.szplt| Writing the forces breakdown file (forces_breakdown_aeroelastic_Iterative.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) ------------------------ Running PostAnalysis ...... su2 Running PreAnalysis ...... su2 Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = Rib_Root, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 3 Name = Skin_Top, index = 1 Name = Skin_Bottom, index = 2 Name = Skin_Tip, index = 3 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Ribs_and_Spars, index = 1 Name = Skin, index = 2 Name = Rib_Root, index = 3 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 746 Number of elements = 898 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 120 Elemental Quad4 = 778 Aero_Reference value is NULL - No aero reference parameters set Getting FEA materials....... Number of materials - 2 Material name - Madeupium Material name - Unobtainium Done getting FEA materials Getting FEA properties....... Number of properties - 3 Property name - Rib_Root Property name - Ribs_and_Spars Property name - Skin Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - pressureAero No "groupName" specified for Load tuple pressureAero, going to use load name Done getting FEA loads Optimization Control tuple is NULL - Default optimization control is used Getting FEA optimization control....... Done getting FEA Optimization Control Design_Variable tuple is NULL - No design variables applied Design_Constraint tuple is NULL - No design constraints applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Reading SU2 AeroLoad File - surface_flow_aeroelastic_Iterative.csv Number of variables = 16 Number of data points = 89 CAPS Info: Bound 'Skin_Top' Normalized Integrated 'Pressure' Rank 0: src = 3.095732e+09, tgt = 3.095732e+09, diff = 6.981874e+01 Reading SU2 AeroLoad File - surface_flow_aeroelastic_Iterative.csv Number of variables = 16 Number of data points = 89 CAPS Info: Bound 'Skin_Bottom' Normalized Integrated 'Pressure' Rank 0: src = 3.014252e+09, tgt = 3.014252e+09, diff = 1.062183e+02 Reading SU2 AeroLoad File - surface_flow_aeroelastic_Iterative.csv Number of variables = 16 Number of data points = 89 CAPS Info: Bound 'Skin_Tip' Normalized Integrated 'Pressure' Rank 0: src = 3.928484e+07, tgt = 3.928484e+07, diff = 3.600868e+00 Extracting external pressure loads from data transfer.... TransferName = Skin_Top Number of Elements = 330 (total = 330) Extracting external pressure loads from data transfer.... TransferName = Skin_Bottom Number of Elements = 330 (total = 660) Extracting external pressure loads from data transfer.... TransferName = Skin_Tip Number of Elements = 30 (total = 690) Writing Astros grid and connectivity file (in free field format) .... Finished writing Astros grid file Writing subElement types (if any) - appending mesh file Writing Astros instruction file.... Writing analysis cards Writing load ADD cards Writing constraint cards--each subcase individually Writing load cards Writing material cards Writing property cards Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG Writing SU2 data transfer files Writing SU2 Motion File - aeroelastic_Iterative_motion.dat Warning: The su2 cfg file will be overwritten! Write SU2 configuration file for version "Harrier (8.0.1)" Running SU2...... ------------------------------------------------------------------------- | ___ _ _ ___ | | / __| | | |_ ) 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/aflr3_CAPS.su2 ---------------- Grid deformation parameters ( Zone 0 ) ---------------- Grid deformation using a linear elasticity method. -------------------- Output Information ( Zone 0 ) ---------------------- Output mesh file name: ../aflr3/aflr3_CAPS.su2. Cell stiffness scaled by distance to nearest solid surface. ------------- Config File Boundary Information ( Zone 0 ) --------------- +-----------------------------------------------------------------------+ | Marker Type| Marker Name| +-----------------------------------------------------------------------+ | Euler wall| BC_3| +-----------------------------------------------------------------------+ | Far-field| BC_1| +-----------------------------------------------------------------------+ | Symmetry plane| BC_2| +-----------------------------------------------------------------------+ Three dimensional problem. 10490 grid points. 54165 volume elements. 3 surface markers. 3448 boundary elements in index 0 (Marker = BC_1). 1565 boundary elements in index 1 (Marker = BC_2). 167 boundary elements in index 2 (Marker = BC_3). 54165 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: 63999.5. 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 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 1.236142 seconds on 1 core. ----------------------- Write deformed grid files ----------------------- |SU2 mesh |../aflr3/aflr3_CAPS.su2 | |CSV file |surface_deformed.csv | |Tecplot binary |volume_deformed.szplt | |Tecplot binary surface |surface_deformed.szplt | 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) ------------------------ ------------------------------------------------------------------------- | ___ _ _ ___ | | / __| | | |_ ) 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: 0.294118. 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_3. Surface(s) plotted in the output file: BC_3. Surface(s) affected by the design variables: BC_3. Input mesh file name: ../aflr3/aflr3_CAPS.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: 3. 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_aeroelastic_Iterative.dat. Surface file name: surface_flow_aeroelastic_Iterative. Volume file name: flow_aeroelastic_Iterative. Restart file name: restart_flow_aeroelastic_Iterative.dat. ------------- Config File Boundary Information ( Zone 0 ) --------------- +-----------------------------------------------------------------------+ | Marker Type| Marker Name| +-----------------------------------------------------------------------+ | Euler wall| BC_3| +-----------------------------------------------------------------------+ | Far-field| BC_1| +-----------------------------------------------------------------------+ | Symmetry plane| 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. 10490 grid points. 54165 volume elements. 3 surface markers. 3448 boundary elements in index 0 (Marker = BC_1). 1565 boundary elements in index 1 (Marker = BC_2). 167 boundary elements in index 2 (Marker = BC_3). 54165 tetrahedra. Setting point connectivity. Renumbering points (Reverse Cuthill McKee Ordering). Recomputing point connectivity. Setting element connectivity. Checking the numerical grid orientation. There has been a re-orientation of 12500 TETRAHEDRON volume elements. There has been a re-orientation of 531 TRIANGLE surface elements. Identifying edges and vertices. Setting the control volume structure. Volume of the computational grid: 106612. Searching for the closest normal neighbors to the surfaces. Storing a mapping from global to local point index. Compute the surface curvature. Max K: 182.951. Mean K: 1.9499. Standard deviation K: 9.51189. Checking for periodicity. Computing mesh quality statistics for the dual control volumes. +--------------------------------------------------------------+ | Mesh Quality Metric| Minimum| Maximum| +--------------------------------------------------------------+ | Orthogonality Angle (deg.)| 2.24714| 85.0345| | CV Face Area Aspect Ratio| 1.18189| 299.436| | CV Sub-Volume Ratio| 1| 73833.9| +--------------------------------------------------------------+ Setting the multigrid structure. +-------------------------------------------+ | MG Level| CVs|Aggl. Rate| CFL| +-------------------------------------------+ | 0| 10490| 1/1.00| 10| | 1| 1870| 1/5.61| 8.44202| | 2| 384| 1/4.87| 7.47081| +-------------------------------------------+ Finding max control volume width. Semi-span length = 11.1394 m. Wetted area = 1268.81 m^2. Area projection in the x-plane = 401.821 m^2, y-plane = 370.824 m^2, z-plane = 51.2847 m^2. Max. coordinate in the x-direction = 3.33392 m, y-direction = 11.1394 m, z-direction = 41.5039 m. Min. coordinate in the x-direction = -12.3774 m, y-direction = -0.516728 m, z-direction = -65.2783 m. Checking if Euler & Symmetry markers are straight/plane: Boundary marker BC_3 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| 211798| 1| m^2/s^2| 211798| | Velocity-X| 100.087| 1| m/s| 100.087| | Velocity-Y| 0| 1| m/s| 0| | Velocity-Z| 0| 1| m/s| 0| | Velocity Magnitude| 100.087| 1| m/s| 100.087| +------------------------------------------------------------------------------+ | Mach Number| -| -| -| 0.294118| +------------------------------------------------------------------------------+ 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| 2.6551e-01| 2.926740| 5.883462| 6.290990| 8.395846| -0.006174| | 0| 0| 1| 0.0000e+00| 0.0000e+00| 2.7330e-01| 3.384735| 5.930721| 6.086129| 8.759759| 0.191208| | 0| 0| 2| 0.0000e+00| 0.0000e+00| 2.6881e-01| 3.465079| 6.005837| 6.089910| 8.822063| 0.206208| ----------------------------- Solver Exit ------------------------------- Maximum number of iterations reached (ITER = 3) before convergence. +-----------------------------------------------------------------------+ | Convergence Field | Value | Criterion | Converged | +-----------------------------------------------------------------------+ | rms[Rho]| 3.46508| < -14| No| +-----------------------------------------------------------------------+ ------------------------------------------------------------------------- +-----------------------------------------------------------------------+ | File Writing Summary | Filename | +-----------------------------------------------------------------------+ |SU2 binary restart |restart_flow_aeroelastic_Iterative.dat| Writing the forces breakdown file (forces_breakdown_aeroelastic_Iterative.dat). |CSV file |surface_flow_aeroelastic_Iterative.csv| Writing the forces breakdown file (forces_breakdown_aeroelastic_Iterative.dat). |Tecplot binary |flow_aeroelastic_Iterative.szplt | Writing the forces breakdown file (forces_breakdown_aeroelastic_Iterative.dat). |Tecplot binary surface |surface_flow_aeroelastic_Iterative.szplt| Writing the forces breakdown file (forces_breakdown_aeroelastic_Iterative.dat). +-----------------------------------------------------------------------+ Warning: there are 269 non-physical points in the solution. Warning: 8 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) ------------------------ Running PostAnalysis ...... su2 Running PreAnalysis ...... su2 Reading SU2 AeroLoad File - surface_flow_aeroelastic_Iterative.csv Number of variables = 16 Number of data points = 89 CAPS Info: Bound 'Skin_Top' Normalized Integrated 'Pressure' Rank 0: src = 1.313302e+09, tgt = 1.313301e+09, diff = 4.393883e+02 Reading SU2 AeroLoad File - surface_flow_aeroelastic_Iterative.csv Number of variables = 16 Number of data points = 89 CAPS Info: Bound 'Skin_Bottom' Normalized Integrated 'Pressure' Rank 0: src = 1.043453e+09, tgt = 1.043453e+09, diff = 9.408228e+01 Reading SU2 AeroLoad File - surface_flow_aeroelastic_Iterative.csv Number of variables = 16 Number of data points = 89 CAPS Info: Bound 'Skin_Tip' Normalized Integrated 'Pressure' Rank 0: src = 1.297344e+07, tgt = 1.297352e+07, diff = 8.441779e+01 Extracting external pressure loads from data transfer.... TransferName = Skin_Top Number of Elements = 330 (total = 330) Extracting external pressure loads from data transfer.... TransferName = Skin_Bottom Number of Elements = 330 (total = 660) Extracting external pressure loads from data transfer.... TransferName = Skin_Tip Number of Elements = 30 (total = 690) Writing Astros grid and connectivity file (in free field format) .... Finished writing Astros grid file Writing subElement types (if any) - appending mesh file Writing Astros instruction file.... Writing analysis cards Writing load ADD cards Writing constraint cards--each subcase individually Writing load cards Writing material cards Writing property cards Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG Writing SU2 data transfer files Writing SU2 Motion File - aeroelastic_Iterative_motion.dat Warning: The su2 cfg file will be overwritten! Write SU2 configuration file for version "Harrier (8.0.1)" Running SU2...... ------------------------------------------------------------------------- | ___ _ _ ___ | | / __| | | |_ ) 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/aflr3_CAPS.su2 ---------------- Grid deformation parameters ( Zone 0 ) ---------------- Grid deformation using a linear elasticity method. -------------------- Output Information ( Zone 0 ) ---------------------- Output mesh file name: ../aflr3/aflr3_CAPS.su2. Cell stiffness scaled by distance to nearest solid surface. ------------- Config File Boundary Information ( Zone 0 ) --------------- +-----------------------------------------------------------------------+ | Marker Type| Marker Name| +-----------------------------------------------------------------------+ | Euler wall| BC_3| +-----------------------------------------------------------------------+ | Far-field| BC_1| +-----------------------------------------------------------------------+ | Symmetry plane| BC_2| +-----------------------------------------------------------------------+ Three dimensional problem. 10490 grid points. 54165 volume elements. 3 surface markers. 3448 boundary elements in index 0 (Marker = BC_1). 1565 boundary elements in index 1 (Marker = BC_2). 167 boundary elements in index 2 (Marker = BC_3). 54165 tetrahedra. ----------------------- Preprocessing computations ---------------------- Setting local point connectivity. Checking the numerical grid orientation of the interior elements. There has been a re-orientation of 12500 TETRAHEDRON volume elements. There has been a re-orientation of 531 TRIANGLE surface elements. Identify edges and vertices. Setting the bound control volume structure. Volume of the computational grid: 106612. 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 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 28.439983 seconds on 1 core. ----------------------- Write deformed grid files ----------------------- |SU2 mesh |../aflr3/aflr3_CAPS.su2 | |CSV file |surface_deformed.csv | |Tecplot binary |volume_deformed.szplt | |Tecplot binary surface |surface_deformed.szplt | 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) ------------------------ ------------------------------------------------------------------------- | ___ _ _ ___ | | / __| | | |_ ) 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: 0.294118. 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_3. Surface(s) plotted in the output file: BC_3. Surface(s) affected by the design variables: BC_3. Input mesh file name: ../aflr3/aflr3_CAPS.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: 3. 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_aeroelastic_Iterative.dat. Surface file name: surface_flow_aeroelastic_Iterative. Volume file name: flow_aeroelastic_Iterative. Restart file name: restart_flow_aeroelastic_Iterative.dat. ------------- Config File Boundary Information ( Zone 0 ) --------------- +-----------------------------------------------------------------------+ | Marker Type| Marker Name| +-----------------------------------------------------------------------+ | Euler wall| BC_3| +-----------------------------------------------------------------------+ | Far-field| BC_1| +-----------------------------------------------------------------------+ | Symmetry plane| 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. 10490 grid points. 54165 volume elements. 3 surface markers. 3448 boundary elements in index 0 (Marker = BC_1). 1565 boundary elements in index 1 (Marker = BC_2). 167 boundary elements in index 2 (Marker = BC_3). 54165 tetrahedra. Setting point connectivity. Renumbering points (Reverse Cuthill McKee Ordering). Recomputing point connectivity. Setting element connectivity. Checking the numerical grid orientation. There has been a re-orientation of 31813 TETRAHEDRON volume elements. There has been a re-orientation of 1516 TRIANGLE surface elements. Identifying edges and vertices. Setting the control volume structure. Volume of the computational grid: 1.29593e+10. Searching for the closest normal neighbors to the surfaces. Storing a mapping from global to local point index. Compute the surface curvature. Max K: 11.0516. Mean K: 0.307357. Standard deviation K: 0.990298. Checking for periodicity. Computing mesh quality statistics for the dual control volumes. +--------------------------------------------------------------+ | Mesh Quality Metric| Minimum| Maximum| +--------------------------------------------------------------+ | Orthogonality Angle (deg.)