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Started by upstream project "ESP_RegCaps" build number 650 originally caused by: Started by an SCM change Running as SYSTEM [EnvInject] - Loading node environment variables. Building remotely on macys_VM in workspace /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64 [WS-CLEANUP] Deleting project workspace... [WS-CLEANUP] Done Cleaning up /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/EGADS Deleting /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/EGADS/trunk/test/capsUnit.txt Deleting /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/EGADS/trunk/pyEGADS/test/__pycache__ Deleting /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/EGADS/trunk/pyEGADS/test/capsUnit.txt Deleting /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/EGADS/trunk/pyEGADS/pyEGADS/__pycache__ Deleting /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/EGADS/trunk/docs/EGADS_dot/src/capsUnit.txt Deleting /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/EGADS/trunk/docs/EGADS_dot/src/circle1_dot Deleting /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/EGADS/trunk/docs/EGADS_dot/src/circle2_dot Deleting /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/EGADS/trunk/docs/EGADS_dot/src/naca_dot Deleting 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svn+ssh://acdl.mit.edu/home/svnroot/JenkinsESP at revision '2024-05-18T22:19:06.737 -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’ U valgrind/valgrind-python.supp At revision 862 Cleaning up /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/OpenCSM/trunk/src Updating svn+ssh://acdl.mit.edu/home/svnroot/OpenCSM/trunk/src at revision '2024-05-18T22:19:06.737 -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’ U udpUtilities.c At revision 2496 Cleaning up /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/OpenCSM/trunk/udc Updating svn+ssh://acdl.mit.edu/home/svnroot/OpenCSM/trunk/udc at revision '2024-05-18T22:19:06.737 -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 2496 Cleaning up /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/OpenCSM/trunk/data Updating svn+ssh://acdl.mit.edu/home/svnroot/OpenCSM/trunk/data at revision '2024-05-18T22:19:06.737 -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’ U vsp3/OPAM1_wing.csm U vsp3/verify_7.6.0/OPAM1_wing.vfy U vsp3/verify_7.7.0/OPAM1_wing.vfy U vsp3/verify_7.8.0/OPAM1_wing.vfy 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 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Slugs/verify_7.6.0/blend12_1.vfy A Slugs/verify_7.6.0/blindeye_1.vfy A Slugs/verify_7.6.0/boxBall_1.vfy A Slugs/verify_7.6.0/boxHole_1.vfy A Slugs/verify_7.6.0/box_1.vfy A Slugs/verify_7.6.0/cylinderHole_1.vfy A Slugs/verify_7.6.0/cylinder_1.vfy A Slugs/verify_7.6.0/damaged_2.vfy A Slugs/verify_7.6.0/demo1_1.vfy A Slugs/verify_7.6.0/duct_1.vfy A Slugs/verify_7.6.0/eyeball_1.vfy A Slugs/verify_7.6.0/holes_1.vfy A Slugs/verify_7.6.0/pieslice_1.vfy A Slugs/verify_7.6.0/sphere_1.vfy A Slugs/verify_7.6.0/torus_1.vfy A Slugs/verify_7.6.0/tutorial1.vfy A Slugs/verify_7.6.0/wing_1.vfy A Slugs/holes_0.stl 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/boxBall_0.jrnl A Slugs/boxBall.plot A Slugs/boxBall_0.stl A Slugs/holes.plot A Slugs/holes_0.csm A Slugs/holes_0.jrnl A Slugs/holes_1.csm AU Slugs/tutorial1.stl A Slugs/sphere_0.stl A Slugs/blend12.plot A Slugs/blend12_0.csm A Slugs/blend12_0.stl A Slugs/blindeye.plot A Slugs/blindeye_0.csm A 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 2496 Cleaning up /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/OpenCSM/trunk/pyOCSM Deleting /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/OpenCSM/trunk/pyOCSM/pyOCSM/__pycache__ Updating svn+ssh://acdl.mit.edu/home/svnroot/OpenCSM/trunk/pyOCSM at revision '2024-05-18T22:19:06.737 -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 2496 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’ 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’ 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/OpenCSM/trunk/udc 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/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 [macys_VM] is in [[macys, macys_VM, reynolds, viggen]] Run condition [Execution node ] enabling perform for step [Execute shell] [DARWIN64] $ /bin/bash -xe /var/folders/qk/9zkf0syn149fvhw9mh7hgd5w0000gp/T/jenkins12575711930547620096.sh + rm -rf /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/CAPS/training/lectures + [[ CAPS/unit != *\S\l\u\g\s* ]] + rm -rf /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/OpenCSM/trunk/data/Slugs + [[ macys_VM == *\v\i\g\g\e\n* ]] + bash -ex /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/JenkinsESP/ESP_Regression.sh + source /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/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 ++ [[ macys_VM == \r\e\y\n\o\l\d\s ]] ++ [[ DARWIN64 == *\.\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 ++ [[ DARWIN64 == \D\A\R\W\I\N\6\4\.\g\c\c ]] ++ export ESP_BLOC=/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64 ++ ESP_BLOC=/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64 ++ export ESP_ROOT=/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64 ++ ESP_ROOT=/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64 ++ export JULIA_DEPOT_PATH=/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/julia ++ JULIA_DEPOT_PATH=/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/julia ++ export AWAVE=awavemod.f ++ AWAVE=awavemod.f ++ export RLM_CONNECT_TIMEOUT=350 ++ RLM_CONNECT_TIMEOUT=350 ++ [[ 7.8 != '' ]] ++ [[ '' != '' ]] ++ [[ macys_VM == *\r\e\y\n\o\l\d\s* ]] ++ [[ macys_VM == *\m\a\c\y\s* ]] ++ export EMPnumProc=2 ++ EMPnumProc=2 ++ export OMP_NUM_THREADS=2 ++ OMP_NUM_THREADS=2 ++ source /Users/jenkins/.bash_profile +++ [[ -r /usr/local/etc/profile.d/bash_completion.sh ]] +++ . /usr/local/etc/profile.d/bash_completion.sh ++++ '[' -z '3.2.57(1)-release' -o -z '' -o -n '' ']' ++++ return +++ export PATH=/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin +++ PATH=/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin +++ export PATH=/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin +++ PATH=/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin ++ [[ macys_VM == *\m\a\c\y\s* ]] ++ export PATH=/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/ ++ PATH=/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/ ++ [[ macys_VM == \m\a\c\y\s ]] ++ export CASARCH=. ++ CASARCH=. ++ '[' '!' -z '' ']' +++ ls -d /Users/jenkins/util/ESP/OpenCASCADE-7.8.0 ++ export CASROOT=/Users/jenkins/util/ESP/OpenCASCADE-7.8.0 ++ CASROOT=/Users/jenkins/util/ESP/OpenCASCADE-7.8.0 ++ export UDUNITS2_XML_PATH=/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/udunits/udunits2.xml ++ UDUNITS2_XML_PATH=/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/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/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib:/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/lib:/opt/intel/oneapi/tbb/2021.3.0/env/../lib:/opt/intel/oneapi/mkl/2021.3.0/lib:/opt/intel/oneapi/compiler/2021.3.0/mac/compiler/lib/intel64_mac:/opt/intel/oneapi/compiler/2021.3.0/mac/compiler/lib ++ DYLD_LIBRARY_PATH=/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib:/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/lib:/opt/intel/oneapi/tbb/2021.3.0/env/../lib:/opt/intel/oneapi/mkl/2021.3.0/lib:/opt/intel/oneapi/compiler/2021.3.0/mac/compiler/lib/intel64_mac:/opt/intel/oneapi/compiler/2021.3.0/mac/compiler/lib ++ export AFLR=/Users/jenkins/util/AFLR/aflr_lib_11.5.14 ++ AFLR=/Users/jenkins/util/AFLR/aflr_lib_11.5.14 ++ [[ macys_VM == *\m\a\c\y\s* ]] ++ export AFLR_ARCH=MacOSX-x86-64 ++ AFLR_ARCH=MacOSX-x86-64 ++ 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:/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/ ++ PATH=/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/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:/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/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:/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/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:/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/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:/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/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:/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/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:/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/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:/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/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:/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/ ++ [[ macys_VM == \m\a\c\y\s ]] ++ [[ macys_VM == \v\i\g\g\e\n ]] ++ [[ macys_VM == \v\i\g\g\e\n ]] ++ 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:/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/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:/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/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:/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/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:/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin ++ '[' -d /Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16 ']' ++ export PATH=/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/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:/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin ++ PATH=/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/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:/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin ++ export PATH=/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/test:/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/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:/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin ++ PATH=/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/test:/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/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:/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin ++ export PYTHONPATH=/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/EGADS/trunk/pyEGADS::/Users/jenkins/util/SU2/SU2-v8.0.0/bin ++ PYTHONPATH=/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/EGADS/trunk/pyEGADS::/Users/jenkins/util/SU2/SU2-v8.0.0/bin ++ export PYTHONPATH=/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/OpenCSM/trunk/pyOCSM:/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/EGADS/trunk/pyEGADS::/Users/jenkins/util/SU2/SU2-v8.0.0/bin ++ PYTHONPATH=/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/OpenCSM/trunk/pyOCSM:/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/EGADS/trunk/pyEGADS::/Users/jenkins/util/SU2/SU2-v8.0.0/bin ++ export PYTHONPATH=/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/CAPS/pyCAPS:/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/OpenCSM/trunk/pyOCSM:/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/EGADS/trunk/pyEGADS::/Users/jenkins/util/SU2/SU2-v8.0.0/bin ++ PYTHONPATH=/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/CAPS/pyCAPS:/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/OpenCSM/trunk/pyOCSM:/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/EGADS/trunk/pyEGADS::/Users/jenkins/util/SU2/SU2-v8.0.0/bin ++ [[ macys_VM == \m\a\c\y\s* ]] ++ mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/bin ++ rm -f /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/bin/python ++ rm -f /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/bin/python-config ++ rm -f /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/bin/virtualenv ++ rm -f '/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/bin/analyze-*' ++ rm -f '/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/bin/intercept-*' ++ [[ macys_VM == \m\a\c\y\s ]] ++ [[ macys_VM == \v\i\g\g\e\n ]] ++ ln -s /usr/local/bin/python3 /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/bin/python ++ ln -s /usr/local/bin/python3-config /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/bin/python-config ++ ln -s /usr/local/bin/virtualenv /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/bin/virtualenv +++ python-config --includes ++ export 'PYTHONINC=. -I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11 -I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11' ++ PYTHONINC='. -I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11 -I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11' +++ python-config --help ++ [[ Usage: /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/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/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/lib/python3.11/config-3.11-darwin -lpython3.11 -ldl -framework CoreFoundation' ++ PYTHONLIB='-L/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/lib/python3.11/config-3.11-darwin -lpython3.11 -ldl -framework CoreFoundation' ++ [[ macys_VM == \m\a\c\y\s ]] ++ [[ macys_VM == \v\i\g\g\e\n ]] ++ export PYTHONUNBUFFERED=true ++ PYTHONUNBUFFERED=true ++ export PYTHONFAULTHANDLER=true ++ PYTHONFAULTHANDLER=true ++ python --version Python 3.11.5 ++ [[ DARWIN64 == \D\A\R\W\I\N\6\4\.\g\c\c ]] ++ export CSMDATA=/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/OpenCSM/trunk/data ++ CSMDATA=/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/OpenCSM/trunk/data + source /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/JenkinsESP/ESPbfr.sh ++ cd /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ ++ tar -xvf /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/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/7.8/CAPS/unit/DARWIN64/ESP/venv created virtual environment CPython3.11.5.final.0-64 in 1301ms creator CPython3Posix(dest=/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/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/7.8/CAPS/unit/DARWIN64/ESP/venv/bin/activate +++ '[' /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/venv/bin/activate = /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/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/7.8/CAPS/unit/DARWIN64/ESP/venv +++ '[' darwin20 = cygwin ']' +++ '[' darwin20 = msys ']' +++ export VIRTUAL_ENV +++ _OLD_VIRTUAL_PATH=/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/test:/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/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:/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin +++ PATH=/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/venv/bin:/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/test:/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/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:/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin +++ export PATH +++ '[' x '!=' x ']' ++++ basename /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/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/7.8/CAPS/unit/DARWIN64/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/7.8/CAPS/unit/DARWIN64/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/7.8/CAPS/unit/DARWIN64/ESP/venv/bin/python -m pip install --only-binary all --upgrade numpy Collecting numpy Using cached numpy-1.26.4-cp311-cp311-macosx_10_9_x86_64.whl.metadata (61 kB) Using cached numpy-1.26.4-cp311-cp311-macosx_10_9_x86_64.whl (20.6 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/7.8/CAPS/unit/DARWIN64/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_10_9_x86_64.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_10_9_x86_64.whl (39.3 MB) Installing collected packages: scipy Successfully installed scipy-1.13.0 ++ pip_install openmdao ++ /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/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_10_9_x86_64.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_10_9_x86_64.whl (121 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 ++ [[ macys_VM == *\v\i\g\g\e\n* ]] ++ pip_install cvxopt ++ /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/venv/bin/python -m pip install --only-binary all --upgrade cvxopt Collecting cvxopt Using cached cvxopt-1.3.2-cp311-cp311-macosx_10_9_x86_64.whl.metadata (1.3 kB) Using cached cvxopt-1.3.2-cp311-cp311-macosx_10_9_x86_64.whl (13.8 MB) Installing collected packages: cvxopt Successfully installed cvxopt-1.3.2 ++ pip_install dill ++ /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/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/7.8/CAPS/unit/DARWIN64/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/7.8/CAPS/unit/DARWIN64/ESP/venv/bin/python -m pip install --only-binary all --upgrade matplotlib Collecting matplotlib Using cached matplotlib-3.9.0-cp311-cp311-macosx_10_12_x86_64.whl.metadata (11 kB) Collecting contourpy>=1.0.1 (from matplotlib) Using cached contourpy-1.2.1-cp311-cp311-macosx_10_9_x86_64.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_x86_64.whl.metadata (159 kB) Collecting kiwisolver>=1.3.1 (from matplotlib) Using cached kiwisolver-1.4.5-cp311-cp311-macosx_10_9_x86_64.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_10_10_x86_64.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_10_12_x86_64.whl (7.9 MB) Using cached contourpy-1.2.1-cp311-cp311-macosx_10_9_x86_64.whl (262 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_x86_64.whl (2.3 MB) Using cached kiwisolver-1.4.5-cp311-cp311-macosx_10_9_x86_64.whl (68 kB) Using cached pillow-10.3.0-cp311-cp311-macosx_10_10_x86_64.whl (3.5 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/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/ ++ cd /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/EGADS/trunk/src ++ make touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include/DARWIN64 rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include/DARWIN64 cp -p ../include/DARWIN64 /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include/DARWIN64 touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include/STANALYZER.make rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include/STANALYZER.make cp -p ../include/STANALYZER.make /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include/STANALYZER.make touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include/egads.h rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include/egads.h cp -p ../include/egads.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include/egads.h touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include/egads_dot.h rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include/egads_dot.h cp -p ../include/egads_dot.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include/egads_dot.h touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include/egads.inc rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include/egads.inc cp -p ../include/egads.inc /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include/egads.inc touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include/egadsErrors.h rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include/egadsErrors.h cp -p ../include/egadsErrors.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include/egadsErrors.h touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include/egadsTypes.h rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include/egadsTypes.h cp -p ../include/egadsTypes.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include/egadsTypes.h touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include/emp.h rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include/emp.h cp -p ../include/emp.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include/emp.h touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include/prm.h rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include/prm.h cp -p ../include/prm.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include/prm.h touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include/wsserver.h rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include/wsserver.h cp -p ../include/wsserver.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include/wsserver.h touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include/wsserver.inc rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include/wsserver.inc cp -p ../include/wsserver.inc /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include/wsserver.inc touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include/wsss.h rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include/wsss.h cp -p ../include/wsss.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include/wsss.h touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include/egadsTris.h rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include/egadsTris.h cp -p egadsTris.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include/egadsTris.h touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include/egadsSplineFit.h rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include/egadsSplineFit.h cp -p egadsSplineFit.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include/egadsSplineFit.h touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include/egadsSplineVels.h rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include/egadsSplineVels.h cp -p egadsSplineVels.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include/egadsSplineVels.h touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include/egadsf90.inc rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include/egadsf90.inc cp -p ../include/egadsf90.inc /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include/egadsf90.inc mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include/Surreal cp Surreal/SurrealD.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include/Surreal/SurrealD.h mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include/Surreal cp Surreal/SurrealD_Lazy.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include/Surreal/SurrealD_Lazy.h mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include/Surreal cp Surreal/SurrealD_Trad.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include/Surreal/SurrealD_Trad.h mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include/Surreal cp Surreal/SurrealS.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include/Surreal/SurrealS.h mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include/Surreal cp Surreal/SurrealS_Lazy.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include/Surreal/SurrealS_Lazy.h mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include/Surreal cp Surreal/SurrealS_Trad.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include/Surreal/SurrealS_Trad.h mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include/Surreal cp Surreal/always_inline.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include/Surreal/always_inline.h clang++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -DREVISION=7.8 -IOCC -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0 -I../include \ -I. egadsGeom.cpp -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egadsGeom.o clang++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -DREVISION=7.8 -IOCC -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0 -I../include \ -I. egadsHLevel.cpp -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egadsHLevel.o clang++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -DREVISION=7.8 -IOCC -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0 -I../include \ -I. egadsTopo.cpp -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egadsTopo.o clang++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -DREVISION=7.8 -IOCC -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0 -I../include \ -I. egadsCopy.cpp -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egadsCopy.o clang++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -DREVISION=7.8 -IOCC -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0 -I../include \ -I. egadsSpline.cpp -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egadsSpline.o clang++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -DREVISION=7.8 -IOCC -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0 -I../include \ -I. egadsIO.cpp -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egadsIO.o clang++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -DREVISION=7.8 -IOCC -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0 -I../include \ -I. egadsSplineFit.cpp -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egadsSplineFit.o clang++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -DREVISION=7.8 -IOCC -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0 -I../include \ -I. egadsSkinning.cpp -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egadsSkinning.o clang++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -DREVISION=7.8 -IOCC -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0 -I../include \ -I. egadsTessSens.cpp -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egadsTessSens.o clang++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -DREVISION=7.8 -IOCC -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0 OCC/BRepLib_FuseEdges.cpp -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/BRepLib_FuseEdges.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I../util \ -I../util/uvmap egadsBase.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egadsBase.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I../util \ -I../util/uvmap egadsMemory.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egadsMemory.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I../util \ -I../util/uvmap egadsAttrs.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egadsAttrs.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I../util \ -I../util/uvmap egadsTess.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egadsTess.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I../util \ -I../util/uvmap egadsTessInp.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egadsTessInp.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I../util \ -I../util/uvmap egadsTris.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egadsTris.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I../util \ -I../util/uvmap egadsQuads.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egadsQuads.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I../util \ -I../util/uvmap egadsFit.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egadsFit.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I../util \ -I../util/uvmap egadsRobust.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egadsRobust.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I../util \ -I../util/uvmap egadsSBO.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egadsSBO.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I../util \ -I../util/uvmap prmCfit.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/prmCfit.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I../util \ -I../util/uvmap prmGrid.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/prmGrid.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I../util \ -I../util/uvmap prmUV.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/prmUV.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I../util \ -I../util/uvmap egadsExport.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egadsExport.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I../util \ -I../util/uvmap egadsEffect.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egadsEffect.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I../util \ -I../util/uvmap egadsSolids.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egadsSolids.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include ../util/emp.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/emp.o clang++ -g -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 -DREVISION=7.8 -IOCC -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0 -I. -I../include \ ../util/evaluate.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/evaluate.o clang++ -g -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 -DREVISION=7.8 -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0 -I. -I../include \ ../util/rational.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/rational.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0 -I../include -I../util \ ../util/regQuads.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/regQuads.o clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/SurrealD1 -O -std=c++11 -I. ../util/SurrealD1_btest.cpp /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/SurrealD1 SurrealD1_test_suite Complete! clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/SurrealD4 -O -std=c++11 -I. ../util/SurrealD4_btest.cpp /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/SurrealD4 SurrealD4_test_suite Complete! clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/SurrealS1 -O -std=c++11 -I. ../util/SurrealS1_btest.cpp /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/SurrealS1 SurrealS1_test_suite Complete! clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/SurrealS4 -O -std=c++11 -I. ../util/SurrealS4_btest.cpp /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/SurrealS4 SurrealS4_test_suite Complete! /Library/Developer/CommandLineTools/usr/bin/make -C ../util clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 uvmap/main/uvmap.c -Iuvmap \ -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/uvmap.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/EG_uvmapFindUV.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/EG_uvmapFindUV.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/EG_uvmapGen.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/EG_uvmapGen.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/EG_uvmapStructFree.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/EG_uvmapStructFree.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/EG_uvmapTest.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/EG_uvmapTest.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/EG_uvmap_Read.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/EG_uvmap_Read.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/EG_uvmap_Write.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/EG_uvmap_Write.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_add.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/uvmap_add.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_bnd_adj.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/uvmap_bnd_adj.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_chk_area_uv.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/uvmap_chk_area_uv.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_chk_edge_ratio.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/uvmap_chk_edge_ratio.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_cpu_message.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/uvmap_cpu_message.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_find_uv.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/uvmap_find_uv.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_from_egads.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/uvmap_from_egads.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_gen.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/uvmap_gen.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_gen_uv.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/uvmap_gen_uv.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_ibeibe.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/uvmap_ibeibe.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_ibfibf.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/uvmap_ibfibf.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_ibfin.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/uvmap_ibfin.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_iccibe.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/uvmap_iccibe.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_iccin.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/uvmap_iccin.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_idibe.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/uvmap_idibe.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_inibe.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/uvmap_inibe.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_inl_uv_bnd.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/uvmap_inl_uv_bnd.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_malloc.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/uvmap_malloc.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_mben_disc.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/uvmap_mben_disc.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_message.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/uvmap_message.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_norm_uv.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/uvmap_norm_uv.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_read.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/uvmap_read.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_solve.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/uvmap_solve.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_struct_tasks.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/uvmap_struct_tasks.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_test.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/uvmap_test.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_to_egads.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/uvmap_to_egads.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_version.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/uvmap_version.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_write.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/uvmap_write.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 egadsUVmap.c -Iuvmap \ -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egadsUVmap.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/libuvmap.a rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/libuvmap.a (cd /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj; ar rs /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/libuvmap.a /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/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/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/libuvmap.a clang -g -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/test/uvmap.exe /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/uvmap.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -luvmap -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/libegads.dylib rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/libegads.dylib (cd /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj; clang -g -dynamiclib -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/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/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -L/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -luvmap -lTKBool -lTKernel -lTKFeat -lTKBO -lTKGeomAlgo -lTKMath -lTKOffset -lTKPrim -lTKTopAlgo -lTKBRep -lTKG2d -lTKG3d -lTKGeomBase -lTKShHealing -lTKDESTEP -lTKDEIGES -lTKXSBase -lTKFillet -lc++ \ -install_name '@rpath/libegads.dylib' \ -compatibility_version 7.8 \ -current_version 1.0.25 ) touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/libegadstatic.a rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/libegadstatic.a cp /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/libuvmap.a /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/libegadstatic.a (cd /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj; \ ar rs /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/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 -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include fgadsBase.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/fgadsBase.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include fgadsMemory.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/fgadsMemory.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include fgadsAttrs.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/fgadsAttrs.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include fgadsTess.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/fgadsTess.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include fgadsHLevel.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/fgadsHLevel.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include fgadsGeom.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/fgadsGeom.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include fgadsTopo.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/fgadsTopo.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/libfgads.a rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/libfgads.a (cd /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj; ar rs /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/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/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/libfgads.a touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/libemp.a rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/libemp.a (cd /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj; ar rs /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/libemp.a emp.o; ) ar: creating archive /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/libemp.a *** EGADS Build Complete! *** ++ cd /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/EGADS/trunk/wvServer ++ make clang++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 map.cpp -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/map.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include base64-decode.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/base64-decode.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include handshake.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/handshake.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include client-handshake.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/client-handshake.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include libwebsockets.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/libwebsockets.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include extension-deflate-stream.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/extension-deflate-stream.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include md5.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/md5.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include extension-x-google-mux.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/extension-x-google-mux.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include parsers.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/parsers.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include extension.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/extension.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include sha-1.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/sha-1.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include server.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/server.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include wv.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/wv.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include browserMessage.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/browserMessage.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include fwv.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/fwv.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/libwsserver.a rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/libwsserver.a (cd /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj; ar rs /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/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/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/fwv.o; ) ar: creating archive /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/libwsserver.a clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -DSTANDALONE server.c \ -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I. -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/servertest.o clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/test/server /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/servertest.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/libwsserver.a \ -lpthread -lz -lm touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/libwsserver.dylib rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/libwsserver.dylib (cd /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj; clang++ -g -dynamiclib -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/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 7.8 \ -current_version 1.0.25 ) ++ cd /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/EGADS/trunk/lite ++ make clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I. -I../src -I../util/uvmap \ liteBase.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/liteBase.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I. -I../src -I../util/uvmap \ liteMemory.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/liteMemory.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I. -I../src -I../util/uvmap \ liteGeom.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/liteGeom.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I. -I../src -I../util/uvmap \ liteTopo.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/liteTopo.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I. -I../src -I../util/uvmap \ liteAttrs.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/liteAttrs.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I. -I../src -I../util/uvmap \ liteImport.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/liteImport.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I. -I../src -I../util/uvmap \ liteString.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/liteString.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -DLITE -I../include -I. -I../src \ ../src/egadsTess.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/liteTess.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -DLITE -I../include -I. -I../src \ ../src/egadsTris.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/liteTris.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I. -I../src \ ../src/egadsQuads.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/liteQuads.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -DLITE -I../include -I. -I../src \ -I../util ../src/egadsTessInp.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/liteTessInp.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -DLITE -I../include -I. -I../src \ ../util/evaluate.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/evaLite.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -DLITE ../util/rational.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/ratLite.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -DLITE -I../include -I../util \ ../util/regQuads.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/liteRegQuads.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -DLITE -I../include -I. -I../src \ ../src/egadsEffect.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/liteEffect.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -DLITE -I../include -I. -I../src \ -I../util/uvmap liteUVmap.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/liteUVmap.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/libegadslite.dylib rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/libegadslite.dylib (cd /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj; clang -g -dynamiclib -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/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/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/libegadslitestatic.a rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/libegadslitestatic.a (cd /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj; ar rs /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/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/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/libegadslitestatic.a ++ cd /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/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 -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include BSplineIGES.c -o \ /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/BSplineIGES.o clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/test/BSplineIGES /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/BSplineIGES.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -legads \ -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f CSys.make clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include CSys.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/CSys.o clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/test/CSys /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/CSys.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f GBO.make clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include GBO.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/GBO.o clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/test/GBO /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/GBO.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f SBO.make clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include SBO.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/SBO.o clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/test/SBO /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/SBO.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f addKnots.make clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include addKnots.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/addKnots.o clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/test/addKnots /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/addKnots.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -legads \ -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f agglom.make clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include agglom.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/agglom.o clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/test/agglom /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/agglom.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./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/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include approx.f -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/approx.o gfortran -g -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/test/approx /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/approx.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -lfgads \ -legads -Wl,-rpath,/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -Wl,-rpath,@loader_path/ -Wl,-rpath,/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lc++ -Wl,-w ++ for file in '`ls *.make`' ++ make -f blend.make clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include blend.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/blend.o clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/test/blend /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/blend.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f chamfer.make clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include chamfer.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/chamfer.o clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/test/chamfer /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/chamfer.