| 0.377156| 85.4318| | CV Face Area Aspect Ratio| 1.29339| 210999| | CV Sub-Volume Ratio| 1| 175159| +--------------------------------------------------------------+ Setting the multigrid structure. +-------------------------------------------+ | MG Level| CVs|Aggl. Rate| CFL| +-------------------------------------------+ | 0| 10490| 1/1.00| 10| | 1| 1872| 1/5.6| 8.44503| | 2| 383| 1/4.89| 7.46432| +-------------------------------------------+ Finding max control volume width. Semi-span length = 13.3552 m. Wetted area = 709349 m^2. Area projection in the x-plane = 464091 m^2, y-plane = 80491.9 m^2, z-plane = 5144.82 m^2. Max. coordinate in the x-direction = 33.2369 m, y-direction = 13.3552 m, z-direction = 5208.87 m. Min. coordinate in the x-direction = -32.8266 m, y-direction = -377.133 m, z-direction = -0.0403729 m. Checking if Euler & Symmetry markers are straight/plane: Boundary marker BC_3 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| 211798| 1| m^2/s^2| 211798| | Velocity-X| 100.087| 1| m/s| 100.087| | Velocity-Y| 0| 1| m/s| 0| | Velocity-Z| 0| 1| m/s| 0| | Velocity Magnitude| 100.087| 1| m/s| 100.087| +------------------------------------------------------------------------------+ | Mach Number| -| -| -| 0.294118| +------------------------------------------------------------------------------+ 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| 2.4092e-01| 6.490649| 9.452455| 9.631451| 11.959755| -0.034218| | 0| 0| 1| 0.0000e+00| 0.0000e+00| 2.5860e-01| 6.894879| 9.409837| 9.483196| 12.282706| -0.034168| | 0| 0| 2| 0.0000e+00| 0.0000e+00| 2.6757e-01| 6.982612| 9.479394| 9.493776| 12.359902| -0.033133| ----------------------------- Solver Exit ------------------------------- Maximum number of iterations reached (ITER = 3) before convergence. +-----------------------------------------------------------------------+ | Convergence Field | Value | Criterion | Converged | +-----------------------------------------------------------------------+ | rms[Rho]| 6.98261| < -14| No| +-----------------------------------------------------------------------+ ------------------------------------------------------------------------- +-----------------------------------------------------------------------+ | File Writing Summary | Filename | +-----------------------------------------------------------------------+ |SU2 binary restart |restart_flow_aeroelastic_Iterative.dat| Writing the forces breakdown file (forces_breakdown_aeroelastic_Iterative.dat). |CSV file |surface_flow_aeroelastic_Iterative.csv| Writing the forces breakdown file (forces_breakdown_aeroelastic_Iterative.dat). |Tecplot binary |flow_aeroelastic_Iterative.szplt | Writing the forces breakdown file (forces_breakdown_aeroelastic_Iterative.dat). |Tecplot binary surface |surface_flow_aeroelastic_Iterative.szplt| Writing the forces breakdown file (forces_breakdown_aeroelastic_Iterative.dat). +-----------------------------------------------------------------------+ Warning: there are 410 non-physical points in the solution. Warning: 34 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) ------------------------ Running PostAnalysis ...... su2 Running PreAnalysis ...... su2 Reading SU2 AeroLoad File - surface_flow_aeroelastic_Iterative.csv Number of variables = 16 Number of data points = 89 CAPS Info: Bound 'Skin_Top' Normalized Integrated 'Pressure' Rank 0: src = 1.777310e+09, tgt = 1.777309e+09, diff = 6.371447e+02 Reading SU2 AeroLoad File - surface_flow_aeroelastic_Iterative.csv Number of variables = 16 Number of data points = 89 CAPS Info: Bound 'Skin_Bottom' Normalized Integrated 'Pressure' Rank 0: src = 1.287029e+09, tgt = 1.287029e+09, diff = 5.623313e+00 Reading SU2 AeroLoad File - surface_flow_aeroelastic_Iterative.csv Number of variables = 16 Number of data points = 89 CAPS Info: Bound 'Skin_Tip' Normalized Integrated 'Pressure' Rank 0: src = 5.336473e+06, tgt = 5.336475e+06, diff = 1.633793e+00 Extracting external pressure loads from data transfer.... TransferName = Skin_Top Number of Elements = 330 (total = 330) Extracting external pressure loads from data transfer.... TransferName = Skin_Bottom Number of Elements = 330 (total = 660) Extracting external pressure loads from data transfer.... TransferName = Skin_Tip Number of Elements = 30 (total = 690) Writing Astros grid and connectivity file (in free field format) .... Finished writing Astros grid file Writing subElement types (if any) - appending mesh file Writing Astros instruction file.... Writing analysis cards Writing load ADD cards Writing constraint cards--each subcase individually Writing load cards Writing material cards Writing property cards Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG Writing SU2 data transfer files Writing SU2 Motion File - aeroelastic_Iterative_motion.dat Warning: The su2 cfg file will be overwritten! Write SU2 configuration file for version "Harrier (8.0.1)" Running SU2...... ------------------------------------------------------------------------- | ___ _ _ ___ | | / __| | | |_ ) 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/aflr3_CAPS.su2 ---------------- Grid deformation parameters ( Zone 0 ) ---------------- Grid deformation using a linear elasticity method. -------------------- Output Information ( Zone 0 ) ---------------------- Output mesh file name: ../aflr3/aflr3_CAPS.su2. Cell stiffness scaled by distance to nearest solid surface. ------------- Config File Boundary Information ( Zone 0 ) --------------- +-----------------------------------------------------------------------+ | Marker Type| Marker Name| +-----------------------------------------------------------------------+ | Euler wall| BC_3| +-----------------------------------------------------------------------+ | Far-field| BC_1| +-----------------------------------------------------------------------+ | Symmetry plane| BC_2| +-----------------------------------------------------------------------+ Three dimensional problem. 10490 grid points. 54165 volume elements. 3 surface markers. 3448 boundary elements in index 0 (Marker = BC_1). 1565 boundary elements in index 1 (Marker = BC_2). 167 boundary elements in index 2 (Marker = BC_3). 54165 tetrahedra. ----------------------- Preprocessing computations ---------------------- Setting local point connectivity. Checking the numerical grid orientation of the interior elements. There has been a re-orientation of 31813 TETRAHEDRON volume elements. There has been a re-orientation of 1516 TRIANGLE surface elements. Identify edges and vertices. Setting the bound control volume structure. Volume of the computational grid: 1.29593e+10. 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 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 29.395368 seconds on 1 core. ----------------------- Write deformed grid files ----------------------- |SU2 mesh |../aflr3/aflr3_CAPS.su2 | |CSV file |surface_deformed.csv | |Tecplot binary |volume_deformed.szplt | |Tecplot binary surface |surface_deformed.szplt | 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) ------------------------ ------------------------------------------------------------------------- | ___ _ _ ___ | | / __| | | |_ ) 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: 0.294118. 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_3. Surface(s) plotted in the output file: BC_3. Surface(s) affected by the design variables: BC_3. Input mesh file name: ../aflr3/aflr3_CAPS.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: 3. 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_aeroelastic_Iterative.dat. Surface file name: surface_flow_aeroelastic_Iterative. Volume file name: flow_aeroelastic_Iterative. Restart file name: restart_flow_aeroelastic_Iterative.dat. ------------- Config File Boundary Information ( Zone 0 ) --------------- +-----------------------------------------------------------------------+ | Marker Type| Marker Name| +-----------------------------------------------------------------------+ | Euler wall| BC_3| +-----------------------------------------------------------------------+ | Far-field| BC_1| +-----------------------------------------------------------------------+ | Symmetry plane| 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. 10490 grid points. 54165 volume elements. 3 surface markers. 3448 boundary elements in index 0 (Marker = BC_1). 1565 boundary elements in index 1 (Marker = BC_2). 167 boundary elements in index 2 (Marker = BC_3). 54165 tetrahedra. Setting point connectivity. Renumbering points (Reverse Cuthill McKee Ordering). Recomputing point connectivity. Setting element connectivity. Checking the numerical grid orientation. There has been a re-orientation of 17632 TETRAHEDRON volume elements. There has been a re-orientation of 1516 TRIANGLE surface elements. Identifying edges and vertices. Setting the control volume structure. Volume of the computational grid: 7.55067e+13. Searching for the closest normal neighbors to the surfaces. Storing a mapping from global to local point index. Compute the surface curvature. Max K: 42.7789. Mean K: 0.268641. Standard deviation K: 1.44892. Checking for periodicity. Computing mesh quality statistics for the dual control volumes. +--------------------------------------------------------------+ | Mesh Quality Metric| Minimum| Maximum| +--------------------------------------------------------------+ | Orthogonality Angle (deg.)| 0.228375| 84.0716| | CV Face Area Aspect Ratio| 1.69341| 3.29101e+07| | CV Sub-Volume Ratio| 1| 8.95906e+08| +--------------------------------------------------------------+ Setting the multigrid structure. +-------------------------------------------+ | MG Level| CVs|Aggl. Rate| CFL| +-------------------------------------------+ | 0| 10490| 1/1.00| 10| | 1| 1889| 1/5.55| 8.47052| | 2| 397| 1/4.76| 7.55418| +-------------------------------------------+ Finding max control volume width. Semi-span length = 79.3623 m. Wetted area = 19427 m^2. Area projection in the x-plane = 6431.92 m^2, y-plane = 5648.53 m^2, z-plane = 632.165 m^2. Max. coordinate in the x-direction = 4.33646 m, y-direction = 79.3623 m, z-direction = 16.332 m. Min. coordinate in the x-direction = -40.9042 m, y-direction = -2.63233 m, z-direction = -834.953 m. Checking if Euler & Symmetry markers are straight/plane: Boundary marker BC_3 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| 211798| 1| m^2/s^2| 211798| | Velocity-X| 100.087| 1| m/s| 100.087| | Velocity-Y| 0| 1| m/s| 0| | Velocity-Z| 0| 1| m/s| 0| | Velocity Magnitude| 100.087| 1| m/s| 100.087| +------------------------------------------------------------------------------+ | Mach Number| -| -| -| 0.294118| +------------------------------------------------------------------------------+ 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| 2.4970e-01| 8.934634| 11.901490| 11.850216| 14.403740| -0.199529| | 0| 0| 1| 0.0000e+00| 0.0000e+00| 2.7220e-01| 9.335753| 11.918618| 11.861994| 14.764113| -0.167720| | 0| 0| 2| 0.0000e+00| 0.0000e+00| 2.6874e-01| 9.369968| 11.908253| 11.855002| 14.795135| -0.168770| ----------------------------- Solver Exit ------------------------------- Maximum number of iterations reached (ITER = 3) before convergence. +-----------------------------------------------------------------------+ | Convergence Field | Value | Criterion | Converged | +-----------------------------------------------------------------------+ | rms[Rho]| 9.36997| < -14| No| +-----------------------------------------------------------------------+ ------------------------------------------------------------------------- +-----------------------------------------------------------------------+ | File Writing Summary | Filename | +-----------------------------------------------------------------------+ |SU2 binary restart |restart_flow_aeroelastic_Iterative.dat| Writing the forces breakdown file (forces_breakdown_aeroelastic_Iterative.dat). |CSV file |surface_flow_aeroelastic_Iterative.csv| Writing the forces breakdown file (forces_breakdown_aeroelastic_Iterative.dat). |Tecplot binary |flow_aeroelastic_Iterative.szplt | Writing the forces breakdown file (forces_breakdown_aeroelastic_Iterative.dat). |Tecplot binary surface |surface_flow_aeroelastic_Iterative.szplt| Writing the forces breakdown file (forces_breakdown_aeroelastic_Iterative.dat). +-----------------------------------------------------------------------+ Warning: there are 605 non-physical points in the solution. Warning: 51 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) ------------------------ Running PostAnalysis ...... su2 real 2m11.885s user 1m47.076s sys 0m7.466s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case aeroelastic_Iterative_SU2_and_Astros.py passed (as expected) ================================================= ================================================= + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/pyCAPSlog.txt + echo 'aeroelasticSimple_Temperature_SU2_and_TACS.py test;' aeroelasticSimple_Temperature_SU2_and_TACS.py test; + python -u aeroelasticSimple_Temperature_SU2_and_TACS.py -outLevel=0 -noPlotData + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/pyCAPSlog.txt Running PreAnalysis ...... su2 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Farfield, index = 1 Name = SymmPlane, index = 2 Name = Skin, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 AFLR2 : --------------------------------------- AFLR2 : AFLR2 LIBRARY AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR2 : TRIA/QUAD GRID GENERATOR AFLR2 : Version Number 9.17.15 AFLR2 : Version Date 04/23/24 @ 12:51AM AFLR2 : Compile OS Darwin 23.4.0 arm64 AFLR2 : Compile Date 04/23/24 @ 12:51AM 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 11.5.14 AFLR4 : Version Date 04/18/24 @ 12:45PM AFLR4 : Compile OS Darwin 23.4.0 arm64 AFLR4 : Compile Date 04/18/24 @ 03:04PM AFLR4 : Copyright 1994-2021, D.L. Marcum AFLR4 : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : EGADS CAD Geometry Setup EGADS : Model has 1 Active Bodies EGADS : Body 0 is a SolidBody EGADS : Body 0 has 1 Shells EGADS : Body 0 has 9 Faces EGADS : Body 0 has 18 Edges EGADS : Body 0 has 10 Loops EGADS : Body 0 has 12 Nodes EGADS : Check Grid BCs EGADS : Grid BCs are OK EGADS : Face Neighbor-Faces Information EGADS : QC = Face Quad Combination Flag EGADS : IER = Face Isolated Edge Refinement Flag EGADS : ER = Face Edge Refinement Factor EGADS : Not applicable for Faces with a FarField Grid BC. EGADS : SF = Face Scale Factor EGADS : Not applicable for Faces with a FarField Grid BC. EGADS : Face Body QC IER ER Scale Neighbor EGADS : ID Active ID Flag Flag Weight Factor Faces EGADS : 1 Yes 0 0 1 0 1 2 3 4 5 EGADS : 2 Yes 0 0 1 0 1 1 3 5 6 EGADS : 3 Yes 0 0 1 0 1 1 2 4 6 7 8 EGADS : 4 Yes 0 0 1 0 1 1 3 5 6 EGADS : 5 Yes 0 0 1 0 1 1 2 4 6 EGADS : 6 Yes 0 0 1 0 1 2 3 4 5 EGADS : 7 Yes 0 0 1 0 1 3 8 9 EGADS : 8 Yes 0 0 1 0 1 3 7 9 EGADS : 9 Yes 0 0 1 0 1 7 8 EGADS : Face Edges Information EGADS : Face Edges EGADS : 1 1 2 -3 -4 EGADS : 2 5 6 -7 -1 EGADS : 3 -2 7 9 -8 -10 -11 EGADS : 4 -12 3 8 -13 EGADS : 5 4 12 -14 -5 EGADS : 6 -6 14 13 -9 EGADS : 7 15 10 -17 -16 EGADS : 8 17 11 -15 -18 EGADS : 9 16 18 EGADS : Face Loops Information EGADS : Face Loops EGADS : 1 1 EGADS : 2 2 EGADS : 3 3 4 EGADS : 4 5 EGADS : 5 6 EGADS : 6 7 EGADS : 7 8 EGADS : 8 9 EGADS : 9 10 EGADS : Loop Edges Information EGADS : Loop Active Edges EGADS : 1 Yes 1 2 -3 -4 EGADS : 2 Yes 5 6 -7 -1 EGADS : 3 Yes -2 7 9 -8 EGADS : 4 Yes -10 -11 EGADS : 5 Yes -12 3 8 -13 EGADS : 6 Yes 4 12 -14 -5 EGADS : 7 Yes -6 14 13 -9 EGADS : 8 Yes 15 10 -17 -16 EGADS : 9 Yes 17 11 -15 -18 EGADS : 10 Yes 16 18 EGADS : Edge Node, Scale Factor, and Neighbor-Faces Information EGADS : ESF = Edge Scale Factor EGADS : Not applicable for DEGENERATE Edges or Edges with a FarField EGADS : Grid BC Neighbor Face. EGADS : Neighbor EGADS : Edge Body Active Node1 Node2 ESF Faces EGADS : 1 0 Yes 2 1 1 1 2 EGADS : 2 0 Yes 1 3 1 1 3 EGADS : 3 0 Yes 4 3 1 1 4 EGADS : 4 0 Yes 2 4 1 1 5 EGADS : 5 0 Yes 2 5 1 2 5 EGADS : 6 0 Yes 5 6 1 2 6 EGADS : 7 0 Yes 1 6 1 2 3 EGADS : 8 0 Yes 3 7 1 3 4 EGADS : 9 0 Yes 6 7 1 3 6 EGADS : 10 0 Yes 8 9 1 3 7 EGADS : 11 0 Yes 9 8 1 3 8 EGADS : 12 0 Yes 4 10 1 4 5 EGADS : 13 0 Yes 10 7 1 4 6 EGADS : 14 0 Yes 5 10 1 5 6 EGADS : 15 0 Yes 11 8 1 7 8 EGADS : 16 0 Yes 11 12 1 7 9 EGADS : 17 0 Yes 12 9 1 7 8 EGADS : 18 0 Yes 12 11 1 8 9 EGADS : Node Information EGADS : Node Active Coordinates EGADS : 1 Yes 0 0 0 EGADS : 2 Yes 0 40 0 EGADS : 3 Yes 0 0 20 EGADS : 4 Yes 0 40 20 EGADS : 5 Yes 20 40 0 EGADS : 6 Yes 20 0 0 EGADS : 7 Yes 20 0 20 EGADS : 8 Yes 1.61374306 0 0 EGADS : 9 Yes 0 0 0 EGADS : 10 Yes 20 40 20 EGADS : 11 Yes 2.53650745 3.87298335 0.334116517 EGADS : 12 Yes 1.57194608 3.87298335 0.249728332 EGADS : Face and Edge Match Information EGADS : No Face Matches Found AFLR4 : Surface Mesh Spacing Setup AFLR4 : Max Bounding Box Length = 40 AFLR4 : Min Bounding Box Length = 40 AFLR4 : Max Ref Bounding Box Length = 40 AFLR4 : Min Ref Bounding Box Length = 40 AFLR4 : Reference Length = 1.61374 AFLR4 : BL Thickness = 0 AFLR4 : Abs Min Surf Spacing = 0.00403436 AFLR4 : Min Surf Spacing = 0.161374 AFLR4 : Max Surf Spacing = 1.21031 AFLR4 : Global Scale Factor = 1 AFLR4 : Geometry Definition Information AFLR4 : Definition Definition Composite Grid BC AFLR4 : ID Type ID Type AFLR4 : 0 glue-only composite - - AFLR4 : 1 CAD geometry 0 STD w/BL AFLR4 : 2 CAD geometry 0 STD w/BL AFLR4 : 3 CAD geometry 0 STD w/BL AFLR4 : 4 CAD geometry 0 STD w/BL AFLR4 : 5 CAD geometry 0 STD w/BL AFLR4 : 6 CAD geometry 0 STD w/BL AFLR4 : 7 CAD geometry 0 STD w/BL AFLR4 : 8 CAD geometry 0 STD w/BL AFLR4 : 9 CAD geometry 0 STD w/BL AFLR4 : Define CAD surface definition 1 AFLR4 : Define CAD surface definition 2 AFLR4 : Define CAD surface definition 3 AFLR4 : Define CAD surface definition 4 AFLR4 : Define CAD surface definition 5 AFLR4 : Define CAD surface definition 6 AFLR4 : Define CAD surface definition 7 AFLR4 : Define CAD surface definition 8 AFLR4 : Define CAD surface definition 9 AFLR4 : Surface Grid Generation AFLR4 : Generate optimal mesh on surface definition 1 AFLR2 : Nodes, Trias,Quads= 1318 2502 0 AFLR4 : Nodes, Trias,Quads= 1293 2452 0 AFLR4 : Generate optimal mesh on surface definition 2 AFLR2 : Nodes, Trias,Quads= 1318 2502 0 AFLR4 : Nodes, Trias,Quads= 1298 2462 0 AFLR4 : Generate optimal mesh on surface definition 3 AFLR2 : Nodes, Trias,Quads= 3418 6687 0 AFLR4 : Nodes, Trias,Quads= 3008 5867 0 AFLR4 : Generate optimal mesh on surface definition 4 AFLR2 : Nodes, Trias,Quads= 1316 2498 0 AFLR4 : Nodes, Trias,Quads= 1297 2460 0 AFLR4 : Generate optimal mesh on surface definition 5 AFLR2 : Nodes, Trias,Quads= 1318 2502 0 AFLR4 : Nodes, Trias,Quads= 1297 2460 0 AFLR4 : Generate optimal mesh on surface definition 6 AFLR2 : Nodes, Trias,Quads= 1319 2504 0 AFLR4 : Nodes, Trias,Quads= 1294 2454 0 AFLR4 : Generate optimal mesh on surface definition 7 AFLR2 : Nodes, Trias,Quads= 200 344 0 AFLR4 : Nodes, Trias,Quads= 160 264 0 AFLR4 : Generate optimal mesh on surface definition 8 AFLR2 : Nodes, Trias,Quads= 193 330 0 AFLR4 : Nodes, Trias,Quads= 155 254 0 AFLR4 : Generate optimal mesh on surface definition 9 AFLR2 : Nodes, Trias,Quads= 17 21 0 AFLR4 : Nodes, Trias,Quads= 11 9 0 DGEOM : Add surface definitions to composite definition 0 DGEOM : Glue composite surface definition 0 DGEOM : Nodes,Faces,BEdges= 9343 18682 928 AFLR4 : Auto Mode Turned OFF OVERALL : CPU Time = 0.124 seconds Body 1 (of 1) Number of nodes = 9343 Number of elements = 18682 Number of triangle elements = 18682 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 9343 Total number of elements = 18682 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Farfield, index = 1 Name = SymmPlane, index = 2 Name = Skin, index = 3 Getting volume mesh AFLR2 : --------------------------------------- AFLR2 : AFLR2 LIBRARY AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR2 : TRIA/QUAD GRID GENERATOR AFLR2 : Version Number 9.17.15 AFLR2 : Version Date 04/23/24 @ 12:51AM AFLR2 : Compile OS Darwin 23.4.0 arm64 AFLR2 : Compile Date 04/23/24 @ 12:51AM 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 11.5.14 AFLR4 : Version Date 04/18/24 @ 12:45PM AFLR4 : Compile OS Darwin 23.4.0 arm64 AFLR4 : Compile Date 04/18/24 @ 03:04PM AFLR4 : Copyright 1994-2021, D.L. Marcum AFLR4 : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 57531 Number of elements = 331031 Number of triangles = 18682 Number of quadrilatarals = 0 Number of tetrahedrals = 312349 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing SU2 file .... Finished writing SU2 file Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Skin Boundary condition name - SymmPlane Done getting CFD boundary conditions Info: No recognized data transfer names found. Warning: The su2 cfg file will be overwritten! Write SU2 configuration file for version "BlackBird (7.5.1) " 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: 0.294118. 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_3. Surface(s) plotted in the output file: BC_3. Surface(s) affected by the design variables: BC_3. Input mesh file name: ../aflr3/aflr3_CAPS.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: 3. 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_aeroelasticSimple_Temperature_SM.dat. Surface file name: surface_flow_aeroelasticSimple_Temperature_SM. Volume file name: flow_aeroelasticSimple_Temperature_SM. Restart file name: restart_flow_aeroelasticSimple_Temperature_SM.dat. ------------- Config File Boundary Information ( Zone 0 ) --------------- +-----------------------------------------------------------------------+ | Marker Type| Marker Name| +-----------------------------------------------------------------------+ | Euler wall| BC_3| +-----------------------------------------------------------------------+ | Far-field| BC_1| +-----------------------------------------------------------------------+ | Symmetry plane| 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. 57531 grid points. 312349 volume elements. 3 surface markers. 12288 boundary elements in index 0 (Marker = BC_1). 5867 boundary elements in index 1 (Marker = BC_2). 527 boundary elements in index 2 (Marker = BC_3). 312349 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: 63999.5. Searching for the closest normal neighbors to the surfaces. Storing a mapping from global to local point index. Compute the surface curvature. Max K: 102.753. Mean K: 0.74689. Standard deviation K: 4.38956. Checking for periodicity. Computing mesh quality statistics for the dual control volumes. +--------------------------------------------------------------+ | Mesh Quality Metric| Minimum| Maximum| +--------------------------------------------------------------+ | Orthogonality Angle (deg.)| 48.3512| 86.0919| | CV Face Area Aspect Ratio| 1.11561| 35.2066| | CV Sub-Volume Ratio| 1| 18.8559| +--------------------------------------------------------------+ Setting the multigrid structure. +-------------------------------------------+ | MG Level| CVs|Aggl. Rate| CFL| +-------------------------------------------+ | 0| 57531| 1/1.00| 10| | 1| 9779| 1/5.88| 8.30913| | 2| 1716| 1/5.7| 6.97784| +-------------------------------------------+ Finding max control volume width. Semi-span length = 3.87298 m. Wetted area = 9.04169 m^2. Area projection in the x-plane = 0.644461 m^2, y-plane = 0.295795 m^2, z-plane = 4.29819 m^2. Max. coordinate in the x-direction = 2.53651 m, y-direction = 3.87298 m, z-direction = 0.379751 m. Min. coordinate in the x-direction = 0 m, y-direction = -2.86125e-18 m, z-direction = -0.0467278 m. Checking if Euler & Symmetry markers are straight/plane: Boundary marker BC_3 is NOT a single plane. Boundary marker BC_2 is 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| 211798| 1| m^2/s^2| 211798| | Velocity-X| 100.087| 1| m/s| 100.087| | Velocity-Y| 0| 1| m/s| 0| | Velocity-Z| 0| 1| m/s| 0| | Velocity Magnitude| 100.087| 1| m/s| 100.087| +------------------------------------------------------------------------------+ | Mach Number| -| -| -| 0.294118| +------------------------------------------------------------------------------+ 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| 1.4732e+00| -1.299765| 0.996854| 0.627451| 4.169341| -0.962501| | 0| 0| 1| 0.0000e+00| 0.0000e+00| 1.3544e+00| -1.689451| 0.841935| 0.460737| 3.766643| -0.517631| | 0| 0| 2| 0.0000e+00| 0.0000e+00| 1.3824e+00| -1.703013| 0.658675| 0.298032| 3.753378| 1.611420| ----------------------------- Solver Exit ------------------------------- Maximum number of iterations reached (ITER = 3) before convergence. +-----------------------------------------------------------------------+ | Convergence Field | Value | Criterion | Converged | +-----------------------------------------------------------------------+ | rms[Rho]| -1.70301| < -14| No| +-----------------------------------------------------------------------+ ------------------------------------------------------------------------- +-----------------------------------------------------------------------+ | File Writing Summary | Filename | +-----------------------------------------------------------------------+ |SU2 binary restart |restart_flow_aeroelasticSimple_Temperature_SM.dat| Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Temperature_SM.dat). |CSV file |surface_flow_aeroelasticSimple_Temperature_SM.csv| Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Temperature_SM.dat). |Tecplot binary |flow_aeroelasticSimple_Temperature_SM.szplt| Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Temperature_SM.dat). |Tecplot binary surface |surface_flow_aeroelasticSimple_Temperature_SM.szplt| Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Temperature_SM.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) ------------------------ Running PostAnalysis ...... su2 Running PreAnalysis ...... tacs Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Skin, index = 1 Name = Rib_Root, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting surface mesh for body 1 (of 1) Body 1 (of 1) Number of nodes = 12 Number of elements = 12 Number of triangle elements = 4 Number of quadrilateral elements = 8 ---------------------------- Total number of nodes = 12 Total number of elements = 12 Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = Rib_Root, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = Skin, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 3 Name = Skin_Top, index = 1 Name = Skin_Bottom, index = 2 Name = Skin_Tip, index = 3 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Skin, index = 1 Name = Rib_Root, index = 2 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 12 Number of elements = 12 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 4 Elemental Quad4 = 8 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 2 Property name - Rib_Root Property name - Skin Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - Skin No "groupName" specified for Load tuple Skin, going to use load name Done getting FEA loads Design_Variable tuple is NULL - No design variables applied Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = Rib_Root, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = Skin, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 3 Name = Skin_Top, index = 1 Name = Skin_Bottom, index = 2 Name = Skin_Tip, index = 3 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Skin, index = 1 Name = Rib_Root, index = 2 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 12 Number of elements = 12 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 4 Elemental Quad4 = 8 Reading SU2 AeroLoad File - surface_flow_aeroelasticSimple_Temperature_SM.csv Number of variables = 16 Number of data points = 273 CAPS Info: Bound 'Skin_Top' Normalized Integrated 'Temperature' Rank 0: src = 1.497349e+03, tgt = 1.497349e+03, diff = 5.478862e-06 Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = Rib_Root, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = Skin, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 3 Name = Skin_Top, index = 1 Name = Skin_Bottom, index = 2 Name = Skin_Tip, index = 3 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Skin, index = 1 Name = Rib_Root, index = 2 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 12 Number of elements = 12 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 4 Elemental Quad4 = 8 Reading SU2 AeroLoad File - surface_flow_aeroelasticSimple_Temperature_SM.csv Number of variables = 16 Number of data points = 273 CAPS Info: Bound 'Skin_Bottom' Normalized Integrated 'Temperature' Rank 0: src = 1.453938e+03, tgt = 1.453938e+03, diff = 6.644339e-06 Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = Rib_Root, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = Skin, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 3 Name = Skin_Top, index = 1 Name = Skin_Bottom, index = 2 Name = Skin_Tip, index = 3 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Skin, index = 1 Name = Rib_Root, index = 2 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 12 Number of elements = 12 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 4 Elemental Quad4 = 8 Reading SU2 AeroLoad File - surface_flow_aeroelasticSimple_Temperature_SM.csv Number of variables = 16 Number of data points = 273 CAPS Info: Bound 'Skin_Tip' Normalized Integrated 'Temperature' Rank 0: src = 2.083892e+01, tgt = 2.083892e+01, diff = 5.435652e-13 Extracting external thermal loads from data transfer.... TransferName = Skin_Top Number of Nodes = 9 (total = 9) Extracting external thermal loads from data transfer.... TransferName = Skin_Bottom Number of Nodes = 9 (total = 18) Extracting external thermal loads from data transfer.... TransferName = Skin_Tip Number of Nodes = 4 (total = 16) Writing Nastran grid and connectivity file (in free field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Running PostAnalysis ...... tacs real 0m23.219s user 0m15.754s sys 0m1.309s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case aeroelasticSimple_Temperature_SU2_and_TACS.py passed (as expected) ================================================= ************************************************* ************************************************* ================================================= Did not run examples for: Mystran ================================================= All tests pass! ================================================= ================================================= ++ cd /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/CAPS/legacy/examples/regressionTest ++ ./execute_PyTestRegression.sh AEROELASTIC ================================================= Legacy Using python : /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/ESP/venv/bin/python ================================================= Running.... AEROELASTIC PyTests ================================================= + rm -rf aeroelasticSimple_Pressure_SU2_and_Astros + echo 'aeroelasticSimple_Pressure_SU2_and_Astros.py test;' + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt aeroelasticSimple_Pressure_SU2_and_Astros.py test; + python -u aeroelasticSimple_Pressure_SU2_and_Astros.py -verbosity=0 -workDir=runDirectory -noPlotData + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt Running PreAnalysis ...... tetgen Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Farfield, index = 1 Name = SymmPlane, index = 2 Name = Skin, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting surface mesh for body 1 (of 1) Running PostAnalysis ...... tetgen Body 1 (of 1) Number of nodes = 12449 Number of elements = 24894 Number of triangle elements = 24894 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 12449 Total number of elements = 24894 Running PreAnalysis ...... tetgen Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Farfield, index = 1 Name = SymmPlane, index = 2 Name = Skin, index = 3 Number of surface: nodes - 12449, elements - 24894 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Running PostAnalysis ...... tetgen Running PreAnalysis ...... su2 Writing SU2 file .... Finished writing SU2 file Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Skin Boundary condition name - SymmPlane Done getting CFD boundary conditions Info: No recognized data transfer names found. Warning: The su2 cfg file will be overwritten! Write SU2 configuration file for version "BlackBird (7.5.1) " 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: 0.294118. 