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -legads \ -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f closure.make gfortran -g -c -O -frecursive -fcray-pointer -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include closure.f -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/closure.o gfortran -g -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/test/closure /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/closure.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -lfgads \ -legads -Wl,-rpath,/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -Wl,-rpath,@loader_path/ -Wl,-rpath,/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lc++ -Wl,-w ++ for file in '`ls *.make`' ++ make -f edge2WB.make clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include edge2WB.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/edge2WB.o clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/test/edge2WB /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/edge2WB.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -legads \ -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f edges.make clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include edges.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/edges.o clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/test/edges /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/edges.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f effective.make clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include effective.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/effective.o clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/test/effective /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/effective.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -legads \ -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f egads2cart.make clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include egads2cart.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egads2cart.o clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/test/egads2cart /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egads2cart.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -legads \ -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f egads2ply.make clang++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I. egads2ply.cpp -std=c++11 \ -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egads2ply.o clang++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -DREVISION=7.8 -I. tinyply.cpp -std=c++11 -w \ -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/tinyply.o clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/test/egads2ply /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egads2ply.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/tinyply.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f egadsGeom_dot.make clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include egadsGeom_dot.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egadsGeom_dot.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include egadsTools_dot.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egadsTools_dot.o clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/test/egadsGeom_dot /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egadsGeom_dot.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egadsTools_dot.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -legads \ -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f egadsHLevel_dot.make clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include egadsHLevel_dot.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egadsHLevel_dot.o clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/test/egadsHLevel_dot /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egadsHLevel_dot.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egadsTools_dot.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -legads \ -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f egadsSpline_dot.make clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include egadsSpline_dot.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egadsSpline_dot.o clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/test/egadsSpline_dot /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egadsSpline_dot.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egadsTools_dot.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -legads \ -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f egadsTopo_dot.make clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include egadsTopo_dot.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egadsTopo_dot.o clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/test/egadsTopo_dot /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egadsTopo_dot.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egadsTools_dot.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -legads \ -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f exportLite.make clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I../util/uvmap \ ../src/egadsExport.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/exportLite.o -DSTANDALONE clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/test/exportLite /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/exportLite.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f extrot.make clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include extrot.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/extrot.o clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/test/extrot /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/extrot.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f fillet.make clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include fillet.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/fillet.o clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/test/fillet /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/fillet.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f fit.make clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include fit.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/fit.o clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/test/fit /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/fit.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f fitTri.make clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include fitTri.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/fitTri.o clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/test/fitTri /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/fitTri.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f fullAttr.make clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include fullAttr.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/fullAttr.o clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/test/fullAttr /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/fullAttr.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -legads \ -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f fuseSheets.make clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include fuseSheets.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/fuseSheets.o clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/test/fuseSheets /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/fuseSheets.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f globalTess.make clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include globalTess.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/globalTess.o clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/test/globalTess /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/globalTess.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -legads \ -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f hollow.make clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include hollow.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/hollow.o clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/test/hollow /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/hollow.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f hollowFace.make clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include hollowFace.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/hollowFace.o clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/test/hollowFace /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/hollowFace.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f intersect.make clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include intersect.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/intersect.o clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/test/intersect /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/intersect.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -legads \ -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f makeCone.make clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include makeCone.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/makeCone.o clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/test/makeCone /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/makeCone.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -legads \ -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f makeFace3D.make clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include makeFace3D.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/makeFace3D.o clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/test/makeFace3D /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/makeFace3D.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -legads \ -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f makeLoop.make clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include makeLoop.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/makeLoop.o clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/test/makeLoop /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/makeLoop.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -legads \ -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f mapTess.make clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include mapTess.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/mapTess.o clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/test/mapTess /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/mapTess.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -legads \ -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f mofb.make clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include mofb.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/mofb.o clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/test/mofb /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/mofb.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f mssb.make clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include mssb.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/mssb.o clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/test/mssb /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/mssb.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f multiContext.make clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include multiContext.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/multiContext.o clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/test/multiContext /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/multiContext.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib \ -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f offset.make clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include offset.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/offset.o clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/test/offset /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/offset.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f rebuild.make clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include rebuild.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/rebuild.o clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/test/rebuild /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/rebuild.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -legads \ -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f refObj.make clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include refObj.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/refObj.o clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/test/refObj /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/refObj.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f replace.make clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include replace.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/replace.o clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/test/replace /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/replace.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -legads \ -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f revolve.make clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include revolve.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/revolve.o clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/test/revolve /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/revolve.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -legads \ -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f ruled.make clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include ruled.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/ruled.o clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/test/ruled /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/ruled.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f saveTess.make clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include saveTess.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/saveTess.o clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/test/saveTess /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/saveTess.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -legads \ -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f scribe.make clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include scribe.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/scribe.o clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/test/scribe /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/scribe.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f sew.make clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include sew.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/sew.o clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/test/sew /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/sew.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f simplePer.make clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include simplePer.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/simplePer.o clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/test/simplePer /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/simplePer.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -legads \ -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f smallEdges.make clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include smallEdges.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/smallEdges.o clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/test/smallEdges /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/smallEdges.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f step.make gfortran -g -c -O -frecursive -fcray-pointer -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include step.f -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/step.o gfortran -g -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/test/step /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/step.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -lfgads -legads \ -Wl,-rpath,/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -Wl,-rpath,@loader_path/ -Wl,-rpath,/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lc++ -Wl,-w ++ for file in '`ls *.make`' ++ make -f sweep.make clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include sweep.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/sweep.o clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/test/sweep /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/sweep.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f test.make clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include testc.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/testc.o clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/test/testc /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/testc.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm gfortran -g -c -O -frecursive -fcray-pointer -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include testf.f -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/testf.o gfortran -g -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/test/testf /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/testf.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -lfgads -legads \ -Wl,-rpath,/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -Wl,-rpath,@loader_path/ -Wl,-rpath,/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lc++ -Wl,-w clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include parsec.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/parsec.o clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/test/parsec /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/parsec.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm gfortran -g -c -O -frecursive -fcray-pointer -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include parsef.f -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/parsef.o gfortran -g -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/test/parsef /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/parsef.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -lfgads -legads \ -Wl,-rpath,/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -Wl,-rpath,@loader_path/ -Wl,-rpath,/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lc++ -Wl,-w ++ for file in '`ls *.make`' ++ make -f tolerance.make clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include tolerance.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/tolerance.o clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/test/tolerance /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/tolerance.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -legads \ -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f union.make gfortran -g -c -O -frecursive -fcray-pointer -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include union.f -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/union.o gfortran -g -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/test/union /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/union.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -lfgads -legads \ -Wl,-rpath,/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -Wl,-rpath,@loader_path/ -Wl,-rpath,/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lc++ -Wl,-w ++ for file in '`ls *.make`' ++ make -f vAttr.make clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include vAttr.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/vAttr.o clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/test/vAttr /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/vAttr.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -lwsserver -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib ++ for file in '`ls *.make`' ++ make -f vCurvature.make clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include vCurvature.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/vCurvature.o clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/test/vCurvature /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/vCurvature.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -lwsserver -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib ++ for file in '`ls *.make`' ++ make -f vEffect.make clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include vEffect.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/vEffect.o clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/test/vEffect /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/vEffect.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -lwsserver -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib ++ for file in '`ls *.make`' ++ make -f vEto.make clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include vEto.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/vEto.o clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/test/vEto /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/vEto.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -lwsserver -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib ++ for file in '`ls *.make`' ++ make -f vFrame.make clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include vFrame.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/vFrame.o clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/test/vFrame /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/vFrame.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -lwsserver -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib ++ for file in '`ls *.make`' ++ make -f vGeom.make clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include vGeom.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/vGeom.o clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/test/vGeom /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/vGeom.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -lwsserver -legads \ -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib ++ for file in '`ls *.make`' ++ make -f vQuad.make clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include vQuad.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/vQuad.o clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/test/vQuad /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/vQuad.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -lwsserver \ -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib ++ for file in '`ls *.make`' ++ make -f vTess.make clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include vTess.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/vTess.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include ../util/retessFaces.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/retessFaces.o clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/test/vTesstatic /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/vTess.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/retessFaces.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -lwsserver -legadstatic -L/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -lTKBool -lTKernel -lTKFeat -lTKBO -lTKGeomAlgo -lTKMath -lTKOffset -lTKPrim -lTKTopAlgo -lTKBRep -lTKG2d -lTKG3d -lTKGeomBase -lTKShHealing -lTKDESTEP -lTKDEIGES -lTKXSBase -lTKFillet \ -lpthread -lz -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/test/vTess /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/vTess.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/retessFaces.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -lwsserver -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib ++ for file in '`ls *.make`' ++ make -f vTessInp.make clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include vTessInp.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/vTessInp.o clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/test/vTessInp /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/vTessInp.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -lwsserver -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib ++ for file in '`ls *.make`' ++ make -f xform.make clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include xform.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/xform.o clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/test/xform /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/xform.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm ++ cd /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/EGADS/trunk/docs/Tutorial ++ make -f tire.make clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include tire.c clang++ -g -o tire tire.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm ++ make -f egads2tri.make clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include egads2tri.c clang++ -g -o egads2tri egads2tri.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm ++ cd /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/EGADS/trunk/docs/EGADS_dot/src ++ make clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I. circle1_dot.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/circle1_dot.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I. pingBodies.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/pingBodies.o clang -g -o circle1_dot /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/circle1_dot.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/pingBodies.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -legads -lm -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I. circle2_dot.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/circle2_dot.o clang -g -o circle2_dot /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/circle2_dot.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/pingBodies.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -legads -lm -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I. naca_dot.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/naca_dot.o clang -g -o naca_dot /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/naca_dot.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/pingBodies.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -legads -lm -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I. ruled_naca_dot.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/ruled_naca_dot.o clang -g -o ruled_naca_dot /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/ruled_naca_dot.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/pingBodies.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -legads -lm -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib ++ cd /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/OpenCSM/trunk/src ++ make clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I. serveCSM.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/serveCSM.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I. OpenCSM.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/OpenCSM.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I. udp.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/udp.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I. tim.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/tim.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/libocsm.dylib rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/libocsm.dylib clang -g -dynamiclib -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/libocsm.dylib /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/OpenCSM.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/udp.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/tim.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -legads -lwsserver -ldl -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -install_name '@rpath/libocsm.dylib' -compatibility_version 1.0.25 -current_version 1.0.25 clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/bin/serveCSM /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/serveCSM.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -locsm -lwsserver -legads -ldl -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I. serveESP.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/serveESP.o clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/bin/serveESP /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/serveESP.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -locsm -lwsserver -legads -ldl -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I. sensCSM.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/sensCSM.o clang -g -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/bin/sensCSM /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/sensCSM.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -locsm -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I. udpBezier.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/udpBezier.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/bezier.so rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/bezier.so clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/bezier.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/udpBezier.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I. udpBiconvex.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/udpBiconvex.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/biconvex.so rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/biconvex.so clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/biconvex.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/udpBiconvex.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I. udpBox.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/udpBox.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/box.so rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/box.so clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/box.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/udpBox.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I. udpBspline.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/udpBspline.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/bspline.so rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/bspline.so clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/bspline.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/udpBspline.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I. udfCatmull.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/udfCatmull.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/catmull.so rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/catmull.so clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/catmull.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/udfCatmull.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I. udfCompare.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/udfCompare.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/compare.so rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/compare.so clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/compare.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/udfCompare.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I. udfCreateBEM.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/udfCreateBEM.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/createBEM.so rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/createBEM.so clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/createBEM.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/udfCreateBEM.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I. udfCreatePoly.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/udfCreatePoly.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/createPoly.so rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/createPoly.so clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/createPoly.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/udfCreatePoly.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I. udpCsm.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/udpCsm.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/csm.so rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/csm.so clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/csm.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/udpCsm.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I. udfDeform.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/udfDeform.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/deform.so rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/deform.so clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/deform.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/udfDeform.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I. udfDroop.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/udfDroop.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/droop.so rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/droop.so clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/droop.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/udfDroop.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I. udfDumpPmtrs.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/udfDumpPmtrs.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/dumpPmtrs.so rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/dumpPmtrs.so clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/dumpPmtrs.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/udfDumpPmtrs.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I. udfEditAttr.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/udfEditAttr.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/editAttr.so rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/editAttr.so clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/editAttr.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/udfEditAttr.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I. udpEllipse.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/udpEllipse.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/ellipse.so rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/ellipse.so clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/ellipse.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/udpEllipse.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I. udpEqn2body.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/udpEqn2body.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/eqn2body.so rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/eqn2body.so clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/eqn2body.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/udpEqn2body.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I. udpFitcurve.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/udpFitcurve.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/fitcurve.so rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/fitcurve.so clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/fitcurve.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/udpFitcurve.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I. udfFlend.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/udfFlend.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/flend.so rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/flend.so clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/flend.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/udfFlend.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I. udpFreeform.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/udpFreeform.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/freeform.so rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/freeform.so clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/freeform.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/udpFreeform.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I. udfGanged.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/udfGanged.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/ganged.so rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/ganged.so clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/ganged.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/udfGanged.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I. udfGuide.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/udfGuide.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/guide.so rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/guide.so clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/guide.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/udfGuide.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I. udpHex.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/udpHex.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/hex.so rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/hex.so clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/hex.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/udpHex.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I. udpImport.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/udpImport.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/import.so rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/import.so clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/import.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/udpImport.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I. udpKulfan.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/udpKulfan.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/kulfan.so rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/kulfan.so clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/kulfan.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/udpKulfan.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I. udfLinalg.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/udfLinalg.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/linalg.so rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/linalg.so clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/linalg.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/udfLinalg.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I. udfMatchBodys.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/udfMatchBodys.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/matchBodys.so rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/matchBodys.so clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/matchBodys.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/udfMatchBodys.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I. udfMechanism.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/udfMechanism.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/mechanism.so rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/mechanism.so clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/mechanism.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/udfMechanism.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I. udpNaca.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/udpNaca.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/naca.so rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/naca.so clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/naca.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/udpNaca.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I. udfNaca6mc.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/udfNaca6mc.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/naca6mc.so rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/naca6mc.so clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/naca6mc.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/udfNaca6mc.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I. udfNacelle.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/udfNacelle.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/nacelle.so rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/nacelle.so clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/nacelle.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/udfNacelle.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I. udpNurbbody.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/udpNurbbody.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/nurbbody.so rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/nurbbody.so clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/nurbbody.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/udpNurbbody.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I. udfNuscale.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/udfNuscale.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/nuscale.so rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/nuscale.so clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/nuscale.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/udfNuscale.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I. udfOffset.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/udfOffset.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/offset.so rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/offset.so clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/offset.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/udfOffset.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I. udpParabaloid.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/udpParabaloid.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/parabaloid.so rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/parabaloid.so clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/parabaloid.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/udpParabaloid.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm clang++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I. udpParsec.cpp -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/udpParsec.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/parsec.so rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/parsec.so clang++ -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/parsec.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/udpParsec.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I. udpPod.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/udpPod.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/pod.so rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/pod.so clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/pod.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/udpPod.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I. udpPoly.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/udpPoly.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/poly.so rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/poly.so clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/poly.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/udpPoly.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I. udfPrintBbox.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/udfPrintBbox.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/printBbox.so rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/printBbox.so clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/printBbox.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/udfPrintBbox.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I. udfPrintBrep.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/udfPrintBrep.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/printBrep.so rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/printBrep.so clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/printBrep.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/udfPrintBrep.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I. udfPrintEgo.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/udfPrintEgo.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/printEgo.so rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/printEgo.so clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/printEgo.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/udfPrintEgo.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I. udpProp.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/udpProp.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/prop.so rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/prop.so clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/prop.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/udpProp.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I. udpRadwaf.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/udpRadwaf.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/radwaf.so rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/radwaf.so clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/radwaf.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/udpRadwaf.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I. udpSample.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/udpSample.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/sample.so rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/sample.so clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/sample.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/udpSample.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I. udpSew.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/udpSew.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/sew.so rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/sew.so clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/sew.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/udpSew.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I. udfShadow.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/udfShadow.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/shadow.so rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/shadow.so clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/shadow.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/udfShadow.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I. udfSlices.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/udfSlices.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/slices.so rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/slices.so clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/slices.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/udfSlices.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I. udpStag.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/udpStag.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/stag.so rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/stag.so clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/stag.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/udpStag.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I. udfStiffener.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/udfStiffener.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/stiffener.so rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/stiffener.so clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/stiffener.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/udfStiffener.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I. udpSupell.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/udpSupell.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/supell.so rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/supell.so clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/supell.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/udpSupell.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I. udfTester1.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/udfTester1.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/tester1.so rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/tester1.so clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/tester1.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/udfTester1.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I. udpTester2.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/udpTester2.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/tester2.so rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/tester2.so clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/tester2.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/udpTester2.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I. udpVsp3.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/udpVsp3.