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_3. Surface(s) plotted in the output file: BC_3. Surface(s) affected by the design variables: BC_3. Input mesh file name: ../runDirectory_AeroelasticSimple_Pressure_tetgen_tetgenAIM/tetgen_CAPS.su2 --------------- Space Numerical Integration ( Zone 0 ) ------------------ Roe (with entropy fix = 0.001) solver for the flow inviscid terms. Standard Roe without low-dissipation function. Second order integration in space, with slope limiter. Venkatakrishnan slope-limiting method, with constant: 0.05. The reference element size is: 1. Gradient for upwind reconstruction: inverse-distance weighted Least-Squares. Gradient for viscous and source terms: inverse-distance weighted Least-Squares. --------------- Time Numerical Integration ( Zone 0 ) ------------------ Local time stepping (steady state simulation). Euler implicit method for the flow equations. FGMRES is used for solving the linear system. Using a ILU(0) preconditioning. Convergence criteria of the linear solver: 1e-06. Max number of linear iterations: 10. V Multigrid Cycle, with 2 multigrid levels. Damping factor for the residual restriction: 0.75. Damping factor for the correction prolongation: 0.75. No CFL adaptation. +-------------------------------------------+ | MG Level| Presmooth|PostSmooth|CorrectSmo| +-------------------------------------------+ | 0| 1| 0| 0| | 1| 2| 0| 0| | 2| 3| 0| 0| +-------------------------------------------+ Courant-Friedrichs-Lewy number: 10 ------------------ Convergence Criteria ( Zone 0 ) --------------------- Maximum number of solver subiterations: 5. Begin convergence monitoring at iteration 5. Residual minimum value: 1e-14. Cauchy series min. value: 1e-10. Number of Cauchy elements: 100. Begin windowed time average at iteration 0. -------------------- Output Information ( Zone 0 ) ---------------------- File writing frequency: +------------------------------------+ | File| Frequency| +------------------------------------+ | RESTART| 250| | SURFACE_CSV| 250| | TECPLOT| 250| | SURFACE_TECPLOT| 250| +------------------------------------+ Writing the convergence history file every 1 inner iterations. Writing the screen convergence history every 1 inner iterations. The tabular file format is CSV (.csv). Convergence history file name: history. Forces breakdown file name: forces_breakdown_aeroelasticSimple_Pressure_SA.dat. Surface file name: surface_flow_aeroelasticSimple_Pressure_SA. Volume file name: flow_aeroelasticSimple_Pressure_SA. Restart file name: restart_flow_aeroelasticSimple_Pressure_SA.dat. ------------- Config File Boundary Information ( Zone 0 ) --------------- +-----------------------------------------------------------------------+ | Marker Type| Marker Name| +-----------------------------------------------------------------------+ | Euler wall| BC_3| +-----------------------------------------------------------------------+ | Far-field| BC_1| +-----------------------------------------------------------------------+ | Symmetry plane| 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. 22458 grid points. 97968 volume elements. 3 surface markers. 342 boundary elements in index 0 (Marker = BC_1). 12856 boundary elements in index 1 (Marker = BC_2). 11696 boundary elements in index 2 (Marker = BC_3). 97968 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: 63999.5. Searching for the closest normal neighbors to the surfaces. Storing a mapping from global to local point index. Compute the surface curvature. Max K: 1594.52. Mean K: 49.8216. Standard deviation K: 81.7526. Checking for periodicity. Computing mesh quality statistics for the dual control volumes. +--------------------------------------------------------------+ | Mesh Quality Metric| Minimum| Maximum| +--------------------------------------------------------------+ | Orthogonality Angle (deg.)| 17.3137| 84.9826| | CV Face Area Aspect Ratio| 1.76874| 29627.5| | CV Sub-Volume Ratio| 1| 307887| +--------------------------------------------------------------+ Setting the multigrid structure. +-------------------------------------------+ | MG Level| CVs|Aggl. Rate| CFL| +-------------------------------------------+ | 0| 22458| 1/1.00| 10| | 1| 4191| 1/5.36| 8.57183| | 2| 992| 1/4.22| 7.95358| +-------------------------------------------+ Finding max control volume width. Semi-span length = 3.87298 m. Wetted area = 10.0438 m^2. Area projection in the x-plane = 0.679139 m^2, y-plane = 0.327414 m^2, z-plane = 4.84583 m^2. Max. coordinate in the x-direction = 2.53651 m, y-direction = 3.87298 m, z-direction = 0.380458 m. Min. coordinate in the x-direction = -0.000478065 m, y-direction = -2.86151e-18 m, z-direction = -0.0467319 m. Checking if Euler & Symmetry markers are straight/plane: Boundary marker BC_3 is NOT a single plane. Boundary marker BC_2 is 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| 211798| 1| m^2/s^2| 211798| | Velocity-X| 100.087| 1| m/s| 100.087| | Velocity-Y| 0| 1| m/s| 0| | Velocity-Z| 0| 1| m/s| 0| | Velocity Magnitude| 100.087| 1| m/s| 100.087| +------------------------------------------------------------------------------+ | Mach Number| -| -| -| 0.294118| +------------------------------------------------------------------------------+ Initialize Jacobian structure (Euler). MG level: 0. Initialize Jacobian structure (Euler). MG level: 1. Initialize Jacobian structure (Euler). MG level: 2. ------------------- Numerics Preprocessing ( Zone 0 ) ------------------- ----------------- Integration Preprocessing ( Zone 0 ) ------------------ ------------------- Iteration Preprocessing ( Zone 0 ) ------------------ Euler/Navier-Stokes/RANS fluid iteration. ------------------------------ Begin Solver ----------------------------- Simulation Run using the Single-zone Driver WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better, see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better, see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better, see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations +----------------------------------------------------------------------------------------------------------------------------------------------+ | Time_Iter| Outer_Iter| Inner_Iter| Cur_Time| Time_Step| Time(sec)| rms[Rho]| rms[RhoU]| rms[RhoV]| rms[RhoE]| CEff| +----------------------------------------------------------------------------------------------------------------------------------------------+ | 0| 0| 0| 0.0000e+00| 0.0000e+00| 5.2922e-01| -1.522041| 0.610909| 0.081705| 3.947065| -0.714275| | 0| 0| 1| 0.0000e+00| 0.0000e+00| 5.1842e-01| -1.291950| 1.174358| 0.979296| 4.180313| -0.204487| | 0| 0| 2| 0.0000e+00| 0.0000e+00| 5.1666e-01| -1.414183| 1.169773| 1.014954| 4.046000| 2.133007| | 0| 0| 3| 0.0000e+00| 0.0000e+00| 5.3025e-01| -1.366227| 1.030327| 0.896439| 4.096843| -18.290094| | 0| 0| 4| 0.0000e+00| 0.0000e+00| 5.2061e-01| -1.459365| 0.949223| 0.900324| 4.001799| -9.240770| ----------------------------- Solver Exit ------------------------------- Maximum number of iterations reached (ITER = 5) before convergence. +-----------------------------------------------------------------------+ | Convergence Field | Value | Criterion | Converged | +-----------------------------------------------------------------------+ | rms[Rho]| -1.45937| < -14| No| +-----------------------------------------------------------------------+ ------------------------------------------------------------------------- +-----------------------------------------------------------------------+ | File Writing Summary | Filename | +-----------------------------------------------------------------------+ |SU2 binary restart |restart_flow_aeroelasticSimple_Pressure_SA.dat| Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Pressure_SA.dat). |CSV file |surface_flow_aeroelasticSimple_Pressure_SA.csv| Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Pressure_SA.dat). |Tecplot binary |flow_aeroelasticSimple_Pressure_SA.szplt| Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Pressure_SA.dat). |Tecplot binary surface |surface_flow_aeroelasticSimple_Pressure_SA.szplt| Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Pressure_SA.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) ------------------------ Running PostAnalysis ...... su2 Executing dataTransfer ...... No variable name provided - defaulting to variable - Pressure Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = Rib_Root, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = Skin, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 3 Name = Skin_Top, index = 1 Name = Skin_Bottom, index = 2 Name = Skin_Tip, index = 3 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Skin, index = 1 Name = Rib_Root, index = 2 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 180 Number of elements = 194 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 32 Elemental Quad4 = 162 Aero_Reference value is NULL - No aero reference parameters set Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 2 Property name - Rib_Root Property name - Skin Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - pressureAero No "groupName" specified for Load tuple pressureAero, going to use load name Done getting FEA loads Optimization Control tuple is NULL - Default optimization control is used Getting FEA optimization control....... Done getting FEA Optimization Control Design_Variable tuple is NULL - No design variables applied Design_Constraint tuple is NULL - No design constraints applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Reading SU2 AeroLoad File - surface_flow_aeroelasticSimple_Pressure_SA.csv Number of variables = 16 Number of data points = 5887 No variable name provided - defaulting to variable - Pressure Reading SU2 AeroLoad File - surface_flow_aeroelasticSimple_Pressure_SA.csv Number of variables = 16 Number of data points = 5887 No variable name provided - defaulting to variable - Pressure Reading SU2 AeroLoad File - surface_flow_aeroelasticSimple_Pressure_SA.csv Number of variables = 16 Number of data points = 5887 Running PreAnalysis ...... astros Extracting external pressure loads from data transfer.... TransferName = Skin_Top Number of Elements = 81 (total = 81) Extracting external pressure loads from data transfer.... TransferName = Skin_Bottom Number of Elements = 81 (total = 162) Extracting external pressure loads from data transfer.... TransferName = Skin_Tip Number of Elements = 16 (total = 178) Writing Astros grid and connectivity file (in free field format) .... Finished writing Astros grid file Writing subElement types (if any) - appending mesh file Writing Astros instruction file.... Writing analysis cards Writing load ADD cards Writing constraint cards--each subcase individually Writing load cards Writing material cards Writing property cards Running Astros...... Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG Running PostAnalysis ...... astros WARNING: 'capsProblem.loadCAPS' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsGeometry.__init__' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsProblem.loadAIM' is deprecated. Please use 'Problem.analysis.create'! WARNING: 'capsAnalysis.__init__' is deprecated. Please use 'Problem.analysis.create'! WARNING: 'capsAnalysis.aimName' is deprecated. Please use 'name'! WARNING: 'capsProblem.__init__' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsAnalysis.getAnalysisInfo' is deprecated. Please use 'Analysis.info'! WARNING: 'capsAnalysis.setAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'! WARNING: 'capsBound.fillVertexSets' is deprecated. Please use 'None'! WARNING: 'capsAnalysis.getAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'! WARNING: 'capsBound.executeTransfer' is deprecated. Please use 'None'! WARNING: 'capsBound.getDestData' is deprecated. Please use 'vertexSet["name"].dataSet["variableName"].getData'! WARNING: 'DataSet.getData' is deprecated. Please use 'DataSet.data'! WARNING: 'capsProblem.closeCAPS' is deprecated. Please use 'close'! real 0m18.769s user 0m14.430s sys 0m1.076s + status=0 + set +x ================================================= Legacy CAPS verification (using pyCAPS) case aeroelasticSimple_Pressure_SU2_and_Astros.py passed (as expected) ================================================= ================================================= + rm -rf aeroelasticSimple_Displacement_SU2_and_Astros + echo 'aeroelasticSimple_Displacement_SU2_and_Astros.py test;' + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt aeroelasticSimple_Displacement_SU2_and_Astros.py test; + python -u aeroelasticSimple_Displacement_SU2_and_Astros.py -verbosity=0 -workDir=runDirectory -noPlotData + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt Running PreAnalysis ...... tetgen Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Farfield, index = 1 Name = SymmPlane, index = 2 Name = Skin, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting surface mesh for body 1 (of 1) Running PostAnalysis ...... tetgen Body 1 (of 1) Number of nodes = 12449 Number of elements = 24894 Number of triangle elements = 24894 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 12449 Total number of elements = 24894 Running PreAnalysis ...... tetgen Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Farfield, index = 1 Name = SymmPlane, index = 2 Name = Skin, index = 3 Number of surface: nodes - 12449, elements - 24894 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Running PostAnalysis ...... tetgen Running PreAnalysis ...... astros Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = Rib_Root, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = Skin, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 3 Name = Skin_Top, index = 1 Name = Skin_Bottom, index = 2 Name = Skin_Tip, index = 3 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Skin, index = 1 Name = Rib_Root, index = 2 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 180 Number of elements = 194 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 32 Elemental Quad4 = 162 Aero_Reference value is NULL - No aero reference parameters set Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 2 Property name - Rib_Root Property name - Skin Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - pressureInternal Done getting FEA loads Optimization Control tuple is NULL - Default optimization control is used Getting FEA optimization control....... Done getting FEA Optimization Control Design_Variable tuple is NULL - No design variables applied Design_Constraint tuple is NULL - No design constraints applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Astros grid and connectivity file (in free field format) .... Finished writing Astros grid file Writing subElement types (if any) - appending mesh file Writing Astros instruction file.... Writing analysis cards Writing load ADD cards Writing constraint cards--each subcase individually Writing load cards Writing material cards Writing property cards Running Astros...... Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG Running PostAnalysis ...... astros Executing dataTransfer ...... No variable name provided - defaulting to variable - Displacement Writing SU2 file .... Finished writing SU2 file Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Skin Boundary condition name - SymmPlane Done getting CFD boundary conditions No variable name provided - defaulting to variable - Displacement No variable name provided - defaulting to variable - Displacement Running PreAnalysis ...... su2 Writing SU2 data transfer files Writing SU2 Motion File - aeroelasticSimple_Displacement_SA_motion.dat Warning: The su2 cfg file will be overwritten! Write SU2 configuration file for version "BlackBird (7.5.1) " Running SU2...... ------------------------------------------------------------------------- | ___ _ _ ___ | | / __| | | |_ ) 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: ../runDirectory_AeroelasticSimple_Displacement_tetgen_tetgenAIM/tetgen_CAPS.su2 ---------------- Grid deformation parameters ( Zone 0 ) ---------------- Grid deformation using a linear elasticity method. -------------------- Output Information ( Zone 0 ) ---------------------- Output mesh file name: ../runDirectory_AeroelasticSimple_Displacement_tetgen_tetgenAIM/tetgen_CAPS.su2. Cell stiffness scaled by distance to nearest solid surface. ------------- Config File Boundary Information ( Zone 0 ) --------------- +-----------------------------------------------------------------------+ | Marker Type| Marker Name| +-----------------------------------------------------------------------+ | Euler wall| BC_3| +-----------------------------------------------------------------------+ | Far-field| BC_1| +-----------------------------------------------------------------------+ | Symmetry plane| BC_2| +-----------------------------------------------------------------------+ Three dimensional problem. 22458 grid points. 97968 volume elements. 3 surface markers. 342 boundary elements in index 0 (Marker = BC_1). 12856 boundary elements in index 1 (Marker = BC_2). 11696 boundary elements in index 2 (Marker = BC_3). 97968 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: 63999.5. 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 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 2.014928 seconds on 1 core. ----------------------- Write deformed grid files ----------------------- |SU2 mesh |../runDirectory_AeroelasticSimple_Displacement_tetgen_tetgenAIM/tetgen_CAPS.su2| |CSV file |surface_deformed.csv | |Tecplot binary |volume_deformed.szplt | |Tecplot binary surface |surface_deformed.szplt | 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) ------------------------ ------------------------------------------------------------------------- | ___ _ _ ___ | | / __| | | |_ ) 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: 0.294118. 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_3. Surface(s) plotted in the output file: BC_3. Surface(s) affected by the design variables: BC_3. Input mesh file name: ../runDirectory_AeroelasticSimple_Displacement_tetgen_tetgenAIM/tetgen_CAPS.su2 --------------- Space Numerical Integration ( Zone 0 ) ------------------ Roe (with entropy fix = 0.001) solver for the flow inviscid terms. Standard Roe without low-dissipation function. Second order integration in space, with slope limiter. Venkatakrishnan slope-limiting method, with constant: 0.05. The reference element size is: 1. Gradient for upwind reconstruction: inverse-distance weighted Least-Squares. Gradient for viscous and source terms: inverse-distance weighted Least-Squares. --------------- Time Numerical Integration ( Zone 0 ) ------------------ Local time stepping (steady state simulation). Euler implicit method for the flow equations. FGMRES is used for solving the linear system. Using a ILU(0) preconditioning. Convergence criteria of the linear solver: 1e-06. Max number of linear iterations: 10. V Multigrid Cycle, with 2 multigrid levels. Damping factor for the residual restriction: 0.75. Damping factor for the correction prolongation: 0.75. No CFL adaptation. +-------------------------------------------+ | MG Level| Presmooth|PostSmooth|CorrectSmo| +-------------------------------------------+ | 0| 1| 0| 0| | 1| 2| 0| 0| | 2| 3| 0| 0| +-------------------------------------------+ Courant-Friedrichs-Lewy number: 10 ------------------ Convergence Criteria ( Zone 0 ) --------------------- Maximum number of solver subiterations: 5. Begin convergence monitoring at iteration 5. Residual minimum value: 1e-14. Cauchy series min. value: 1e-10. Number of Cauchy elements: 100. Begin windowed time average at iteration 0. -------------------- Output Information ( Zone 0 ) ---------------------- File writing frequency: +------------------------------------+ | File| Frequency| +------------------------------------+ | RESTART| 250| | SURFACE_CSV| 250| | TECPLOT| 250| | SURFACE_TECPLOT| 250| +------------------------------------+ Writing the convergence history file every 1 inner iterations. Writing the screen convergence history every 1 inner iterations. The tabular file format is CSV (.csv). Convergence history file name: history. Forces breakdown file name: forces_breakdown_aeroelasticSimple_Displacement_SA.dat. Surface file name: surface_flow_aeroelasticSimple_Displacement_SA. Volume file name: flow_aeroelasticSimple_Displacement_SA. Restart file name: restart_flow_aeroelasticSimple_Displacement_SA.dat. ------------- Config File Boundary Information ( Zone 0 ) --------------- +-----------------------------------------------------------------------+ | Marker Type| Marker Name| +-----------------------------------------------------------------------+ | Euler wall| BC_3| +-----------------------------------------------------------------------+ | Far-field| BC_1| +-----------------------------------------------------------------------+ | Symmetry plane| 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. 22458 grid points. 97968 volume elements. 3 surface markers. 342 boundary elements in index 0 (Marker = BC_1). 12856 boundary elements in index 1 (Marker = BC_2). 11696 boundary elements in index 2 (Marker = BC_3). 97968 tetrahedra. Setting point connectivity. Renumbering points (Reverse Cuthill McKee Ordering). Recomputing point connectivity. Setting element connectivity. Checking the numerical grid orientation. There has been a re-orientation of 4253 TETRAHEDRON volume elements. There has been a re-orientation of 769 TRIANGLE surface elements. Identifying edges and vertices. Setting the control volume structure. Volume of the computational grid: 63997.7. Searching for the closest normal neighbors to the surfaces. Storing a mapping from global to local point index. Compute the surface curvature. Max K: 1963.01. Mean K: 62.1333. Standard deviation K: 144.97. Checking for periodicity. Computing mesh quality statistics for the dual control volumes. +--------------------------------------------------------------+ | Mesh Quality Metric| Minimum| Maximum| +--------------------------------------------------------------+ | Orthogonality Angle (deg.)| 8.16378| 85.1944| | CV Face Area Aspect Ratio| 1.7384| 28783.8| | CV Sub-Volume Ratio| 1.0001| 5.21961e+07| +--------------------------------------------------------------+ Setting the multigrid structure. +-------------------------------------------+ | MG Level| CVs|Aggl. Rate| CFL| +-------------------------------------------+ | 0| 22458| 1/1.00| 10| | 1| 4173| 1/5.38| 8.55954| | 2| 997| 1/4.19| 7.96692| +-------------------------------------------+ Finding max control volume width. Semi-span length = 3.89957 m. Wetted area = 12.4716 m^2. Area projection in the x-plane = 3.09373 m^2, y-plane = 1.33974 m^2, z-plane = 4.79112 m^2. Max. coordinate in the x-direction = 2.53729 m, y-direction = 3.89957 m, z-direction = 0.526515 m. Min. coordinate in the x-direction = -0.00039489 m, y-direction = -2.86151e-18 m, z-direction = -0.706932 m. Checking if Euler & Symmetry markers are straight/plane: Boundary marker BC_3 is NOT a single plane. Boundary marker BC_2 is 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| 211798| 1| m^2/s^2| 211798| | Velocity-X| 100.087| 1| m/s| 100.087| | Velocity-Y| 0| 1| m/s| 0| | Velocity-Z| 0| 1| m/s| 0| | Velocity Magnitude| 100.087| 1| m/s| 100.087| +------------------------------------------------------------------------------+ | Mach Number| -| -| -| 0.294118| +------------------------------------------------------------------------------+ Initialize Jacobian structure (Euler). MG level: 0. Initialize Jacobian structure (Euler). MG level: 1. Initialize Jacobian structure (Euler). MG level: 2. ------------------- Numerics Preprocessing ( Zone 0 ) ------------------- ----------------- Integration Preprocessing ( Zone 0 ) ------------------ ------------------- Iteration Preprocessing ( Zone 0 ) ------------------ Euler/Navier-Stokes/RANS fluid iteration. ------------------------------ Begin Solver ----------------------------- Simulation Run using the Single-zone Driver WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better, see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better, see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better, see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations +----------------------------------------------------------------------------------------------------------------------------------------------+ | Time_Iter| Outer_Iter| Inner_Iter| Cur_Time| Time_Step| Time(sec)| rms[Rho]| rms[RhoU]| rms[RhoV]| rms[RhoE]| CEff| +----------------------------------------------------------------------------------------------------------------------------------------------+ | 0| 0| 0| 0.0000e+00| 0.0000e+00| 5.7666e-01| -0.784125| 1.664191| 1.554873| 4.684981| 0.028551| | 0| 0| 1| 0.0000e+00| 0.0000e+00| 5.7728e-01| -0.427798| 2.028776| 1.838391| 5.048702| -0.004715| | 0| 0| 2| 0.0000e+00| 0.0000e+00| 5.8930e-01| -0.631087| 2.053272| 1.915749| 4.839618| -0.052975| | 0| 0| 3| 0.0000e+00| 0.0000e+00| 5.9812e-01| -0.671366| 1.905122| 1.751247| 4.790616| -0.181235| | 0| 0| 4| 0.0000e+00| 0.0000e+00| 5.9940e-01| -0.664709| 1.752476| 1.560621| 4.800511| 0.076501| ----------------------------- Solver Exit ------------------------------- Maximum number of iterations reached (ITER = 5) before convergence. +-----------------------------------------------------------------------+ | Convergence Field | Value | Criterion | Converged | +-----------------------------------------------------------------------+ | rms[Rho]| -0.664709| < -14| No| +-----------------------------------------------------------------------+ ------------------------------------------------------------------------- +-----------------------------------------------------------------------+ | File Writing Summary | Filename | +-----------------------------------------------------------------------+ |SU2 binary restart |restart_flow_aeroelasticSimple_Displacement_SA.dat| Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Displacement_SA.dat). |CSV file |surface_flow_aeroelasticSimple_Displacement_SA.csv| Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Displacement_SA.dat). |Tecplot binary |flow_aeroelasticSimple_Displacement_SA.szplt| Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Displacement_SA.dat). |Tecplot binary surface |surface_flow_aeroelasticSimple_Displacement_SA.szplt| Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Displacement_SA.dat). +-----------------------------------------------------------------------+ Warning: there are 392 non-physical points in the solution. Warning: 159 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) ------------------------ Running PostAnalysis ...... su2 WARNING: 'capsProblem.loadCAPS' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsGeometry.__init__' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsProblem.loadAIM' is deprecated. Please use 'Problem.analysis.create'! WARNING: 'capsAnalysis.__init__' is deprecated. Please use 'Problem.analysis.create'! WARNING: 'capsAnalysis.aimName' is deprecated. Please use 'name'! WARNING: 'capsProblem.__init__' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsAnalysis.getAnalysisInfo' is deprecated. Please use 'Analysis.info'! WARNING: 'capsAnalysis.setAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'! WARNING: 'capsBound.fillVertexSets' is deprecated. Please use 'None'! WARNING: 'capsBound.executeTransfer' is deprecated. Please use 'None'! WARNING: 'capsBound.getDestData' is deprecated. Please use 'vertexSet["name"].dataSet["variableName"].getData'! WARNING: 'DataSet.getData' is deprecated. Please use 'DataSet.data'! WARNING: 'capsAnalysis.getAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'! WARNING: 'capsProblem.closeCAPS' is deprecated. Please use 'close'! real 0m22.845s user 0m19.630s sys 0m1.505s + status=0 + set +x ================================================= Legacy CAPS verification (using pyCAPS) case aeroelasticSimple_Displacement_SU2_and_Astros.py passed (as expected) ================================================= ================================================= + rm -rf aeroelasticSimple_Iterative_SU2_and_Astros + echo 'aeroelasticSimple_Iterative_SU2_and_Astros.py test;' + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt aeroelasticSimple_Iterative_SU2_and_Astros.py test; + python -u aeroelasticSimple_Iterative_SU2_and_Astros.py -verbosity=0 -workDir=runDirectory + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt Running PreAnalysis ...... egads Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Farfield, index = 1 Name = SymmPlane, index = 2 Name = Skin, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting surface mesh for body 1 (of 1) Running PostAnalysis ...... egads Body 1 (of 1) Number of nodes = 12449 Number of elements = 24894 Number of triangle elements = 24894 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 12449 Total number of elements = 24894 Running PreAnalysis ...... tetgen Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Farfield, index = 1 Name = SymmPlane, index = 2 Name = Skin, index = 3 Number of surface: nodes - 12449, elements - 24894 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000T1.00e-16A Delaunizing vertices... Delaunay seconds: 1.1936 Creating surface mesh ... Surface mesh seconds: 0.021627 Recovering boundaries... Boundary recovery seconds: 0.145404 Removing exterior tetrahedra ... Spreading region attributes. Exterior tets removal seconds: 0.020653 Recovering Delaunayness... Delaunay recovery seconds: 0.033194 Refining mesh... 16594 insertions, added 9098 points, 313535 tetrahedra in queue. 5525 insertions, added 640 points, 44178 tetrahedra in queue. 7365 insertions, added 201 points, 1735 tetrahedra in queue. Refinement seconds: 1.65115 Smoothing vertices... Mesh smoothing seconds: 0.853487 Improving mesh... Mesh improvement seconds: 0.020803 Writing nodes. Writing elements. Writing faces. Writing edges. Output seconds: 0.00384 Total running seconds: 3.94428 Statistics: Input points: 12449 Input facets: 24894 Input segments: 37341 Input holes: 0 Input regions: 0 Mesh points: 22458 Mesh tetrahedra: 97968 Mesh faces: 208383 Mesh faces on exterior boundary: 24894 Mesh faces on input facets: 24894 Mesh edges on input segments: 37341 Steiner points inside domain: 10009 Done meshing using TetGen! Running PostAnalysis ...... tetgen Executing dataTransfer "Displacement"...... Running PreAnalysis ...... su2 Writing SU2 file .... Finished writing SU2 file Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Skin Boundary condition name - SymmPlane Done getting CFD boundary conditions Writing SU2 data transfer files Writing SU2 Motion File - aeroelasticSimple_Iterative_motion.dat Warning: The su2 cfg file will be overwritten! Write SU2 configuration file for version "BlackBird (7.5.1) " 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: 0.294118. 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_3. Surface(s) plotted in the output file: BC_3. Surface(s) affected by the design variables: BC_3. Input mesh file name: ../runDirectory_AeroelasticSimple_Iterative_SA_tetgen_tetgenAIM/tetgen_CAPS.su2 --------------- Space Numerical Integration ( Zone 0 ) ------------------ Roe (with entropy fix = 0.001) solver for the flow inviscid terms. Standard Roe without low-dissipation function. Second order integration in space, with slope limiter. Venkatakrishnan slope-limiting method, with constant: 0.05. The reference element size is: 1. Gradient for upwind reconstruction: inverse-distance weighted Least-Squares. Gradient for viscous and source terms: inverse-distance weighted Least-Squares. --------------- Time Numerical Integration ( Zone 0 ) ------------------ Local time stepping (steady state simulation). Euler implicit method for the flow equations. FGMRES is used for solving the linear system. Using a ILU(0) preconditioning. Convergence criteria of the linear solver: 1e-06. Max number of linear iterations: 10. V Multigrid Cycle, with 2 multigrid levels. Damping factor for the residual restriction: 0.75. Damping factor for the correction prolongation: 0.75. No CFL adaptation. +-------------------------------------------+ | MG Level| Presmooth|PostSmooth|CorrectSmo| +-------------------------------------------+ | 0| 1| 0| 0| | 1| 2| 0| 0| | 2| 3| 0| 0| +-------------------------------------------+ Courant-Friedrichs-Lewy number: 10 ------------------ Convergence Criteria ( Zone 0 ) --------------------- Maximum number of solver subiterations: 5. Begin convergence monitoring at iteration 5. Residual minimum value: 1e-14. Cauchy series min. value: 1e-10. Number of Cauchy elements: 100. Begin windowed time average at iteration 0. -------------------- Output Information ( Zone 0 ) ---------------------- File writing frequency: +------------------------------------+ | File| Frequency| +------------------------------------+ | RESTART| 250| | SURFACE_CSV| 250| | TECPLOT| 250| | SURFACE_TECPLOT| 250| +------------------------------------+ Writing the convergence history file every 1 inner iterations. Writing the screen convergence history every 1 inner iterations. The tabular file format is CSV (.csv). Convergence history file name: history. Forces breakdown file name: forces_breakdown_aeroelasticSimple_Iterative.dat. Surface file name: surface_flow_aeroelasticSimple_Iterative. Volume file name: flow_aeroelasticSimple_Iterative. Restart file name: restart_flow_aeroelasticSimple_Iterative.dat. ------------- Config File Boundary Information ( Zone 0 ) --------------- +-----------------------------------------------------------------------+ | Marker Type| Marker Name| +-----------------------------------------------------------------------+ | Euler wall| BC_3| +-----------------------------------------------------------------------+ | Far-field| BC_1| +-----------------------------------------------------------------------+ | Symmetry plane| 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. 