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/vsp3.so rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/vsp3.so clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/vsp3.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/udpVsp3.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I. udpWaffle.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/udpWaffle.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/waffle.so rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/waffle.so clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/waffle.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/udpWaffle.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I. udpWarp.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/udpWarp.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/warp.so rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/warp.so clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/warp.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/udpWarp.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I. eggPDT2.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/eggPDT2.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/PDT2.so rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/PDT2.so clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/PDT2.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/eggPDT2.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I. udpNaca456.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/udpNaca456.o gfortran -g -c -O -frecursive -fcray-pointer naca456.f90 -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/naca456.o -J /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/naca456.so rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/naca456.so gfortran -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/naca456.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/udpNaca456.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/naca456.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm -Wl,-w clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I. timEreped.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/timEreped.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/ereped.so rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/ereped.so clang++ -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/ereped.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/timEreped.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -locsm -lwsserver -legads -ldl -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I. timMitten.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/timMitten.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/mitten.so rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/mitten.so clang++ -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/mitten.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/timMitten.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -locsm -lwsserver -legads -ldl -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I. timPlotter.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/timPlotter.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/plotter.so rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/plotter.so clang++ -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/plotter.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/timPlotter.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -locsm -lwsserver -legads -ldl -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I. timPlugs.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/timPlugs.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/plugs.so rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/plugs.so clang++ -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/plugs.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/timPlugs.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -locsm -lwsserver -legads -ldl -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I. timSlugs.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/timSlugs.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/slugs.so rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/slugs.so clang++ -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/slugs.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/timSlugs.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -locsm -lwsserver -legads -ldl -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I. timVspSetup.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/timVspSetup.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/vspSetup.so rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/vspSetup.so clang++ -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/vspSetup.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/timVspSetup.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -locsm -lwsserver -legads -ldl -lm touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include/OpenCSM.h rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include/OpenCSM.h cp -p OpenCSM.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include/OpenCSM.h touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include/common.h rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include/common.h cp -p common.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include/common.h touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include/udp.h rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include/udp.h cp -p udp.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include/udp.h touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include/esp.h rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include/esp.h cp -p esp.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include/esp.h touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include/tim.h rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include/tim.h cp -p tim.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include/tim.h touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include/egg.h rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include/egg.h cp -p egg.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include/egg.h touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include/udpUtilities.h rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include/udpUtilities.h cp -p udpUtilities.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include/udpUtilities.h touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include/udpUtilities.c rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include/udpUtilities.c cp -p udpUtilities.c /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include/udpUtilities.c ++ cd /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/EGADS/trunk/docs/UDP_UDF/data ++ make clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include udpTire.c -o tire.o clang -g -o tire tire.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -legads -lm -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -DUDP -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include udpTire.c touch tire.so rm tire.so clang -g -bundle -o tire.so udpTire.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -legads -lm -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib ++ [[ '' == '' ]] ++ cd /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/CAPS ++ make (cd src; make) touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include/caps.h rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include/caps.h cp -p ../include/caps.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include/caps.h touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include/capsErrors.h rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include/capsErrors.h cp -p ../include/capsErrors.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include/capsErrors.h touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include/capsTypes.h rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include/capsTypes.h cp -p ../include/capsTypes.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include/capsTypes.h touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include/aimUtil.h rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include/aimUtil.h cp -p ../include/aimUtil.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include/aimUtil.h touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include/aimMesh.h rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include/aimMesh.h cp -p ../include/aimMesh.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include/aimMesh.h clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I../include \ -I/usr/include/udunits2 aimUtil.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/aimUtil.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include \ -I/usr/include/udunits2 aimTransferUtil.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/aimTransferUtil.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I../include \ aimMesh.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/aimMesh.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/libaimUtil.a rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/libaimUtil.a ar -rs /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/libaimUtil.a /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/aimUtil.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/aimMesh.o \ /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/aimTransferUtil.o ar: creating archive /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/libaimUtil.a clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I. \ -I/usr/include/udunits2 capsBase.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/capsBase.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I. \ -I/usr/include/udunits2 capsAnalysis.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/capsAnalysis.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I. \ -I/usr/include/udunits2 capsApprox.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/capsApprox.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I. \ -I/usr/include/udunits2 capsAttr.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/capsAttr.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I. \ -I/usr/include/udunits2 capsAIM.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/capsAIM.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I. \ -I/usr/include/udunits2 capsBound.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/capsBound.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I. \ -I/usr/include/udunits2 capsProblem.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/capsProblem.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I. \ -I/usr/include/udunits2 capsValue.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/capsValue.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I. \ -I/usr/include/udunits2 capsUnits.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/capsUnits.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I. \ -I/usr/include/udunits2 conjGrad.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/conjGrad.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I. \ -I/usr/include/udunits2 capsFunIDs.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/capsFunIDs.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I. \ -I/usr/include/udunits2 capsChkInpt.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/capsChkInpt.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I. \ -I/usr/include/udunits2 printObject.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/printObject.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/libcaps.dylib rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/libcaps.dylib (cd /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj; clang -g -dynamiclib -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/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/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/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/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/libcapsstatic.a rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/libcapsstatic.a (cd /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj; ar -rs /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/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/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/libcapsstatic.a clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include testingAIM.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/testingAIM.o rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/testingAIM.so rm: /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/testingAIM.so: No such file or directory make[1]: [/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/testingAIM.so] Error 1 (ignored) clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/testingAIM.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/testingAIM.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -laimUtil -legads -locsm -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include testingWriter.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/testingWriter.o rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/testingWriter.so rm: /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/testingWriter.so: No such file or directory make[1]: [/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/testingWriter.so] Error 1 (ignored) clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/testingWriter.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/testingWriter.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -laimUtil -ldl -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include phaseUtil.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/phaseUtil.o clang -g -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/bin/phaseUtil /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/phaseUtil.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -lcaps -ludunits2 -locsm -legads -ldl -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm (cd aim; make) /Library/Developer/CommandLineTools/usr/bin/make -C utils clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I. -DHAVE_PYTHON -I. -I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11 -I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11 -Icython attrUtils.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/attrUtils.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I. -DHAVE_PYTHON -I. -I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11 -I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11 -Icython meshUtils.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/meshUtils.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I. -DHAVE_PYTHON -I. -I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11 -I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11 -Icython cfdUtils.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/cfdUtils.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I. -DHAVE_PYTHON -I. -I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11 -I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11 -Icython miscUtils.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/miscUtils.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I. -DHAVE_PYTHON -I. -I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11 -I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11 -Icython feaUtils.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/feaUtils.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I. -DHAVE_PYTHON -I. -I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11 -I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11 -Icython vlmUtils.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/vlmUtils.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I. -DHAVE_PYTHON -I. -I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11 -I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11 -Icython nastranUtils.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/nastranUtils.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I. -DHAVE_PYTHON -I. -I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11 -I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11 -Icython tecplotUtils.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/tecplotUtils.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I. -DHAVE_PYTHON -I. -I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11 -I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11 -Icython arrayUtils.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/arrayUtils.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I. -DHAVE_PYTHON -I. -I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11 -I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11 -Icython deprecateUtils.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/deprecateUtils.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I. -DHAVE_PYTHON -I. -I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11 -I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11 -Icython cardUtils.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/cardUtils.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I. -DHAVE_PYTHON -I. -I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11 -I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11 -Icython nastranCards.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/nastranCards.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I. -DHAVE_PYTHON -I. -I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11 -I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11 -Icython jsonUtils.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/jsonUtils.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I. -DHAVE_PYTHON -I. -I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11 -I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11 -Icython cython/nastranOP2Reader.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/nastranOP2Reader.o clang++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I. vlmSpanSpace.cpp -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/vlmSpanSpace.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/libutils.a rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/libutils.a (cd /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj; ar -rs /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/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/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/libutils.a /Library/Developer/CommandLineTools/usr/bin/ranlib: file: /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/libutils.a(attrUtils.o) has no symbols mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include/aim/utils cp -p -f arrayUtils.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include/aim/utils/arrayUtils.h cp -p -f attrTypes.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include/aim/utils/attrTypes.h cp -p -f attrUtils.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include/aim/utils/attrUtils.h cp -p -f cardTypes.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include/aim/utils/cardTypes.h cp -p -f cardUtils.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include/aim/utils/cardUtils.h cp -p -f cfdTypes.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include/aim/utils/cfdTypes.h cp -p -f cfdUtils.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include/aim/utils/cfdUtils.h cp -p -f deprecateUtils.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include/aim/utils/deprecateUtils.h cp -p -f feaTypes.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include/aim/utils/feaTypes.h cp -p -f feaUtils.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include/aim/utils/feaUtils.h cp -p -f jsonUtils.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include/aim/utils/jsonUtils.h cp -p -f meshTypes.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include/aim/utils/meshTypes.h cp -p -f meshUtils.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include/aim/utils/meshUtils.h cp -p -f miscTypes.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include/aim/utils/miscTypes.h cp -p -f miscUtils.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include/aim/utils/miscUtils.h cp -p -f nastranCards.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include/aim/utils/nastranCards.h cp -p -f nastranUtils.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include/aim/utils/nastranUtils.h cp -p -f tecplotUtils.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include/aim/utils/tecplotUtils.h cp -p -f vlmSpanSpace.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include/aim/utils/vlmSpanSpace.h cp -p -f vlmTypes.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include/aim/utils/vlmTypes.h cp -p -f vlmUtils.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include/aim/utils/vlmUtils.h /Library/Developer/CommandLineTools/usr/bin/make -C abaqus clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I../utils \ abaqusAIM.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/abaqusAIM.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -DHAVE_PYTHON -I. -I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11 -I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11 -Icython -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I../utils \ abaqusUtils.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/abaqusUtils.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I../utils \ -I. -I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11 -I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11 cython/abaqusFILReader.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/abaqusFILReader.o echo "Building Abaqus with Python" Building Abaqus with Python clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/abaqusAIM.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/abaqusAIM.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/abaqusUtils.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/abaqusFILReader.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -lutils -laimUtil -locsm -legads -ludunits2 -L/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/lib/python3.11/config-3.11-darwin -lpython3.11 -ldl -framework CoreFoundation -lm -ldl -Wl,-rpath /usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/lib/python3.11/config-3.11-darwin /Library/Developer/CommandLineTools/usr/bin/make -C aflr2 clang -g -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/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-x86-64/lib -laflr2c -lm \ -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/aflr2_version /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/aflr2_version clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.14/src \ -I../utils aflr2AIM.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/aflr2AIM.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.14/src \ -I../utils aflr2_Interface.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/aflr2_Interface.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/aflr2AIM.so rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/aflr2AIM.so clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/aflr2AIM.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/aflr2AIM.o \ /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/aflr2_Interface.o -L/Users/jenkins/util/AFLR/aflr_lib_11.5.14/MacOSX-x86-64/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/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -lutils \ -laimUtil -locsm -legads -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lc++ -lm /Library/Developer/CommandLineTools/usr/bin/make -C aflr3 clang -g -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/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-x86-64/lib -laflr3 \ -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/aflr3_version /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/aflr3_version 16.32.50 clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I../utils -I/Users/jenkins/util/AFLR/aflr_lib_11.5.14/src \ aflr3AIM.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/aflr3AIM.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I../utils -I/Users/jenkins/util/AFLR/aflr_lib_11.5.14/src \ aflr3_Interface.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/aflr3_Interface.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/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/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/EG_getEffBodyTopos.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/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/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egads_aflr4_check_tess_coord.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/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/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egads_aflr4_check_tess_ordering.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/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/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egads_aflr4_get_bedge_coord.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/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/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egads_aflr4_get_edge_spacing.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/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/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egads_aflr4_get_faceOrder.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/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/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egads_aflr4_get_face_spacing.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/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/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egads_aflr4_get_surf_grid.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/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/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egads_aflr4_create_tess.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/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/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egads_aflr4_tess_to_dgeom.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/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/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egads_aflr4_version.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/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/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egads_auto_cad_geom_setup.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/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/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_add_attr.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/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/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_add_ff.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/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/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_add_ret_attr.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/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/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_bodyFlag.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/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/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_check_bc.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/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/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_data_cleanup.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/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/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_edgeData.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/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/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_edgeFace.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/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/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_edit.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/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/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_faceEdge.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/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/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_faceFace.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/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/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_faceFlag.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/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/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_faceLoop.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/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/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_file_read.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/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/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_file_write.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/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/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_idef2idef.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/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/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_loopEdge.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/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/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_nodeData.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/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/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_reset_attr.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/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/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_setup.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/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/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_write_topo_data.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/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/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egads_eval_curv_at_uv.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/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/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egads_eval_edge_arclen.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/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/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egads_eval_norm_at_uv.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/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/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egads_eval_uv_at_t.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/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/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egads_eval_uv_at_xyz.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/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/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egads_eval_uv_bounds.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/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/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egads_eval_xyz_at_u.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/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/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egads_eval_xyz_at_uv.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/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/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egads_face_node_map.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/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/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_faceMatch.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/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/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egads_data.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/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/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egads_mzone.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/aflr3AIM.so rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/aflr3AIM.so clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/aflr3AIM.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/aflr3AIM.o \ /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/aflr3_Interface.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/EG_getEffBodyTopos.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egads_aflr4_check_tess_coord.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egads_aflr4_check_tess_ordering.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egads_aflr4_get_bedge_coord.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egads_aflr4_get_edge_spacing.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egads_aflr4_get_faceOrder.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egads_aflr4_get_face_spacing.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egads_aflr4_get_surf_grid.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egads_aflr4_create_tess.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egads_aflr4_tess_to_dgeom.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egads_aflr4_version.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egads_auto_cad_geom_setup.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_add_attr.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_add_ff.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_add_ret_attr.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_bodyFlag.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_check_bc.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_data_cleanup.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_edgeData.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_edgeFace.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_edit.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_faceEdge.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_faceFace.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_faceFlag.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_faceLoop.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_file_read.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_file_write.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_idef2idef.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_loopEdge.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_nodeData.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_reset_attr.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_setup.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_write_topo_data.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egads_eval_curv_at_uv.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egads_eval_edge_arclen.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egads_eval_norm_at_uv.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egads_eval_uv_at_t.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egads_eval_uv_at_xyz.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egads_eval_uv_bounds.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egads_eval_xyz_at_u.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egads_eval_xyz_at_uv.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egads_face_node_map.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_faceMatch.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egads_data.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egads_mzone.o -L/Users/jenkins/util/AFLR/aflr_lib_11.5.14/MacOSX-x86-64/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/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -lutils \ -laimUtil -locsm -legads -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lc++ -lm /Library/Developer/CommandLineTools/usr/bin/make -C aflr4 clang -g -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/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-x86-64/lib -laflr4 -lm \ -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/aflr4_version /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/aflr4_version clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.14/src -I../utils aflr4AIM.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/aflr4AIM.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.14/src \ -I../utils aflr4_Interface.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/aflr4_Interface.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/aflr4AIM.so rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/aflr4AIM.so clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/aflr4AIM.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/aflr4AIM.o \ /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/aflr4_Interface.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/EG_getEffBodyTopos.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egads_aflr4_check_tess_coord.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egads_aflr4_check_tess_ordering.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egads_aflr4_get_bedge_coord.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egads_aflr4_get_edge_spacing.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egads_aflr4_get_faceOrder.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egads_aflr4_get_face_spacing.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egads_aflr4_get_surf_grid.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egads_aflr4_create_tess.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egads_aflr4_tess_to_dgeom.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egads_aflr4_version.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egads_auto_cad_geom_setup.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_add_attr.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_add_ff.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_add_ret_attr.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_bodyFlag.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_check_bc.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_data_cleanup.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_edgeData.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_edgeFace.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_edit.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_faceEdge.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_faceFace.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_faceFlag.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_faceLoop.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_file_read.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_file_write.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_idef2idef.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_loopEdge.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_nodeData.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_reset_attr.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_setup.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_write_topo_data.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egads_eval_curv_at_uv.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egads_eval_edge_arclen.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egads_eval_norm_at_uv.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egads_eval_uv_at_t.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egads_eval_uv_at_xyz.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egads_eval_uv_bounds.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egads_eval_xyz_at_u.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egads_eval_xyz_at_uv.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egads_face_node_map.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_faceMatch.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egads_data.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egads_mzone.o -L/Users/jenkins/util/AFLR/aflr_lib_11.5.14/MacOSX-x86-64/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/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -lutils \ -laimUtil -locsm -legads -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lc++ -lm /Library/Developer/CommandLineTools/usr/bin/make -C astros clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I../utils astrosAIM.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/astrosAIM.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I../utils astrosUtils.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/astrosUtils.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I../utils astrosCards.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/astrosCards.o clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/astrosAIM.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/astrosAIM.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/astrosUtils.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/astrosCards.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm -L/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/lib/python3.11/config-3.11-darwin -lpython3.11 -ldl -framework CoreFoundation /Library/Developer/CommandLineTools/usr/bin/make -C avl clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I../utils avlAIM.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/avlAIM.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_BODY.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/avlRead_BODY.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_CNC.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/avlRead_CNC.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_CPOML.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/avlRead_CPOML.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_DERMATB.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/avlRead_DERMATB.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_DERMATM.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/avlRead_DERMATM.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_DERMATS.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/avlRead_DERMATS.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_ELE.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/avlRead_ELE.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_HINGE.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/avlRead_HINGE.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_STRP.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/avlRead_STRP.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_SURF.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/avlRead_SURF.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_TOT.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/avlRead_TOT.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_VM.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/avlRead_VM.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/avlAIM.so rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/avlAIM.so clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/avlAIM.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/avlAIM.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/avlRead_BODY.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/avlRead_CNC.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/avlRead_CPOML.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/avlRead_DERMATB.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/avlRead_DERMATM.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/avlRead_DERMATS.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/avlRead_ELE.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/avlRead_HINGE.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/avlRead_STRP.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/avlRead_SURF.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/avlRead_TOT.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/avlRead_VM.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -laimUtil -lutils -locsm -legads -ludunits2 -ldl \ -lc++ -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm /Library/Developer/CommandLineTools/usr/bin/make -C awave clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I../utils awaveAIM.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/awaveAIM.o clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/awaveAIM.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/awaveAIM.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/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/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/awave.o gfortran -g -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/test/awave /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/awave.o -Wl,-w /Library/Developer/CommandLineTools/usr/bin/make -C cart3d clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -DCAPS_MESHUTILS -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I../utils -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include/libCart3D -I./xddm \ cart3dAIM.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/cart3dAIM.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include/c3dio \ -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include/libCart3D -I./xddm \ writeTrix.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/writeTrix.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include/c3dio \ -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include/libCart3D \ surfTrix.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/surfTrix.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -pedantic -I./xddm -I. \ `xml2-config --cflags` ./xddm/xddm.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/xddm.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include bodyTess.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/bodyTess.o clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/cart3dAIM.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/cart3dAIM.o \ /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/writeTrix.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/surfTrix.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/xddm.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/bodyTess.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -lutils \ -laimUtil -locsm -legads -ludunits2 -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include/ \ -lc3dio -lCart3D -ldl -lxml2 -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include cart3dTest.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/cart3dTest.o clang -g -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/test/cart3dTest /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/cart3dTest.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -lcaps -locsm -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm -ldl clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I./xddm \ -I. `xml2-config --cflags` ESPxddm.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/ESPxddm.o clang -g -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/bin/ESPxddm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/ESPxddm.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/writeTrix.o \ /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/surfTrix.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/xddm.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/bodyTess.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -locsm -legads \ -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include/ -lc3dio -lCart3D \ -lpthread -ldl -Wl,-rpath,/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -Wl,-rpath,@loader_path/ -Wl,-rpath,/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lxml2 -lm /Library/Developer/CommandLineTools/usr/bin/make -C cbaero clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I../utils -I../meshWriter/fastWriter cbaeroAIM.