22458 grid points. 97968 volume elements. 3 surface markers. 342 boundary elements in index 0 (Marker = BC_1). 12856 boundary elements in index 1 (Marker = BC_2). 11696 boundary elements in index 2 (Marker = BC_3). 97968 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: 63999.5. Searching for the closest normal neighbors to the surfaces. Storing a mapping from global to local point index. Compute the surface curvature. Max K: 1594.52. Mean K: 49.8216. Standard deviation K: 81.7526. Checking for periodicity. Computing mesh quality statistics for the dual control volumes. +--------------------------------------------------------------+ | Mesh Quality Metric| Minimum| Maximum| +--------------------------------------------------------------+ | Orthogonality Angle (deg.)| 17.3137| 84.9826| | CV Face Area Aspect Ratio| 1.76874| 29627.5| | CV Sub-Volume Ratio| 1| 307887| +--------------------------------------------------------------+ Setting the multigrid structure. +-------------------------------------------+ | MG Level| CVs|Aggl. Rate| CFL| +-------------------------------------------+ | 0| 22458| 1/1.00| 10| | 1| 4191| 1/5.36| 8.57183| | 2| 992| 1/4.22| 7.95358| +-------------------------------------------+ Finding max control volume width. Semi-span length = 3.87298 m. Wetted area = 10.0438 m^2. Area projection in the x-plane = 0.679139 m^2, y-plane = 0.327414 m^2, z-plane = 4.84583 m^2. Max. coordinate in the x-direction = 2.53651 m, y-direction = 3.87298 m, z-direction = 0.380458 m. Min. coordinate in the x-direction = -0.000478065 m, y-direction = -2.86151e-18 m, z-direction = -0.0467319 m. Checking if Euler & Symmetry markers are straight/plane: Boundary marker BC_3 is NOT a single plane. Boundary marker BC_2 is 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| 211798| 1| m^2/s^2| 211798| | Velocity-X| 100.087| 1| m/s| 100.087| | Velocity-Y| 0| 1| m/s| 0| | Velocity-Z| 0| 1| m/s| 0| | Velocity Magnitude| 100.087| 1| m/s| 100.087| +------------------------------------------------------------------------------+ | Mach Number| -| -| -| 0.294118| +------------------------------------------------------------------------------+ Initialize Jacobian structure (Euler). MG level: 0. Initialize Jacobian structure (Euler). MG level: 1. Initialize Jacobian structure (Euler). MG level: 2. ------------------- Numerics Preprocessing ( Zone 0 ) ------------------- ----------------- Integration Preprocessing ( Zone 0 ) ------------------ ------------------- Iteration Preprocessing ( Zone 0 ) ------------------ Euler/Navier-Stokes/RANS fluid iteration. ------------------------------ Begin Solver ----------------------------- Simulation Run using the Single-zone Driver WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better, see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better, see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better, see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations +----------------------------------------------------------------------------------------------------------------------------------------------+ | Time_Iter| Outer_Iter| Inner_Iter| Cur_Time| Time_Step| Time(sec)| rms[Rho]| rms[RhoU]| rms[RhoV]| rms[RhoE]| CEff| +----------------------------------------------------------------------------------------------------------------------------------------------+ | 0| 0| 0| 0.0000e+00| 0.0000e+00| 4.8922e-01| -1.522041| 0.610909| 0.081705| 3.947065| -0.714275| | 0| 0| 1| 0.0000e+00| 0.0000e+00| 4.9383e-01| -1.291950| 1.174358| 0.979296| 4.180313| -0.204487| | 0| 0| 2| 0.0000e+00| 0.0000e+00| 4.9863e-01| -1.414183| 1.169773| 1.014954| 4.046000| 2.133007| | 0| 0| 3| 0.0000e+00| 0.0000e+00| 5.0024e-01| -1.366227| 1.030327| 0.896439| 4.096843| -18.290094| | 0| 0| 4| 0.0000e+00| 0.0000e+00| 5.0372e-01| -1.459365| 0.949223| 0.900324| 4.001799| -9.240770| ----------------------------- Solver Exit ------------------------------- Maximum number of iterations reached (ITER = 5) before convergence. +-----------------------------------------------------------------------+ | Convergence Field | Value | Criterion | Converged | +-----------------------------------------------------------------------+ | rms[Rho]| -1.45937| < -14| No| +-----------------------------------------------------------------------+ ------------------------------------------------------------------------- +-----------------------------------------------------------------------+ | File Writing Summary | Filename | +-----------------------------------------------------------------------+ |SU2 binary restart |restart_flow_aeroelasticSimple_Iterative.dat| Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Iterative.dat). |CSV file |surface_flow_aeroelasticSimple_Iterative.csv| Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Iterative.dat). |Tecplot binary |flow_aeroelasticSimple_Iterative.szplt| Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Iterative.dat). |Tecplot binary surface |surface_flow_aeroelasticSimple_Iterative.szplt| Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Iterative.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) ------------------------ Running PostAnalysis ...... su2 Executing dataTransfer "Pressure"...... Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = Rib_Root, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = Skin, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 3 Name = Skin_Top, index = 1 Name = Skin_Bottom, index = 2 Name = Skin_Tip, index = 3 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Skin, index = 1 Name = Rib_Root, index = 2 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 180 Number of elements = 194 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 32 Elemental Quad4 = 162 Aero_Reference value is NULL - No aero reference parameters set Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 2 Property name - Rib_Root Property name - Skin Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - pressureAero No "groupName" specified for Load tuple pressureAero, going to use load name Done getting FEA loads Optimization Control tuple is NULL - Default optimization control is used Getting FEA optimization control....... Done getting FEA Optimization Control Design_Variable tuple is NULL - No design variables applied Design_Constraint tuple is NULL - No design constraints applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Reading SU2 AeroLoad File - surface_flow_aeroelasticSimple_Iterative.csv Number of variables = 16 Number of data points = 5887 Reading SU2 AeroLoad File - surface_flow_aeroelasticSimple_Iterative.csv Number of variables = 16 Number of data points = 5887 Reading SU2 AeroLoad File - surface_flow_aeroelasticSimple_Iterative.csv Number of variables = 16 Number of data points = 5887 Running PreAnalysis ...... astros Extracting external pressure loads from data transfer.... TransferName = Skin_Top Number of Elements = 81 (total = 81) Extracting external pressure loads from data transfer.... TransferName = Skin_Bottom Number of Elements = 81 (total = 162) Extracting external pressure loads from data transfer.... TransferName = Skin_Tip Number of Elements = 16 (total = 178) Writing Astros grid and connectivity file (in free field format) .... Finished writing Astros grid file Writing subElement types (if any) - appending mesh file Writing Astros instruction file.... Writing analysis cards Writing load ADD cards Writing constraint cards--each subcase individually Writing load cards Writing material cards Writing property cards Running Astros...... Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG Running PostAnalysis ...... astros Executing dataTransfer "Displacement"...... Running PreAnalysis ...... su2 Writing SU2 data transfer files Writing SU2 Motion File - aeroelasticSimple_Iterative_motion.dat Warning: The su2 cfg file will be overwritten! Write SU2 configuration file for version "BlackBird (7.5.1) " Running SU2...... ------------------------------------------------------------------------- | ___ _ _ ___ | | / __| | | |_ ) 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: ../runDirectory_AeroelasticSimple_Iterative_SA_tetgen_tetgenAIM/tetgen_CAPS.su2 ---------------- Grid deformation parameters ( Zone 0 ) ---------------- Grid deformation using a linear elasticity method. -------------------- Output Information ( Zone 0 ) ---------------------- Output mesh file name: ../runDirectory_AeroelasticSimple_Iterative_SA_tetgen_tetgenAIM/tetgen_CAPS.su2. Cell stiffness scaled by distance to nearest solid surface. ------------- Config File Boundary Information ( Zone 0 ) --------------- +-----------------------------------------------------------------------+ | Marker Type| Marker Name| +-----------------------------------------------------------------------+ | Euler wall| BC_3| +-----------------------------------------------------------------------+ | Far-field| BC_1| +-----------------------------------------------------------------------+ | Symmetry plane| BC_2| +-----------------------------------------------------------------------+ Three dimensional problem. 22458 grid points. 97968 volume elements. 3 surface markers. 342 boundary elements in index 0 (Marker = BC_1). 12856 boundary elements in index 1 (Marker = BC_2). 11696 boundary elements in index 2 (Marker = BC_3). 97968 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: 63999.5. 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 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 2.083863 seconds on 1 core. ----------------------- Write deformed grid files ----------------------- |SU2 mesh |../runDirectory_AeroelasticSimple_Iterative_SA_tetgen_tetgenAIM/tetgen_CAPS.su2| |CSV file |surface_deformed.csv | |Tecplot binary |volume_deformed.szplt | |Tecplot binary surface |surface_deformed.szplt | 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) ------------------------ ------------------------------------------------------------------------- | ___ _ _ ___ | | / __| | | |_ ) 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: 0.294118. 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_3. Surface(s) plotted in the output file: BC_3. Surface(s) affected by the design variables: BC_3. Input mesh file name: ../runDirectory_AeroelasticSimple_Iterative_SA_tetgen_tetgenAIM/tetgen_CAPS.su2 --------------- Space Numerical Integration ( Zone 0 ) ------------------ Roe (with entropy fix = 0.001) solver for the flow inviscid terms. Standard Roe without low-dissipation function. Second order integration in space, with slope limiter. Venkatakrishnan slope-limiting method, with constant: 0.05. The reference element size is: 1. Gradient for upwind reconstruction: inverse-distance weighted Least-Squares. Gradient for viscous and source terms: inverse-distance weighted Least-Squares. --------------- Time Numerical Integration ( Zone 0 ) ------------------ Local time stepping (steady state simulation). Euler implicit method for the flow equations. FGMRES is used for solving the linear system. Using a ILU(0) preconditioning. Convergence criteria of the linear solver: 1e-06. Max number of linear iterations: 10. V Multigrid Cycle, with 2 multigrid levels. Damping factor for the residual restriction: 0.75. Damping factor for the correction prolongation: 0.75. No CFL adaptation. +-------------------------------------------+ | MG Level| Presmooth|PostSmooth|CorrectSmo| +-------------------------------------------+ | 0| 1| 0| 0| | 1| 2| 0| 0| | 2| 3| 0| 0| +-------------------------------------------+ Courant-Friedrichs-Lewy number: 10 ------------------ Convergence Criteria ( Zone 0 ) --------------------- Maximum number of solver subiterations: 5. Begin convergence monitoring at iteration 5. Residual minimum value: 1e-14. Cauchy series min. value: 1e-10. Number of Cauchy elements: 100. Begin windowed time average at iteration 0. -------------------- Output Information ( Zone 0 ) ---------------------- File writing frequency: +------------------------------------+ | File| Frequency| +------------------------------------+ | RESTART| 250| | SURFACE_CSV| 250| | TECPLOT| 250| | SURFACE_TECPLOT| 250| +------------------------------------+ Writing the convergence history file every 1 inner iterations. Writing the screen convergence history every 1 inner iterations. The tabular file format is CSV (.csv). Convergence history file name: history. Forces breakdown file name: forces_breakdown_aeroelasticSimple_Iterative.dat. Surface file name: surface_flow_aeroelasticSimple_Iterative. Volume file name: flow_aeroelasticSimple_Iterative. Restart file name: restart_flow_aeroelasticSimple_Iterative.dat. ------------- Config File Boundary Information ( Zone 0 ) --------------- +-----------------------------------------------------------------------+ | Marker Type| Marker Name| +-----------------------------------------------------------------------+ | Euler wall| BC_3| +-----------------------------------------------------------------------+ | Far-field| BC_1| +-----------------------------------------------------------------------+ | Symmetry plane| 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. 22458 grid points. 97968 volume elements. 3 surface markers. 342 boundary elements in index 0 (Marker = BC_1). 12856 boundary elements in index 1 (Marker = BC_2). 11696 boundary elements in index 2 (Marker = BC_3). 97968 tetrahedra. Setting point connectivity. Renumbering points (Reverse Cuthill McKee Ordering). Recomputing point connectivity. Setting element connectivity. Checking the numerical grid orientation. There has been a re-orientation of 21731 TETRAHEDRON volume elements. There has been a re-orientation of 3540 TRIANGLE surface elements. Identifying edges and vertices. Setting the control volume structure. Volume of the computational grid: 71088.9. Searching for the closest normal neighbors to the surfaces. Storing a mapping from global to local point index. Compute the surface curvature. Max K: 3450.52. Mean K: 44.2578. Standard deviation K: 175.787. Checking for periodicity. Computing mesh quality statistics for the dual control volumes. +--------------------------------------------------------------+ | Mesh Quality Metric| Minimum| Maximum| +--------------------------------------------------------------+ | Orthogonality Angle (deg.)