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/cbaeroAIM.o clang -g -bundle /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/cbaeroAIM.o -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/cbaeroAIM.so -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -lutils -laimUtil -locsm -legads -ludunits2 -lm -ldl /Library/Developer/CommandLineTools/usr/bin/make -C cgt clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include egads2cgt.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egads2cgt.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include aflr4egads.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/aflr4egads.o clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/test/egads2cgt /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egads2cgt.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/aflr4egads.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -legads -lcaps -locsm -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./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 -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I../utils delaundoAIM.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/delaundoAIM.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/delaundoAIM.so rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/delaundoAIM.so clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/delaundoAIM.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/delaundoAIM.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl \ -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm /Library/Developer/CommandLineTools/usr/bin/make -C egadsTess clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I../utils egadsTessAIM.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egadsTessAIM.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/egadsTessAIM.so rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/egadsTessAIM.so clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/egadsTessAIM.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/egadsTessAIM.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl \ -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm /Library/Developer/CommandLineTools/usr/bin/make -C friction clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -Wno-format -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I../utils frictionAIM.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/frictionAIM.o clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/frictionAIM.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/frictionAIM.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/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/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/friction.o gfortran -g -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/test/friction /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/friction.o -Wl,-w -static-libgfortran -static-libgcc /Library/Developer/CommandLineTools/usr/bin/make -C fun3d clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -DHAVE_PYTHON -DCYTHON_PEP489_MULTI_PHASE_INIT=0 \ -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I../utils -I../meshWriter/ugridWriter \ -I. -I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11 -I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11 -Icython fun3dAIM.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/fun3dAIM.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I../utils -I../meshWriter/ugridWriter \ fun3dUtils.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/fun3dUtils.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -DCYTHON_PEP489_MULTI_PHASE_INIT=0 \ -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I../utils \ -I. -I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11 -I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11 cython/fun3dNamelist.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/fun3dNamelist.o Building FUN3D with Python clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/fun3dAIM.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/fun3dAIM.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/fun3dUtils.o \ /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/fun3dNamelist.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -lutils -laimUtil -locsm \ -legads -ludunits2 -ldl -L/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/lib/python3.11/config-3.11-darwin -lpython3.11 -ldl -framework CoreFoundation -lm -Wl,-rpath /usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/lib/python3.11/config-3.11-darwin /Library/Developer/CommandLineTools/usr/bin/make -C hsm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I../utils hsmAIM.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/hsmAIM.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I../utils hsmUtils.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/hsmUtils.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I../utils hsmAdj.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/hsmAdj.o clang++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -Wno-comment rcm/rcm.cpp -DREVISION=7.8 \ -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/rcm.o clang++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 rcm/genrcmi.cpp -DREVISION=7.8 \ -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/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/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/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/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/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/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/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/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/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/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/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/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/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/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/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/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/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/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/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/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/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/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/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/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/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/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/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/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/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/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/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/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/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/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/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/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/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/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/sbsolve.o /Library/Developer/CommandLineTools/usr/bin/make -C src /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/libhsm.a touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/libhsm.a rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/libhsm.a (cd /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj; ar -rs /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/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/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/libhsm.a touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/hsmAIM.so rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/hsmAIM.so gfortran -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/hsmAIM.so \ /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/hsmAIM.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/hsmUtils.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/hsmAdj.o \ /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/rcm.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/genrcmi.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -lutils -laimUtil -locsm \ -legads -ludunits2 -lhsm -ldl -Wl,-rpath,/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -Wl,-rpath,@loader_path/ -Wl,-rpath,/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lc++ -Wl,-w /Library/Developer/CommandLineTools/usr/bin/make -C interference clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include interferenceAIM.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/interferenceAIM.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I. cloudFns.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/cloudFns.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/interferenceAIM.so rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/interferenceAIM.so clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/interferenceAIM.so \ /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/interferenceAIM.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/cloudFns.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib \ -laimUtil -locsm -legads -ludunits2 -ldl -lc++ -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm /Library/Developer/CommandLineTools/usr/bin/make -C jfd3 clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I../utils jfd3AIM.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/jfd3AIM.o clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/jfd3AIM.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/jfd3AIM.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm /Library/Developer/CommandLineTools/usr/bin/make -C masstran clang++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I../utils masstranAIM.cpp \ -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/masstranAIM.o clang++ -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/masstranAIM.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/masstranAIM.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/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 -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include bstlWriter.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/bstlWriter.o clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/bstlWriter.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/bstlWriter.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -laimUtil -legads -locsm -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm /Library/Developer/CommandLineTools/usr/bin/make -C bvtkWriter clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include bvtkWriter.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/bvtkWriter.o clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/bvtkWriter.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/bvtkWriter.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -laimUtil -legads -locsm -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm /Library/Developer/CommandLineTools/usr/bin/make -C exodusWriter make[3]: Nothing to be done for `default'. /Library/Developer/CommandLineTools/usr/bin/make -C fastWriter clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include fastWriter.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/fastWriter.o clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/fastWriter.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/fastWriter.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -laimUtil -legads -locsm -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm /Library/Developer/CommandLineTools/usr/bin/make -C libmeshbWriter clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include libmeshbWriter.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/libmeshbWriter.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -IlibMeshb/sources -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include libMeshb/sources/libmeshb7.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/libmeshb7.o clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/libmeshbWriter.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/libmeshbWriter.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/libmeshb7.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -laimUtil -legads -locsm -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm /Library/Developer/CommandLineTools/usr/bin/make -C stlWriter clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include stlWriter.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/stlWriter.o clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/stlWriter.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/stlWriter.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -laimUtil -legads -locsm -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm /Library/Developer/CommandLineTools/usr/bin/make -C su2Writer clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include su2Writer.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/su2Writer.o clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/su2Writer.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/su2Writer.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -laimUtil -legads -locsm -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm /Library/Developer/CommandLineTools/usr/bin/make -C tecplotWriter clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include tecplotWriter.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/tecplotWriter.o clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/tecplotWriter.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/tecplotWriter.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -laimUtil -legads -locsm -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm /Library/Developer/CommandLineTools/usr/bin/make -C ugridWriter clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include ugridWriter.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/ugridWriter.o clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/ugridWriter.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/ugridWriter.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -laimUtil -legads -locsm -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm /Library/Developer/CommandLineTools/usr/bin/make -C vtkWriter clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include vtkWriter.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/vtkWriter.o clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/vtkWriter.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/vtkWriter.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -laimUtil -legads -locsm -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm /Library/Developer/CommandLineTools/usr/bin/make -C mses clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I../utils msesAIM.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/msesAIM.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I../utils msesUtils.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/msesUtils.o clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/msesAIM.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/msesAIM.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/msesUtils.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm /Library/Developer/CommandLineTools/usr/bin/make -C mystran clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I../utils mystranAIM.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/mystranAIM.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I../utils mystranUtils.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/mystranUtils.o clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/mystranAIM.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/mystranAIM.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/mystranUtils.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm -L/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/lib/python3.11/config-3.11-darwin -lpython3.11 -ldl -framework CoreFoundation /Library/Developer/CommandLineTools/usr/bin/make -C nastran clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I../utils nastranAIM.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/nastranAIM.o clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/nastranAIM.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/nastranAIM.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm -L/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/lib/python3.11/config-3.11-darwin -lpython3.11 -ldl -framework CoreFoundation /Library/Developer/CommandLineTools/usr/bin/make -C plato Not compiling platoAIM: SEACAS must be set -- Please fix the environment.... /Library/Developer/CommandLineTools/usr/bin/make -C pointwise clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I../utils pointwiseAIM.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/pointwiseAIM.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I../utils hashElement.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/hashElement.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/pointwiseAIM.so rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/pointwiseAIM.so clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/pointwiseAIM.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/pointwiseAIM.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/hashElement.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl \ -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm -lpthread /Library/Developer/CommandLineTools/usr/bin/make -C refine clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I../utils -I../meshWriter/libmeshbWriter refineAIM.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/refineAIM.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/refineAIM.so rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/refineAIM.so clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/refineAIM.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/refineAIM.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/libmeshb7.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl \ -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm /Library/Developer/CommandLineTools/usr/bin/make -C sierraSD Not compiling sierraSDAIM: SEACAS must be set -- Please fix the environment.... /Library/Developer/CommandLineTools/usr/bin/make -C sierraSM Not compiling sierraSMAIM: SEACAS must be set -- Please fix the environment.... /Library/Developer/CommandLineTools/usr/bin/make -C skeleton clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I../utils skeletonAIM.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/skeletonAIM.o clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/skeletonAIM.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/skeletonAIM.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm /Library/Developer/CommandLineTools/usr/bin/make -C spinnaker make[2]: Nothing to be done for `default'. /Library/Developer/CommandLineTools/usr/bin/make -C su2 clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I../meshWriter/su2Writer -I../utils su2AIM.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/su2AIM.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I../utils su2Utils.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/su2Utils.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I../utils su2_4_Cardinal.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/su2_4_Cardinal.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I../utils su2_5_Raven.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/su2_5_Raven.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I../utils su2_6_Falcon.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/su2_6_Falcon.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I../utils su2_7_Blackbird.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/su2_7_Blackbird.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I../utils su2_801_Harrier.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/su2_801_Harrier.o clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/su2AIM.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/su2AIM.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/su2Utils.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/su2_4_Cardinal.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/su2_5_Raven.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/su2_6_Falcon.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/su2_7_Blackbird.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/su2_801_Harrier.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm /Library/Developer/CommandLineTools/usr/bin/make -C tacs clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I../utils tacsAIM.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/tacsAIM.o clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/tacsAIM.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/tacsAIM.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm -L/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/lib/python3.11/config-3.11-darwin -lpython3.11 -ldl -framework CoreFoundation /Library/Developer/CommandLineTools/usr/bin/make -C tetgen clang++ -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I../utils tetgenAIM.cpp \ -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/tetgenAIM.o clang++ -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I/Users/jenkins/util/tetgen/tetgen1.6.0 -I../utils \ -DTETLIBRARY tetgen_Interface.cpp -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/tetgen_Interface.o clang++ -g -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/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/tetgen.o clang++ -g -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/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/predicates.o clang++ -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/tetgenAIM.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/tetgenAIM.o \ /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/tetgen_Interface.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/tetgen.o \ /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/predicates.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -lutils -laimUtil -locsm \ -legads -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm /Library/Developer/CommandLineTools/usr/bin/make -C tsfoil clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I../utils \ tsfoilAIM.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/tsfoilAIM.o clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/tsfoilAIM.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/tsfoilAIM.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm /Library/Developer/CommandLineTools/usr/bin/make -C unitTest mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/aimUnitTest mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/aimUnitTest/pyCAPS cp -p -f pyCAPS/Mesh_Formats.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/aimUnitTest/pyCAPS/Mesh_Formats.py cp -p -f pyCAPS/test_aflr2.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/aimUnitTest/pyCAPS/test_aflr2.py cp -p -f pyCAPS/test_aflr3.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/aimUnitTest/pyCAPS/test_aflr3.py cp -p -f pyCAPS/test_aflr4.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/aimUnitTest/pyCAPS/test_aflr4.py cp -p -f pyCAPS/test_astros.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/aimUnitTest/pyCAPS/test_astros.py cp -p -f pyCAPS/test_avl.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/aimUnitTest/pyCAPS/test_avl.py cp -p -f pyCAPS/test_cart3d.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/aimUnitTest/pyCAPS/test_cart3d.py cp -p -f pyCAPS/test_cbaero.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/aimUnitTest/pyCAPS/test_cbaero.py cp -p -f pyCAPS/test_egadsTess.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/aimUnitTest/pyCAPS/test_egadsTess.py cp -p -f pyCAPS/test_fun3d.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/aimUnitTest/pyCAPS/test_fun3d.py cp -p -f pyCAPS/test_masstran.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/aimUnitTest/pyCAPS/test_masstran.py cp -p -f pyCAPS/test_mses.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/aimUnitTest/pyCAPS/test_mses.py cp -p -f pyCAPS/test_pointwise.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/aimUnitTest/pyCAPS/test_pointwise.py cp -p -f pyCAPS/test_refine.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/aimUnitTest/pyCAPS/test_refine.py cp -p -f pyCAPS/test_su2.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/aimUnitTest/pyCAPS/test_su2.py cp -p -f pyCAPS/test_tacs.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/aimUnitTest/pyCAPS/test_tacs.py cp -p -f pyCAPS/test_tetgen.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/aimUnitTest/pyCAPS/test_tetgen.py cp -p -f pyCAPS/test_xfoil.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/aimUnitTest/pyCAPS/test_xfoil.py cp -p -f pyCAPS/test_zaero.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/aimUnitTest/pyCAPS/test_zaero.py cp -p -f pyCAPS/Makefile /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/aimUnitTest/pyCAPS/Makefile mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/aimUnitTest/csmData cp -p -f csmData/airfoilSection.csm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/aimUnitTest/csmData/airfoilSection.csm cp -p -f csmData/avlSections.csm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/aimUnitTest/csmData/avlSections.csm cp -p -f csmData/cfd2D.csm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/aimUnitTest/csmData/cfd2D.csm cp -p -f csmData/cfdMultiBody.csm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/aimUnitTest/csmData/cfdMultiBody.csm cp -p -f csmData/cfdSingleBody.csm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/aimUnitTest/csmData/cfdSingleBody.csm cp -p -f csmData/cornerGeom.csm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/aimUnitTest/csmData/cornerGeom.csm cp -p -f csmData/feaSimplePlate.csm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/aimUnitTest/csmData/feaSimplePlate.csm cp -p -f csmData/feaWingBEMAero.csm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/aimUnitTest/csmData/feaWingBEMAero.csm cp -p -f csmData/feaWingOMLAero.csm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/aimUnitTest/csmData/feaWingOMLAero.csm cp -p -f csmData/kulfanSection.csm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/aimUnitTest/csmData/kulfanSection.csm cp -p -f csmData/kulfanSymmetricSection.csm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/aimUnitTest/csmData/kulfanSymmetricSection.csm cp -p -f csmData/masstran.csm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/aimUnitTest/csmData/masstran.csm cp -p -f csmData/multiRegions.csm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/aimUnitTest/csmData/multiRegions.csm mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/aimUnitTest/cCAPS /Library/Developer/CommandLineTools/usr/bin/make -C xfoil clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I../utils \ xfoilAIM.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/xfoilAIM.o clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/xfoilAIM.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/xfoilAIM.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm /Library/Developer/CommandLineTools/usr/bin/make -C zaero clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I../utils zaeroAIM.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/zaeroAIM.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I../utils zaeroUtils.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/zaeroUtils.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I../utils zaeroLinearFlutter.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/zaeroLinearFlutter.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I../utils zaeroTrim.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/zaeroTrim.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I../utils zaeroTypes.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/zaeroTypes.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I../utils zaeroCards.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/zaeroCards.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I../utils zaeroGeneral.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/zaeroGeneral.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I../utils zaeroGraphical.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/zaeroGraphical.o clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/zaeroAIM.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/zaeroAIM.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/zaeroUtils.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/zaeroLinearFlutter.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/zaeroTrim.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/zaeroTypes.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/zaeroCards.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/zaeroGeneral.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/zaeroGraphical.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -lutils -laimUtil -locsm -legads -ludunits2 -lm -ldl (cd Slugs/src; make) clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I. Slugs.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/Slugs.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I. Fitter.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/Fitter.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I. RedBlackTree.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/RedBlackTree.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I. Tessellate.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/Tessellate.o clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/bin/Slugs /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/Slugs.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/Fitter.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/RedBlackTree.o \ /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/Tessellate.o -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -lwsserver -legads \ -lpthread -lz -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I. TestFit.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/TestFit.o clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/bin/TestFit /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/TestFit.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/Fitter.o -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -legads \ -lpthread -lz -lm (cd test; make -f aim.make) clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include aim.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/aim.o clang -g -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/test/aim /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/aim.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -lcaps -locsm -legads \ -lwsserver -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib cp -p -f testingAIM.csm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/test/testingAIM.csm (cd test; make -f autoExec.make) clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include autoExec.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/autoExec.o clang -g -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/test/autoExec /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/autoExec.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -lcaps -locsm \ -legads -lwsserver -lpthread -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lz -lm -ldl (cd test; make -f newPhase.make) clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include newPhase.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/newPhase.o clang -g -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/test/newPhase /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/newPhase.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib \ -lcaps -locsm -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm -ldl (cd test; make -f basic.make) clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include basic.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/basic.o clang -g -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/test/basic /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/basic.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -lcaps -locsm -legads\ -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm -ldl (cd test; make -f geomIn.make) clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include geomIn.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/geomIn.o clang -g -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/test/geomIn /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/geomIn.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -lcaps -locsm -legads\ -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm -ldl (cd test; make -f utilsTest.make) clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include aimTransferUtilTest.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/aimTransferUtilTest.o clang -g -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/test/aimTransferUtilTest /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/aimTransferUtilTest.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -lcaps -laimUtil -locsm -legads \ -lpthread -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -ludunits2 -lm -ldl clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I../aim/utils miscUtilsTest.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/miscUtilsTest.o clang -g -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/test/miscUtilsTest /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/miscUtilsTest.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -laimUtil -locsm -legads \ -lpthread -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -ludunits2 -lm -ldl clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I../aim/utils vlmUtilsTest.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/vlmUtilsTest.o clang -g -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/test/vlmUtilsTest /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/vlmUtilsTest.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -lutils -laimUtil -locsm -legads \ -lpthread -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -ludunits2 -lm -ldl (cd test; make -f vVS.make) clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include vVS.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/vVS.o clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/test/vVS /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/vVS.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -lwsserver -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib (cd examples; make) mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/examples mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/examples/analysisData mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/examples/csmData mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/examples/cCAPS mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/examples/pyCAPS mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/examples/regressionTest mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/examples/corsairlite cp -p -f pyCAPS/abaqus_AGARD445_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/examples/pyCAPS/abaqus_AGARD445_PyTest.py cp -p -f pyCAPS/abaqus_SingleLoadCase_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/examples/pyCAPS/abaqus_SingleLoadCase_PyTest.py cp -p -f pyCAPS/aeroelasticModal_Fun3D_and_Astros.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/examples/pyCAPS/aeroelasticModal_Fun3D_and_Astros.py cp -p -f pyCAPS/aeroelasticModal_Fun3D_and_Mystran.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/examples/pyCAPS/aeroelasticModal_Fun3D_and_Mystran.py cp -p -f pyCAPS/aeroelasticModal_Fun3D_and_Nastran.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/examples/pyCAPS/aeroelasticModal_Fun3D_and_Nastran.py cp -p -f pyCAPS/aeroelasticSimple_Displacement_Fun3D_and_Mystran.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/examples/pyCAPS/aeroelasticSimple_Displacement_Fun3D_and_Mystran.py cp -p -f pyCAPS/aeroelasticSimple_Displacement_SU2_and_Astros.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/examples/pyCAPS/aeroelasticSimple_Displacement_SU2_and_Astros.py cp -p -f pyCAPS/aeroelasticSimple_Displacement_SU2_and_Mystran.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/examples/pyCAPS/aeroelasticSimple_Displacement_SU2_and_Mystran.py cp -p -f pyCAPS/aeroelasticSimple_Iterative_Cart3D_and_Mystran.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/examples/pyCAPS/aeroelasticSimple_Iterative_Cart3D_and_Mystran.py cp -p -f pyCAPS/aeroelasticSimple_Iterative_Fun3D_and_Mystran.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/examples/pyCAPS/aeroelasticSimple_Iterative_Fun3D_and_Mystran.py cp -p -f pyCAPS/aeroelasticSimple_Iterative_SU2_and_Astros.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/examples/pyCAPS/aeroelasticSimple_Iterative_SU2_and_Astros.py cp -p -f pyCAPS/aeroelasticSimple_Iterative_SU2_and_Mystran.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/examples/pyCAPS/aeroelasticSimple_Iterative_SU2_and_Mystran.py cp -p -f pyCAPS/aeroelasticSimple_Pressure_Fun3D_and_Mystran.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/examples/pyCAPS/aeroelasticSimple_Pressure_Fun3D_and_Mystran.py cp -p -f pyCAPS/aeroelasticSimple_Pressure_SU2_and_Astros.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/examples/pyCAPS/aeroelasticSimple_Pressure_SU2_and_Astros.py cp -p -f pyCAPS/aeroelasticSimple_Pressure_SU2_and_Mystran.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/examples/pyCAPS/aeroelasticSimple_Pressure_SU2_and_Mystran.py cp -p -f pyCAPS/aeroelasticSimple_Temperature_SU2_and_TACS.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/examples/pyCAPS/aeroelasticSimple_Temperature_SU2_and_TACS.py cp -p -f pyCAPS/aeroelastic_Iterative_Fun3D_and_Mystran.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/examples/pyCAPS/aeroelastic_Iterative_Fun3D_and_Mystran.py cp -p -f pyCAPS/aeroelastic_Iterative_SU2_and_Astros.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/examples/pyCAPS/aeroelastic_Iterative_SU2_and_Astros.py cp -p -f pyCAPS/aeroelastic_Iterative_SU2_and_Mystran.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/examples/pyCAPS/aeroelastic_Iterative_SU2_and_Mystran.py cp -p -f pyCAPS/aflr2_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/examples/pyCAPS/aflr2_PyTest.py cp -p -f pyCAPS/aflr4_Generic_Missile.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/examples/pyCAPS/aflr4_Generic_Missile.py cp -p -f pyCAPS/aflr4_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/examples/pyCAPS/aflr4_PyTest.py cp -p -f pyCAPS/aflr4_QuadMesh_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/examples/pyCAPS/aflr4_QuadMesh_PyTest.py cp -p -f pyCAPS/aflr4_Symmetry_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/examples/pyCAPS/aflr4_Symmetry_PyTest.py cp -p -f pyCAPS/aflr4_TipTreat_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/examples/pyCAPS/aflr4_TipTreat_PyTest.py cp -p -f pyCAPS/aflr4_and_Tetgen_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/examples/pyCAPS/aflr4_and_Tetgen_PyTest.py cp -p -f pyCAPS/aflr4_and_aflr3_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/examples/pyCAPS/aflr4_and_aflr3_PyTest.py cp -p -f pyCAPS/aflr4_and_aflr3_Symmetry_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/examples/pyCAPS/aflr4_and_aflr3_Symmetry_PyTest.py cp -p -f pyCAPS/aflr4_tetgen_Regions_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/examples/pyCAPS/aflr4_tetgen_Regions_PyTest.py cp -p -f pyCAPS/astros_AGARD445_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/examples/pyCAPS/astros_AGARD445_PyTest.py cp -p -f pyCAPS/astros_Aeroelastic_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/examples/pyCAPS/astros_Aeroelastic_PyTest.py cp -p -f pyCAPS/astros_CompositeWingFreq_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/examples/pyCAPS/astros_CompositeWingFreq_PyTest.py cp -p -f pyCAPS/astros_Composite_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/examples/pyCAPS/astros_Composite_PyTest.py cp -p -f pyCAPS/astros_Flutter_15degree.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/examples/pyCAPS/astros_Flutter_15degree.py cp -p -f pyCAPS/astros_MultipleLoadCase_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/examples/pyCAPS/astros_MultipleLoadCase_PyTest.py cp -p -f pyCAPS/astros_OptControl_PyTest.py 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-p -f csmData/avlWingTail.csm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/examples/csmData/avlWingTail.csm cp -p -f csmData/avlWings.csm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/examples/csmData/avlWings.csm cp -p -f csmData/awaveWingTailFuselage.csm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/examples/csmData/awaveWingTailFuselage.csm cp -p -f csmData/cfd2D.csm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/examples/csmData/cfd2D.csm cp -p -f csmData/cfd2DArbShape.csm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/examples/csmData/cfd2DArbShape.csm cp -p -f csmData/cfdMultiBody.csm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/examples/csmData/cfdMultiBody.csm cp -p -f csmData/cfdSymmetry.csm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/examples/csmData/cfdSymmetry.csm cp -p -f csmData/cfdX43a.csm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/examples/csmData/cfdX43a.csm cp -p -f csmData/cfd_airfoilSection.csm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/examples/csmData/cfd_airfoilSection.csm cp -p -f csmData/compositeWing.csm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/examples/csmData/compositeWing.csm cp -p -f csmData/cyli_box_shell.csm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/examples/csmData/cyli_box_shell.csm cp -p -f csmData/cyli_box_solid.csm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/examples/csmData/cyli_box_solid.csm cp -p -f csmData/feaAGARD445.csm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/examples/csmData/feaAGARD445.csm cp -p -f csmData/feaBoxes.csm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/examples/csmData/feaBoxes.csm cp -p -f csmData/feaCantileverPlate.csm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/examples/csmData/feaCantileverPlate.csm cp -p -f csmData/feaJoinedPlate.csm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/examples/csmData/feaJoinedPlate.csm cp -p -f csmData/feaSimplePlate.csm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/examples/csmData/feaSimplePlate.csm cp -p -f csmData/feaThreeBar.csm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/examples/csmData/feaThreeBar.csm cp -p -f csmData/feaWingBEM.csm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/examples/csmData/feaWingBEM.csm cp -p -f csmData/feaWingBEMAero.csm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/examples/csmData/feaWingBEMAero.csm cp -p -f csmData/frictionWingTailFuselage.csm 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/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/examples/csmData/spheres.csm cp -p -f csmData/table.csm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/examples/csmData/table.csm cp -p -f csmData/tiptreat.csm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/examples/csmData/tiptreat.csm cp -p -f csmData/avlWing.udc /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/examples/csmData/avlWing.udc mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/examples/analysisData/nastran cp -p -f analysisData/nastran/NastranAeroWingBEM.f06 /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/examples/analysisData/nastran/NastranAeroWingBEM.f06 cp -p -f analysisData/nastran/NastranCompositePlate.f06 /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/examples/analysisData/nastran/NastranCompositePlate.f06 cp -p -f 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/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/examples/analysisData/nastran/NastranMultiLoadPlate.f06 cp -p -f analysisData/nastran/NastranOptMultiLoadPlate.f06 /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/examples/analysisData/nastran/NastranOptMultiLoadPlate.f06 cp -p -f analysisData/nastran/NastranSingleLoadPlate.f06 /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/examples/analysisData/nastran/NastranSingleLoadPlate.f06 cp -p -f analysisData/nastran/NastranThreeBar.f06 /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/examples/analysisData/nastran/NastranThreeBar.f06 cp -p -f analysisData/nastran/NastranThreeBarDesign.f06 /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/examples/analysisData/nastran/NastranThreeBarDesign.f06 cp -p -f analysisData/nastran/NastranThreeBarFreq.f06 /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/examples/analysisData/nastran/NastranThreeBarFreq.f06 cp -p -f analysisData/nastran/NastranThreeBarLinkDesign.f06 /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/examples/analysisData/nastran/NastranThreeBarLinkDesign.f06 cp -p -f analysisData/nastran/NastranThreeBarMultiLoad.f06 /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/examples/analysisData/nastran/NastranThreeBarMultiLoad.f06 cp -p -f analysisData/nastran/NastranTrim15Deg.f06 /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/examples/analysisData/nastran/NastranTrim15Deg.f06 cp -p -f analysisData/nastran/NastranWingBEM.f06 /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/examples/analysisData/nastran/NastranWingBEM.f06 mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/examples/corsairlite/capsPhase/csm mkdir -p 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/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/examples/corsairlite/multifidelity/pyCAPS/fullModelNACA.py cp -p -f regressionTest/execute_CTestRegression.sh /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/examples/regressionTest/execute_CTestRegression.sh cp -p -f regressionTest/execute_PyTestRegression.sh /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/examples/regressionTest/execute_PyTestRegression.sh (make -C cCAPS -f aeroelastic_SU2.make) clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include aeroelasticSimple_Iterative_SU2_and_MystranTest.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/aeroelasticSimple_Iterative_SU2_and_MystranTest.o clang -g -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/examples/cCAPS/aeroelasticSimple_Iterative_SU2_and_MystranTest /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/aeroelasticSimple_Iterative_SU2_and_MystranTest.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -lcaps -locsm -legads \ -ludunits2 -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm -ldl (make -C cCAPS -f avlTest.make) clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include avlTest.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/avlTest.o clang -g -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/examples/cCAPS/avlTest /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/avlTest.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -lcaps -legads -locsm \ -ludunits2 -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm -ldl (make -C cCAPS -f awaveTest.make) clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include awaveTest.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/awaveTest.o clang -g -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/examples/cCAPS/awaveTest /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/awaveTest.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -lcaps -legads -locsm \ -ludunits2 -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm -ldl (make -C cCAPS -f frictionTest.make) clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include frictionTest.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/frictionTest.o clang -g -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/examples/cCAPS/frictionTest /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/frictionTest.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -lcaps -locsm -legads \ -ludunits2 -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm -ldl (make -C cCAPS -f fun3d.make) clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include fun3dAFLR2Test.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/fun3dAFLR2Test.o clang -g -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/examples/cCAPS/fun3dAFLR2Test /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/fun3dAFLR2Test.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm -ldl clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include fun3dTetgenTest.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/fun3dTetgenTest.o clang -g -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/examples/cCAPS/fun3dTetgenTest /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/fun3dTetgenTest.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm -ldl clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include aeroelasticTest.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/aeroelasticTest.o clang -g -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/examples/cCAPS/aeroelasticTest /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/aeroelasticTest.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm -ldl (make -C cCAPS -f hsm.make) clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include hsmTest.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/hsmTest.o clang -g -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/examples/cCAPS/hsmTest /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/hsmTest.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm -ldl clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include hsmSimplePlateTest.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/hsmSimplePlateTest.o clang -g -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/examples/cCAPS/hsmSimplePlateTest /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/hsmSimplePlateTest.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm -ldl clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include hsmCantileverPlateTest.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/hsmCantileverPlateTest.o clang -g -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/examples/cCAPS/hsmCantileverPlateTest /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/hsmCantileverPlateTest.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm -ldl clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include hsmJoinedPlateTest.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/hsmJoinedPlateTest.o clang -g -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/examples/cCAPS/hsmJoinedPlateTest /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/hsmJoinedPlateTest.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm -ldl (make -C cCAPS -f interferenceTest.make) clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include interferenceTest.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/interferenceTest.o clang -g -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/examples/cCAPS/interferenceTest /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/interferenceTest.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm -ldl (make -C cCAPS -f msesTest.make) clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include msesTest.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/msesTest.o clang -g -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/examples/cCAPS/msesTest /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/msesTest.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -lcaps -legads -locsm \ -ludunits2 -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm -ldl (make -C cCAPS -f mystran.make) clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include mystranTest.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/mystranTest.o clang -g -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/examples/cCAPS/mystranTest /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/mystranTest.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm -ldl (make -C cCAPS -f pointwiseTest.make) clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include pointwiseTest.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/pointwiseTest.o clang -g -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/examples/cCAPS/pointwiseTest /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/pointwiseTest.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -lcaps -locsm -legads \ -ludunits2 -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm -ldl +++ find /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/CAPS/training/ -name Makefile ++ for i in '`find $WORKSPACE/CAPS/training/ -name Makefile`' ++ [[ /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/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/7.8/CAPS/unit/DARWIN64/CAPS/training//2023/data/session01/Makefile == *\l\e\c\t\u\r\e\s* ]] +++ dirname /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/CAPS/training//2023/data/session01/Makefile ++ cd /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/CAPS/training//2023/data/session01 ++ make clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include template_avl.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/template_avl.o clang -g -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/test/template_avl /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/template_avl.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -lcaps -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm -ldl ++ for i in '`find $WORKSPACE/CAPS/training/ -name Makefile`' ++ [[ /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/CAPS/training//data/session01/Makefile == *\l\e\c\t\u\r\e\s* ]] +++ dirname /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/CAPS/training//data/session01/Makefile ++ cd /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/CAPS/training//data/session01 ++ make make: Nothing to be done for `default'. ++ cd /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/OpenCSM/trunk/src ++ make -f serveESP.make clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I. timCapsMode.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/timCapsMode.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/capsMode.so rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/capsMode.so clang++ -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/capsMode.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/timCapsMode.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -lcaps -locsm -lwsserver -legads -ldl -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I. timFlowchart.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/timFlowchart.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/flowchart.so rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/flowchart.so clang++ -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/flowchart.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/timFlowchart.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -lcaps -locsm -lwsserver -legads -ldl -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I. timViewer.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/timViewer.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/viewer.so rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/viewer.so clang++ -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/viewer.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/timViewer.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -lcaps -locsm -lwsserver -legads -ldl -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include -I. -I. -I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11 -I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11 timPyscript.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/timPyscript.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/pyscript.so rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/pyscript.so clang++ -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/pyscript.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/obj/timPyscript.o -L/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/lib/python3.11/config-3.11-darwin -lpython3.11 -ldl -framework CoreFoundation -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -lcaps -locsm -lwsserver -legads -ldl -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -Wl,-rpath /usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/lib/python3.11/config-3.11-darwin ++ ln -f -s /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/OpenCSM/trunk/udc /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64 +++ find /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/OpenCSM/trunk/data/training/ -name Makefile + mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/test + cd /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/test + source /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/JenkinsESP/RunRegression.sh ++ [[ 0 == 1 ]] ++ [[ 0 == 2 ]] ++ [[ /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64 == '' ]] ++ [[ CAPS/unit == '' ]] ++ [[ 7.8 == '' ]] ++ [[ ! -d /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/JenkinsESP ]] ++ rm -f csmFiles.txt ++ [[ CAPS/unit =~ [0-9]+.[0-9]+ ]] ++ export ESPTEST=CAPS/unit ++ ESPTEST=CAPS/unit ++ [[ CAPS/unit == \C\A\P\S* ]] ++ [[ ! -d /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/CAPS ]] ++ export CAPSTARGET=unit ++ CAPSTARGET=unit ++ [[ unit == \u\n\i\t ]] ++ cd /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/EGADS/trunk/test ++ ./runUnitTest.sh ++ tee -a capsUnit.txt ================================================= + /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/test/egadsGeom_dot + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/EGADS/trunk/test/egadslog.txt real 0m3.458s user 0m3.065s sys 0m0.079s + status=0 + set +x ================================================= EGADS test egadsGeom_dot passed (as expected) ================================================= ================================================= + /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/test/egadsSpline_dot + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/EGADS/trunk/test/egadslog.txt real 0m40.976s user 0m39.997s sys 0m0.568s + status=0 + set +x ================================================= EGADS test egadsSpline_dot passed (as expected) ================================================= ================================================= + /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/test/egadsTopo_dot + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/EGADS/trunk/test/egadslog.txt real 0m0.312s user 0m0.208s sys 0m0.022s + status=0 + set +x ================================================= EGADS test egadsTopo_dot passed (as expected) ================================================= ================================================= + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/EGADS/trunk/test/egadslog.txt + /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/test/egadsHLevel_dot real 0m0.331s user 0m0.284s sys 0m0.019s + status=1 + set +x ================================================= EGADS test egadsHLevel_dot failed (as expected) ================================================= All tests pass! ++ cd /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/EGADS/trunk/docs/Tutorial ++ ./tire ++ tee -a capsUnit.txt EG_open -> status=0 EG_makeTopology -> status=0 EG_saveModel -> status=0 EG_close -> status=0 EGADS Info: 77 Objects, 197 Reference in Use (of 1955) at Close! EGADS Info: 73 unattached Objects (197 References) removed! EG_close -> status=0 ++ cd /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/EGADS/trunk/docs/EGADS_dot/src ++ make test ++ tee -a capsUnit.txt ./circle1_dot Circle np1 = 65 EGADS Info: 44 Objects, 88 Reference in Use (of 160) at Close! EGADS Info: 44 unattached Objects (88 References) removed! EGADS_SUCCESS! ./circle2_dot Circle np1 = 65 EGADS Info: 84 Objects, 168 Reference in Use (of 280) at Close! EGADS Info: 84 unattached Objects (168 References) removed! EGADS_SUCCESS! ./naca_dot sharpte = 0 Ping NACA Edge 1 np1 = 20 Ping NACA Edge 2 np1 = 20 Ping NACA Edge 3 np1 = 2 Ping NACA Face 1 np1 = 50 sharpte = 1 Ping NACA Edge 1 np1 = 20 Ping NACA Edge 2 np1 = 20 Ping NACA Face 1 np1 = 49 EGADS Info: 76 Objects, 172 Reference in Use (of 296) at Close! EGADS Info: 76 unattached Objects (172 References) removed! EGADS_SUCCESS! ./ruled_naca_dot sharpte = 0 Ping Ruled NACA Edge 1 np1 = 33 Ping Ruled NACA Edge 2 np1 = 13 Ping Ruled NACA Edge 3 np1 = 129 Ping Ruled NACA Edge 4 np1 = 13 Ping Ruled NACA Edge 5 np1 = 13 Ping Ruled NACA Edge 6 np1 = 33 Ping Ruled NACA Edge 7 np1 = 13 Ping Ruled NACA Edge 8 np1 = 2 Ping Ruled NACA Edge 9 np1 = 2 Ping Ruled NACA Face 1 np1 = 1427 Ping Ruled NACA Face 2 np1 = 513 Ping Ruled NACA Face 3 np1 = 66 Ping Ruled NACA Face 4 np1 = 25 Ping Ruled NACA Face 5 np1 = 25 sharpte = 1 Ping Ruled NACA Edge 1 np1 = 33 Ping Ruled NACA Edge 2 np1 = 13 Ping Ruled NACA Edge 3 np1 = 129 Ping Ruled NACA Edge 4 np1 = 13 Ping Ruled NACA Edge 5 np1 = 13 Ping Ruled NACA Edge 6 np1 = 13 Ping Ruled NACA Face 1 np1 = 1427 Ping Ruled NACA Face 2 np1 = 536 Ping Ruled NACA Face 3 np1 = 24 Ping Ruled NACA Face 4 np1 = 24 EGADS Info: 200 Objects, 345 Reference in Use (of 880) at Close! EGADS Info: 105 unattached Objects (345 References) removed! EGADS_SUCCESS! ++ cd /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/EGADS/trunk/pyEGADS/test ++ make ++ tee -a capsUnit.txt python --version Python 3.11.5 python -u -m unittest discover .................................................... PCurve Map: 48 (alloc 48)! Surface Map: 12 (alloc 24)! Curve Map: 28 (alloc 28)! Writing PCurves... Writing Curves... Writing Surfaces... Writing 16 Nodes... Writing 28 Edges... Writing 12 Loops... Writing 12 Faces... Writing 1 Shells... EGADS Info: 0 Objects, 0 Reference in Use (of 972) at Close! ................... ---------------------------------------------------------------------- Ran 71 tests in 3.843s OK ++ cd /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/EGADS/trunk/docs/Tutorial ++ tee -a capsUnit.txt ++ python -u tire.py EGADS Info: 0 Objects, 0 Reference in Use (of 2791) at Close! ++ cd /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/EGADS/trunk/jlEGADS ++ make test ++ tee -a capsUnit.txt Creating file with egads constants Installing known registries into `~/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/julia` Updating registry at `~/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/julia/registries/General.toml` Resolving package versions... Installed Clang_jll ─── v14.0.6+4 Installed CEnum ─────── v0.5.0 Installed JLLWrappers ─ v1.5.0 Installed Preferences ─ v1.4.3 Installed Clang ─────── v0.18.3 Updating `~/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/julia/environments/v1.9/Project.toml` [40e3b903] + Clang v0.18.3 Updating `~/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/julia/environments/v1.9/Manifest.toml` [fa961155] + CEnum v0.5.0 [40e3b903] + Clang v0.18.3 [692b3bcd] + JLLWrappers v1.5.0 [21216c6a] + Preferences v1.4.3 ⌅ [0ee61d77] + Clang_jll v14.0.6+4 [0dad84c5] + ArgTools v1.1.1 [56f22d72] + Artifacts [2a0f44e3] + Base64 [ade2ca70] + Dates [f43a241f] + Downloads v1.6.0 [7b1f6079] + FileWatching [b77e0a4c] + InteractiveUtils [b27032c2] + LibCURL v0.6.3 [76f85450] + LibGit2 [8f399da3] + Libdl [56ddb016] + Logging [d6f4376e] + Markdown [ca575930] + NetworkOptions v1.2.0 [44cfe95a] + Pkg v1.9.2 [de0858da] + Printf [3fa0cd96] + REPL [9a3f8284] + Random [ea8e919c] + SHA v0.7.0 [9e88b42a] + Serialization [6462fe0b] + Sockets [fa267f1f] + TOML v1.0.3 [a4e569a6] + Tar v1.10.0 [cf7118a7] + UUIDs [4ec0a83e] + Unicode [deac9b47] + LibCURL_jll v7.84.0+0 [29816b5a] + LibSSH2_jll v1.10.2+0 [c8ffd9c3] + MbedTLS_jll v2.28.2+0 [14a3606d] + MozillaCACerts_jll v2022.10.11 [83775a58] + Zlib_jll v1.2.13+0 [8f36deef] + libLLVM_jll v14.0.6+3 [8e850ede] + nghttp2_jll v1.48.0+0 [3f19e933] + p7zip_jll v17.4.0+0 Info Packages marked with ⌅ have new versions available but compatibility constraints restrict them from upgrading. To see why use `status --outdated -m` Precompiling project... [32m ✓ [39m[90mMbedTLS_jll[39m [32m ✓ [39m[90mZlib_jll[39m [32m ✓ [39m[90mlibLLVM_jll[39m [32m ✓ [39m[90mCEnum[39m [32m ✓ [39m[90mPreferences[39m [32m ✓ [39m[90mLibSSH2_jll[39m [32m ✓ [39m[90mJLLWrappers[39m [32m ✓ [39m[90mClang_jll[39m [32m ✓ [39mClang 9 dependencies successfully precompiled in 14 seconds Downloading artifact: GCCBootstrap-x86_64-apple-darwin14.v4.8.5.x86_64-linux-musl.unpacked [ Info: Parsing headers... [ Info: Processing header: /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include/egadsTypes.h [ Info: Processing header: /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/include/egadsErrors.h [ Info: Building the DAG... [ Info: Emit Julia expressions... [ Info: [FunctionPrinter]: print to dumb.jl [ Info: [CommonPrinter]: print to /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/EGADS/trunk/jlEGADS/egadscommon/egads_types_ctts.jl [ Info: Done! Dev egads : add package to Julia dependency Resolving package versions... Updating `~/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/julia/environments/v1.9/Project.toml` [bba4f53b] + egads v0.1.0 `../../../../../EGADS/trunk/jlEGADS/egads` Updating `~/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/julia/environments/v1.9/Manifest.toml` [bba4f53b] + egads v0.1.0 `../../../../../EGADS/trunk/jlEGADS/egads` Test egads Testing egads Status `/private/var/folders/qk/9zkf0syn149fvhw9mh7hgd5w0000gp/T/jl_RddiGo/Project.toml` [bba4f53b] egads v0.1.0 `~/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/EGADS/trunk/jlEGADS/egads` [fa267f1f] TOML v1.0.3 `@stdlib/TOML` [8dfed614] Test `@stdlib/Test` Status `/private/var/folders/qk/9zkf0syn149fvhw9mh7hgd5w0000gp/T/jl_RddiGo/Manifest.toml` [fa961155] CEnum v0.5.0 [40e3b903] Clang v0.18.3 [692b3bcd] JLLWrappers v1.5.0 [21216c6a] Preferences v1.4.3 [bba4f53b] egads v0.1.0 `~/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/EGADS/trunk/jlEGADS/egads` ⌅ [0ee61d77] Clang_jll v14.0.6+4 [0dad84c5] ArgTools v1.1.1 `@stdlib/ArgTools` [56f22d72] Artifacts `@stdlib/Artifacts` [2a0f44e3] Base64 `@stdlib/Base64` [ade2ca70] Dates `@stdlib/Dates` [f43a241f] Downloads v1.6.0 `@stdlib/Downloads` [7b1f6079] FileWatching `@stdlib/FileWatching` [b77e0a4c] InteractiveUtils `@stdlib/InteractiveUtils` [b27032c2] LibCURL v0.6.3 `@stdlib/LibCURL` [76f85450] LibGit2 `@stdlib/LibGit2` [8f399da3] Libdl `@stdlib/Libdl` [56ddb016] Logging `@stdlib/Logging` [d6f4376e] Markdown `@stdlib/Markdown` [ca575930] NetworkOptions v1.2.0 `@stdlib/NetworkOptions` [44cfe95a] Pkg v1.9.2 `@stdlib/Pkg` [de0858da] Printf `@stdlib/Printf` [3fa0cd96] REPL `@stdlib/REPL` [9a3f8284] Random `@stdlib/Random` [ea8e919c] SHA v0.7.0 `@stdlib/SHA` [9e88b42a] Serialization `@stdlib/Serialization` [6462fe0b] Sockets `@stdlib/Sockets` [fa267f1f] TOML v1.0.3 `@stdlib/TOML` [a4e569a6] Tar v1.10.0 `@stdlib/Tar` [8dfed614] Test `@stdlib/Test` [cf7118a7] UUIDs `@stdlib/UUIDs` [4ec0a83e] Unicode `@stdlib/Unicode` [deac9b47] LibCURL_jll v7.84.0+0 `@stdlib/LibCURL_jll` [29816b5a] LibSSH2_jll v1.10.2+0 `@stdlib/LibSSH2_jll` [c8ffd9c3] MbedTLS_jll v2.28.2+0 `@stdlib/MbedTLS_jll` [14a3606d] MozillaCACerts_jll v2022.10.11 `@stdlib/MozillaCACerts_jll` [83775a58] Zlib_jll v1.2.13+0 `@stdlib/Zlib_jll` [8f36deef] libLLVM_jll v14.0.6+3 `@stdlib/libLLVM_jll` [8e850ede] nghttp2_jll v1.48.0+0 `@stdlib/nghttp2_jll` [3f19e933] p7zip_jll v17.4.0+0 `@stdlib/p7zip_jll` Info Packages marked with ⌅ have new versions available but compatibility constraints restrict them from upgrading. Precompiling project... [32m ✓ [39m[90mZlib_jll[39m [32m ✓ [39m[90mCEnum[39m [32m ✓ [39m[90mlibLLVM_jll[39m [32m ✓ [39m[90mMbedTLS_jll[39m [32m ✓ [39m[90mPreferences[39m [32m ✓ [39m[90mLibSSH2_jll[39m [32m ✓ [39m[90mJLLWrappers[39m [32m ✓ [39m[90mClang_jll[39m [32m ✓ [39m[90mClang[39m [32m ✓ [39megads 10 dependencies successfully precompiled in 24 seconds [33m1[39m dependency had warnings during precompilation:[33m ┌ [39megads [bba4f53b-aa41-4608-a097-29d2775fda82][33m │ [39m[ Info: ESP_ROOT_LIB /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib[33m └ [39m Testing Running tests... [ Info: RUNNING TEST test_NMwireBody [ Info: RUNNING TEST test_addKnots [ Info: RUNNING TEST test_approximate [ Info: RUNNING TEST test_attribution [ Info: RUNNING TEST test_attribution_for_lite [ Info: RUNNING TEST test_blend_and_ruled [ Info: RUNNING TEST test_booleanOperations [ Info: RUNNING TEST test_chamferHollow [ Info: RUNNING TEST test_effective [ Info: RUNNING TEST test_evaluate [ Info: RUNNING TEST test_filletBody [ Info: RUNNING TEST test_fitTriangles [ Info: RUNNING TEST test_fuseSheets [ Info: RUNNING TEST test_geoProperties [ Info: RUNNING TEST test_getEdgeUV [ Info: RUNNING TEST test_inTopology [ Info: RUNNING TEST test_intersection [ Info: RUNNING TEST test_isIsoPCurve [ Info: RUNNING TEST test_isoCline [ Info: RUNNING TEST test_makeBezier [ Info: RUNNING TEST test_makeGeometry_curves [ Info: RUNNING TEST test_makeGeometry_surfaces [ Info: RUNNING TEST test_makeLoopFace [ Info: RUNNING TEST test_makeTransform [ Info: RUNNING TEST test_make_export_IO_model [ Info: RUNNING TEST test_mapBody [ Info: RUNNING TEST test_match_sew_replace_topology [ Info: RUNNING TEST test_memo [ Info: RUNNING TEST test_modifyTess [ Info: RUNNING TEST test_otherCurve [ Info: RUNNING TEST test_quadTess [ Info: RUNNING TEST test_revision [ Info: ********* EGADS version 1.25 OCC Interim Release with OpenCASCADE 7.8.0 ********* [ Info: RUNNING TEST test_rotate [ Info: RUNNING TEST test_skinning [ Info: RUNNING TEST test_sweepExtrude [ Info: RUNNING TEST test_tessBody [ Info: RUNNING TEST test_tolerance Test Summary: | Pass Total Time Julia egads API | 203 203 31.5s 31.643143 seconds (21.94 M allocations: 1.337 GiB, 2.17% gc time, 89.38% compilation time) EGADS Info: 0 Objects, 0 Reference in Use (of 68) at Close! EGADS Info: 0 Objects, 0 Reference in Use (of 47) at Close! Testing egads tests passed Dev egadslite : add package to Julia dependency Resolving package versions... Updating `~/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/julia/environments/v1.9/Project.toml` [8839a610] + egadslite v0.1.0 `../../../../../EGADS/trunk/jlEGADS/egadslite` Updating `~/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/julia/environments/v1.9/Manifest.toml` [8839a610] + egadslite v0.1.0 `../../../../../EGADS/trunk/jlEGADS/egadslite` Test egadslite Testing egadslite Status `/private/var/folders/qk/9zkf0syn149fvhw9mh7hgd5w0000gp/T/jl_9KrhbI/Project.toml` [8bb1440f] DelimitedFiles v1.9.1 [8839a610] egadslite v0.1.0 `~/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/EGADS/trunk/jlEGADS/egadslite` [fa267f1f] TOML v1.0.3 `@stdlib/TOML` [8dfed614] Test `@stdlib/Test` Status `/private/var/folders/qk/9zkf0syn149fvhw9mh7hgd5w0000gp/T/jl_9KrhbI/Manifest.toml` [fa961155] CEnum v0.5.0 [40e3b903] Clang v0.18.3 [8bb1440f] DelimitedFiles v1.9.1 [692b3bcd] JLLWrappers v1.5.0 [21216c6a] Preferences v1.4.3 [8839a610] egadslite v0.1.0 `~/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/EGADS/trunk/jlEGADS/egadslite` ⌅ [0ee61d77] Clang_jll v14.0.6+4 [0dad84c5] ArgTools v1.1.1 `@stdlib/ArgTools` [56f22d72] Artifacts `@stdlib/Artifacts` [2a0f44e3] Base64 `@stdlib/Base64` [ade2ca70] Dates `@stdlib/Dates` [f43a241f] Downloads v1.6.0 `@stdlib/Downloads` [7b1f6079] FileWatching `@stdlib/FileWatching` [b77e0a4c] InteractiveUtils `@stdlib/InteractiveUtils` [b27032c2] LibCURL v0.6.3 `@stdlib/LibCURL` [76f85450] LibGit2 `@stdlib/LibGit2` [8f399da3] Libdl `@stdlib/Libdl` [56ddb016] Logging `@stdlib/Logging` [d6f4376e] Markdown `@stdlib/Markdown` [a63ad114] Mmap `@stdlib/Mmap` [ca575930] NetworkOptions v1.2.0 `@stdlib/NetworkOptions` [44cfe95a] Pkg v1.9.2 `@stdlib/Pkg` [de0858da] Printf `@stdlib/Printf` [3fa0cd96] REPL `@stdlib/REPL` [9a3f8284] Random `@stdlib/Random` [ea8e919c] SHA v0.7.0 `@stdlib/SHA` [9e88b42a] Serialization `@stdlib/Serialization` [6462fe0b] Sockets `@stdlib/Sockets` [fa267f1f] TOML v1.0.3 `@stdlib/TOML` [a4e569a6] Tar v1.10.0 `@stdlib/Tar` [8dfed614] Test `@stdlib/Test` [cf7118a7] UUIDs `@stdlib/UUIDs` [4ec0a83e] Unicode `@stdlib/Unicode` [deac9b47] LibCURL_jll v7.84.0+0 `@stdlib/LibCURL_jll` [29816b5a] LibSSH2_jll v1.10.2+0 `@stdlib/LibSSH2_jll` [c8ffd9c3] MbedTLS_jll v2.28.2+0 `@stdlib/MbedTLS_jll` [14a3606d] MozillaCACerts_jll v2022.10.11 `@stdlib/MozillaCACerts_jll` [83775a58] Zlib_jll v1.2.13+0 `@stdlib/Zlib_jll` [8f36deef] libLLVM_jll v14.0.6+3 `@stdlib/libLLVM_jll` [8e850ede] nghttp2_jll v1.48.0+0 `@stdlib/nghttp2_jll` [3f19e933] p7zip_jll v17.4.0+0 `@stdlib/p7zip_jll` Info Packages marked with ⌅ have new versions available but compatibility constraints restrict them from upgrading. Precompiling project... [32m ✓ [39mDelimitedFiles [32m ✓ [39megadslite 2 dependencies successfully precompiled in 3 seconds. 9 already precompiled. [33m1[39m dependency had warnings during precompilation:[33m ┌ [39megadslite [8839a610-0e5e-4b77-8553-273f46a3dff9][33m │ [39m[ Info: ESP_ROOT_LIB /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib[33m └ [39m Testing Running tests... [ Info: ********* EGADSLITE version 1.25 OCC (lite version) ********* Test Summary: | Pass Total Time Julia egadslite API: unit testing | 41 41 1.3s 1.406653 seconds (925.02 k allocations: 58.126 MiB, 3.33% gc time, 94.88% compilation time) Testing egadslite tests passed ++ cd /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/CAPS ++ make unit ++ tee -a capsUnit.txt (cd src; make) make[1]: Nothing to be done for `default'. (cd aim; make) /Library/Developer/CommandLineTools/usr/bin/make -C utils make[2]: Nothing to be done for `default'. /Library/Developer/CommandLineTools/usr/bin/make -C abaqus make[2]: `/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/abaqusAIM.so' is up to date. /Library/Developer/CommandLineTools/usr/bin/make -C aflr2 make[2]: Nothing to be done for `default'. /Library/Developer/CommandLineTools/usr/bin/make -C aflr3 make[2]: Nothing to be done for `default'. /Library/Developer/CommandLineTools/usr/bin/make -C aflr4 make[2]: Nothing to be done for `default'. /Library/Developer/CommandLineTools/usr/bin/make -C astros make[2]: `/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/astrosAIM.so' is up to date. /Library/Developer/CommandLineTools/usr/bin/make -C avl make[2]: `/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/avlAIM.so' is up to date. /Library/Developer/CommandLineTools/usr/bin/make -C awave make[2]: Nothing to be done for `default'. /Library/Developer/CommandLineTools/usr/bin/make -C cart3d make[2]: Nothing to be done for `default'. /Library/Developer/CommandLineTools/usr/bin/make -C cbaero make[2]: Nothing to be done for `default'. /Library/Developer/CommandLineTools/usr/bin/make -C cgt make[2]: `/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/test/egads2cgt' is up to date. /Library/Developer/CommandLineTools/usr/bin/make -C custom make[2]: Nothing to be done for `default'. /Library/Developer/CommandLineTools/usr/bin/make -C delaundo make[2]: `/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/delaundoAIM.so' is up to date. /Library/Developer/CommandLineTools/usr/bin/make -C egadsTess make[2]: `/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/egadsTessAIM.so' is up to date. /Library/Developer/CommandLineTools/usr/bin/make -C friction make[2]: Nothing to be done for `default'. /Library/Developer/CommandLineTools/usr/bin/make -C fun3d make[2]: `/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/fun3dAIM.so' is up to date. /Library/Developer/CommandLineTools/usr/bin/make -C hsm make[2]: Nothing to be done for `default'. /Library/Developer/CommandLineTools/usr/bin/make -C interference make[2]: `/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/interferenceAIM.so' is up to date. /Library/Developer/CommandLineTools/usr/bin/make -C jfd3 make[2]: `/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/jfd3AIM.so' is up to date. /Library/Developer/CommandLineTools/usr/bin/make -C masstran make[2]: Nothing to be done for `default'. /Library/Developer/CommandLineTools/usr/bin/make -C meshWriter /Library/Developer/CommandLineTools/usr/bin/make -C bstlWriter make[3]: Nothing to be done for `default'. /Library/Developer/CommandLineTools/usr/bin/make -C bvtkWriter make[3]: Nothing to be done for `default'. /Library/Developer/CommandLineTools/usr/bin/make -C exodusWriter make[3]: Nothing to be done for `default'. /Library/Developer/CommandLineTools/usr/bin/make -C fastWriter make[3]: Nothing to be done for `default'. /Library/Developer/CommandLineTools/usr/bin/make -C libmeshbWriter make[3]: Nothing to be done for `default'. /Library/Developer/CommandLineTools/usr/bin/make -C stlWriter make[3]: Nothing to be done for `default'. /Library/Developer/CommandLineTools/usr/bin/make -C su2Writer make[3]: Nothing to be done for `default'. /Library/Developer/CommandLineTools/usr/bin/make -C tecplotWriter make[3]: Nothing to be done for `default'. /Library/Developer/CommandLineTools/usr/bin/make -C ugridWriter make[3]: Nothing to be done for `default'. /Library/Developer/CommandLineTools/usr/bin/make -C vtkWriter make[3]: Nothing to be done for `default'. /Library/Developer/CommandLineTools/usr/bin/make -C mses make[2]: `/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/msesAIM.so' is up to date. /Library/Developer/CommandLineTools/usr/bin/make -C mystran make[2]: `/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/mystranAIM.so' is up to date. /Library/Developer/CommandLineTools/usr/bin/make -C nastran make[2]: `/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/nastranAIM.so' is up to date. /Library/Developer/CommandLineTools/usr/bin/make -C plato Not compiling platoAIM: SEACAS must be set -- Please fix the environment.... /Library/Developer/CommandLineTools/usr/bin/make -C pointwise make[2]: Nothing to be done for `default'. /Library/Developer/CommandLineTools/usr/bin/make -C refine make[2]: `/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/refineAIM.so' is up to date. /Library/Developer/CommandLineTools/usr/bin/make -C sierraSD Not compiling sierraSDAIM: SEACAS must be set -- Please fix the environment.... /Library/Developer/CommandLineTools/usr/bin/make -C sierraSM Not compiling sierraSMAIM: SEACAS must be set -- Please fix the environment.... /Library/Developer/CommandLineTools/usr/bin/make -C skeleton make[2]: `/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/skeletonAIM.so' is up to date. /Library/Developer/CommandLineTools/usr/bin/make -C spinnaker make[2]: Nothing to be done for `default'. /Library/Developer/CommandLineTools/usr/bin/make -C su2 make[2]: `/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/su2AIM.so' is up to date. /Library/Developer/CommandLineTools/usr/bin/make -C tacs make[2]: `/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/tacsAIM.so' is up to date. /Library/Developer/CommandLineTools/usr/bin/make -C tetgen make[2]: Nothing to be done for `default'. /Library/Developer/CommandLineTools/usr/bin/make -C tsfoil make[2]: `/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/tsfoilAIM.so' is up to date. /Library/Developer/CommandLineTools/usr/bin/make -C unitTest make[2]: Nothing to be done for `all'. /Library/Developer/CommandLineTools/usr/bin/make -C xfoil make[2]: `/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/lib/xfoilAIM.so' is up to date. /Library/Developer/CommandLineTools/usr/bin/make -C zaero make[2]: Nothing to be done for `default'. (cd Slugs/src; make) make[1]: Nothing to be done for `all'. (cd test; make -f aim.make) make[1]: Nothing to be done for `default'. (cd test; make -f autoExec.make) make[1]: Nothing to be done for `default'. (cd test; make -f newPhase.make) make[1]: `/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/test/newPhase' is up to date. (cd test; make -f basic.make) make[1]: `/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/test/basic' is up to date. (cd test; make -f geomIn.make) make[1]: `/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/test/geomIn' is up to date. (cd test; make -f utilsTest.make) make[1]: Nothing to be done for `default'. (cd test; make -f vVS.make) make[1]: `/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/test/vVS' is up to date. (cd examples; make) (make -C cCAPS -f aeroelastic_SU2.make) make[2]: `/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/examples/cCAPS/aeroelasticSimple_Iterative_SU2_and_MystranTest' is up to date. (make -C cCAPS -f avlTest.make) make[2]: `/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/examples/cCAPS/avlTest' is up to date. (make -C cCAPS -f awaveTest.make) make[2]: `/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/examples/cCAPS/awaveTest' is up to date. (make -C cCAPS -f frictionTest.make) make[2]: `/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/examples/cCAPS/frictionTest' is up to date. (make -C cCAPS -f fun3d.make) make[2]: Nothing to be done for `fun3d'. (make -C cCAPS -f hsm.make) make[2]: `hsm' is up to date. (make -C cCAPS -f interferenceTest.make) make[2]: `/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/examples/cCAPS/interferenceTest' is up to date. (make -C cCAPS -f msesTest.make) make[2]: `/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/examples/cCAPS/msesTest' is up to date. (make -C cCAPS -f mystran.make) make[2]: `/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/examples/cCAPS/mystranTest' is up to date. (make -C cCAPS -f pointwiseTest.make) make[2]: `/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/examples/cCAPS/pointwiseTest' is up to date. /Library/Developer/CommandLineTools/usr/bin/make -C pyCAPS/unitTest test python --version Python 3.11.5 python -u -m unittest discover ..Mapping Csys attributes ................ Number of unique Csys attributes = 2 Name = leftWingSkin, index = 1 Name = riteWingSkin, index = 2 Getting FEA coordinate systems....... Number of coordinate systems - 2 Coordinate system name - leftWingSkin Coordinate system name - riteWingSkin Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 1 Name = Upper_Left, index = 1 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing1, index = 1 Name = Wing2, index = 2 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 143 Number of elements = 282 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 282 Elemental Quad4 = 0 Setting FEA Data Mesh for body = 1 Number of nodal coordinates = 155 Number of elements = 306 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 306 Elemental Quad4 = 0 Combining multiple FEA meshes! Combined Number of nodal coordinates = 298 Combined Number of elements = 588 Combined Elemental Nodes = 0 Combined Elemental Rods = 0 Combined Elemental Tria3 = 588 Combined Elemental Quad4 = 0 Getting FEA materials....... Number of materials - 2 Material name - madeupium Material name - unobtainium Done getting FEA materials Getting FEA properties....... Number of properties - 2 Property name - Wing1 Property name - Wing2 Done getting FEA properties Updating mesh element types based on properties input ... EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! ..Writing D3 Javascript library - d3.v3.min.js ........... EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! .. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! . EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! No analysis directory provided - defaulting to altName Mapping Csys attributes ................ Number of unique Csys attributes = 2 Name = leftWingSkin, index = 1 Name = riteWingSkin, index = 2 Getting FEA coordinate systems....... Number of coordinate systems - 2 Coordinate system name - leftWingSkin Coordinate system name - riteWingSkin Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 1 Name = Upper_Left, index = 1 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing1, index = 1 Name = Wing2, index = 2 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 209 Number of elements = 414 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 414 Elemental Quad4 = 0 Setting FEA Data Mesh for body = 1 Number of nodal coordinates = 186 Number of elements = 368 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 368 Elemental Quad4 = 0 Combining multiple FEA meshes! Combined Number of nodal coordinates = 395 Combined Number of elements = 782 Combined Elemental Nodes = 0 Combined Elemental Rods = 0 Combined Elemental Tria3 = 782 Combined Elemental Quad4 = 0 Getting FEA materials....... Number of materials - 2 Material name - madeupium Material name - unobtainium Done getting FEA materials Getting FEA properties....... Number of properties - 2 Property name - Wing1 Property name - Wing2 Done getting FEA properties Updating mesh element types based on properties input ..........--> Opening DESPMTR file "unitGeom.param" updating CFGPMTR series [ 1, 1] = 8412.000000 updating CFGPMTR series2 [ 1, 1] = 20.000000 updating CFGPMTR VIEW:CFD [ 1, 1] = 1.000000 updating CFGPMTR nrow [ 1, 1] = 3.000000 updating CFGPMTR ncol [ 1, 1] = 2.000000 updating DESPMTR area [ 1, 1] = 40.000000 updating DESPMTR aspect [ 1, 1] = 5.000000 updating DESPMTR taper [ 1, 1] = 0.500000 updating DESPMTR twist [ 1, 1] = 15.000000 updating DESPMTR wing:lesweep [ 1, 1] = 30.000000 updating DESPMTR wing:dihedral [ 1, 1] = 1.000000 updating DESPMTR wing:chord:root [ 1, 1] = 1.560000 updating DESPMTR htail [ 1, 1] = 1.000000 updating DESPMTR htail:chord [ 1, 1] = 2.000000 updating DESPMTR vtail:chord [ 1, 1] = 3.000000 updating DESPMTR vtail [ 1, 1] = 4.000000 updating DESPMTR sphereR [ 1, 1] = 80.000000 updating DESPMTR v@1:d_name [ 1, 1] = 1.000000 updating DESPMTR despMat [ 1, 1] = 11.000000 updating DESPMTR despMat [ 1, 2] = 12.000000 updating DESPMTR despMat [ 2, 1] = 13.000000 updating DESPMTR despMat [ 2, 2] = 14.000000 updating DESPMTR despMat [ 3, 1] = 15.000000 updating DESPMTR despMat [ 3, 2] = 16.000000 updating DESPMTR despCol [ 1, 1] = 11.000000 updating DESPMTR despCol [ 2, 1] = 13.000000 updating DESPMTR despCol [ 3, 1] = 15.000000 updating DESPMTR despRow [ 1, 1] = 11.000000 updating DESPMTR despRow [ 1, 2] = 12.000000 updating DESPMTR despRow [ 1, 3] = 13.000000 ERROR:: DESPMTR file "unitGeom.param" not found CAPS Error: ocsmSaveDespmtrs = -201 (caps_readParameters)! EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! .. EGADS Error: No Attribute -> __numRemaining__ (EG_attributeDel)! EGADS Error: No Attribute -> __numRemaining__ (EG_attributeDel)! EGADS Error: No Attribute -> _body (EG_attributeDel)! EGADS Error: No Attribute -> _nface (EG_attributeDel)! EGADS Error: No Attribute -> __trace__ (EG_attributeDel)! EGADS Error: No Attribute -> _body (EG_attributeDel)! EGADS Error: No Attribute -> _nface (EG_attributeDel)! EGADS Error: No Attribute -> __trace__ (EG_attributeDel)! EGADS Error: No Attribute -> _body (EG_attributeDel)! EGADS Error: No Attribute -> _nface (EG_attributeDel)! EGADS Error: No Attribute -> __trace__ (EG_attributeDel)! EGADS Error: No Attribute -> _body (EG_attributeDel)! EGADS Error: No Attribute -> _nface (EG_attributeDel)! EGADS Error: No Attribute -> __trace__ (EG_attributeDel)! . EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! .. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! . EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! . EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! ..Linked Parameter Beta to analysis su2 input Beta Linked Parameter Alpha to analysis su2 input Alpha No linkable data found for Altitude No linkable data found for Strings No linkable data found for Strings2 Linked Parameter Beta to analysis su2 input Beta Linked Parameter Alpha to analysis su2 input Alpha ............ EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! . EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! . EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! .. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! . EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! . EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! .. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! CAPS Info: Hit last success -- going live! .... EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! .. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! .. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! .. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! . EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! ... EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! . EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! . EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! . EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! . EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! . EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! . EGADS Error: No Attribute -> __numRemaining__ (EG_attributeDel)! EGADS Error: No Attribute -> _body (EG_attributeDel)! EGADS Error: No Attribute -> _nface (EG_attributeDel)! EGADS Error: No Attribute -> __trace__ (EG_attributeDel)! EGADS Error: No Attribute -> _body (EG_attributeDel)! EGADS Error: No Attribute -> _nface (EG_attributeDel)! EGADS Error: No Attribute -> __trace__ (EG_attributeDel)! EGADS Error: No Attribute -> _body (EG_attributeDel)! EGADS Error: No Attribute -> _nface (EG_attributeDel)! EGADS Error: No Attribute -> __trace__ (EG_attributeDel)! EGADS Error: No Attribute -> _body (EG_attributeDel)! EGADS Error: No Attribute -> _nface (EG_attributeDel)! EGADS Error: No Attribute -> __trace__ (EG_attributeDel)! EGADS Error: No Attribute -> __numRemaining__ (EG_attributeDel)! .. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! --> Opening DESPMTR file "unitGeom.param" updating CFGPMTR series [ 1, 1] = 8412.000000 updating CFGPMTR series2 [ 1, 1] = 20.000000 updating CFGPMTR VIEW:CFD [ 1, 1] = 1.000000 updating CFGPMTR nrow [ 1, 1] = 3.000000 updating CFGPMTR ncol [ 1, 1] = 2.000000 updating DESPMTR area [ 1, 1] = 40.000000 updating DESPMTR aspect [ 1, 1] = 5.000000 updating DESPMTR taper [ 1, 1] = 0.500000 updating DESPMTR twist [ 1, 1] = 15.000000 updating DESPMTR wing:lesweep [ 1, 1] = 30.000000 updating DESPMTR wing:dihedral [ 1, 1] = 1.000000 updating DESPMTR wing:chord:root [ 1, 1] = 1.560000 updating DESPMTR htail [ 1, 1] = 1.000000 updating DESPMTR htail:chord [ 1, 1] = 2.000000 updating DESPMTR vtail:chord [ 1, 1] = 3.000000 updating DESPMTR vtail [ 1, 1] = 4.000000 updating DESPMTR sphereR [ 1, 1] = 80.000000 updating DESPMTR v@1:d_name [ 1, 1] = 1.000000 updating DESPMTR despMat [ 1, 1] = 11.000000 updating DESPMTR despMat [ 1, 2] = 12.000000 updating DESPMTR despMat [ 2, 1] = 13.000000 updating DESPMTR despMat [ 2, 2] = 14.000000 updating DESPMTR despMat [ 3, 1] = 15.000000 updating DESPMTR despMat [ 3, 2] = 16.000000 updating DESPMTR despCol [ 1, 1] = 11.000000 updating DESPMTR despCol [ 2, 1] = 13.000000 updating DESPMTR despCol [ 3, 1] = 15.000000 updating DESPMTR despRow [ 1, 1] = 11.000000 updating DESPMTR despRow [ 1, 2] = 12.000000 updating DESPMTR despRow [ 1, 3] = 13.000000 ERROR:: DESPMTR file "unitGeom.param" not found CAPS Error: ocsmSaveDespmtrs = -201 (caps_readParameters)! . EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! . EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! . EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! ............... EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! ---------------------------------------------------------------------- Ran 100 tests in 191.253s OK 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.setAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'! WARNING: 'capsGeometry.setGeometryVal' is deprecated. Please use 'Problem.geometry.despmtr["varname"].value'! WARNING: 'capsAnalysis.getAnalysisOutVal' is deprecated. Please use 'Analysis.output["varname"].value'! WARNING: 'capsProblem.__init__' is deprecated. Please use 'Problem.__init__'! /Library/Developer/CommandLineTools/usr/bin/make -C legacy/unitTest test python --version Python 3.11.5 python -u -m unittest discover ......sAnalysis Info: Name = UnitTest_fun3dAIM Intent = None AnalysisDir = /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/CAPS/legacy/unitTest/basicTest/Scratch/UnitTest_fun3dAIM Version = 1.25 Execution Flag = 0 Number of Fields = 8 Field name (Rank): Pressure ( 1 ) P ( 1 ) Cp ( 1 ) CoefficientOfPressure ( 1 ) Temperature ( 1 ) Displacement ( 3 ) EigenVector ( 3 ) EigenVector_# ( 3 ) Dirty state = 3 - Both analysis and geometry inputs are dirty Analysis Info: Name = UnitTest_fun3dAIM Intent = None AnalysisDir = /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/CAPS/legacy/unitTest/basicTest/Scratch/UnitTest_fun3dAIM Version = 1.25 Execution Flag = 0 Number of Fields = 8 Field name (Rank): Pressure ( 1 ) P ( 1 ) Cp ( 1 ) CoefficientOfPressure ( 1 ) Temperature ( 1 ) .Displacement ( 3 ) EigenVector ( 3 ) EigenVector_# ( 3 ) Dirty state = 3 - Both analysis and geometry inputs are dirty Analysis object with the name, fun3dAIM, has already been initilized An altName of fun3dAIM_1 will be used! Analysis object with the name, fun3dAIM, has already been initilized An altName of fun3dAIM_2 will be used! Analysis Info: Name = UnitTest7_fun3dAIM Intent = None AnalysisDir = /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/CAPS/legacy/unitTest/basicTest/Scratch/UnitTest7_fun3dAIM Version = 1.25 Execution Flag = 0 Number of Fields = 8 Field name (Rank): Pressure ( 1 ) P ( 1 ) Cp ( 1 ) CoefficientOfPressure ( 1 ) Temperature ( 1 ) Displacement ( 3 ) EigenVector ( 3 ) EigenVector_# ( 3 ) Dirty state = 3 - Both analysis and geometry inputs are dirty Analysis object with the name, fun3dAIM, has already been initilized An altName of fun3dAIM_3 will be used! Analysis Info: Name = UnitTest8_fun3dAIM Intent = None AnalysisDir = /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/CAPS/legacy/unitTest/basicTest/Scratch/UnitTest8_fun3dAIM Version = 1.25 Execution Flag = 0 Number of Fields = 8 Field name (Rank): Pressure ( 1 ) P ( 1 ) Cp ( 1 ) CoefficientOfPressure ( 1 ) Temperature ( 1 ) Displacement ( 3 ) EigenVector ( 3 ) EigenVector_# ( 3 ) Dirty state = 3 - Both analysis and geometry inputs are dirty Analysis object with the name, fun3dAIM, has already been initilized An altName of fun3dAIM_4 will be used! Analysis Info: Name = UnitTest9_fun3dAIM Intent = STRUCTURE AnalysisDir = /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/CAPS/legacy/unitTest/basicTest/Scratch/UnitTest9_fun3dAIM Version = 1.25 Execution Flag = 0 Number of Fields = 8 Field name (Rank): Pressure ( 1 ) P ( 1 ) Cp ( 1 ) CoefficientOfPressure ( 1 ) Temperature ( 1 ) Displacement ( 3 ) EigenVector ( 3 ) EigenVector_# ( 3 ) Dirty state = 3 - Both analysis and geometry inputs are dirty Analysis object with the name, fun3dAIM, has already been initilized An altName of fun3dAIM_5 will be used! Analysis Info: Name = UnitTest10_fun3dAIM Intent = ['CFD', 'STRUCTURE'] AnalysisDir = /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/CAPS/legacy/unitTest/basicTest/Scratch/UnitTest10_fun3dAIM Version = 1.25 Execution Flag = 0 Number of Fields = 8 Field name (Rank): Pressure ( 1 ) P ( 1 ) Cp ( 1 ) CoefficientOfPressure ( 1 ) Temperature ( 1 ) Displacement ( 3 ) EigenVector ( 3 ) EigenVector_# ( 3 ) Dirty state = 3 - Both analysis and geometry inputs are dirty ...Error: Invalid attribute level! Defaulting to 'Face' .. Analysis object with the name, fun3dAIM, has already been initilized An altName of fun3dAIM_6 will be used! . Analysis object with the name, fun3dAIM, has already been initilized An altName of fun3dAIM_7 will be used! . Analysis object with the name, fun3dAIM, has already been initilized An altName of fun3dAIM_8 will be used! . Analysis object with the name, fun3dAIM, has already been initilized An altName of fun3dAIM_9 will be used! Analysis object with the name, egadsTessAIM, has already been initilized An altName of egadsTessAIM_1 will be used! . Analysis object with the name, fun3dAIM, has already been initilized An altName of fun3dAIM_10 will be used! Analysis object with the name, egadsTessAIM, has already been initilized An altName of egadsTessAIM_2 will be used! . Analysis object with the name, fun3dAIM, has already been initilized An altName of fun3dAIM_11 will be used! Analysis object with the name, egadsTessAIM, has already been initilized An altName of egadsTessAIM_3 will be used! . Analysis object with the name, fun3dAIM, has already been initilized An altName of fun3dAIM_12 will be used! . Analysis object with the name, fun3dAIM, has already been initilized An altName of fun3dAIM_13 will be used! ...No data transfer method (transferMethod) provided - defaulting to "Interpolate" No data transfer method (transferMethod) provided - defaulting to "Interpolate" .No data transfer method (transferMethod) provided - defaulting to "Interpolate" ....No data transfer method (transferMethod) provided - defaulting to "Interpolate" .No data transfer method (transferMethod) provided - defaulting to "Interpolate" . EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! .s.. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! ..Error: Invalid attribute level! Defaulting to 'Face' ........ EGADS Error: No Attribute -> __numRemaining__ (EG_attributeDel)! EGADS Error: No Attribute -> _body (EG_attributeDel)! EGADS Error: No Attribute -> _nface (EG_attributeDel)! EGADS Error: No Attribute -> __trace__ (EG_attributeDel)! EGADS Error: No Attribute -> _body (EG_attributeDel)! EGADS Error: No Attribute -> _nface (EG_attributeDel)! EGADS Error: No Attribute -> __trace__ (EG_attributeDel)! EGADS Error: No Attribute -> _body (EG_attributeDel)! EGADS Error: No Attribute -> _nface (EG_attributeDel)! EGADS Error: No Attribute -> __trace__ (EG_attributeDel)! EGADS Error: No Attribute -> _body (EG_attributeDel)! EGADS Error: No Attribute -> _nface (EG_attributeDel)! EGADS Error: No Attribute -> __trace__ (EG_attributeDel)! .... EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! .s..... EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! .Linked Parameter Beta to analysis fun3d input Beta Linked Parameter Alpha to analysis fun3d input Alpha Mapping Csys attributes ................ Number of unique Csys attributes = 2 Name = leftWingSkin, index = 1 Name = riteWingSkin, index = 2 Getting FEA coordinate systems....... Number of coordinate systems - 2 Coordinate system name - leftWingSkin Coordinate system name - riteWingSkin Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 1 Name = Upper_Left, index = 1 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing1, index = 1 Name = Wing2, index = 2 70000EE73000 Odd Degenerate test for side 1: 9! 70000EE73000 Odd Degenerate test for side 2: 9! Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 395 Number of elements = 786 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 786 Elemental Quad4 = 0 1110FAE00 Odd Degenerate test for side 1: 9! 1110FAE00 Odd Degenerate test for side 2: 9! Setting FEA Data Mesh for body = 1 Number of nodal coordinates = 623 Number of elements = 1242 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 1242 Elemental Quad4 = 0 Combining multiple FEA meshes! Combined Number of nodal coordinates = 1018 Combined Number of elements = 2028 Combined Elemental Nodes = 0 Combined Elemental Rods = 0 Combined Elemental Tria3 = 2028 Combined Elemental Quad4 = 0 Getting FEA materials....... Number of materials - 2 Material name - madeupium Material name - unobtainium Done getting FEA materials Getting FEA properties....... Number of properties - 2 Property name - Wing1 Property name - Wing2 Done getting FEA properties Updating mesh element types based on properties input ................ ---------------------------------------------------------------------- Ran 72 tests in 102.642s OK (skipped=3) 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.setAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'! WARNING: 'capsAnalysis.getAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'! WARNING: 'capsAnalysis.addAttribute' is deprecated. Please use 'Analysis.attr.create'! WARNING: 'capsAnalysis.getAttribute' is deprecated. Please use 'Analysis.attr["name"].value'! WARNING: 'capsAnalysis.getAnalysisInfo' is deprecated. Please use 'Analysis.info'! WARNING: 'capsAnalysis.getAnalysisOutVal' is deprecated. Please use 'Analysis.output["varname"].value'! WARNING: 'capsAnalysis.getAttributeVal' is deprecated. Please use 'Analysis.geometry.attrList'! WARNING: 'capsAnalysis.getBoundingBox' is deprecated. Please use 'Analysis.bodies'! WARNING: 'capsAnalysis.aimName' is deprecated. Please use 'name'! WARNING: 'capsAnalysis.saveGeometry' is deprecated. Please use 'Analysis.geometry.save'! WARNING: 'capsProblem.closeCAPS' is deprecated. Please use 'close'! WARNING: 'capsGeometry.setGeometryVal' is deprecated. Please use 'Problem.geometry.despmtr["varname"].value'! WARNING: 'capsGeometry.buildGeometry' is deprecated. Please use 'Problem.geometry.build'! WARNING: 'capsGeometry.getAttributeMap' is deprecated. Please use 'Problem.geometry.attrMap'! WARNING: 'capsGeometry.getAttributeVal' is deprecated. Please use 'Problem.geometry.attrList'! WARNING: 'capsGeometry.getBoundingBox' is deprecated. Please use 'Problem.geometry.bodies'! WARNING: 'capsGeometry.getGeometryOutVal' is deprecated. Please use 'Problem.geometry.outpmtr["varname"].value'! WARNING: 'capsGeometry.getGeometryVal' is deprecated. Please use 'Problem.geometry.despmtr["varname"].value'! WARNING: 'capsGeometry.saveGeometry' is deprecated. Please use 'Problem.geometry.save'! WARNING: 'capsGeometry.viewGeometry' is deprecated. Please use 'Problem.geometry.view'! WARNING: 'capsProblem.addAttribute' is deprecated. Please use 'Problem.attr.create'! WARNING: 'capsProblem.getAttribute' is deprecated. Please use 'Problem.attr["name"].value'! WARNING: 'capsProblem.createValue' is deprecated. Please use 'Problem.parameter.create'! WARNING: '_capsValue.__init__' is deprecated. Please use 'Problem.parameter.create'! WARNING: 'capsProblem.setVerbosity' is deprecated. Please use 'Problem.setOutLevel'! WARNING: 'capsProblem.autoLinkValue' is deprecated. Please use 'Problem.autoLinkParameter'! Legacy pyCAPS unit testing done! /Library/Developer/CommandLineTools/usr/bin/make -C aim/skeleton test python -u case.py Loading file into our Problem Default num = 8.0 Current num = 16.0 aim_newGeometry = 0! GeometryIn: 1: num 2 (1,1) 2: x 2 (8,1) 3: ymin 2 (8,1) 4: zmin 2 (8,1) 5: zmax 2 (8,1) GeometryOut: 1: pVol 6 (1,1) 2: cVol 6 (1,1) AnalysisIn: 1: InputVariable 0 (1,1) (null) 2: num 2 (1,1) (null) 3: Mach 2 (1,1) (null) 4: Mesh_Format 3 (1,1) (null) 5: Table 4 (1,3) (null) Computed sqrtNum = 4.0 /Library/Developer/CommandLineTools/usr/bin/make -C aim/unitTest/pyCAPS test python --version Python 3.11.5 python -u -m unittest discover --verbose test_journal (test_aflr2.TestAFLR2.test_journal) ... Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 5 Name = 2DSlice, index = 1 Name = TunnelWall, index = 2 Name = OutFlow, index = 3 Name = InFlow, index = 4 Name = Airfoil, index = 5 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = TunnelWall, index = 1 Name = OutFlow, index = 2 Name = InFlow, index = 3 Name = Airfoil, index = 4 Getting 2D mesh for body 1 (of 1) AFLR2 : --------------------------------------- AFLR2 : AFLR2 LIBRARY AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR2 : TRIA/QUAD GRID GENERATOR AFLR2 : Version Number 9.17.15 AFLR2 : Version Date 04/23/24 @ 12:51AM AFLR2 : Compile OS Darwin 23.4.0 x86_64 AFLR2 : Compile Date 04/23/24 @ 11:49AM AFLR2 : Copyright 1994-2021, D.L. Marcum AFLR2 : --------------------------------------- AFLR2 IC : INPUT DATA CHECK AFLR2 IC : Nodes, Faces = 2244 0 AFLR2 : CPU Time = 0.000 seconds AFLR2 EG : EDGE GRID RE-GENERATION AFLR2 EG : Nodes, Edges = 2244 2244 AFLR2 : CPU Time = 0.000 seconds AFLR2 IG : INITIAL GRID GENERATION AFLR2 IG : Nodes, Faces = 0 2 AFLR2 IG : Nodes, Faces = 450 902 AFLR2 IG : Nodes, Faces = 900 1802 AFLR2 IG : Nodes, Faces = 1145 2292 AFLR2 IG : Nodes, Faces = 1260 2522 AFLR2 IG : Nodes, Faces = 1350 2702 AFLR2 IG : Nodes, Faces = 1360 2722 AFLR2 IG : Nodes, Faces = 1460 2922 AFLR2 IG : Nodes, Faces = 1560 3122 AFLR2 IG : Nodes, Faces = 1660 3322 AFLR2 IG : Nodes, Faces = 1760 3522 AFLR2 IG : Nodes, Faces = 1800 3602 AFLR2 IG : Nodes, Faces = 1860 3722 AFLR2 IG : Nodes, Faces = 1960 3922 AFLR2 IG : Nodes, Faces = 2060 4122 AFLR2 IG : Nodes, Faces = 2085 4172 AFLR2 IG : Nodes, Faces = 2244 4490 AFLR2 IG : Nodes, Faces = 2248 4490 AFLR2 IG : Nodes, Faces = 2244 2244 AFLR2 : CPU Time = 0.037 seconds AFLR2 GG : FIELD GRID GENERATION AFLR2 GG : Nodes, Faces = 2244 2244 AFLR2 GG : Nodes, Faces = 4283 6322 AFLR2 GG : Nodes, Faces = 6128 10012 AFLR2 GG : Nodes, Faces = 7863 13482 AFLR2 GG : Nodes, Faces = 9464 16684 AFLR2 GG : Nodes, Faces = 10948 19652 AFLR2 GG : Nodes, Faces = 12322 22400 AFLR2 GG : Nodes, Faces = 13619 24994 AFLR2 GG : Nodes, Faces = 14829 27414 AFLR2 GG : Nodes, Faces = 15981 29718 AFLR2 GG : Nodes, Faces = 17082 31920 AFLR2 GG : Nodes, Faces = 18110 33976 AFLR2 GG : Nodes, Faces = 19081 35918 AFLR2 GG : Nodes, Faces = 20014 37784 AFLR2 GG : Nodes, Faces = 20924 39604 AFLR2 GG : Nodes, Faces = 21782 41320 AFLR2 GG : Nodes, Faces = 22595 42946 AFLR2 GG : Nodes, Faces = 23377 44510 AFLR2 GG : Nodes, Faces = 24129 46014 AFLR2 GG : Nodes, Faces = 24840 47436 AFLR2 GG : Nodes, Faces = 25522 48800 AFLR2 GG : Nodes, Faces = 26170 50096 AFLR2 GG : Nodes, Faces = 26793 51342 AFLR2 GG : Nodes, Faces = 27346 52448 AFLR2 GG : Nodes, Faces = 27846 53448 AFLR2 GG : Nodes, Faces = 28280 54316 AFLR2 GG : Nodes, Faces = 28652 55060 AFLR2 GG : Nodes, Faces = 28920 55596 AFLR2 GG : Nodes, Faces = 29143 56042 AFLR2 GG : Nodes, Faces = 29358 56472 AFLR2 GG : Nodes, Faces = 29550 56856 AFLR2 GG : Nodes, Faces = 29693 57142 AFLR2 GG : Nodes, Faces = 29805 57366 AFLR2 GG : Nodes, Faces = 29875 57506 AFLR2 GG : Nodes, Faces = 29895 57546 AFLR2 GG : Nodes, Faces = 29897 57550 AFLR2 : CPU Time = 0.110 seconds AFLR2 QI : QUALITY IMPROVEMENT AFLR2 QI : Nodes, Faces = 29897 57550 AFLR2 : CPU Time = 0.014 seconds AFLR2 : DONE Writing AFLR3 file .... Finished writing AFLR3 file Number of nodes = 29897 Number of elements = 59794 Number of tris = 57550 Number of quad = 0 Getting 2D mesh for body 1 (of 1) AFLR2 IC : INPUT DATA CHECK AFLR2 IC : Nodes, Faces = 2224 0 AFLR2 : CPU Time = 0.000 seconds AFLR2 EG : EDGE GRID RE-GENERATION AFLR2 EG : Nodes, Edges = 2224 2224 AFLR2 : CPU Time = 0.000 seconds AFLR2 IG : INITIAL GRID GENERATION AFLR2 IG : Nodes, Faces = 0 2 AFLR2 IG : Nodes, Faces = 446 894 AFLR2 IG : Nodes, Faces = 892 1786 AFLR2 IG : Nodes, Faces = 918 1838 AFLR2 IG : Nodes, Faces = 1033 2068 AFLR2 IG : Nodes, Faces = 1133 2268 AFLR2 IG : Nodes, Faces = 1233 2468 AFLR2 IG : Nodes, Faces = 1333 2668 AFLR2 IG : Nodes, Faces = 1338 2678 AFLR2 IG : Nodes, Faces = 1433 2868 AFLR2 IG : Nodes, Faces = 1533 3068 AFLR2 IG : Nodes, Faces = 1633 3268 AFLR2 IG : Nodes, Faces = 1733 3468 AFLR2 IG : Nodes, Faces = 1784 3570 AFLR2 IG : Nodes, Faces = 1833 3668 AFLR2 IG : Nodes, Faces = 1858 3718 AFLR2 IG : Nodes, Faces = 2224 4450 AFLR2 IG : Nodes, Faces = 2228 4450 AFLR2 IG : Nodes, Faces = 2224 2224 AFLR2 : CPU Time = 0.034 seconds AFLR2 GG : FIELD GRID GENERATION AFLR2 GG : Nodes, Faces = 2224 2224 AFLR2 GG : Nodes, Faces = 4122 6020 AFLR2 GG : Nodes, Faces = 5812 9400 AFLR2 GG : Nodes, Faces = 7299 12374 AFLR2 GG : Nodes, Faces = 8574 14924 AFLR2 GG : Nodes, Faces = 9729 17234 AFLR2 GG : Nodes, Faces = 10787 19350 AFLR2 GG : Nodes, Faces = 11767 21310 AFLR2 GG : Nodes, Faces = 12683 23142 AFLR2 GG : Nodes, Faces = 13516 24808 AFLR2 GG : Nodes, Faces = 14278 26332 AFLR2 GG : Nodes, Faces = 14999 27774 AFLR2 GG : Nodes, Faces = 15682 29140 AFLR2 GG : Nodes, Faces = 16312 30400 AFLR2 GG : Nodes, Faces = 16899 31574 AFLR2 GG : Nodes, Faces = 17451 32678 AFLR2 GG : Nodes, Faces = 17959 33694 AFLR2 GG : Nodes, Faces = 18443 34662 AFLR2 GG : Nodes, Faces = 18877 35530 AFLR2 GG : Nodes, Faces = 19283 36342 AFLR2 GG : Nodes, Faces = 19650 37076 AFLR2 GG : Nodes, Faces = 19994 37764 AFLR2 GG : Nodes, Faces = 20325 38426 AFLR2 GG : Nodes, Faces = 20638 39052 AFLR2 GG : Nodes, Faces = 20940 39656 AFLR2 GG : Nodes, Faces = 21240 40256 AFLR2 GG : Nodes, Faces = 21523 40822 AFLR2 GG : Nodes, Faces = 21792 41360 AFLR2 GG : Nodes, Faces = 22053 41882 AFLR2 GG : Nodes, Faces = 22305 42386 AFLR2 GG : Nodes, Faces = 22521 42818 AFLR2 GG : Nodes, Faces = 22696 43168 AFLR2 GG : Nodes, Faces = 22829 43434 AFLR2 GG : Nodes, Faces = 22953 43682 AFLR2 GG : Nodes, Faces = 23050 43876 AFLR2 GG : Nodes, Faces = 23110 43996 AFLR2 GG : Nodes, Faces = 23139 44054 AFLR2 GG : Nodes, Faces = 23157 44090 AFLR2 GG : Nodes, Faces = 23175 44126 AFLR2 GG : Nodes, Faces = 23183 44142 AFLR2 GG : Nodes, Faces = 23187 44150 AFLR2 : CPU Time = 0.099 seconds AFLR2 QI : QUALITY IMPROVEMENT AFLR2 QI : Nodes, Faces = 23187 44150 AFLR2 : CPU Time = 0.011 seconds AFLR2 : DONE Writing AFLR3 file .... Finished writing AFLR3 file Number of nodes = 23187 Number of elements = 46374 Number of tris = 44150 Number of quad = 0 EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 5 Name = 2DSlice, index = 1 Name = TunnelWall, index = 2 Name = OutFlow, index = 3 Name = InFlow, index = 4 Name = Airfoil, index = 5 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = TunnelWall, index = 1 Name = OutFlow, index = 2 Name = InFlow, index = 3 Name = Airfoil, index = 4 Getting 2D mesh for body 1 (of 1) AFLR2 : --------------------------------------- AFLR2 : AFLR2 LIBRARY AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR2 : TRIA/QUAD GRID GENERATOR AFLR2 : Version Number 9.17.15 AFLR2 : Version Date 04/23/24 @ 12:51AM AFLR2 : Compile OS Darwin 23.4.0 x86_64 AFLR2 : Compile Date 04/23/24 @ 11:49AM AFLR2 : Copyright 1994-2021, D.L. Marcum AFLR2 : --------------------------------------- AFLR2 IC : INPUT DATA CHECK AFLR2 IC : Nodes, Faces = 2244 0 AFLR2 : CPU Time = 0.000 seconds AFLR2 EG : EDGE GRID RE-GENERATION AFLR2 EG : Nodes, Edges = 2244 2244 AFLR2 : CPU Time = 0.001 seconds AFLR2 IG : INITIAL GRID GENERATION AFLR2 IG : Nodes, Faces = 0 2 AFLR2 IG : Nodes, Faces = 450 902 AFLR2 IG : Nodes, Faces = 900 1802 AFLR2 IG : Nodes, Faces = 1145 2292 AFLR2 IG : Nodes, Faces = 1260 2522 AFLR2 IG : Nodes, Faces = 1350 2702 AFLR2 IG : Nodes, Faces = 1360 2722 AFLR2 IG : Nodes, Faces = 1460 2922 AFLR2 IG : Nodes, Faces = 1560 3122 AFLR2 IG : Nodes, Faces = 1660 3322 AFLR2 IG : Nodes, Faces = 1760 3522 AFLR2 IG : Nodes, Faces = 1800 3602 AFLR2 IG : Nodes, Faces = 1860 3722 AFLR2 IG : Nodes, Faces = 1960 3922 AFLR2 IG : Nodes, Faces = 2060 4122 AFLR2 IG : Nodes, Faces = 2085 4172 AFLR2 IG : Nodes, Faces = 2244 4490 AFLR2 IG : Nodes, Faces = 2248 4490 AFLR2 IG : Nodes, Faces = 2244 2244 AFLR2 : CPU Time = 0.040 seconds AFLR2 GG : FIELD GRID GENERATION AFLR2 GG : Nodes, Faces = 2244 2244 AFLR2 GG : Nodes, Faces = 4283 6322 AFLR2 GG : Nodes, Faces = 6128 10012 AFLR2 GG : Nodes, Faces = 7863 13482 AFLR2 GG : Nodes, Faces = 9464 16684 AFLR2 GG : Nodes, Faces = 10948 19652 AFLR2 GG : Nodes, Faces = 12322 22400 AFLR2 GG : Nodes, Faces = 13619 24994 AFLR2 GG : Nodes, Faces = 14829 27414 AFLR2 GG : Nodes, Faces = 15981 29718 AFLR2 GG : Nodes, Faces = 17082 31920 AFLR2 GG : Nodes, Faces = 18110 33976 AFLR2 GG : Nodes, Faces = 19081 35918 AFLR2 GG : Nodes, Faces = 20014 37784 AFLR2 GG : Nodes, Faces = 20924 39604 AFLR2 GG : Nodes, Faces = 21782 41320 AFLR2 GG : Nodes, Faces = 22595 42946 AFLR2 GG : Nodes, Faces = 23377 44510 AFLR2 GG : Nodes, Faces = 24129 46014 AFLR2 GG : Nodes, Faces = 24840 47436 AFLR2 GG : Nodes, Faces = 25522 48800 AFLR2 GG : Nodes, Faces = 26170 50096 AFLR2 GG : Nodes, Faces = 26793 51342 AFLR2 GG : Nodes, Faces = 27346 52448 AFLR2 GG : Nodes, Faces = 27846 53448 AFLR2 GG : Nodes, Faces = 28280 54316 AFLR2 GG : Nodes, Faces = 28652 55060 AFLR2 GG : Nodes, Faces = 28920 55596 AFLR2 GG : Nodes, Faces = 29143 56042 AFLR2 GG : Nodes, Faces = 29358 56472 AFLR2 GG : Nodes, Faces = 29550 56856 AFLR2 GG : Nodes, Faces = 29693 57142 AFLR2 GG : Nodes, Faces = 29805 57366 AFLR2 GG : Nodes, Faces = 29875 57506 AFLR2 GG : Nodes, Faces = 29895 57546 AFLR2 GG : Nodes, Faces = 29897 57550 AFLR2 : CPU Time = 0.118 seconds AFLR2 QI : QUALITY IMPROVEMENT AFLR2 QI : Nodes, Faces = 29897 57550 AFLR2 : CPU Time = 0.011 seconds AFLR2 : DONE Writing AFLR3 file .... Finished writing AFLR3 file Number of nodes = 29897 Number of elements = 59794 Number of tris = 57550 Number of quad = 0 CAPS Info: Hit last success -- going live! Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 5 Name = 2DSlice, index = 1 Name = TunnelWall, index = 2 Name = OutFlow, index = 3 Name = InFlow, index = 4 Name = Airfoil, index = 5 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = TunnelWall, index = 1 Name = OutFlow, index = 2 Name = InFlow, index = 3 Name = Airfoil, index = 4 CAPS Info: Hit last success -- going live! Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 5 Name = 2DSlice, index = 1 Name = TunnelWall, index = 2 Name = OutFlow, index = 3 Name = InFlow, index = 4 Name = Airfoil, index = 5 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = TunnelWall, index = 1 Name = OutFlow, index = 2 Name = InFlow, index = 3 Name = Airfoil, index = 4 CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 5 Name = 2DSlice, index = 1 Name = TunnelWall, index = 2 Name = OutFlow, index = 3 Name = InFlow, index = 4 Name = Airfoil, index = 5 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = TunnelWall, index = 1 Name = OutFlow, index = 2 Name = InFlow, index = 3 Name = Airfoil, index = 4 Getting 2D mesh for body 1 (of 1) AFLR2 : --------------------------------------- AFLR2 : AFLR2 LIBRARY AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR2 : TRIA/QUAD GRID GENERATOR AFLR2 : Version Number 9.17.15 AFLR2 : Version Date 04/23/24 @ 12:51AM AFLR2 : Compile OS Darwin 23.4.0 x86_64 AFLR2 : Compile Date 04/23/24 @ 11:49AM AFLR2 : Copyright 1994-2021, D.L. Marcum AFLR2 : --------------------------------------- AFLR2 IC : INPUT DATA CHECK AFLR2 IC : Nodes, Faces = 2224 0 AFLR2 : CPU Time = 0.000 seconds AFLR2 EG : EDGE GRID RE-GENERATION AFLR2 EG : Nodes, Edges = 2224 2224 AFLR2 : CPU Time = 0.000 seconds AFLR2 IG : INITIAL GRID GENERATION AFLR2 IG : Nodes, Faces = 0 2 AFLR2 IG : Nodes, Faces = 446 894 AFLR2 IG : Nodes, Faces = 892 1786 AFLR2 IG : Nodes, Faces = 918 1838 AFLR2 IG : Nodes, Faces = 1033 2068 AFLR2 IG : Nodes, Faces = 1133 2268 AFLR2 IG : Nodes, Faces = 1233 2468 AFLR2 IG : Nodes, Faces = 1333 2668 AFLR2 IG : Nodes, Faces = 1338 2678 AFLR2 IG : Nodes, Faces = 1433 2868 AFLR2 IG : Nodes, Faces = 1533 3068 AFLR2 IG : Nodes, Faces = 1633 3268 AFLR2 IG : Nodes, Faces = 1733 3468 AFLR2 IG : Nodes, Faces = 1784 3570 AFLR2 IG : Nodes, Faces = 1833 3668 AFLR2 IG : Nodes, Faces = 1858 3718 AFLR2 IG : Nodes, Faces = 2224 4450 AFLR2 IG : Nodes, Faces = 2228 4450 AFLR2 IG : Nodes, Faces = 2224 2224 AFLR2 : CPU Time = 0.024 seconds AFLR2 GG : FIELD GRID GENERATION AFLR2 GG : Nodes, Faces = 2224 2224 AFLR2 GG : Nodes, Faces = 4122 6020 AFLR2 GG : Nodes, Faces = 5812 9400 AFLR2 GG : Nodes, Faces = 7299 12374 AFLR2 GG : Nodes, Faces = 8574 14924 AFLR2 GG : Nodes, Faces = 9729 17234 AFLR2 GG : Nodes, Faces = 10787 19350 AFLR2 GG : Nodes, Faces = 11767 21310 AFLR2 GG : Nodes, Faces = 12683 23142 AFLR2 GG : Nodes, Faces = 13516 24808 AFLR2 GG : Nodes, Faces = 14278 26332 AFLR2 GG : Nodes, Faces = 14999 27774 AFLR2 GG : Nodes, Faces = 15682 29140 AFLR2 GG : Nodes, Faces = 16312 30400 AFLR2 GG : Nodes, Faces = 16899 31574 AFLR2 GG : Nodes, Faces = 17451 32678 AFLR2 GG : Nodes, Faces = 17959 33694 AFLR2 GG : Nodes, Faces = 18443 34662 AFLR2 GG : Nodes, Faces = 18877 35530 AFLR2 GG : Nodes, Faces = 19283 36342 AFLR2 GG : Nodes, Faces = 19650 37076 AFLR2 GG : Nodes, Faces = 19994 37764 AFLR2 GG : Nodes, Faces = 20325 38426 AFLR2 GG : Nodes, Faces = 20638 39052 AFLR2 GG : Nodes, Faces = 20940 39656 AFLR2 GG : Nodes, Faces = 21240 40256 AFLR2 GG : Nodes, Faces = 21523 40822 AFLR2 GG : Nodes, Faces = 21792 41360 AFLR2 GG : Nodes, Faces = 22053 41882 AFLR2 GG : Nodes, Faces = 22305 42386 AFLR2 GG : Nodes, Faces = 22521 42818 AFLR2 GG : Nodes, Faces = 22696 43168 AFLR2 GG : Nodes, Faces = 22829 43434 AFLR2 GG : Nodes, Faces = 22953 43682 AFLR2 GG : Nodes, Faces = 23050 43876 AFLR2 GG : Nodes, Faces = 23110 43996 AFLR2 GG : Nodes, Faces = 23139 44054 AFLR2 GG : Nodes, Faces = 23157 44090 AFLR2 GG : Nodes, Faces = 23175 44126 AFLR2 GG : Nodes, Faces = 23183 44142 AFLR2 GG : Nodes, Faces = 23187 44150 AFLR2 : CPU Time = 0.055 seconds AFLR2 QI : QUALITY IMPROVEMENT AFLR2 QI : Nodes, Faces = 23187 44150 AFLR2 : CPU Time = 0.005 seconds AFLR2 : DONE Writing AFLR3 file .... Finished writing AFLR3 file Number of nodes = 23187 Number of elements = 46374 Number of tris = 44150 Number of quad = 0 CAPS Info: Hit last success -- going live! Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 5 Name = 2DSlice, index = 1 Name = TunnelWall, index = 2 Name = OutFlow, index = 3 Name = InFlow, index = 4 Name = Airfoil, index = 5 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = TunnelWall, index = 1 Name = OutFlow, index = 2 Name = InFlow, index = 3 Name = Airfoil, index = 4 ok test_phase (test_aflr2.TestAFLR2.test_phase) ... Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 5 Name = 2DSlice, index = 1 Name = TunnelWall, index = 2 Name = OutFlow, index = 3 Name = InFlow, index = 4 Name = Airfoil, index = 5 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = TunnelWall, index = 1 Name = OutFlow, index = 2 Name = InFlow, index = 3 Name = Airfoil, index = 4 Getting 2D mesh for body 1 (of 1) AFLR2 : --------------------------------------- AFLR2 : AFLR2 LIBRARY AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR2 : TRIA/QUAD GRID GENERATOR AFLR2 : Version Number 9.17.15 AFLR2 : Version Date 04/23/24 @ 12:51AM AFLR2 : Compile OS Darwin 23.4.0 x86_64 AFLR2 : Compile Date 04/23/24 @ 11:49AM AFLR2 : Copyright 1994-2021, D.L. Marcum AFLR2 : --------------------------------------- AFLR2 IC : INPUT DATA CHECK AFLR2 IC : Nodes, Faces = 2244 0 AFLR2 : CPU Time = 0.002 seconds AFLR2 EG : EDGE GRID RE-GENERATION AFLR2 EG : Nodes, Edges = 2244 2244 AFLR2 : CPU Time = 0.000 seconds AFLR2 IG : INITIAL GRID GENERATION AFLR2 IG : Nodes, Faces = 0 2 AFLR2 IG : Nodes, Faces = 450 902 AFLR2 IG : Nodes, Faces = 900 1802 AFLR2 IG : Nodes, Faces = 1145 2292 AFLR2 IG : Nodes, Faces = 1260 2522 AFLR2 IG : Nodes, Faces = 1350 2702 AFLR2 IG : Nodes, Faces = 1360 2722 AFLR2 IG : Nodes, Faces = 1460 2922 AFLR2 IG : Nodes, Faces = 1560 3122 AFLR2 IG : Nodes, Faces = 1660 3322 AFLR2 IG : Nodes, Faces = 1760 3522 AFLR2 IG : Nodes, Faces = 1800 3602 AFLR2 IG : Nodes, Faces = 1860 3722 AFLR2 IG : Nodes, Faces = 1960 3922 AFLR2 IG : Nodes, Faces = 2060 4122 AFLR2 IG : Nodes, Faces = 2085 4172 AFLR2 IG : Nodes, Faces = 2244 4490 AFLR2 IG : Nodes, Faces = 2248 4490 AFLR2 IG : Nodes, Faces = 2244 2244 AFLR2 : CPU Time = 0.050 seconds AFLR2 GG : FIELD GRID GENERATION AFLR2 GG : Nodes, Faces = 2244 2244 AFLR2 GG : Nodes, Faces = 4283 6322 AFLR2 GG : Nodes, Faces = 6128 10012 AFLR2 GG : Nodes, Faces = 7863 13482 AFLR2 GG : Nodes, Faces = 9464 16684 AFLR2 GG : Nodes, Faces = 10948 19652 AFLR2 GG : Nodes, Faces = 12322 22400 AFLR2 GG : Nodes, Faces = 13619 24994 AFLR2 GG : Nodes, Faces = 14829 27414 AFLR2 GG : Nodes, Faces = 15981 29718 AFLR2 GG : Nodes, Faces = 17082 31920 AFLR2 GG : Nodes, Faces = 18110 33976 AFLR2 GG : Nodes, Faces = 19081 35918 AFLR2 GG : Nodes, Faces = 20014 37784 AFLR2 GG : Nodes, Faces = 20924 39604 AFLR2 GG : Nodes, Faces = 21782 41320 AFLR2 GG : Nodes, Faces = 22595 42946 AFLR2 GG : Nodes, Faces = 23377 44510 AFLR2 GG : Nodes, Faces = 24129 46014 AFLR2 GG : Nodes, Faces = 24840 47436 AFLR2 GG : Nodes, Faces = 25522 48800 AFLR2 GG : Nodes, Faces = 26170 50096 AFLR2 GG : Nodes, Faces = 26793 51342 AFLR2 GG : Nodes, Faces = 27346 52448 AFLR2 GG : Nodes, Faces = 27846 53448 AFLR2 GG : Nodes, Faces = 28280 54316 AFLR2 GG : Nodes, Faces = 28652 55060 AFLR2 GG : Nodes, Faces = 28920 55596 AFLR2 GG : Nodes, Faces = 29143 56042 AFLR2 GG : Nodes, Faces = 29358 56472 AFLR2 GG : Nodes, Faces = 29550 56856 AFLR2 GG : Nodes, Faces = 29693 57142 AFLR2 GG : Nodes, Faces = 29805 57366 AFLR2 GG : Nodes, Faces = 29875 57506 AFLR2 GG : Nodes, Faces = 29895 57546 AFLR2 GG : Nodes, Faces = 29897 57550 AFLR2 : CPU Time = 0.163 seconds AFLR2 QI : QUALITY IMPROVEMENT AFLR2 QI : Nodes, Faces = 29897 57550 AFLR2 : CPU Time = 0.010 seconds AFLR2 : DONE Writing AFLR3 file .... Finished writing AFLR3 file Number of nodes = 29897 Number of elements = 59794 Number of tris = 57550 Number of quad = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 5 Name = 2DSlice, index = 1 Name = TunnelWall, index = 2 Name = OutFlow, index = 3 Name = InFlow, index = 4 Name = Airfoil, index = 5 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = TunnelWall, index = 1 Name = OutFlow, index = 2 Name = InFlow, index = 3 Name = Airfoil, index = 4 Getting 2D mesh for body 1 (of 1) AFLR2 : --------------------------------------- AFLR2 : AFLR2 LIBRARY AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR2 : TRIA/QUAD GRID GENERATOR AFLR2 : Version Number 9.17.15 AFLR2 : Version Date 04/23/24 @ 12:51AM AFLR2 : Compile OS Darwin 23.4.0 x86_64 AFLR2 : Compile Date 04/23/24 @ 11:49AM AFLR2 : Copyright 1994-2021, D.L. Marcum AFLR2 : --------------------------------------- AFLR2 IC : INPUT DATA CHECK AFLR2 IC : Nodes, Faces = 48 0 AFLR2 : CPU Time = 0.000 seconds AFLR2 EG : EDGE GRID RE-GENERATION AFLR2 EG : Nodes, Edges = 48 48 AFLR2 : CPU Time = 0.000 seconds AFLR2 IG : INITIAL GRID GENERATION AFLR2 IG : Nodes, Faces = 0 2 AFLR2 IG : Nodes, Faces = 10 22 AFLR2 IG : Nodes, Faces = 20 42 AFLR2 IG : Nodes, Faces = 30 62 AFLR2 IG : Nodes, Faces = 40 82 AFLR2 IG : Nodes, Faces = 45 92 AFLR2 IG : Nodes, Faces = 46 94 AFLR2 IG : Nodes, Faces = 48 98 AFLR2 IG : Nodes, Faces = 52 98 AFLR2 IG : Nodes, Faces = 48 48 AFLR2 : CPU Time = 0.000 seconds AFLR2 GG : FIELD GRID GENERATION AFLR2 GG : Nodes, Faces = 48 48 AFLR2 GG : Nodes, Faces = 88 128 AFLR2 GG : Nodes, Faces = 109 170 AFLR2 GG : Nodes, Faces = 124 200 AFLR2 GG : Nodes, Faces = 136 224 AFLR2 GG : Nodes, Faces = 148 248 AFLR2 GG : Nodes, Faces = 161 274 AFLR2 GG : Nodes, Faces = 171 294 AFLR2 GG : Nodes, Faces = 181 314 AFLR2 GG : Nodes, Faces = 187 326 AFLR2 GG : Nodes, Faces = 190 332 AFLR2 : CPU Time = 0.000 seconds AFLR2 QI : QUALITY IMPROVEMENT AFLR2 QI : Nodes, Faces = 190 332 AFLR2 : CPU Time = 0.000 seconds AFLR2 : DONE Writing AFLR3 file .... Finished writing AFLR3 file Number of nodes = 190 Number of elements = 380 Number of tris = 332 Number of quad = 0 ok test_reenter (test_aflr2.TestAFLR2.test_reenter) ... Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 5 Name = 2DSlice, index = 1 Name = TunnelWall, index = 2 Name = OutFlow, index = 3 Name = InFlow, index = 4 Name = Airfoil, index = 5 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = TunnelWall, index = 1 Name = OutFlow, index = 2 Name = InFlow, index = 3 Name = Airfoil, index = 4 Getting mesh sizing parameters Mesh sizing name - 2DSlice Mesh sizing name - Airfoil Mesh sizing name - InFlow Mesh sizing name - OutFlow Mesh sizing name - TunnelWall Done getting mesh sizing parameters Getting 2D mesh for body 1 (of 1) AFLR2 : --------------------------------------- AFLR2 : AFLR2 LIBRARY AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR2 : TRIA/QUAD GRID GENERATOR AFLR2 : Version Number 9.17.15 AFLR2 : Version Date 04/23/24 @ 12:51AM AFLR2 : Compile OS Darwin 23.4.0 x86_64 AFLR2 : Compile Date 04/23/24 @ 11:49AM AFLR2 : Copyright 1994-2021, D.L. Marcum AFLR2 : --------------------------------------- AFLR2 IC : INPUT DATA CHECK AFLR2 IC : Nodes, Faces = 344 0 AFLR2 : CPU Time = 0.000 seconds AFLR2 EG : EDGE GRID RE-GENERATION AFLR2 EG : Nodes, Edges = 344 344 AFLR2 : CPU Time = 0.000 seconds AFLR2 IG : INITIAL GRID GENERATION AFLR2 IG : Nodes, Faces = 0 2 AFLR2 IG : Nodes, Faces = 70 142 AFLR2 IG : Nodes, Faces = 140 282 AFLR2 IG : Nodes, Faces = 210 422 AFLR2 IG : Nodes, Faces = 280 562 AFLR2 IG : Nodes, Faces = 339 680 AFLR2 IG : Nodes, Faces = 340 682 AFLR2 IG : Nodes, Faces = 344 690 AFLR2 IG : Nodes, Faces = 348 690 AFLR2 IG : Nodes, Faces = 344 344 AFLR2 : CPU Time = 0.002 seconds AFLR2 GG : FIELD GRID GENERATION AFLR2 GG : Nodes, Faces = 344 344 AFLR2 GG : Nodes, Faces = 679 1014 AFLR2 GG : Nodes, Faces = 1006 1668 AFLR2 GG : Nodes, Faces = 1321 2298 AFLR2 GG : Nodes, Faces = 1604 2864 AFLR2 GG : Nodes, Faces = 1886 3428 AFLR2 GG : Nodes, Faces = 2155 3966 AFLR2 GG : Nodes, Faces = 2409 4474 AFLR2 GG : Nodes, Faces = 2649 4954 AFLR2 GG : Nodes, Faces = 2867 5390 AFLR2 GG : Nodes, Faces = 3063 5782 AFLR2 GG : Nodes, Faces = 3243 6142 AFLR2 GG : Nodes, Faces = 3400 6456 AFLR2 GG : Nodes, Faces = 3540 6736 AFLR2 GG : Nodes, Faces = 3665 6986 AFLR2 GG : Nodes, Faces = 3786 7228 AFLR2 GG : Nodes, Faces = 3900 7456 AFLR2 GG : Nodes, Faces = 4010 7676 AFLR2 GG : Nodes, Faces = 4114 7884 AFLR2 GG : Nodes, Faces = 4209 8074 AFLR2 GG : Nodes, Faces = 4292 8240 AFLR2 GG : Nodes, Faces = 4368 8392 AFLR2 GG : Nodes, Faces = 4439 8534 AFLR2 GG : Nodes, Faces = 4503 8662 AFLR2 GG : Nodes, Faces = 4560 8776 AFLR2 GG : Nodes, Faces = 4611 8878 AFLR2 GG : Nodes, Faces = 4650 8956 AFLR2 GG : Nodes, Faces = 4677 9010 AFLR2 GG : Nodes, Faces = 4695 9046 AFLR2 GG : Nodes, Faces = 4705 9066 AFLR2 : CPU Time = 0.023 seconds AFLR2 QI : QUALITY IMPROVEMENT AFLR2 QI : Nodes, Faces = 4705 9066 AFLR2 : CPU Time = 0.002 seconds AFLR2 : DONE Writing AFLR3 file .... Finished writing AFLR3 file Number of nodes = 4705 Number of elements = 9410 Number of tris = 9066 Number of quad = 0 Writing Binary VTK file .... Finished writing Binary VTK file Writing vtk file .... Writing vtk general file .... Finished writing vtk file libMeshb expects 2D meshes in the x-y plane... attempting to rotate mesh!Swapping z and y coordinates! Writing FAST file .... Finished writing FAST file Writing SU2 file .... SU2 expects 2D meshes in the x-y plane... attempting to rotate mesh! Swapping z and y coordinates! Finished writing SU2 file Writing Binary STL file .... Finished writing Binary STL file Writing ASCII STL file .... Finished writing ASCII STL file Writing Tecplot file .... Finished writing Tecplot file Getting mesh sizing parameters Mesh sizing name - 2DSlice Mesh sizing name - Airfoil Mesh sizing name - InFlow Mesh sizing name - OutFlow Mesh sizing name - TunnelWall Done getting mesh sizing parameters Getting 2D mesh for body 1 (of 1) AFLR2 IC : INPUT DATA CHECK AFLR2 IC : Nodes, Faces = 344 0 AFLR2 : CPU Time = 0.000 seconds AFLR2 EG : EDGE GRID RE-GENERATION AFLR2 EG : Nodes, Edges = 344 344 AFLR2 : CPU Time = 0.000 seconds AFLR2 IG : INITIAL GRID GENERATION AFLR2 IG : Nodes, Faces = 0 2 AFLR2 IG : Nodes, Faces = 70 142 AFLR2 IG : Nodes, Faces = 140 282 AFLR2 IG : Nodes, Faces = 210 422 AFLR2 IG : Nodes, Faces = 280 562 AFLR2 IG : Nodes, Faces = 339 680 AFLR2 IG : Nodes, Faces = 340 682 AFLR2 IG : Nodes, Faces = 344 690 AFLR2 IG : Nodes, Faces = 348 690 AFLR2 IG : Nodes, Faces = 344 344 AFLR2 : CPU Time = 0.001 seconds AFLR2 GG : FIELD GRID GENERATION AFLR2 GGp: Nodes, Faces = 344 344 AFLR2 GGp: Nodes, Faces = 682 1020 AFLR2 GGp: Nodes, Faces = 1010 1676 AFLR2 GGp: Nodes, Faces = 1316 2288 AFLR2 GGp: Nodes, Faces = 1592 2840 AFLR2 GGp: Nodes, Faces = 1855 3366 AFLR2 GGp: Nodes, Faces = 2106 3868 AFLR2 GGp: Nodes, Faces = 2341 4338 AFLR2 GGp: Nodes, Faces = 2551 4758 AFLR2 GGp: Nodes, Faces = 2741 5138 AFLR2 GGp: Nodes, Faces = 2917 5490 AFLR2 GGp: Nodes, Faces = 3082 5820 AFLR2 GGp: Nodes, Faces = 3240 6136 AFLR2 GGp: Nodes, Faces = 3379 6414 AFLR2 GGp: Nodes, Faces = 3513 6682 AFLR2 GGp: Nodes, Faces = 3642 6940 AFLR2 GGp: Nodes, Faces = 3748 7152 AFLR2 GGp: Nodes, Faces = 3846 7348 AFLR2 GGp: Nodes, Faces = 3931 7518 AFLR2 GGp: Nodes, Faces = 3999 7654 AFLR2 GGp: Nodes, Faces = 4044 7744 AFLR2 GGp: Nodes, Faces = 4058 7772 AFLR2 : CPU Time = 0.013 seconds AFLR2 QI : QUALITY IMPROVEMENT AFLR2 QI : Nodes, Faces = 4058 7772 AFLR2 QI : Nodes, Faces = 4057 364 AFLR2 QI : Nodes, Faces = 4057 3703 AFLR2 QI : Nodes, Faces = 4057 7770 AFLR2 QI : Nodes, Faces = 4056 344 AFLR2 QI : Nodes, Faces = 4056 3712 AFLR2 QI : Nodes, Faces = 4056 7768 AFLR2 QI : Nodes, Faces = 4055 348 AFLR2 QI : Nodes, Faces = 4055 3709 AFLR2 QI : Nodes, Faces = 4055 7766 AFLR2 QI : Nodes, Faces = 4055 392 AFLR2 QI : Nodes, Faces = 4055 3687 AFLR2 QI : Nodes, Faces = 4055 7766 AFLR2 QI : Nodes, Faces = 4055 386 AFLR2 QI : Nodes, Faces = 4055 3690 AFLR2 QI : Nodes, Faces = 4055 386 AFLR2 QI : Nodes, Faces = 4055 3690 AFLR2 : CPU Time = 0.009 seconds AFLR2 : DONE Writing AFLR3 file .... Finished writing AFLR3 file Number of nodes = 4055 Number of elements = 4420 Number of tris = 386 Number of quad = 3690 Writing Binary VTK file .... Finished writing Binary VTK file Writing vtk file .... Writing vtk general file .... Finished writing vtk file libMeshb expects 2D meshes in the x-y plane... attempting to rotate mesh!Swapping z and y coordinates! Writing SU2 file .... SU2 expects 2D meshes in the x-y plane... attempting to rotate mesh! Swapping z and y coordinates! Finished writing SU2 file Writing Binary STL file .... Finished writing Binary STL file Writing ASCII STL file .... Finished writing ASCII STL file Writing Tecplot file .... Finished writing Tecplot file ok test_setInput (test_aflr2.TestAFLR2.test_setInput) ... Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 5 Name = 2DSlice, index = 1 Name = TunnelWall, index = 2 Name = OutFlow, index = 3 Name = InFlow, index = 4 Name = Airfoil, index = 5 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = TunnelWall, index = 1 Name = OutFlow, index = 2 Name = InFlow, index = 3 Name = Airfoil, index = 4 Getting mesh sizing parameters Mesh sizing name - 2DSlice Mesh sizing name - Airfoil Mesh sizing name - InFlow Mesh sizing name - OutFlow Mesh sizing name - TunnelWall Done getting mesh sizing parameters Getting 2D mesh for body 1 (of 1) AFLR2 : --------------------------------------- AFLR2 : AFLR2 LIBRARY AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR2 : TRIA/QUAD GRID GENERATOR AFLR2 : Version Number 9.17.15 AFLR2 : Version Date 04/23/24 @ 12:51AM AFLR2 : Compile OS Darwin 23.4.0 x86_64 AFLR2 : Compile Date 04/23/24 @ 11:49AM AFLR2 : Copyright 1994-2021, D.L. Marcum AFLR2 : --------------------------------------- AFLR2 IC : INPUT DATA CHECK AFLR2 IC : Nodes, Faces = 344 0 AFLR2 : CPU Time = 0.000 seconds AFLR2 EG : EDGE GRID RE-GENERATION AFLR2 EG : Nodes, Edges = 344 344 AFLR2 : CPU Time = 0.000 seconds AFLR2 IG : INITIAL GRID GENERATION AFLR2 IG : Nodes, Faces = 0 2 AFLR2 IG : Nodes, Faces = 70 142 AFLR2 IG : Nodes, Faces = 140 282 AFLR2 IG : Nodes, Faces = 210 422 AFLR2 IG : Nodes, Faces = 280 562 AFLR2 IG : Nodes, Faces = 339 680 AFLR2 IG : Nodes, Faces = 340 682 AFLR2 IG : Nodes, Faces = 344 690 AFLR2 IG : Nodes, Faces = 348 690 AFLR2 IG : Nodes, Faces = 344 344 AFLR2 : CPU Time = 0.001 seconds AFLR2 GG : FIELD GRID GENERATION AFLR2 GGp: Nodes, Faces = 344 344 AFLR2 GGp: Nodes, Faces = 682 1020 AFLR2 GGp: Nodes, Faces = 1010 1676 AFLR2 GGp: Nodes, Faces = 1316 2288 AFLR2 GGp: Nodes, Faces = 1592 2840 AFLR2 GGp: Nodes, Faces = 1855 3366 AFLR2 GGp: Nodes, Faces = 2106 3868 AFLR2 GGp: Nodes, Faces = 2341 4338 AFLR2 GGp: Nodes, Faces = 2551 4758 AFLR2 GGp: Nodes, Faces = 2741 5138 AFLR2 GGp: Nodes, Faces = 2917 5490 AFLR2 GGp: Nodes, Faces = 3082 5820 AFLR2 GGp: Nodes, Faces = 3240 6136 AFLR2 GGp: Nodes, Faces = 3379 6414 AFLR2 GGp: Nodes, Faces = 3513 6682 AFLR2 GGp: Nodes, Faces = 3642 6940 AFLR2 GGp: Nodes, Faces = 3748 7152 AFLR2 GGp: Nodes, Faces = 3846 7348 AFLR2 GGp: Nodes, Faces = 3931 7518 AFLR2 GGp: Nodes, Faces = 3999 7654 AFLR2 GGp: Nodes, Faces = 4044 7744 AFLR2 GGp: Nodes, Faces = 4058 7772 AFLR2 : CPU Time = 0.011 seconds AFLR2 QI : QUALITY IMPROVEMENT AFLR2 QI : Nodes, Faces = 4058 7772 AFLR2 QI : Nodes, Faces = 4057 364 AFLR2 QI : Nodes, Faces = 4057 3703 AFLR2 QI : Nodes, Faces = 4057 7770 AFLR2 QI : Nodes, Faces = 4056 344 AFLR2 QI : Nodes, Faces = 4056 3712 AFLR2 QI : Nodes, Faces = 4056 7768 AFLR2 QI : Nodes, Faces = 4055 348 AFLR2 QI : Nodes, Faces = 4055 3709 AFLR2 QI : Nodes, Faces = 4055 7766 AFLR2 QI : Nodes, Faces = 4055 392 AFLR2 QI : Nodes, Faces = 4055 3687 AFLR2 QI : Nodes, Faces = 4055 7766 AFLR2 QI : Nodes, Faces = 4055 386 AFLR2 QI : Nodes, Faces = 4055 3690 AFLR2 QI : Nodes, Faces = 4055 386 AFLR2 QI : Nodes, Faces = 4055 3690 AFLR2 : CPU Time = 0.006 seconds AFLR2 : DONE Writing AFLR3 file .... Finished writing AFLR3 file Number of nodes = 4055 Number of elements = 4420 Number of tris = 386 Number of quad = 3690 Writing Tecplot file .... Finished writing Tecplot file ok test_Multiple_Mesh (test_aflr3.TestAFLR3.test_Multiple_Mesh) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62031) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 7 Name = box, index = 1 Name = cylinder, index = 2 Name = cone, index = 3 Name = torus, index = 4 Name = sphere, index = 5 Name = boxhole, index = 6 Name = bullet, index = 7 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 AFLR4 : Proximity BG Surface Grid Generation Skipped AFLR4 : No Modifications Required Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 7 Name = box, index = 1 Name = cylinder, index = 2 Name = cone, index = 3 Name = torus, index = 4 Name = sphere, index = 5 Name = boxhole, index = 6 Name = bullet, index = 7 Getting volume mesh for body 1 (of 7) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = box, index = 1 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 x86_64 AFLR2 : Compile Date 04/23/24 @ 11:49AM 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 x86_64 AFLR4 : Compile Date 04/23/24 @ 11:49AM AFLR4 : Copyright 1994-2021, D.L. Marcum AFLR4 : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 1 (of 7): Number of nodes = 1189 Number of elements = 6249 Number of triangles = 1332 Number of quadrilatarals = 0 Number of tetrahedrals = 4917 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 2 (of 7) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = cylinder, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 2 (of 7): Number of nodes = 6237 Number of elements = 34620 Number of triangles = 4438 Number of quadrilatarals = 0 Number of tetrahedrals = 30182 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 3 (of 7) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = cone, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 3 (of 7): Number of nodes = 13613 Number of elements = 76414 Number of triangles = 8142 Number of quadrilatarals = 0 Number of tetrahedrals = 68272 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 4 (of 7) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = torus, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 4 (of 7): Number of nodes = 41618 Number of elements = 236483 Number of triangles = 19838 Number of quadrilatarals = 0 Number of tetrahedrals = 216645 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 5 (of 7) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = sphere, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 5 (of 7): Number of nodes = 4369 Number of elements = 24223 Number of triangles = 3016 Number of quadrilatarals = 0 Number of tetrahedrals = 21207 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 6 (of 7) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = boxhole, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 6 (of 7): Number of nodes = 11007 Number of elements = 60837 Number of triangles = 8632 Number of quadrilatarals = 0 Number of tetrahedrals = 52205 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 7 (of 7) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = bullet, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 7 (of 7): Number of nodes = 10474 Number of elements = 58678 Number of triangles = 6352 Number of quadrilatarals = 0 Number of tetrahedrals = 52326 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file AFLR4 : Proximity BG Surface Grid Generation Skipped AFLR4 : No Modifications Required Getting volume mesh for body 1 (of 7) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 2 (of 7) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 3 (of 7) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 4 (of 7) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 5 (of 7) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 6 (of 7) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 7 (of 7) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 88507 Number of elements = 497504 Number of triangles = 51750 Number of quadrilatarals = 0 Number of tetrahedrals = 445754 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file ok test_all (test_aflr3.TestAFLR3.test_all) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62031) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 8 Name = box, index = 1 Name = cylinder, index = 2 Name = cone, index = 3 Name = torus, index = 4 Name = sphere, index = 5 Name = boxhole, index = 6 Name = bullet, index = 7 Name = farfield, index = 8 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 8 Name = box, index = 1 Name = cylinder, index = 2 Name = cone, index = 3 Name = torus, index = 4 Name = sphere, index = 5 Name = boxhole, index = 6 Name = bullet, index = 7 Name = farfield, index = 8 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 x86_64 AFLR2 : Compile Date 04/23/24 @ 11:49AM 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 x86_64 AFLR4 : Compile Date 04/23/24 @ 11:49AM AFLR4 : Copyright 1994-2021, D.L. Marcum AFLR4 : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 16456 Number of elements = 93635 Number of triangles = 7926 Number of quadrilatarals = 0 Number of tetrahedrals = 85709 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file ok test_box (test_aflr3.TestAFLR3.test_box) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 2589 Number of elements = 13809 Number of triangles = 2758 Number of quadrilatarals = 0 Number of tetrahedrals = 11051 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file ok test_boxhole (test_aflr3.TestAFLR3.test_boxhole) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = boxhole, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = boxhole, index = 1 Name = farfield, index = 2 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 3654 Number of elements = 19800 Number of triangles = 3394 Number of quadrilatarals = 0 Number of tetrahedrals = 16406 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file ok test_bullet (test_aflr3.TestAFLR3.test_bullet) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = bullet, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = bullet, index = 1 Name = farfield, index = 2 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 5456 Number of elements = 30308 Number of triangles = 3656 Number of quadrilatarals = 0 Number of tetrahedrals = 26652 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file ok test_cone (test_aflr3.TestAFLR3.test_cone) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = cone, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = cone, index = 1 Name = farfield, index = 2 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 4694 Number of elements = 25935 Number of triangles = 3326 Number of quadrilatarals = 0 Number of tetrahedrals = 22609 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file ok test_cylinder (test_aflr3.TestAFLR3.test_cylinder) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = cylinder, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = cylinder, index = 1 Name = farfield, index = 2 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 5554 Number of elements = 30862 Number of triangles = 3756 Number of quadrilatarals = 0 Number of tetrahedrals = 27106 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file ok test_faceMatch (test_aflr3.TestAFLR3.test_faceMatch) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 2260 Number of elements = 12133 Number of triangles = 2222 Number of quadrilatarals = 0 Number of tetrahedrals = 9911 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 2) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 2 (of 2) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 2392 Number of elements = 12577 Number of triangles = 2666 Number of quadrilatarals = 0 Number of tetrahedrals = 9911 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 2) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 1 (of 2): Number of nodes = 1208 Number of elements = 6360 Number of triangles = 1334 Number of quadrilatarals = 0 Number of tetrahedrals = 5026 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 2 (of 2) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 2 (of 2): Number of nodes = 1184 Number of elements = 6217 Number of triangles = 1332 Number of quadrilatarals = 0 Number of tetrahedrals = 4885 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 3341 Number of elements = 18069 Number of triangles = 3110 Number of quadrilatarals = 0 Number of tetrahedrals = 14959 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 3) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 2 (of 3) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 3 (of 3) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 3606 Number of elements = 18961 Number of triangles = 4002 Number of quadrilatarals = 0 Number of tetrahedrals = 14959 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 1 (of 3): Number of nodes = 1208 Number of elements = 6360 Number of triangles = 1334 Number of quadrilatarals = 0 Number of tetrahedrals = 5026 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 2 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 2 (of 3): Number of nodes = 1184 Number of elements = 6217 Number of triangles = 1332 Number of quadrilatarals = 0 Number of tetrahedrals = 4885 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 3 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 3 (of 3): Number of nodes = 1214 Number of elements = 6384 Number of triangles = 1336 Number of quadrilatarals = 0 Number of tetrahedrals = 5048 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 4414 Number of elements = 23974 Number of triangles = 3998 Number of quadrilatarals = 0 Number of tetrahedrals = 19976 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 4) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 2 (of 4) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 3 (of 4) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 4 (of 4) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 4811 Number of elements = 25310 Number of triangles = 5334 Number of quadrilatarals = 0 Number of tetrahedrals = 19976 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 4) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 1 (of 4): Number of nodes = 1208 Number of elements = 6360 Number of triangles = 1334 Number of quadrilatarals = 0 Number of tetrahedrals = 5026 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 2 (of 4) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 2 (of 4): Number of nodes = 1184 Number of elements = 6217 Number of triangles = 1332 Number of quadrilatarals = 0 Number of tetrahedrals = 4885 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 3 (of 4) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 3 (of 4): Number of nodes = 1214 Number of elements = 6384 Number of triangles = 1336 Number of quadrilatarals = 0 Number of tetrahedrals = 5048 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 4 (of 4) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 4 (of 4): Number of nodes = 1205 Number of elements = 6349 Number of triangles = 1332 