| 0.528154| 84.5175| | CV Face Area Aspect Ratio| 1.63485| 2.20226e+06| | CV Sub-Volume Ratio| 1.00334| 1.35114e+09| +--------------------------------------------------------------+ Setting the multigrid structure. +-------------------------------------------+ | MG Level| CVs|Aggl. Rate| CFL| +-------------------------------------------+ | 0| 22458| 1/1.00| 10| | 1| 4190| 1/5.36| 8.57115| | 2| 994| 1/4.22| 7.95892| +-------------------------------------------+ Finding max control volume width. Semi-span length = 8.61817 m. Wetted area = 456.842 m^2. Area projection in the x-plane = 154.037 m^2, y-plane = 105.111 m^2, z-plane = 14.1919 m^2. Max. coordinate in the x-direction = 3.24152 m, y-direction = 8.61817 m, z-direction = 5.78348 m. Min. coordinate in the x-direction = -0.153528 m, y-direction = -2.86151e-18 m, z-direction = -69.415 m. Checking if Euler & Symmetry markers are straight/plane: Boundary marker BC_3 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| 211798| 1| m^2/s^2| 211798| | Velocity-X| 100.087| 1| m/s| 100.087| | Velocity-Y| 0| 1| m/s| 0| | Velocity-Z| 0| 1| m/s| 0| | Velocity Magnitude| 100.087| 1| m/s| 100.087| +------------------------------------------------------------------------------+ | Mach Number| -| -| -| 0.294118| +------------------------------------------------------------------------------+ Initialize Jacobian structure (Euler). MG level: 0. Initialize Jacobian structure (Euler). MG level: 1. Initialize Jacobian structure (Euler). MG level: 2. ------------------- Numerics Preprocessing ( Zone 0 ) ------------------- ----------------- Integration Preprocessing ( Zone 0 ) ------------------ ------------------- Iteration Preprocessing ( Zone 0 ) ------------------ Euler/Navier-Stokes/RANS fluid iteration. ------------------------------ Begin Solver ----------------------------- Simulation Run using the Single-zone Driver WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better, see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better, see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better, see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations +----------------------------------------------------------------------------------------------------------------------------------------------+ | Time_Iter| Outer_Iter| Inner_Iter| Cur_Time| Time_Step| Time(sec)| rms[Rho]| rms[RhoU]| rms[RhoV]| rms[RhoE]| CEff| +----------------------------------------------------------------------------------------------------------------------------------------------+ | 0| 0| 0| 0.0000e+00| 0.0000e+00| 5.9253e-01| 2.530787| 5.497300| 5.493688| 7.999893| -0.196612| | 0| 0| 1| 0.0000e+00| 0.0000e+00| 5.7634e-01| 2.723271| 5.401079| 5.452994| 8.198801| -0.207797| | 0| 0| 2| 0.0000e+00| 0.0000e+00| 6.0061e-01| 2.780043| 5.317559| 5.512648| 8.202985| -0.168580| | 0| 0| 3| 0.0000e+00| 0.0000e+00| 6.0266e-01| 2.917678| 5.542097| 5.624420| 8.371507| -0.168482| | 0| 0| 4| 0.0000e+00| 0.0000e+00| 5.9593e-01| 2.872964| 5.484211| 5.548561| 8.321401| -0.167723| ----------------------------- Solver Exit ------------------------------- Maximum number of iterations reached (ITER = 5) before convergence. +-----------------------------------------------------------------------+ | Convergence Field | Value | Criterion | Converged | +-----------------------------------------------------------------------+ | rms[Rho]| 2.87296| < -14| No| +-----------------------------------------------------------------------+ ------------------------------------------------------------------------- +-----------------------------------------------------------------------+ | File Writing Summary | Filename | +-----------------------------------------------------------------------+ |SU2 binary restart |restart_flow_aeroelasticSimple_Iterative.dat| Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Iterative.dat). |CSV file |surface_flow_aeroelasticSimple_Iterative.csv| Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Iterative.dat). |Tecplot binary |flow_aeroelasticSimple_Iterative.szplt| Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Iterative.dat). |Tecplot binary surface |surface_flow_aeroelasticSimple_Iterative.szplt| Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Iterative.dat). +-----------------------------------------------------------------------+ Warning: there are 1252 non-physical points in the solution. Warning: 565 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) ------------------------ Running PostAnalysis ...... su2 Executing dataTransfer "Pressure"...... Reading SU2 AeroLoad File - surface_flow_aeroelasticSimple_Iterative.csv Number of variables = 16 Number of data points = 5887 Reading SU2 AeroLoad File - surface_flow_aeroelasticSimple_Iterative.csv Number of variables = 16 Number of data points = 5887 Reading SU2 AeroLoad File - surface_flow_aeroelasticSimple_Iterative.csv Number of variables = 16 Number of data points = 5887 Running PreAnalysis ...... astros Extracting external pressure loads from data transfer.... TransferName = Skin_Top Number of Elements = 81 (total = 81) Extracting external pressure loads from data transfer.... TransferName = Skin_Bottom Number of Elements = 81 (total = 162) Extracting external pressure loads from data transfer.... TransferName = Skin_Tip Number of Elements = 16 (total = 178) Writing Astros grid and connectivity file (in free field format) .... Finished writing Astros grid file Writing subElement types (if any) - appending mesh file Writing Astros instruction file.... Writing analysis cards Writing load ADD cards Writing constraint cards--each subcase individually Writing load cards Writing material cards Writing property cards Running Astros...... Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG Running PostAnalysis ...... astros WARNING: 'capsProblem.loadCAPS' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsGeometry.__init__' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsProblem.loadAIM' is deprecated. Please use 'Problem.analysis.create'! WARNING: 'capsAnalysis.__init__' is deprecated. Please use 'Problem.analysis.create'! WARNING: 'capsProblem.__init__' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsAnalysis.getAnalysisInfo' is deprecated. Please use 'Analysis.info'! WARNING: 'capsAnalysis.setAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'! WARNING: 'capsBound.fillVertexSets' is deprecated. Please use 'None'! WARNING: 'capsBound.executeTransfer' is deprecated. Please use 'None'! WARNING: 'capsBound.getDestData' is deprecated. Please use 'vertexSet["name"].dataSet["variableName"].getData'! WARNING: 'DataSet.getData' is deprecated. Please use 'DataSet.data'! WARNING: 'capsProblem.closeCAPS' is deprecated. Please use 'close'! real 0m33.974s user 0m26.147s sys 0m2.051s + status=0 + set +x ================================================= Legacy CAPS verification (using pyCAPS) case aeroelasticSimple_Iterative_SU2_and_Astros.py passed (as expected) ================================================= ================================================= + rm -rf aeroelastic_Iterative_SU2_and_Astros + echo 'aeroelastic_Iterative_SU2_and_Astros.py test;' + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt aeroelastic_Iterative_SU2_and_Astros.py test; + python -u aeroelastic_Iterative_SU2_and_Astros.py -verbosity=0 -workDir=runDirectory + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt Running PreAnalysis ...... egads Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Farfield, index = 1 Name = SymmPlane, index = 2 Name = Skin, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting surface mesh for body 1 (of 1) Running PostAnalysis ...... egads Body 1 (of 1) Number of nodes = 25806 Number of elements = 51608 Number of triangle elements = 51608 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 25806 Total number of elements = 51608 Running PreAnalysis ...... tetgen Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Farfield, index = 1 Name = SymmPlane, index = 2 Name = Skin, index = 3 Number of surface: nodes - 25806, elements - 51608 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000T1.00e-16A Delaunizing vertices... Delaunay seconds: 2.79514 Creating surface mesh ... Surface mesh seconds: 0.046754 Recovering boundaries... Boundary recovery seconds: 0.291965 Removing exterior tetrahedra ... Spreading region attributes. Exterior tets removal seconds: 0.061206 Recovering Delaunayness... Delaunay recovery seconds: 0.043923 Refining mesh... 34399 insertions, added 14653 points, 499798 tetrahedra in queue. 11454 insertions, added 489 points, 75634 tetrahedra in queue. 15269 insertions, added 394 points, 7840 tetrahedra in queue. 20353 insertions, added 576 points, 9806 tetrahedra in queue. Refinement seconds: 13.9834 Smoothing vertices... Mesh smoothing seconds: 1.53191 Improving mesh... Mesh improvement seconds: 0.058478 Writing nodes. Writing elements. Writing faces. Writing edges. Output seconds: 0.015201 Total running seconds: 18.8291 Statistics: Input points: 25806 Input facets: 51608 Input segments: 77412 Input holes: 0 Input regions: 0 Mesh points: 41918 Mesh tetrahedra: 173436 Mesh faces: 372676 Mesh faces on exterior boundary: 51608 Mesh faces on input facets: 51608 Mesh edges on input segments: 77412 Steiner points inside domain: 16112 Done meshing using TetGen! Running PostAnalysis ...... tetgen Executing dataTransfer "Displacement"...... Running PreAnalysis ...... su2 Writing SU2 file .... Finished writing SU2 file Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Skin Boundary condition name - SymmPlane Done getting CFD boundary conditions Writing SU2 data transfer files Writing SU2 Motion File - aeroelastic_Iterative_motion.dat Warning: The su2 cfg file will be overwritten! Write SU2 configuration file for version "BlackBird (7.5.1) " 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: 0.294118. 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_3. Surface(s) plotted in the output file: BC_3. Surface(s) affected by the design variables: BC_3. Input mesh file name: ../runDirectory_Aeroelastic_Iterative_SA_tetgen_tetgenAIM/tetgen_CAPS.su2 --------------- Space Numerical Integration ( Zone 0 ) ------------------ Roe (with entropy fix = 0.001) solver for the flow inviscid terms. Standard Roe without low-dissipation function. Second order integration in space, with slope limiter. Venkatakrishnan slope-limiting method, with constant: 0.05. The reference element size is: 1. Gradient for upwind reconstruction: inverse-distance weighted Least-Squares. Gradient for viscous and source terms: inverse-distance weighted Least-Squares. --------------- Time Numerical Integration ( Zone 0 ) ------------------ Local time stepping (steady state simulation). Euler implicit method for the flow equations. FGMRES is used for solving the linear system. Using a ILU(0) preconditioning. Convergence criteria of the linear solver: 1e-06. Max number of linear iterations: 10. V Multigrid Cycle, with 2 multigrid levels. Damping factor for the residual restriction: 0.75. Damping factor for the correction prolongation: 0.75. No CFL adaptation. +-------------------------------------------+ | MG Level| Presmooth|PostSmooth|CorrectSmo| +-------------------------------------------+ | 0| 1| 0| 0| | 1| 2| 0| 0| | 2| 3| 0| 0| +-------------------------------------------+ Courant-Friedrichs-Lewy number: 10 ------------------ Convergence Criteria ( Zone 0 ) --------------------- Maximum number of solver subiterations: 5. Begin convergence monitoring at iteration 5. Residual minimum value: 1e-14. Cauchy series min. value: 1e-10. Number of Cauchy elements: 100. Begin windowed time average at iteration 0. -------------------- Output Information ( Zone 0 ) ---------------------- File writing frequency: +------------------------------------+ | File| Frequency| +------------------------------------+ | RESTART| 250| | SURFACE_CSV| 250| | TECPLOT| 250| | SURFACE_TECPLOT| 250| +------------------------------------+ Writing the convergence history file every 1 inner iterations. Writing the screen convergence history every 1 inner iterations. The tabular file format is CSV (.csv). Convergence history file name: history. Forces breakdown file name: forces_breakdown_aeroelastic_Iterative.dat. Surface file name: surface_flow_aeroelastic_Iterative. Volume file name: flow_aeroelastic_Iterative. Restart file name: restart_flow_aeroelastic_Iterative.dat. ------------- Config File Boundary Information ( Zone 0 ) --------------- +-----------------------------------------------------------------------+ | Marker Type| Marker Name| +-----------------------------------------------------------------------+ | Euler wall| BC_3| +-----------------------------------------------------------------------+ | Far-field| BC_1| +-----------------------------------------------------------------------+ | Symmetry plane| 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. 41918 grid points. 173436 volume elements. 3 surface markers. 534 boundary elements in index 0 (Marker = BC_1). 31587 boundary elements in index 1 (Marker = BC_2). 19487 boundary elements in index 2 (Marker = BC_3). 173436 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: 63999.5. Searching for the closest normal neighbors to the surfaces. Storing a mapping from global to local point index. Compute the surface curvature. Max K: 1061.04. Mean K: 24.5917. Standard deviation K: 61.8627. Checking for periodicity. Computing mesh quality statistics for the dual control volumes. +--------------------------------------------------------------+ | Mesh Quality Metric| Minimum| Maximum| +--------------------------------------------------------------+ | Orthogonality Angle (deg.)| 5.97672| 84.9716| | CV Face Area Aspect Ratio| 1.64884| 13243.7| | CV Sub-Volume Ratio| 1| 110691| +--------------------------------------------------------------+ Setting the multigrid structure. +-------------------------------------------+ | MG Level| CVs|Aggl. Rate| CFL| +-------------------------------------------+ | 0| 41918| 1/1.00| 10| | 1| 7975| 1/5.26| 8.62716| | 2| 1938| 1/4.12| 8.07545| +-------------------------------------------+ Finding max control volume width. Semi-span length = 3.87298 m. Wetted area = 10.1966 m^2. Area projection in the x-plane = 0.682428 m^2, y-plane = 0.335229 m^2, z-plane = 4.92027 m^2. Max. coordinate in the x-direction = 2.53651 m, y-direction = 3.87298 m, z-direction = 0.380458 m. Min. coordinate in the x-direction = -0.000478065 m, y-direction = -2.86151e-18 m, z-direction = -0.0467319 m. Checking if Euler & Symmetry markers are straight/plane: Boundary marker BC_3 is NOT a single plane. Boundary marker BC_2 is 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| 211798| 1| m^2/s^2| 211798| | Velocity-X| 100.087| 1| m/s| 100.087| | Velocity-Y| 0| 1| m/s| 0| | Velocity-Z| 0| 1| m/s| 0| | Velocity Magnitude| 100.087| 1| m/s| 100.087| +------------------------------------------------------------------------------+ | Mach Number| -| -| -| 0.294118| +------------------------------------------------------------------------------+ 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| 1.0424e+00| -1.910881| 0.181576| -0.221362| 3.558225| -0.650644| | 0| 0| 1| 0.0000e+00| 0.0000e+00| 1.0152e+00| -1.256296| 1.079780| 0.952916| 4.219359| -0.210790| | 0| 0| 2| 0.0000e+00| 0.0000e+00| 1.0107e+00| -1.253941| 1.171268| 1.253954| 4.219665| 2.082520| | 0| 0| 3| 0.0000e+00| 0.0000e+00| 9.9294e-01| -1.211082| 0.979967| 1.082535| 4.247470| -13.609700| | 0| 0| 4| 0.0000e+00| 0.0000e+00| 9.9616e-01| -1.128108| 1.010612| 1.011752| 4.340161| -7.775302| ----------------------------- Solver Exit ------------------------------- Maximum number of iterations reached (ITER = 5) before convergence. +-----------------------------------------------------------------------+ | Convergence Field | Value | Criterion | Converged | +-----------------------------------------------------------------------+ | rms[Rho]| -1.12811| < -14| No| +-----------------------------------------------------------------------+ ------------------------------------------------------------------------- +-----------------------------------------------------------------------+ | File Writing Summary | Filename | +-----------------------------------------------------------------------+ |SU2 binary restart |restart_flow_aeroelastic_Iterative.dat| Writing the forces breakdown file (forces_breakdown_aeroelastic_Iterative.dat). |CSV file |surface_flow_aeroelastic_Iterative.csv| Writing the forces breakdown file (forces_breakdown_aeroelastic_Iterative.dat). |Tecplot binary |flow_aeroelastic_Iterative.szplt | Writing the forces breakdown file (forces_breakdown_aeroelastic_Iterative.dat). |Tecplot binary surface |surface_flow_aeroelastic_Iterative.szplt| Writing the forces breakdown file (forces_breakdown_aeroelastic_Iterative.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) ------------------------ Running PostAnalysis ...... su2 Executing dataTransfer "Pressure"...... Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = Rib_Root, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 3 Name = Skin_Top, index = 1 Name = Skin_Bottom, index = 2 Name = Skin_Tip, index = 3 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Ribs_and_Spars, index = 1 Name = Skin, index = 2 Name = Rib_Root, index = 3 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 746 Number of elements = 898 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 120 Elemental Quad4 = 778 Aero_Reference value is NULL - No aero reference parameters set Getting FEA materials....... Number of materials - 2 Material name - Madeupium Material name - Unobtainium Done getting FEA materials Getting FEA properties....... Number of properties - 3 Property name - Rib_Root Property name - Ribs_and_Spars Property name - Skin Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - pressureAero No "groupName" specified for Load tuple pressureAero, going to use load name Done getting FEA loads Optimization Control tuple is NULL - Default optimization control is used Getting FEA optimization control....... Done getting FEA Optimization Control Design_Variable tuple is NULL - No design variables applied Design_Constraint tuple is NULL - No design constraints applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Reading SU2 AeroLoad File - surface_flow_aeroelastic_Iterative.csv Number of variables = 16 Number of data points = 9796 Reading SU2 AeroLoad File - surface_flow_aeroelastic_Iterative.csv Number of variables = 16 Number of data points = 9796 Reading SU2 AeroLoad File - surface_flow_aeroelastic_Iterative.csv Number of variables = 16 Number of data points = 9796 Running PreAnalysis ...... astros Extracting external pressure loads from data transfer.... TransferName = Skin_Top Number of Elements = 330 (total = 330) Extracting external pressure loads from data transfer.... TransferName = Skin_Bottom Number of Elements = 330 (total = 660) Extracting external pressure loads from data transfer.... TransferName = Skin_Tip Number of Elements = 30 (total = 690) Writing Astros grid and connectivity file (in free field format) .... Finished writing Astros grid file Writing subElement types (if any) - appending mesh file Writing Astros instruction file.... Writing analysis cards Writing load ADD cards Writing constraint cards--each subcase individually Writing load cards Writing material cards Writing property cards Running Astros...... Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG Running PostAnalysis ...... astros Executing dataTransfer "Displacement"...... Running PreAnalysis ...... su2 Writing SU2 data transfer files Writing SU2 Motion File - aeroelastic_Iterative_motion.dat Warning: The su2 cfg file will be overwritten! Write SU2 configuration file for version "BlackBird (7.5.1) " Running SU2...... ------------------------------------------------------------------------- | ___ _ _ ___ | | / __| | | |_ ) 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: ../runDirectory_Aeroelastic_Iterative_SA_tetgen_tetgenAIM/tetgen_CAPS.su2 ---------------- Grid deformation parameters ( Zone 0 ) ---------------- Grid deformation using a linear elasticity method. -------------------- Output Information ( Zone 0 ) ---------------------- Output mesh file name: ../runDirectory_Aeroelastic_Iterative_SA_tetgen_tetgenAIM/tetgen_CAPS.su2. Cell stiffness scaled by distance to nearest solid surface. ------------- Config File Boundary Information ( Zone 0 ) --------------- +-----------------------------------------------------------------------+ | Marker Type| Marker Name| +-----------------------------------------------------------------------+ | Euler wall| BC_3| +-----------------------------------------------------------------------+ | Far-field| BC_1| +-----------------------------------------------------------------------+ | Symmetry plane| BC_2| +-----------------------------------------------------------------------+ Three dimensional problem. 41918 grid points. 173436 volume elements. 3 surface markers. 534 boundary elements in index 0 (Marker = BC_1). 31587 boundary elements in index 1 (Marker = BC_2). 19487 boundary elements in index 2 (Marker = BC_3). 173436 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: 63999.5. 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 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 4.764089 seconds on 1 core. ----------------------- Write deformed grid files ----------------------- |SU2 mesh |../runDirectory_Aeroelastic_Iterative_SA_tetgen_tetgenAIM/tetgen_CAPS.su2| |CSV file |surface_deformed.csv | |Tecplot binary |volume_deformed.szplt | |Tecplot binary surface |surface_deformed.szplt | 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) ------------------------ ------------------------------------------------------------------------- | ___ _ _ ___ | | / __| | | |_ ) 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: 0.294118. 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_3. Surface(s) plotted in the output file: BC_3. Surface(s) affected by the design variables: BC_3. Input mesh file name: ../runDirectory_Aeroelastic_Iterative_SA_tetgen_tetgenAIM/tetgen_CAPS.su2 --------------- Space Numerical Integration ( Zone 0 ) ------------------ Roe (with entropy fix = 0.001) solver for the flow inviscid terms. Standard Roe without low-dissipation function. Second order integration in space, with slope limiter. Venkatakrishnan slope-limiting method, with constant: 0.05. The reference element size is: 1. Gradient for upwind reconstruction: inverse-distance weighted Least-Squares. Gradient for viscous and source terms: inverse-distance weighted Least-Squares. --------------- Time Numerical Integration ( Zone 0 ) ------------------ Local time stepping (steady state simulation). Euler implicit method for the flow equations. FGMRES is used for solving the linear system. Using a ILU(0) preconditioning. Convergence criteria of the linear solver: 1e-06. Max number of linear iterations: 10. V Multigrid Cycle, with 2 multigrid levels. Damping factor for the residual restriction: 0.75. Damping factor for the correction prolongation: 0.75. No CFL adaptation. +-------------------------------------------+ | MG Level| Presmooth|PostSmooth|CorrectSmo| +-------------------------------------------+ | 0| 1| 0| 0| | 1| 2| 0| 0| | 2| 3| 0| 0| +-------------------------------------------+ Courant-Friedrichs-Lewy number: 10 ------------------ Convergence Criteria ( Zone 0 ) --------------------- Maximum number of solver subiterations: 5. Begin convergence monitoring at iteration 5. Residual minimum value: 1e-14. Cauchy series min. value: 1e-10. Number of Cauchy elements: 100. Begin windowed time average at iteration 0. -------------------- Output Information ( Zone 0 ) ---------------------- File writing frequency: +------------------------------------+ | File| Frequency| +------------------------------------+ | RESTART| 250| | SURFACE_CSV| 250| | TECPLOT| 250| | SURFACE_TECPLOT| 250| +------------------------------------+ Writing the convergence history file every 1 inner iterations. Writing the screen convergence history every 1 inner iterations. The tabular file format is CSV (.csv). Convergence history file name: history. Forces breakdown file name: forces_breakdown_aeroelastic_Iterative.dat. Surface file name: surface_flow_aeroelastic_Iterative. Volume file name: flow_aeroelastic_Iterative. Restart file name: restart_flow_aeroelastic_Iterative.dat. ------------- Config File Boundary Information ( Zone 0 ) --------------- +-----------------------------------------------------------------------+ | Marker Type| Marker Name| +-----------------------------------------------------------------------+ | Euler wall| BC_3| +-----------------------------------------------------------------------+ | Far-field| BC_1| +-----------------------------------------------------------------------+ | Symmetry plane| 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. 41918 grid points. 173436 volume elements. 3 surface markers. 534 boundary elements in index 0 (Marker = BC_1). 31587 boundary elements in index 1 (Marker = BC_2). 19487 boundary elements in index 2 (Marker = BC_3). 173436 tetrahedra. Setting point connectivity. Renumbering points (Reverse Cuthill McKee Ordering). Recomputing point connectivity. Setting element connectivity. Checking the numerical grid orientation. There has been a re-orientation of 78798 TETRAHEDRON volume elements. There has been a re-orientation of 22029 TRIANGLE surface elements. Identifying edges and vertices. Setting the control volume structure. Volume of the computational grid: 8.27584e+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: 112344. Mean K: 31.2695. Standard deviation K: 1107.54. Checking for periodicity. Computing mesh quality statistics for the dual control volumes. +--------------------------------------------------------------+ | Mesh Quality Metric| Minimum| Maximum| +--------------------------------------------------------------+ | Orthogonality Angle (deg.)| 0.058769| 82.8407| | CV Face Area Aspect Ratio| 1.57009| 1.27347e+17| | CV Sub-Volume Ratio| 1.00111| 9.4723e+08| +--------------------------------------------------------------+ Setting the multigrid structure. +-------------------------------------------+ | MG Level| CVs|Aggl. Rate| CFL| +-------------------------------------------+ | 0| 41918| 1/1.00| 10| | 1| 7998| 1/5.24| 8.63545| | 2| 1942| 1/4.12| 8.08101| +-------------------------------------------+ Finding max control volume width. Semi-span length = 52.245 m. Wetted area = 18384.9 m^2. Area projection in the x-plane = 9598 m^2, y-plane = 3966.08 m^2, z-plane = 250.784 m^2. Max. coordinate in the x-direction = 11.3024 m, y-direction = 52.245 m, z-direction = 20.8385 m. Min. coordinate in the x-direction = -2.09156 m, y-direction = -0.777071 m, z-direction = -679.673 m. Checking if Euler & Symmetry markers are straight/plane: Boundary marker BC_3 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| 211798| 1| m^2/s^2| 211798| | Velocity-X| 100.087| 1| m/s| 100.087| | Velocity-Y| 0| 1| m/s| 0| | Velocity-Z| 0| 1| m/s| 0| | Velocity Magnitude| 100.087| 1| m/s| 100.087| +------------------------------------------------------------------------------+ | Mach Number| -| -| -| 0.294118| +------------------------------------------------------------------------------+ 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| 1.0453e+00| 4.453318| 7.419351| 7.485787| 9.922424| -0.030800| | 0| 0| 1| 0.0000e+00| 0.0000e+00| 1.0507e+00| 4.580743| 7.294697| 7.357056| 10.040688| -0.020745| | 0| 0| 2| 0.0000e+00| 0.0000e+00| 1.0954e+00| 4.705500| 7.402924| 7.481854| 10.297560| -0.001897| | 0| 0| 3| 0.0000e+00| 0.0000e+00| 1.1069e+00| 4.762909| 7.375298| 7.499765| 10.387224| 0.052939| | 0| 0| 4| 0.0000e+00| 0.0000e+00| 1.1223e+00| 4.816907| 7.426480| 7.487920| 10.392108| -0.001850| ----------------------------- Solver Exit ------------------------------- Maximum number of iterations reached (ITER = 5) before convergence. +-----------------------------------------------------------------------+ | Convergence Field | Value | Criterion | Converged | +-----------------------------------------------------------------------+ | rms[Rho]| 4.81691| < -14| No| +-----------------------------------------------------------------------+ ------------------------------------------------------------------------- +-----------------------------------------------------------------------+ | File Writing Summary | Filename | +-----------------------------------------------------------------------+ |SU2 binary restart |restart_flow_aeroelastic_Iterative.dat| Writing the forces breakdown file (forces_breakdown_aeroelastic_Iterative.dat). |CSV file |surface_flow_aeroelastic_Iterative.csv| Writing the forces breakdown file (forces_breakdown_aeroelastic_Iterative.dat). |Tecplot binary |flow_aeroelastic_Iterative.szplt | Writing the forces breakdown file (forces_breakdown_aeroelastic_Iterative.dat). |Tecplot binary surface |surface_flow_aeroelastic_Iterative.szplt| Writing the forces breakdown file (forces_breakdown_aeroelastic_Iterative.dat). +-----------------------------------------------------------------------+ Warning: there are 1722 non-physical points in the solution. Warning: 748 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) ------------------------ Running PostAnalysis ...... su2 Executing dataTransfer "Pressure"...... Reading SU2 AeroLoad File - surface_flow_aeroelastic_Iterative.csv Number of variables = 16 Number of data points = 9796 Reading SU2 AeroLoad File - surface_flow_aeroelastic_Iterative.csv Number of variables = 16 Number of data points = 9796 Reading SU2 AeroLoad File - surface_flow_aeroelastic_Iterative.csv Number of variables = 16 Number of data points = 9796 Running PreAnalysis ...... astros Extracting external pressure loads from data transfer.... TransferName = Skin_Top Number of Elements = 330 (total = 330) Extracting external pressure loads from data transfer.... TransferName = Skin_Bottom Number of Elements = 330 (total = 660) Extracting external pressure loads from data transfer.... TransferName = Skin_Tip Number of Elements = 30 (total = 690) Writing Astros grid and connectivity file (in free field format) .... Finished writing Astros grid file Writing subElement types (if any) - appending mesh file Writing Astros instruction file.... Writing analysis cards Writing load ADD cards Writing constraint cards--each subcase individually Writing load cards Writing material cards Writing property cards Running Astros...... Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG Running PostAnalysis ...... astros WARNING: 'capsProblem.loadCAPS' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsGeometry.__init__' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsProblem.loadAIM' is deprecated. Please use 'Problem.analysis.create'! WARNING: 'capsAnalysis.__init__' is deprecated. Please use 'Problem.analysis.create'! WARNING: 'capsProblem.__init__' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsAnalysis.getAnalysisInfo' is deprecated. Please use 'Analysis.info'! WARNING: 'capsAnalysis.setAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'! WARNING: 'capsBound.fillVertexSets' is deprecated. Please use 'None'! WARNING: 'capsBound.executeTransfer' is deprecated. Please use 'None'! WARNING: 'capsBound.getDestData' is deprecated. Please use 'vertexSet["name"].dataSet["variableName"].getData'! WARNING: 'DataSet.getData' is deprecated. Please use 'DataSet.data'! WARNING: 'capsProblem.closeCAPS' is deprecated. Please use 'close'! real 1m39.771s user 1m21.069s sys 0m5.606s + status=0 + set +x ================================================= Legacy CAPS verification (using pyCAPS) case aeroelastic_Iterative_SU2_and_Astros.py passed (as expected) ================================================= ************************************************* ************************************************* ================================================= Legacy Did not run examples for: Mystran ================================================= All tests pass! ================================================= ================================================= [Execution node] check if [viggen] is in [[windows10x64]] Run condition [Execution node ] preventing perform for step [Execute Windows batch command] [GNU C Compiler (gcc)] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64') [GNU C Compiler (gcc)] Successfully parsed console log [GNU C Compiler (gcc)] -> found 0 issues (skipped 0 duplicates) [GNU C Compiler (gcc)] Skipping post processing [GNU C Compiler (gcc)] No filter has been set, publishing all 0 issues [GNU C Compiler (gcc)] Repository miner is not configured, skipping repository mining [Clang] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64') [Clang] -> found 0 issues (skipped 0 duplicates) [Clang] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64') [Clang] -> found 0 issues (skipped 0 duplicates) [Clang] Successfully parsed console log [Clang] -> found 0 issues (skipped 0 duplicates) [Clang] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64') [Clang] Skipping post processing [Clang] No filter has been set, publishing all 0 issues [Clang] Repository miner is not configured, skipping repository mining [Static Analysis] Successfully parsed console log [Static Analysis] -> found 0 issues (skipped 0 duplicates) [Static Analysis] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64') [Static Analysis] Successfully parsed console log [Static Analysis] -> found 0 issues (skipped 0 duplicates) [Static Analysis] Skipping post processing [Static Analysis] No filter has been set, publishing all 0 issues [Static Analysis] Repository miner is not configured, skipping repository mining [Static Analysis] Successfully parsed console log [Static Analysis] -> found 0 issues (skipped 0 duplicates) [Static Analysis] Successfully parsed console log [Static Analysis] -> found 0 issues (skipped 0 duplicates) [Static Analysis] Successfully parsed console log [Static Analysis] -> found 0 issues (skipped 0 duplicates) [Static Analysis] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/AEROELASTIC/DARWIN_ARM64') [Static Analysis] Skipping post processing [Static Analysis] No filter has been set, publishing all 0 issues [Static Analysis] Repository miner is not configured, skipping repository mining [Static Analysis] Reference build recorder is not configured [Static Analysis] 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 0 issues (found 0 new issues, fixed 0 issues) [Static Analysis] Attaching ResultAction with ID 'analysis' to build 'ESP_RegCaps/CASREV=7.7,ESPTEST=CAPS/AEROELASTIC,ESP_ARCH=DARWIN_ARM64,buildnode=viggen #649'. [Checks API] No suitable checks publisher found. [PostBuildScript] - [INFO] Executing post build scripts. [PostBuildScript] - [INFO] build step #0 should only be executed on MATRIX [WS-CLEANUP] Deleting project workspace... [WS-CLEANUP] done Finished: SUCCESS