Number of quadrilatarals = 0 Number of tetrahedrals = 5017 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 5490 Number of elements = 29891 Number of triangles = 4886 Number of quadrilatarals = 0 Number of tetrahedrals = 25005 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 5) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 2 (of 5) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 3 (of 5) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 4 (of 5) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 5 (of 5) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 6019 Number of elements = 31671 Number of triangles = 6666 Number of quadrilatarals = 0 Number of tetrahedrals = 25005 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 5) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 1 (of 5): Number of nodes = 1208 Number of elements = 6360 Number of triangles = 1334 Number of quadrilatarals = 0 Number of tetrahedrals = 5026 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 2 (of 5) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 2 (of 5): Number of nodes = 1184 Number of elements = 6217 Number of triangles = 1332 Number of quadrilatarals = 0 Number of tetrahedrals = 4885 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 3 (of 5) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 3 (of 5): Number of nodes = 1214 Number of elements = 6384 Number of triangles = 1336 Number of quadrilatarals = 0 Number of tetrahedrals = 5048 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 4 (of 5) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 4 (of 5): Number of nodes = 1205 Number of elements = 6349 Number of triangles = 1332 Number of quadrilatarals = 0 Number of tetrahedrals = 5017 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 5 (of 5) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 5 (of 5): Number of nodes = 1208 Number of elements = 6361 Number of triangles = 1332 Number of quadrilatarals = 0 Number of tetrahedrals = 5029 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 6542 Number of elements = 35667 Number of triangles = 5774 Number of quadrilatarals = 0 Number of tetrahedrals = 29893 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 6) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 2 (of 6) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 3 (of 6) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 4 (of 6) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 5 (of 6) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 6 (of 6) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 7203 Number of elements = 37891 Number of triangles = 7998 Number of quadrilatarals = 0 Number of tetrahedrals = 29893 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 6) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 1 (of 6): Number of nodes = 1208 Number of elements = 6360 Number of triangles = 1334 Number of quadrilatarals = 0 Number of tetrahedrals = 5026 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 2 (of 6) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 2 (of 6): Number of nodes = 1184 Number of elements = 6217 Number of triangles = 1332 Number of quadrilatarals = 0 Number of tetrahedrals = 4885 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 3 (of 6) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 3 (of 6): Number of nodes = 1214 Number of elements = 6384 Number of triangles = 1336 Number of quadrilatarals = 0 Number of tetrahedrals = 5048 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 4 (of 6) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 4 (of 6): Number of nodes = 1205 Number of elements = 6349 Number of triangles = 1332 Number of quadrilatarals = 0 Number of tetrahedrals = 5017 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 5 (of 6) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 5 (of 6): Number of nodes = 1208 Number of elements = 6361 Number of triangles = 1332 Number of quadrilatarals = 0 Number of tetrahedrals = 5029 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 6 (of 6) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 6 (of 6): Number of nodes = 1184 Number of elements = 6220 Number of triangles = 1332 Number of quadrilatarals = 0 Number of tetrahedrals = 4888 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 7601 Number of elements = 41489 Number of triangles = 6662 Number of quadrilatarals = 0 Number of tetrahedrals = 34827 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 7) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 2 (of 7) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 3 (of 7) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 4 (of 7) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 5 (of 7) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 6 (of 7) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 7 (of 7) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 8394 Number of elements = 44157 Number of triangles = 9330 Number of quadrilatarals = 0 Number of tetrahedrals = 34827 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 7) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 1 (of 7): Number of nodes = 1208 Number of elements = 6360 Number of triangles = 1334 Number of quadrilatarals = 0 Number of tetrahedrals = 5026 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 2 (of 7) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 2 (of 7): Number of nodes = 1184 Number of elements = 6217 Number of triangles = 1332 Number of quadrilatarals = 0 Number of tetrahedrals = 4885 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 3 (of 7) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 3 (of 7): Number of nodes = 1214 Number of elements = 6384 Number of triangles = 1336 Number of quadrilatarals = 0 Number of tetrahedrals = 5048 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 4 (of 7) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 4 (of 7): Number of nodes = 1205 Number of elements = 6349 Number of triangles = 1332 Number of quadrilatarals = 0 Number of tetrahedrals = 5017 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 5 (of 7) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 5 (of 7): Number of nodes = 1208 Number of elements = 6361 Number of triangles = 1332 Number of quadrilatarals = 0 Number of tetrahedrals = 5029 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 6 (of 7) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 6 (of 7): Number of nodes = 1184 Number of elements = 6220 Number of triangles = 1332 Number of quadrilatarals = 0 Number of tetrahedrals = 4888 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 7 (of 7) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 7 (of 7): Number of nodes = 1191 Number of elements = 6266 Number of triangles = 1332 Number of quadrilatarals = 0 Number of tetrahedrals = 4934 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 19800 Number of elements = 109798 Number of triangles = 15540 Number of quadrilatarals = 0 Number of tetrahedrals = 94258 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 19) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 2 (of 19) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 3 (of 19) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 4 (of 19) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 5 (of 19) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 6 (of 19) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 7 (of 19) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 8 (of 19) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 9 (of 19) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 10 (of 19) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 11 (of 19) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 12 (of 19) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 13 (of 19) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 14 (of 19) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 15 (of 19) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 16 (of 19) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 17 (of 19) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 18 (of 19) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 19 (of 19) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 22741 Number of elements = 119570 Number of triangles = 25312 Number of quadrilatarals = 0 Number of tetrahedrals = 94258 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 19) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 1 (of 19): Number of nodes = 1208 Number of elements = 6360 Number of triangles = 1334 Number of quadrilatarals = 0 Number of tetrahedrals = 5026 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 2 (of 19) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 2 (of 19): Number of nodes = 1184 Number of elements = 6217 Number of triangles = 1332 Number of quadrilatarals = 0 Number of tetrahedrals = 4885 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 3 (of 19) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 3 (of 19): Number of nodes = 1214 Number of elements = 6384 Number of triangles = 1336 Number of quadrilatarals = 0 Number of tetrahedrals = 5048 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 4 (of 19) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 4 (of 19): Number of nodes = 1205 Number of elements = 6349 Number of triangles = 1332 Number of quadrilatarals = 0 Number of tetrahedrals = 5017 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 5 (of 19) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 5 (of 19): Number of nodes = 1208 Number of elements = 6361 Number of triangles = 1332 Number of quadrilatarals = 0 Number of tetrahedrals = 5029 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 6 (of 19) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 6 (of 19): Number of nodes = 1184 Number of elements = 6220 Number of triangles = 1332 Number of quadrilatarals = 0 Number of tetrahedrals = 4888 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 7 (of 19) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 7 (of 19): Number of nodes = 1191 Number of elements = 6266 Number of triangles = 1332 Number of quadrilatarals = 0 Number of tetrahedrals = 4934 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 8 (of 19) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 8 (of 19): Number of nodes = 1193 Number of elements = 6272 Number of triangles = 1332 Number of quadrilatarals = 0 Number of tetrahedrals = 4940 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 9 (of 19) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 9 (of 19): Number of nodes = 1176 Number of elements = 6165 Number of triangles = 1330 Number of quadrilatarals = 0 Number of tetrahedrals = 4835 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 10 (of 19) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 10 (of 19): Number of nodes = 1203 Number of elements = 6314 Number of triangles = 1332 Number of quadrilatarals = 0 Number of tetrahedrals = 4982 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 11 (of 19) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 11 (of 19): Number of nodes = 1192 Number of elements = 6269 Number of triangles = 1332 Number of quadrilatarals = 0 Number of tetrahedrals = 4937 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 12 (of 19) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 12 (of 19): Number of nodes = 1192 Number of elements = 6269 Number of triangles = 1332 Number of quadrilatarals = 0 Number of tetrahedrals = 4937 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 13 (of 19) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 13 (of 19): Number of nodes = 1198 Number of elements = 6296 Number of triangles = 1332 Number of quadrilatarals = 0 Number of tetrahedrals = 4964 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 14 (of 19) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 14 (of 19): Number of nodes = 1223 Number of elements = 6443 Number of triangles = 1332 Number of quadrilatarals = 0 Number of tetrahedrals = 5111 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 15 (of 19) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 15 (of 19): Number of nodes = 1184 Number of elements = 6224 Number of triangles = 1332 Number of quadrilatarals = 0 Number of tetrahedrals = 4892 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 16 (of 19) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 16 (of 19): Number of nodes = 1195 Number of elements = 6287 Number of triangles = 1332 Number of quadrilatarals = 0 Number of tetrahedrals = 4955 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 17 (of 19) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 17 (of 19): Number of nodes = 1197 Number of elements = 6311 Number of triangles = 1332 Number of quadrilatarals = 0 Number of tetrahedrals = 4979 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 18 (of 19) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 18 (of 19): Number of nodes = 1203 Number of elements = 6310 Number of triangles = 1332 Number of quadrilatarals = 0 Number of tetrahedrals = 4978 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 19 (of 19) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 19 (of 19): Number of nodes = 1191 Number of elements = 6253 Number of triangles = 1332 Number of quadrilatarals = 0 Number of tetrahedrals = 4921 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file ok test_faceMatch_MultiDomain (test_aflr3.TestAFLR3.test_faceMatch_MultiDomain) ... ../csmData/MultiDomain/example1.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 8857 Number of elements = 49191 Number of triangles = 6284 Number of quadrilatarals = 0 Number of tetrahedrals = 42907 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 2) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 2 (of 2) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 8989 Number of elements = 49635 Number of triangles = 6728 Number of quadrilatarals = 0 Number of tetrahedrals = 42907 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 2) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 1 (of 2): Number of nodes = 7796 Number of elements = 43368 Number of triangles = 5396 Number of quadrilatarals = 0 Number of tetrahedrals = 37972 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 2 (of 2) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 2 (of 2): Number of nodes = 1193 Number of elements = 6267 Number of triangles = 1332 Number of quadrilatarals = 0 Number of tetrahedrals = 4935 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file ../csmData/MultiDomain/example2.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 9944 Number of elements = 55193 Number of triangles = 7174 Number of quadrilatarals = 0 Number of tetrahedrals = 48019 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 3) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 2 (of 3) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 3 (of 3) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 10218 Number of elements = 56081 Number of triangles = 8062 Number of quadrilatarals = 0 Number of tetrahedrals = 48019 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 1 (of 3): Number of nodes = 7818 Number of elements = 43469 Number of triangles = 5398 Number of quadrilatarals = 0 Number of tetrahedrals = 38071 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 2 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 2 (of 3): Number of nodes = 1202 Number of elements = 6320 Number of triangles = 1332 Number of quadrilatarals = 0 Number of tetrahedrals = 4988 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 3 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 3 (of 3): Number of nodes = 1198 Number of elements = 6292 Number of triangles = 1332 Number of quadrilatarals = 0 Number of tetrahedrals = 4960 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file ../csmData/MultiDomain/example3.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 9609 Number of elements = 53228 Number of triangles = 6994 Number of quadrilatarals = 0 Number of tetrahedrals = 46234 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 3) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 2 (of 3) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 3 (of 3) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 9829 Number of elements = 53956 Number of triangles = 7722 Number of quadrilatarals = 0 Number of tetrahedrals = 46234 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 1 (of 3): Number of nodes = 7789 Number of elements = 43295 Number of triangles = 5394 Number of quadrilatarals = 0 Number of tetrahedrals = 37901 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 2 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 2 (of 3): Number of nodes = 1186 Number of elements = 6230 Number of triangles = 1332 Number of quadrilatarals = 0 Number of tetrahedrals = 4898 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 3 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 3 (of 3): Number of nodes = 854 Number of elements = 4431 Number of triangles = 996 Number of quadrilatarals = 0 Number of tetrahedrals = 3435 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file ../csmData/MultiDomain/example4.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 9348 Number of elements = 51734 Number of triangles = 6812 Number of quadrilatarals = 0 Number of tetrahedrals = 44922 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 3) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 2 (of 3) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 3 (of 3) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 9531 Number of elements = 52330 Number of triangles = 7408 Number of quadrilatarals = 0 Number of tetrahedrals = 44922 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 1 (of 3): Number of nodes = 7804 Number of elements = 43358 Number of triangles = 5386 Number of quadrilatarals = 0 Number of tetrahedrals = 37972 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 2 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 2 (of 3): Number of nodes = 1200 Number of elements = 6311 Number of triangles = 1332 Number of quadrilatarals = 0 Number of tetrahedrals = 4979 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 3 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 3 (of 3): Number of nodes = 527 Number of elements = 2661 Number of triangles = 690 Number of quadrilatarals = 0 Number of tetrahedrals = 1971 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file ../csmData/MultiDomain/example6.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 9183 Number of elements = 50871 Number of triangles = 6632 Number of quadrilatarals = 0 Number of tetrahedrals = 44239 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 3) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 2 (of 3) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 3 (of 3) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 9322 Number of elements = 51307 Number of triangles = 7068 Number of quadrilatarals = 0 Number of tetrahedrals = 44239 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 1 (of 3): Number of nodes = 7927 Number of elements = 44116 Number of triangles = 5382 Number of quadrilatarals = 0 Number of tetrahedrals = 38734 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 2 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 2 (of 3): Number of nodes = 868 Number of elements = 4530 Number of triangles = 996 Number of quadrilatarals = 0 Number of tetrahedrals = 3534 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 3 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 3 (of 3): Number of nodes = 527 Number of elements = 2661 Number of triangles = 690 Number of quadrilatarals = 0 Number of tetrahedrals = 1971 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file ../csmData/MultiDomain/example7.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 10181 Number of elements = 56797 Number of triangles = 6782 Number of quadrilatarals = 0 Number of tetrahedrals = 50015 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 3) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 2 (of 3) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 3 (of 3) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 10671 Number of elements = 58561 Number of triangles = 8546 Number of quadrilatarals = 0 Number of tetrahedrals = 50015 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 1 (of 3): Number of nodes = 7741 Number of elements = 43010 Number of triangles = 5362 Number of quadrilatarals = 0 Number of tetrahedrals = 37648 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 2 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 2 (of 3): Number of nodes = 2692 Number of elements = 14435 Number of triangles = 2800 Number of quadrilatarals = 0 Number of tetrahedrals = 11635 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 3 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 3 (of 3): Number of nodes = 238 Number of elements = 1116 Number of triangles = 384 Number of quadrilatarals = 0 Number of tetrahedrals = 732 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file ../csmData/MultiDomain/example8.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 1500 Number of elements = 7757 Number of triangles = 1986 Number of quadrilatarals = 0 Number of tetrahedrals = 5771 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 3) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 2 (of 3) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 3 (of 3) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 1564 Number of elements = 7881 Number of triangles = 2110 Number of quadrilatarals = 0 Number of tetrahedrals = 5771 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 1 (of 3): Number of nodes = 1160 Number of elements = 6087 Number of triangles = 1308 Number of quadrilatarals = 0 Number of tetrahedrals = 4779 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 2 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 2 (of 3): Number of nodes = 360 Number of elements = 1635 Number of triangles = 718 Number of quadrilatarals = 0 Number of tetrahedrals = 917 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 3 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 3 (of 3): Number of nodes = 44 Number of elements = 159 Number of triangles = 84 Number of quadrilatarals = 0 Number of tetrahedrals = 75 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file ../csmData/MultiDomain/example9.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 5075 Number of elements = 27761 Number of triangles = 4072 Number of quadrilatarals = 0 Number of tetrahedrals = 23689 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 2) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 2 (of 2) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 5221 Number of elements = 28313 Number of triangles = 4624 Number of quadrilatarals = 0 Number of tetrahedrals = 23689 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 2) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 1 (of 2): Number of nodes = 4882 Number of elements = 26790 Number of triangles = 4040 Number of quadrilatarals = 0 Number of tetrahedrals = 22750 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 2 (of 2) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 2 (of 2): Number of nodes = 339 Number of elements = 1523 Number of triangles = 584 Number of quadrilatarals = 0 Number of tetrahedrals = 939 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file ../csmData/MultiDomain/multi_prim.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 32776 Number of elements = 189806 Number of triangles = 8496 Number of quadrilatarals = 0 Number of tetrahedrals = 181310 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 5) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 2 (of 5) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 3 (of 5) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 4 (of 5) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 5 (of 5) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 36115 Number of elements = 203130 Number of triangles = 21820 Number of quadrilatarals = 0 Number of tetrahedrals = 181310 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 5) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 1 (of 5): Number of nodes = 28584 Number of elements = 162362 Number of triangles = 15158 Number of quadrilatarals = 0 Number of tetrahedrals = 147204 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 2 (of 5) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 2 (of 5): Number of nodes = 1425 Number of elements = 7592 Number of triangles = 1456 Number of quadrilatarals = 0 Number of tetrahedrals = 6136 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 3 (of 5) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 3 (of 5): Number of nodes = 4138 Number of elements = 22901 Number of triangles = 2938 Number of quadrilatarals = 0 Number of tetrahedrals = 19963 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 4 (of 5) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 4 (of 5): Number of nodes = 711 Number of elements = 3685 Number of triangles = 844 Number of quadrilatarals = 0 Number of tetrahedrals = 2841 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 5 (of 5) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 5 (of 5): Number of nodes = 1257 Number of elements = 6590 Number of triangles = 1424 Number of quadrilatarals = 0 Number of tetrahedrals = 5166 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file ../csmData/MultiDomain/cyl_seam.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 16639 Number of elements = 94369 Number of triangles = 8800 Number of quadrilatarals = 0 Number of tetrahedrals = 85569 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 2) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 2 (of 2) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 18563 Number of elements = 101745 Number of triangles = 16176 Number of quadrilatarals = 0 Number of tetrahedrals = 85569 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 2) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 1 (of 2): Number of nodes = 12009 Number of elements = 67436 Number of triangles = 7140 Number of quadrilatarals = 0 Number of tetrahedrals = 60296 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 2 (of 2) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 2 (of 2): Number of nodes = 6554 Number of elements = 34309 Number of triangles = 9036 Number of quadrilatarals = 0 Number of tetrahedrals = 25273 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file ok test_journal (test_aflr3.TestAFLR3.test_journal) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 2865 Number of elements = 12676 Number of triangles = 5452 Number of quadrilatarals = 0 Number of tetrahedrals = 7224 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 2477 Number of elements = 10753 Number of triangles = 4552 Number of quadrilatarals = 0 Number of tetrahedrals = 6201 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 2865 Number of elements = 12676 Number of triangles = 5452 Number of quadrilatarals = 0 Number of tetrahedrals = 7224 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 2477 Number of elements = 10753 Number of triangles = 4552 Number of quadrilatarals = 0 Number of tetrahedrals = 6201 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 ok test_phase (test_aflr3.TestAFLR3.test_phase) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 2865 Number of elements = 12676 Number of triangles = 5452 Number of quadrilatarals = 0 Number of tetrahedrals = 7224 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 2477 Number of elements = 10753 Number of triangles = 4552 Number of quadrilatarals = 0 Number of tetrahedrals = 6201 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file ok test_reenter (test_aflr3.TestAFLR3.test_reenter) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 2865 Number of elements = 12676 Number of triangles = 5452 Number of quadrilatarals = 0 Number of tetrahedrals = 7224 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Binary VTK file .... Finished writing Binary VTK file Writing vtk file .... Writing vtk general file .... Finished writing vtk file Writing FAST file .... Finished writing FAST file Writing SU2 file .... Finished writing SU2 file Writing Binary STL file .... Finished writing Binary STL file Writing ASCII STL file .... Finished writing ASCII STL file Writing Tecplot file .... Finished writing Tecplot file Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 2477 Number of elements = 10753 Number of triangles = 4552 Number of quadrilatarals = 0 Number of tetrahedrals = 6201 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Binary VTK file .... Finished writing Binary VTK file Writing vtk file .... Writing vtk general file .... Finished writing vtk file Writing FAST file .... Finished writing FAST file Writing SU2 file .... Finished writing SU2 file Writing Binary STL file .... Finished writing Binary STL file Writing ASCII STL file .... Finished writing ASCII STL file Writing Tecplot file .... Finished writing Tecplot file ok test_setInput (test_aflr3.TestAFLR3.test_setInput) ... EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! ok test_sphere (test_aflr3.TestAFLR3.test_sphere) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = sphere, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = sphere, index = 1 Name = farfield, index = 2 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 4989 Number of elements = 27641 Number of triangles = 3462 Number of quadrilatarals = 0 Number of tetrahedrals = 24179 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file ok test_torus (test_aflr3.TestAFLR3.test_torus) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = torus, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = torus, index = 1 Name = farfield, index = 2 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 6401 Number of elements = 35742 Number of triangles = 4048 Number of quadrilatarals = 0 Number of tetrahedrals = 31694 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file ok test_transp (test_aflr3.TestAFLR3.test_transp) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Wake, index = 3 Name = Farfield, index = 4 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 4 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Wake, index = 3 Name = Farfield, index = 4 AFLR4 : Proximity BG Surface Grid Generation Skipped AFLR4 : No Modifications Required Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 4 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Wake, index = 3 Name = Farfield, index = 4 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Wake, index = 3 Name = Farfield, index = 4 Getting mesh sizing parameters Mesh sizing name - Wake Done getting mesh sizing parameters Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 59702 Number of elements = 348382 Number of triangles = 12928 Number of quadrilatarals = 0 Number of tetrahedrals = 335454 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Getting mesh sizing parameters Mesh sizing name - Wake Done getting mesh sizing parameters Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 58332 Number of elements = 339688 Number of triangles = 12428 Number of quadrilatarals = 0 Number of tetrahedrals = 327260 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Getting mesh sizing parameters Mesh sizing name - Wake Done getting mesh sizing parameters Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 59702 Number of elements = 347882 Number of triangles = 12428 Number of quadrilatarals = 0 Number of tetrahedrals = 335454 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file ok test_MultiBody_quad (test_aflr4.TestAFLR4.test_MultiBody_quad) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Wake, index = 3 Name = Farfield, index = 4 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 4 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Wake, index = 3 Name = Farfield, index = 4 AFLR4 : Proximity BG Surface Grid Generation Skipped AFLR4 : No Modifications Required ok test_SingleBody_output (test_aflr4.TestAFLR4.test_SingleBody_output) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Getting mesh sizing parameters Mesh sizing name - trailingEdge Done getting mesh sizing parameters ok test_all (test_aflr4.TestAFLR4.test_all) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62031) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 8 Name = box, index = 1 Name = cylinder, index = 2 Name = cone, index = 3 Name = torus, index = 4 Name = sphere, index = 5 Name = boxhole, index = 6 Name = bullet, index = 7 Name = farfield, index = 8 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 ok test_box (test_aflr4.TestAFLR4.test_box) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 ok test_boxhole (test_aflr4.TestAFLR4.test_boxhole) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = boxhole, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 ok test_bullet (test_aflr4.TestAFLR4.test_bullet) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = bullet, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 ok test_cone (test_aflr4.TestAFLR4.test_cone) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = cone, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 ok test_cylinder (test_aflr4.TestAFLR4.test_cylinder) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = cylinder, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 ok test_faceMatch (test_aflr4.TestAFLR4.test_faceMatch) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 ok test_faceMatch_MultiDomain (test_aflr4.TestAFLR4.test_faceMatch_MultiDomain) ... ../csmData/MultiDomain/example1.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file ../csmData/MultiDomain/example2.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file ../csmData/MultiDomain/example3.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file ../csmData/MultiDomain/example4.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file ../csmData/MultiDomain/example6.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file ../csmData/MultiDomain/example7.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file ../csmData/MultiDomain/example8.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file ../csmData/MultiDomain/example9.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file ../csmData/MultiDomain/multi_prim.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file ../csmData/MultiDomain/cyl_seam.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file ok test_invalid_Mesh_Lenght_Scale (test_aflr4.TestAFLR4.test_invalid_Mesh_Lenght_Scale) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 ok test_journal (test_aflr4.TestAFLR4.test_journal) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62031) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62031) ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62031) CAPS Info: Hit last success -- going live! ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62031) CAPS Info: Hit last success -- going live! ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62031) CAPS Info: Hit last success -- going live! ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62031) CAPS Info: Hit last success -- going live! ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62031) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62031) CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62031) CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62031) CAPS Info: Hit last success -- going live! ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62031) CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62031) CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62031) ok test_phase (test_aflr4.TestAFLR4.test_phase) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62031) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62031) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 ok test_reenter (test_aflr4.TestAFLR4.test_reenter) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Writing Binary VTK file .... Finished writing Binary VTK file Writing vtk file .... Writing vtk surface file .... capsGroups found: 1: Farfield 2: Wing1 Finished writing vtk file Writing FAST file .... Finished writing FAST file Writing SU2 file .... Finished writing SU2 file Writing Binary STL file .... Finished writing Binary STL file Writing ASCII STL file .... Finished writing ASCII STL file Writing Tecplot file .... Finished writing Tecplot file Writing ugrid file .... Finished writing ugrid file Writing Binary VTK file .... Finished writing Binary VTK file Writing vtk file .... Writing vtk surface file .... capsGroups found: 1: Farfield 2: Wing1 Finished writing vtk file Writing FAST file .... Finished writing FAST file Writing SU2 file .... Finished writing SU2 file Writing Binary STL file .... Finished writing Binary STL file Writing ASCII STL file .... Finished writing ASCII STL file Writing Tecplot file .... Finished writing Tecplot file Writing ugrid file .... Finished writing ugrid file ok test_setInput (test_aflr4.TestAFLR4.test_setInput) ... ok EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! test_sphere (test_aflr4.TestAFLR4.test_sphere) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = sphere, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 ok test_torus (test_aflr4.TestAFLR4.test_torus) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = torus, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 ok test_Aeroelastic (test_astros.TestAstros.test_Aeroelastic) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Rib_Root, index = 1 Name = Skin, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting surface mesh for body 1 (of 2) Getting surface mesh for body 2 (of 2) Body 1 (of 2) Number of nodes = 1 Number of elements = 0 Number of triangle elements = 0 Number of quadrilateral elements = 0 Body 2 (of 2) Number of nodes = 46 Number of elements = 44 Number of triangle elements = 0 Number of quadrilateral elements = 44 ---------------------------- Total number of nodes = 47 Total number of elements = 44 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_Point, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 1 Name = Skin_Top, index = 1 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 1 Name = Rib_Root, index = 1 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 = Rib_Root, index = 1 Name = Skin, index = 2 Name = Wing, index = 3 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Rib_Root, index = 1 Name = Skin, index = 2 Name = Wing, index = 3 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 1 Number of elements = 1 Elemental Nodes = 1 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 0 Setting FEA Data Mesh for body = 1 Number of nodal coordinates = 46 Number of elements = 44 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 44 Combining multiple FEA meshes! Combined Number of nodal coordinates = 47 Combined Number of elements = 45 Combined Elemental Nodes = 1 Combined Elemental Rods = 0 Combined Elemental Tria3 = 0 Combined Elemental Quad4 = 44 Getting vortex lattice surface data VLM surface name - Skin_Top Done getting vortex lattice surface data Getting FEA vortex lattice mesh Surface 1: Number of points found for aero-spline = 3 Surface 2: Number of points found for aero-spline = 6 (Re-)Combining all aerodynamic surfaces into a 'Wing', 'Canard', and/or 'Fin' single surfaces ! Aero_Reference value is NULL - No aero reference parameters set Getting FEA materials....... Number of materials - 1 Material name - Unobtainium No "materialType" specified for Material tuple Unobtainium, defaulting to "Isotropic" Done getting FEA materials Getting FEA properties....... Number of properties - 2 Property name - Rib_Root No "material" specified for Property tuple Rib_Root, defaulting to an index of 1 Property name - Skin No "material" specified for Property tuple Skin, defaulting to an index of 1 Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - ribConstraint No "constraintType" specified for Constraint tuple ribConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Getting FEA supports....... Number of supports - 1 Support name - ribSupport Done getting FEA supports Getting FEA connections....... Number of connection tuples - 1 Connection name - Rib_Root No "groupName" specified for Connection tuple Rib_Root! Looking for automatic connections from the use of capsConnectLink for Rib_Root 8 automatic connections were made for capsConnect Rib_Root (node id 1) Done getting FEA connections Load tuple is NULL - No loads applied 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 Getting FEA analyses....... Number of analyses - 1 Analysis name - Trim1 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 connection cards - appending mesh file Writing Astros instruction file.... Writing aeros card Writing analysis cards Writing constraint cards--each subcase individually Writing support cards Writing material cards Writing property cards Writing aeroelastic cards Running Astros...... Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG IEEE_DENORMAL Done running Astros! ok test_Plate (test_astros.TestAstros.test_Plate) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Face 1 TFI quading disabled with attribute .qParams Getting surface mesh for body 1 (of 1) Body 1 (of 1) Number of nodes = 25 Number of elements = 16 Number of triangle elements = 0 Number of quadrilateral elements = 16 ---------------------------- Total number of nodes = 25 Total number of elements = 16 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 = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 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 = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 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 - 1 Property name - plate 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 - appliedPressure 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 .... 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 IEEE_DENORMAL 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 - 1 Property name - plate 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 - appliedPressure 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 large 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 IEEE_DENORMAL 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 - 1 Property name - plate 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 - appliedPressure 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 Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG IEEE_DENORMAL ok test_MassProp_Units (test_avl.TestAVL.test_MassProp_Units) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 5 Name = Wing, index = 1 Name = hTail, index = 2 Name = vTail, index = 3 Name = VTail1, index = 4 Name = VTail2, index = 5 Getting vortex lattice surface data VLM surface name - Wing Done getting vortex lattice surface data Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 5 Name = Wing, index = 1 Name = hTail, index = 2 Name = vTail, index = 3 Name = VTail1, index = 4 Name = VTail2, index = 5 Getting vortex lattice surface data VLM surface name - Wing Done getting vortex lattice surface data Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Writing surface - Wing (ID = 0) Section 1 of 4 (ID = 3) Control surface 1 of 1 Section 2 of 4 (ID = 2) Control surface 1 of 1 Section 3 of 4 (ID = 1) Control surface 1 of 1 Section 4 of 4 (ID = 0) Control surface 1 of 1 Writing mass properties file: caps.mass Parsing MassProp Note: The following floating-point exceptions are signalling: IEEE_DIVIDE_BY_ZERO Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Writing mass properties file: caps.mass Parsing MassProp Note: The following floating-point exceptions are signalling: IEEE_DIVIDE_BY_ZERO Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Writing mass properties file: caps.mass Parsing MassProp Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Writing mass properties file: caps.mass Parsing MassProp Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Writing mass properties file: caps.mass Parsing MassProp Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Writing mass properties file: caps.mass Parsing MassProp Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Writing mass properties file: caps.mass Parsing MassProp Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Writing mass properties file: caps.mass Parsing MassProp Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Writing mass properties file: caps.mass Parsing MassProp ok test_MassProp_noUnits (test_avl.TestAVL.test_MassProp_noUnits) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 5 Name = Wing, index = 1 Name = hTail, index = 2 Name = vTail, index = 3 Name = VTail1, index = 4 Name = VTail2, index = 5 Getting vortex lattice surface data VLM surface name - Wing Done getting vortex lattice surface data Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 5 Name = Wing, index = 1 Name = hTail, index = 2 Name = vTail, index = 3 Name = VTail1, index = 4 Name = VTail2, index = 5 Getting vortex lattice surface data VLM surface name - Wing Done getting vortex lattice surface data Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Writing surface - Wing (ID = 0) Section 1 of 4 (ID = 3) Control surface 1 of 1 Section 2 of 4 (ID = 2) Control surface 1 of 1 Section 3 of 4 (ID = 1) Control surface 1 of 1 Section 4 of 4 (ID = 0) Control surface 1 of 1 Writing mass properties file: caps.mass Parsing MassProp Note: The following floating-point exceptions are signalling: IEEE_DIVIDE_BY_ZERO Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Writing mass properties file: caps.mass Parsing MassProp Note: The following floating-point exceptions are signalling: IEEE_DIVIDE_BY_ZERO Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Writing mass properties file: caps.mass Parsing MassProp Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Writing mass properties file: caps.mass Parsing MassProp Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Writing mass properties file: caps.mass Parsing MassProp Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Writing mass properties file: caps.mass Parsing MassProp ok test_alpha_custom_increment (test_avl.TestAVL.test_alpha_custom_increment) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 5 Name = Wing, index = 1 Name = hTail, index = 2 Name = vTail, index = 3 Name = VTail1, index = 4 Name = VTail2, index = 5 Getting vortex lattice surface data VLM surface name - Wing Done getting vortex lattice surface data Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Writing surface - Wing (ID = 0) Section 1 of 4 (ID = 3) Control surface 1 of 1 Section 2 of 4 (ID = 2) Control surface 1 of 1 Section 3 of 4 (ID = 1) Control surface 1 of 1 Section 4 of 4 (ID = 0) Control surface 1 of 1 Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. ok test_geom_change (test_avl.TestAVL.test_geom_change) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 5 Name = Wing, index = 1 Name = hTail, index = 2 Name = vTail, index = 3 Name = VTail1, index = 4 Name = VTail2, index = 5 Getting vortex lattice surface data VLM surface name - Wing Done getting vortex lattice surface data Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Writing surface - Wing (ID = 0) Section 1 of 4 (ID = 3) Control surface 1 of 1 Section 2 of 4 (ID = 2) Control surface 1 of 1 Section 3 of 4 (ID = 1) Control surface 1 of 1 Section 4 of 4 (ID = 0) Control surface 1 of 1 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 5 Name = Wing, index = 1 Name = hTail, index = 2 Name = vTail, index = 3 Name = VTail1, index = 4 Name = VTail2, index = 5 Getting vortex lattice surface data VLM surface name - Wing Done getting vortex lattice surface data Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Writing surface - Wing (ID = 0) Section 1 of 4 (ID = 3) Control surface 1 of 1 Section 2 of 4 (ID = 2) Control surface 1 of 1 Section 3 of 4 (ID = 1) Control surface 1 of 1 Section 4 of 4 (ID = 0) Control surface 1 of 1 ok test_numSpan (test_avl.TestAVL.test_numSpan) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 5 Name = Wing, index = 1 Name = hTail, index = 2 Name = vTail, index = 3 Name = VTail1, index = 4 Name = VTail2, index = 5 Getting vortex lattice surface data VLM surface name - Wing Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 5 Name = Wing, index = 1 Name = hTail, index = 2 Name = vTail, index = 3 Name = VTail1, index = 4 Name = VTail2, index = 5 Getting vortex lattice surface data VLM surface name - Wing ok test_phase (test_avl.TestAVL.test_phase) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 5 Name = Wing, index = 1 Name = hTail, index = 2 Name = vTail, index = 3 Name = VTail1, index = 4 Name = VTail2, index = 5 Getting vortex lattice surface data VLM surface name - Wing Done getting vortex lattice surface data Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Writing surface - Wing (ID = 0) Section 1 of 4 (ID = 3) Control surface 1 of 1 Section 2 of 4 (ID = 2) Control surface 1 of 1 Section 3 of 4 (ID = 1) Control surface 1 of 1 Section 4 of 4 (ID = 0) Control surface 1 of 1 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 5 Name = Wing, index = 1 Name = hTail, index = 2 Name = vTail, index = 3 Name = VTail1, index = 4 Name = VTail2, index = 5 Getting vortex lattice surface data VLM surface name - Wing Done getting vortex lattice surface data Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. ok test_wing_Vtail (test_avl.TestAVL.test_wing_Vtail) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 5 Name = Wing, index = 1 Name = hTail, index = 2 Name = vTail, index = 3 Name = VTail1, index = 4 Name = VTail2, index = 5 Getting vortex lattice surface data VLM surface name - VTail1 No "groupName" variable provided or no matches found, going to use tuple name VLM surface name - VTail2 No "groupName" variable provided or no matches found, going to use tuple name VLM surface name - Wing Done getting vortex lattice surface data Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Writing surface - VTail1 (ID = 0) Section 1 of 2 (ID = 1) Section 2 of 2 (ID = 0) Writing surface - VTail2 (ID = 1) Section 1 of 2 (ID = 0) Section 2 of 2 (ID = 1) Writing surface - Wing (ID = 2) Section 1 of 4 (ID = 3) Control surface 1 of 1 Section 2 of 4 (ID = 2) Control surface 1 of 1 Section 3 of 4 (ID = 1) Control surface 1 of 1 Section 4 of 4 (ID = 0) Control surface 1 of 1 ok test_wing_tail (test_avl.TestAVL.test_wing_tail) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 5 Name = Wing, index = 1 Name = hTail, index = 2 Name = vTail, index = 3 Name = VTail1, index = 4 Name = VTail2, index = 5 Getting vortex lattice surface data VLM surface name - Wing VLM surface name - hTail VLM surface name - vTail No "groupName" variable provided or no matches found, going to use tuple name Done getting vortex lattice surface data Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Warning: Control Elevator not found in controls tuple! Only defaults will be used. Warning: Control Elevator not found in controls tuple! Only defaults will be used. Warning: Control Elevator not found in controls tuple! Only defaults will be used. Warning: Control Rudder not found in controls tuple! Only defaults will be used. Warning: Control Rudder not found in controls tuple! Only defaults will be used. Writing surface - Wing (ID = 0) Section 1 of 4 (ID = 3) Control surface 1 of 1 Section 2 of 4 (ID = 2) Control surface 1 of 1 Section 3 of 4 (ID = 1) Control surface 1 of 1 Section 4 of 4 (ID = 0) Control surface 1 of 1 Writing surface - hTail (ID = 1) Section 1 of 3 (ID = 2) Control surface 1 of 1 Section 2 of 3 (ID = 1) Control surface 1 of 1 Section 3 of 3 (ID = 0) Control surface 1 of 1 Writing surface - vTail (ID = 2) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 ok test_wing_tail_control (test_avl.TestAVL.test_wing_tail_control) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 5 Name = Wing, index = 1 Name = hTail, index = 2 Name = vTail, index = 3 Name = VTail1, index = 4 Name = VTail2, index = 5 Getting vortex lattice control surface data VLM control surface name - Elevator VLM control surface name - LeftAileron VLM control surface name - RightAileron VLM control surface name - Rudder Done getting vortex lattice control surface data Getting vortex lattice surface data VLM surface name - Wing VLM surface name - hTail VLM surface name - vTail No "groupName" variable provided or no matches found, going to use tuple name Done getting vortex lattice surface data Writing surface - Wing (ID = 0) Section 1 of 4 (ID = 3) Control surface 1 of 1 Section 2 of 4 (ID = 2) Control surface 1 of 1 Section 3 of 4 (ID = 1) Control surface 1 of 1 Section 4 of 4 (ID = 0) Control surface 1 of 1 Writing surface - hTail (ID = 1) Section 1 of 3 (ID = 2) Control surface 1 of 1 Section 2 of 3 (ID = 1) Control surface 1 of 1 Section 3 of 3 (ID = 0) Control surface 1 of 1 Writing surface - vTail (ID = 2) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 ok test_TargetCL (test_cart3d.TestCart3D.test_TargetCL) ... skipped 'No flowCart executable' test_outputs (test_cart3d.TestCart3D.test_outputs) ... skipped 'No flowCart executable' test_reenter (test_cart3d.TestCart3D.test_reenter) ... skipped 'No flowCart executable' test_sensitivity_AnalysisIn (test_cart3d.TestCart3D.test_sensitivity_AnalysisIn) ... skipped 'No flowCart executable' test_sensitivity_GeometryIn (test_cart3d.TestCart3D.test_sensitivity_GeometryIn) ... skipped 'No flowCart executable' test_Output (test_cbaero.TestCBAERO.test_Output) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = Wing1, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 2 Name = Wing1, index = 1 Name = trailingEdge, index = 2 Writing FAST file .... Finished writing FAST file Writing CBAero input file - cbaero_CAPS.cbaero Writing CBAero tagged regions - TaggedRegions Writing CBAero setup file - cbaero_CAPS.stp ok test_inputs (test_cbaero.TestCBAERO.test_inputs) ... Writing CBAero input file - cbaero_CAPS.cbaero Writing CBAero tagged regions - TaggedRegions Writing CBAero setup file - cbaero_CAPS.stp ok test_MultiBody (test_egadsTess.TestEGADS.test_MultiBody) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Wake, index = 3 Name = Farfield, index = 4 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 4 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Wake, index = 3 Name = Farfield, index = 4 Getting mesh sizing parameters Mesh sizing name - Farfield Done getting mesh sizing parameters ok test_SingleBody_AnalysisOutVal (test_egadsTess.TestEGADS.test_SingleBody_AnalysisOutVal) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Getting mesh sizing parameters Mesh sizing name - Farfield Done getting mesh sizing parameters ok test_all (test_egadsTess.TestEGADS.test_all) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62031) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 9 Name = box, index = 1 Name = cylinder, index = 2 Name = cone, index = 3 Name = torus, index = 4 Name = sphere, index = 5 Name = boxhole, index = 6 Name = bullet, index = 7 Name = nodeBody, index = 8 Name = farfield, index = 9 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 112A55E00 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1! 112A55E00 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1! 700007FC5000 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1! 700007FC5000 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 4 7, sen = 1! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 9 Name = box, index = 1 Name = cylinder, index = 2 Name = cone, index = 3 Name = torus, index = 4 Name = sphere, index = 5 Name = boxhole, index = 6 Name = bullet, index = 7 Name = nodeBody, index = 8 Name = farfield, index = 9 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 112A55E00 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1! 112A55E00 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1! 700007FC5000 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1! 700007FC5000 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 4 7, sen = 1! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 9 Name = box, index = 1 Name = cylinder, index = 2 Name = cone, index = 3 Name = torus, index = 4 Name = sphere, index = 5 Name = boxhole, index = 6 Name = bullet, index = 7 Name = nodeBody, index = 8 Name = farfield, index = 9 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 700007FC5000 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1! 700007FC5000 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1! 112A55E00 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1! 112A55E00 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 4 7, sen = 1! ok test_box (test_egadsTess.TestEGADS.test_box) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 ok test_boxhole (test_egadsTess.TestEGADS.test_boxhole) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = boxhole, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 112A55E00 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1! 112A55E00 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1! 700007FC5000 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1! 700007FC5000 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 4 7, sen = 1! ok test_bullet (test_egadsTess.TestEGADS.test_bullet) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = bullet, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 ok test_cone (test_egadsTess.TestEGADS.test_cone) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = cone, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 ok test_cylinder (test_egadsTess.TestEGADS.test_cylinder) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = cylinder, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 ok test_invalid_Mesh_Lenght_Scale (test_egadsTess.TestEGADS.test_invalid_Mesh_Lenght_Scale) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 ok test_journal (test_egadsTess.TestEGADS.test_journal) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62031) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Getting mesh sizing parameters Mesh sizing name - box Done getting mesh sizing parameters Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Getting mesh sizing parameters Mesh sizing name - box Done getting mesh sizing parameters EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62031) ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62031) CAPS Info: Hit last success -- going live! ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62031) CAPS Info: Hit last success -- going live! ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62031) CAPS Info: Hit last success -- going live! ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62031) CAPS Info: Hit last success -- going live! ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62031) CAPS Info: Hit last success -- going live! ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62031) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Getting mesh sizing parameters Mesh sizing name - box Done getting mesh sizing parameters ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62031) CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Getting mesh sizing parameters Mesh sizing name - box Done getting mesh sizing parameters ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62031) CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Getting mesh sizing parameters Mesh sizing name - box Done getting mesh sizing parameters ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62031) CAPS Info: Hit last success -- going live! ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62031) CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Getting mesh sizing parameters Mesh sizing name - box Done getting mesh sizing parameters ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62031) CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Getting mesh sizing parameters Mesh sizing name - box Done getting mesh sizing parameters ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62031) CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Getting mesh sizing parameters Mesh sizing name - box Done getting mesh sizing parameters ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62031) ok test_nodeBody (test_egadsTess.TestEGADS.test_nodeBody) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = nodeBody, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 ok test_phase (test_egadsTess.TestEGADS.test_phase) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62031) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Getting mesh sizing parameters Mesh sizing name - box Done getting mesh sizing parameters ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62031) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Getting mesh sizing parameters Mesh sizing name - box Done getting mesh sizing parameters Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Getting mesh sizing parameters Mesh sizing name - box Done getting mesh sizing parameters ok test_reenter (test_egadsTess.TestEGADS.test_reenter) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Getting mesh sizing parameters Mesh sizing name - Farfield Done getting mesh sizing parameters Writing Binary VTK file .... Finished writing Binary VTK file Writing vtk file .... Writing vtk surface file .... capsGroups found: 1: Farfield 2: Wing1 Finished writing vtk file Writing FAST file .... Finished writing FAST file Writing SU2 file .... Finished writing SU2 file Writing Binary STL file .... Finished writing Binary STL file Writing ASCII STL file .... Finished writing ASCII STL file Writing Tecplot file .... Finished writing Tecplot file Writing ugrid file .... Finished writing ugrid file Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Getting mesh sizing parameters Mesh sizing name - Farfield Done getting mesh sizing parameters Writing Binary VTK file .... Finished writing Binary VTK file Writing vtk file .... Writing vtk surface file .... capsGroups found: 1: Farfield 2: Wing1 Finished writing vtk file Writing FAST file .... Finished writing FAST file Writing SU2 file .... Finished writing SU2 file Writing Binary STL file .... Finished writing Binary STL file Writing ASCII STL file .... Finished writing ASCII STL file Writing Tecplot file .... Finished writing Tecplot file Writing ugrid file .... Finished writing ugrid file ok test_setInput (test_egadsTess.TestEGADS.test_setInput) ... ok test_sphere (test_egadsTess.TestEGADS.test_sphere) ... EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = sphere, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 ok test_torus (test_egadsTess.TestEGADS.test_torus) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = torus, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 ok test_Design_SensFile (test_fun3d.TestFUN3D.test_Design_SensFile) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Getting mesh sizing parameters Mesh sizing name - Farfield Done getting mesh sizing parameters Getting surface mesh for body 1 (of 3) Getting surface mesh for body 2 (of 3) Getting surface mesh for body 3 (of 3) Body 1 (of 3) Number of nodes = 7820 Number of elements = 15636 Number of triangle elements = 15636 Number of quadrilateral elements = 0 Body 2 (of 3) Number of nodes = 5889 Number of elements = 11774 Number of triangle elements = 11774 Number of quadrilateral elements = 0 Body 3 (of 3) Number of nodes = 524 Number of elements = 1044 Number of triangle elements = 1044 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 14233 Total number of elements = 28454 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Number of surface: nodes - 14233, elements - 28454 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000T1.00e-16A Delaunizing vertices... Delaunay seconds: 0.186092 Creating surface mesh ... Surface mesh seconds: 0.036518 Recovering boundaries... Boundary recovery seconds: 0.107324 Removing exterior tetrahedra ... Spreading region attributes. Exterior tets removal seconds: 0.053035 Recovering Delaunayness... Delaunay recovery seconds: 0.056446 Refining mesh... 18972 insertions, added 13254 points, 701278 tetrahedra in queue. 6317 insertions, added 2883 points, 614952 tetrahedra in queue. 8421 insertions, added 2047 points, 103425 tetrahedra in queue. Refinement seconds: 2.22881 Smoothing vertices... Mesh smoothing seconds: 2.2177 Improving mesh... Mesh improvement seconds: 0.043755 Writing nodes. Writing elements. Writing faces. Writing edges. Output seconds: 0.016466 Total running seconds: 4.94709 Statistics: Input points: 14233 Input facets: 28454 Input segments: 42681 Input holes: 2 Input regions: 0 Mesh points: 33078 Mesh tetrahedra: 159812 Mesh faces: 333851 Mesh faces on exterior boundary: 28454 Mesh faces on input facets: 28454 Mesh edges on input segments: 42681 Steiner points inside domain: 18845 Done meshing using TetGen! Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - Wing2 Done getting CFD boundary conditions Getting CFD design variables....... Number of design variables - 5 Design Variable name - Mach Warning: No initial value set for Mach Design Variable name - area Design Variable name - aspect Design Variable name - taper Design Variable name - twist Done getting CFD design variables Python library was linked, but will not be used! Creating FUN3D directory tree Writing MAPBC file .... Finished writing MAPBC file Warning: The fun3d.nml file will be overwritten! Writing fun3d.nml Info: No recognized data transfer names found. ok test_Design_Sensitivity (test_fun3d.TestFUN3D.test_Design_Sensitivity) ... Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - Wing2 Done getting CFD boundary conditions Getting CFD design variables....... Number of design variables - 6 Design Variable name - Alpha Design Variable name - Beta Warning: No initial value set for Beta Design Variable name - area Design Variable name - aspect Design Variable name - taper Design Variable name - twist Done getting CFD design variables Getting CFD functional....... Number of design variables - 2 Objective name - Composite Objective name - Lift^2 Done getting CFD functional Python library was linked, but will not be used! Creating FUN3D directory tree Writing rubber.data Writing MAPBC file .... Finished writing MAPBC file Warning: The fun3d.nml file will be overwritten! Writing fun3d.nml Info: No recognized data transfer names found. Reading rubber.data Creating FUN3D directory tree DesignVariable = Alpha DesignVariable = Beta DesignVariable = area DesignVariable = aspect DesignVariable = taper DesignVariable = twist Writing sensitivity file for body 1, File - Rubberize/model.tec.1.sd1 Writing sensitivity file for body 2, File - Rubberize/model.tec.2.sd1 Writing sensitivity file for body 3, File - Rubberize/model.tec.3.sd1 Writing rubber.data Writing MAPBC file .... Finished writing MAPBC file Using Python to write FUN3D namelist (fun3d.nml) Overwrite_NML is set to 'True' - a new namelist will be created Creating namelist Done writing nml file with Python Info: No recognized data transfer names found. Reading rubber.data Getting CFD design variables....... Number of design variables - 1 Design Variable name - Alpha Done getting CFD design variables Getting CFD functional....... Number of design variables - 2 Objective name - Composite Objective name - Lift^2 Done getting CFD functional Creating FUN3D directory tree DesignVariable = Alpha Writing rubber.data Writing MAPBC file .... Finished writing MAPBC file Using Python to write FUN3D namelist (fun3d.nml) Overwrite_NML is set to 'True' - a new namelist will be created Creating namelist Done writing nml file with Python Info: No recognized data transfer names found. Reading rubber.data ok test_Mesh_Morph_Sensitivity (test_fun3d.TestFUN3D.test_Mesh_Morph_Sensitivity) ... Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - Wing2 Done getting CFD boundary conditions Getting CFD design variables....... Number of design variables - 6 Design Variable name - Alpha Design Variable name - Beta Warning: No initial value set for Beta Design Variable name - area Design Variable name - aspect Design Variable name - taper Design Variable name - twist Done getting CFD design variables Getting CFD functional....... Number of design variables - 2 Objective name - Composite Objective name - Lift^2 Done getting CFD functional Python library was linked, but will not be used! Creating FUN3D directory tree DesignVariable = Alpha DesignVariable = Beta DesignVariable = area DesignVariable = aspect DesignVariable = taper DesignVariable = twist Writing sensitivity file for body 1, File - Rubberize/model.tec.1.sd1 Writing sensitivity file for body 2, File - Rubberize/model.tec.2.sd1 Writing sensitivity file for body 3, File - Rubberize/model.tec.3.sd1 Writing rubber.data Writing surface file for 1 (of 3) in body 1 File - Flow/fun3d_CAPS_body1.dat Writing surface file for 1 (of 3) in body 1 File - Flow/fun3d_CAPS_body1.dat Writing surface file for 1 (of 3) in body 1 File - Flow/fun3d_CAPS_body1.dat Writing MAPBC file .... Finished writing MAPBC file Warning: The fun3d.nml file will be overwritten! Writing fun3d.nml Info: No recognized data transfer names found. Reading rubber.data Projecting tessellation 1 (of 3) on to new body Projecting tessellation 2 (of 3) on to new body Projecting tessellation 3 (of 3) on to new body Python library was linked, but will not be used! Creating FUN3D directory tree DesignVariable = Alpha DesignVariable = Beta DesignVariable = area DesignVariable = aspect DesignVariable = taper DesignVariable = twist Writing sensitivity file for body 1, File - Rubberize/model.tec.1.sd1 Writing sensitivity file for body 2, File - Rubberize/model.tec.2.sd1 Writing sensitivity file for body 3, File - Rubberize/model.tec.3.sd1 Writing surface file for 1 (of 3) in body 1 File - Flow/fun3d_CAPS_body1.dat Writing surface file for 1 (of 3) in body 1 File - Flow/fun3d_CAPS_body1.dat Writing surface file for 1 (of 3) in body 1 File - Flow/fun3d_CAPS_body1.dat Writing MAPBC file .... Finished writing MAPBC file Warning: The fun3d.nml file will be overwritten! Writing fun3d.nml Info: No recognized data transfer names found. Reading rubber.data Projecting tessellation 1 (of 3) on to new body Projecting tessellation 2 (of 3) on to new body Projecting tessellation 3 (of 3) on to new body Python library was linked, but will not be used! Creating FUN3D directory tree DesignVariable = Alpha DesignVariable = Beta DesignVariable = area DesignVariable = aspect DesignVariable = taper DesignVariable = twist Writing sensitivity file for body 1, File - Rubberize/model.tec.1.sd1 Writing sensitivity file for body 2, File - Rubberize/model.tec.2.sd1 Writing sensitivity file for body 3, File - Rubberize/model.tec.3.sd1 Writing surface file for 1 (of 3) in body 1 File - Flow/fun3d_CAPS_body1.dat Writing surface file for 1 (of 3) in body 1 File - Flow/fun3d_CAPS_body1.dat Writing surface file for 1 (of 3) in body 1 File - Flow/fun3d_CAPS_body1.dat Writing MAPBC file .... Finished writing MAPBC file Warning: The fun3d.nml file will be overwritten! Writing fun3d.nml Info: No recognized data transfer names found. Reading rubber.data ok test_cythonNML (test_fun3d.TestFUN3D.test_cythonNML) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Getting mesh sizing parameters Mesh sizing name - Farfield Done getting mesh sizing parameters Getting surface mesh for body 1 (of 3) Getting surface mesh for body 2 (of 3) Getting surface mesh for body 3 (of 3) Body 1 (of 3) Number of nodes = 7820 Number of elements = 15636 Number of triangle elements = 15636 Number of quadrilateral elements = 0 Body 2 (of 3) Number of nodes = 5889 Number of elements = 11774 Number of triangle elements = 11774 Number of quadrilateral elements = 0 Body 3 (of 3) Number of nodes = 524 Number of elements = 1044 Number of triangle elements = 1044 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 14233 Total number of elements = 28454 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Number of surface: nodes - 14233, elements - 28454 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000T1.00e-16A Delaunizing vertices... Delaunay seconds: 0.178137 Creating surface mesh ... Surface mesh seconds: 0.035875 Recovering boundaries... Boundary recovery seconds: 0.11415 Removing exterior tetrahedra ... Spreading region attributes. Exterior tets removal seconds: 0.05717 Recovering Delaunayness... Delaunay recovery seconds: 0.062786 Refining mesh... 18972 insertions, added 13254 points, 701278 tetrahedra in queue. 6317 insertions, added 2883 points, 614952 tetrahedra in queue. 8421 insertions, added 2047 points, 103425 tetrahedra in queue. Refinement seconds: 2.36923 Smoothing vertices... Mesh smoothing seconds: 2.30726 Improving mesh... Mesh improvement seconds: 0.041496 Writing nodes. Writing elements. Writing faces. Writing edges. Output seconds: 0.015899 Total running seconds: 5.18294 Statistics: Input points: 14233 Input facets: 28454 Input segments: 42681 Input holes: 2 Input regions: 0 Mesh points: 33078 Mesh tetrahedra: 159812 Mesh faces: 333851 Mesh faces on exterior boundary: 28454 Mesh faces on input facets: 28454 Mesh edges on input segments: 42681 Steiner points inside domain: 18845 Done meshing using TetGen! Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - Wing2 Done getting CFD boundary conditions Writing MAPBC file .... Finished writing MAPBC file Using Python to write FUN3D namelist (fun3d.nml) Reading /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/CAPS/aim/unitTest/pyCAPS/workDir_fun3dTest/Scratch/fun3dAIM4/fun3d.nml ..... Appending namelist Done writing nml file with Python Info: No recognized data transfer names found. ok test_cythonNMLError (test_fun3d.TestFUN3D.test_cythonNMLError) ... ok test_cythonNMLReentrance (test_fun3d.TestFUN3D.test_cythonNMLReentrance) ... Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - Wing2 Done getting CFD boundary conditions Writing MAPBC file .... Finished writing MAPBC file Using Python to write FUN3D namelist (fun3d.nml) /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/CAPS/aim/unitTest/pyCAPS/workDir_fun3dTest/Scratch/fun3dAIM6/fun3d.nml not found! Creating namelist Done writing nml file with Python Info: No recognized data transfer names found. Writing MAPBC file .... Finished writing MAPBC file Using Python to write FUN3D namelist (fun3d.nml) Reading /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/CAPS/aim/unitTest/pyCAPS/workDir_fun3dTest/Scratch/fun3dAIM6/fun3d.nml ..... Appending namelist Done writing nml file with Python Info: No recognized data transfer names found. ok test_invalidBoundary (test_fun3d.TestFUN3D.test_invalidBoundary) ... Getting CFD boundary conditions Boundary condition name - Wing1 ok test_invalidBoundaryName (test_fun3d.TestFUN3D.test_invalidBoundaryName) ... Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - X ok test_journal (test_fun3d.TestFUN3D.test_journal) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Getting mesh sizing parameters Mesh sizing name - Farfield Done getting mesh sizing parameters Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Number of surface: nodes - 5079, elements - 10146 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - Wing2 Done getting CFD boundary conditions Getting CFD design variables....... Number of design variables - 4 Design Variable name - area Design Variable name - aspect Design Variable name - taper Design Variable name - twist Done getting CFD design variables Python library was linked, but will not be used! Creating FUN3D directory tree Writing MAPBC file .... Finished writing MAPBC file Warning: The fun3d.nml file will be overwritten! Writing fun3d.nml Info: No recognized data transfer names found. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Getting mesh sizing parameters Mesh sizing name - Farfield Done getting mesh sizing parameters Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Number of surface: nodes - 5079, elements - 10146 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - Wing2 Done getting CFD boundary conditions Getting CFD design variables....... Number of design variables - 4 Design Variable name - area Design Variable name - aspect Design Variable name - taper Design Variable name - twist Done getting CFD design variables Python library was linked, but will not be used! Creating FUN3D directory tree Writing MAPBC file .... Finished writing MAPBC file Warning: The fun3d.nml file will be overwritten! Writing fun3d.nml Info: No recognized data transfer names found. CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Getting mesh sizing parameters Mesh sizing name - Farfield Done getting mesh sizing parameters CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Getting mesh sizing parameters Mesh sizing name - Farfield Done getting mesh sizing parameters Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - Wing2 Done getting CFD boundary conditions Getting CFD design variables....... Number of design variables - 4 Design Variable name - area Design Variable name - aspect Design Variable name - taper Design Variable name - twist Done getting CFD design variables CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! ok test_moving_body (test_fun3d.TestFUN3D.test_moving_body) ... Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - Wing2 Done getting CFD boundary conditions Python library was linked, but will not be used! Writing MAPBC file .... Finished writing MAPBC file Warning: The fun3d.nml file will be overwritten! Writing fun3d.nml Info: No recognized data transfer names found. Writing moving_body.input ok test_overwriteNML (test_fun3d.TestFUN3D.test_overwriteNML) ... Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - Wing2 Done getting CFD boundary conditions Python library was linked, but will not be used! Writing MAPBC file .... Finished writing MAPBC file Since Python was not linked and/or being used, the "Overwrite_NML" input needs to be set to "True" to give permission to create a new fun3d.nml. fun3d.nml will NOT be updated!! Info: No recognized data transfer names found. ok test_phase (test_fun3d.TestFUN3D.test_phase) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Getting mesh sizing parameters Mesh sizing name - Farfield Done getting mesh sizing parameters Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Number of surface: nodes - 14233, elements - 28454 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - Wing2 Done getting CFD boundary conditions Python library was linked, but will not be used! Writing MAPBC file .... Finished writing MAPBC file Since Python was not linked and/or being used, the "Overwrite_NML" input needs to be set to "True" to give permission to create a new fun3d.nml. fun3d.nml will NOT be updated!! Info: No recognized data transfer names found. Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Getting mesh sizing parameters Mesh sizing name - Farfield Done getting mesh sizing parameters Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - Wing2 Done getting CFD boundary conditions Python library was linked, but will not be used! Writing MAPBC file .... Finished writing MAPBC file Since Python was not linked and/or being used, the "Overwrite_NML" input needs to be set to "True" to give permission to create a new fun3d.nml. fun3d.nml will NOT be updated!! Info: No recognized data transfer names found. ok test_reenter (test_fun3d.TestFUN3D.test_reenter) ... Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - Wing2 Done getting CFD boundary conditions Python library was linked, but will not be used! Writing MAPBC file .... Finished writing MAPBC file Warning: The fun3d.nml file will be overwritten! Writing fun3d.nml Info: No recognized data transfer names found. Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - Wing2 Done getting CFD boundary conditions Python library was linked, but will not be used! Writing MAPBC file .... Finished writing MAPBC file Warning: The fun3d.nml file will be overwritten! Writing fun3d.nml Info: No recognized data transfer names found. ok test_symmetry (test_fun3d.TestFUN3D.test_symmetry) ... Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - Wing2 Done getting CFD boundary conditions Python library was linked, but will not be used! Writing MAPBC file .... Finished writing MAPBC file Since Python was not linked and/or being used, the "Overwrite_NML" input needs to be set to "True" to give permission to create a new fun3d.nml. fun3d.nml will NOT be updated!! Info: No recognized data transfer names found. ok test_box1 (test_masstran.TestMasstran.test_box1) ... 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 = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = box1, index = 1 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 2402 Number of elements = 2400 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 2400 Getting FEA materials....... Number of materials - 2 Material name - madeupium Material name - unobtainium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - box1 Done getting FEA properties Updating mesh element types based on properties input Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 7 Design_Variable name - H Design_Variable name - L Design_Variable name - W Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Number of design variable relations - 3 Done getting FEA design variables ===> L 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 = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = box1, index = 1 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 2402 Number of elements = 2400 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 2400 Updating mesh element types based on properties input 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 = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = box1, index = 1 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 2402 Number of elements = 2400 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 2400 Updating mesh element types based on properties input ===> W 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 = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = box1, index = 1 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 2402 Number of elements = 2400 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 2400 Updating mesh element types based on properties input 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 = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = box1, index = 1 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 2402 Number of elements = 2400 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 2400 Updating mesh element types based on properties input ===> H 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 = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = box1, index = 1 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 2402 Number of elements = 2400 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 2400 Updating mesh element types based on properties input 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 = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = box1, index = 1 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 2402 Number of elements = 2400 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 2400 Updating mesh element types based on properties input ===> x0 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 = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = box1, index = 1 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 2402 Number of elements = 2400 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 2400 Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Number of design variable relations - 3 Done getting FEA design variables Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Number of design variable relations - 3 Done getting FEA design variables ===> x1 Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Number of design variable relations - 3 Done getting FEA design variables Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Number of design variable relations - 3 Done getting FEA design variables ===> m0 Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Number of design variable relations - 3 Done getting FEA design variables Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Number of design variable relations - 3 Done getting FEA design variables ===> m1 Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Number of design variable relations - 3 Done getting FEA design variables Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Number of design variable relations - 3 Done getting FEA design variables ok test_box2 (test_masstran.TestMasstran.test_box2) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = box1, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 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 = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = box1, index = 1 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 1692 Number of elements = 3380 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 3380 Elemental Quad4 = 0 Getting FEA properties....... Number of properties - 1 Property name - box1 Done getting FEA properties Updating mesh element types based on properties input Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 7 Design_Variable name - H Design_Variable name - L Design_Variable name - W Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Number of design variable relations - 3 Done getting FEA design variables ===> L 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 = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = box1, index = 1 Projecting tessellation 1 (of 1) on to new body Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 1692 Number of elements = 3380 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 3380 Elemental Quad4 = 0 Updating mesh element types based on properties input 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 = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = box1, index = 1 Projecting tessellation 1 (of 1) on to new body Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 1692 Number of elements = 3380 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 3380 Elemental Quad4 = 0 Updating mesh element types based on properties input ===> W 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 = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = box1, index = 1 Projecting tessellation 1 (of 1) on to new body Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 1692 Number of elements = 3380 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 3380 Elemental Quad4 = 0 Updating mesh element types based on properties input 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 = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = box1, index = 1 Projecting tessellation 1 (of 1) on to new body Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 1692 Number of elements = 3380 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 3380 Elemental Quad4 = 0 Updating mesh element types based on properties input ===> H 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 = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = box1, index = 1 Projecting tessellation 1 (of 1) on to new body Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 1692 Number of elements = 3380 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 3380 Elemental Quad4 = 0 Updating mesh element types based on properties input 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 = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = box1, index = 1 Projecting tessellation 1 (of 1) on to new body Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 1692 Number of elements = 3380 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 3380 Elemental Quad4 = 0 Updating mesh element types based on properties input ===> x0 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 = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = box1, index = 1 Projecting tessellation 1 (of 1) on to new body Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 1692 Number of elements = 3380 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 3380 Elemental Quad4 = 0 Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Number of design variable relations - 3 Done getting FEA design variables Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Number of design variable relations - 3 Done getting FEA design variables ===> x1 Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Number of design variable relations - 3 Done getting FEA design variables Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Number of design variable relations - 3 Done getting FEA design variables ===> m0 Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Number of design variable relations - 3 Done getting FEA design variables Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Number of design variable relations - 3 Done getting FEA design variables ===> m1 Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Number of design variable relations - 3 Done getting FEA design variables Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Number of design variable relations - 3 Done getting FEA design variables ok test_box3 (test_masstran.TestMasstran.test_box3) ... 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 = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box1, index = 1 Name = box2, index = 2 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 2402 Number of elements = 2400 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 2400 Getting FEA properties....... Number of properties - 2 Property name - box1 Property name - box2 Done getting FEA properties Updating mesh element types based on properties input Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 7 Design_Variable name - H Design_Variable name - L Design_Variable name - W Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Design_Variable_Relation name - thick_box2 Number of design variable relations - 4 Done getting FEA design variables ===> L 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 = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box1, index = 1 Name = box2, index = 2 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 2402 Number of elements = 2400 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 2400 Updating mesh element types based on properties input 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 = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box1, index = 1 Name = box2, index = 2 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 2402 Number of elements = 2400 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 2400 Updating mesh element types based on properties input ===> W 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 = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box1, index = 1 Name = box2, index = 2 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 2402 Number of elements = 2400 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 2400 Updating mesh element types based on properties input 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 = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box1, index = 1 Name = box2, index = 2 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 2402 Number of elements = 2400 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 2400 Updating mesh element types based on properties input ===> H 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 = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box1, index = 1 Name = box2, index = 2 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 2402 Number of elements = 2400 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 2400 Updating mesh element types based on properties input 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 = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box1, index = 1 Name = box2, index = 2 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 2402 Number of elements = 2400 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 2400 Updating mesh element types based on properties input ===> x0 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 = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box1, index = 1 Name = box2, index = 2 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 2402 Number of elements = 2400 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 2400 Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Design_Variable_Relation name - thick_box2 Number of design variable relations - 4 Done getting FEA design variables Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Design_Variable_Relation name - thick_box2 Number of design variable relations - 4 Done getting FEA design variables ===> x1 Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Design_Variable_Relation name - thick_box2 Number of design variable relations - 4 Done getting FEA design variables Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Design_Variable_Relation name - thick_box2 Number of design variable relations - 4 Done getting FEA design variables ===> m0 Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Design_Variable_Relation name - thick_box2 Number of design variable relations - 4 Done getting FEA design variables Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Design_Variable_Relation name - thick_box2 Number of design variable relations - 4 Done getting FEA design variables ===> m1 Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Design_Variable_Relation name - thick_box2 Number of design variable relations - 4 Done getting FEA design variables Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Design_Variable_Relation name - thick_box2 Number of design variable relations - 4 Done getting FEA design variables ok test_journal (test_masstran.TestMasstran.test_journal) ... 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 = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box1, index = 1 Name = point, index = 2 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 2168 Number of elements = 4332 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 4332 Elemental Quad4 = 0 Setting FEA Data Mesh for body = 1 Number of nodal coordinates = 4009 Number of elements = 8014 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 8014 Elemental Quad4 = 0 Setting FEA Data Mesh for body = 2 Number of nodal coordinates = 1 Number of elements = 1 Elemental Nodes = 1 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 0 Combining multiple FEA meshes! Combined Number of nodal coordinates = 6178 Combined Number of elements = 12347 Combined Elemental Nodes = 1 Combined Elemental Rods = 0 Combined Elemental Tria3 = 12346 Combined Elemental Quad4 = 0 Getting FEA materials....... Number of materials - 2 Material name - madeupium Material name - unobtainium Done getting FEA materials Getting FEA properties....... Number of properties - 2 Property name - box1 Property name - point Done getting FEA properties Updating mesh element types based on properties input 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 = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box1, index = 1 Name = point, index = 2 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 2168 Number of elements = 4332 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 4332 Elemental Quad4 = 0 Setting FEA Data Mesh for body = 1 Number of nodal coordinates = 4000 Number of elements = 7996 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 7996 Elemental Quad4 = 0 Setting FEA Data Mesh for body = 2 Number of nodal coordinates = 1 Number of elements = 1 Elemental Nodes = 1 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 0 Combining multiple FEA meshes! Combined Number of nodal coordinates = 6169 Combined Number of elements = 12329 Combined Elemental Nodes = 1 Combined Elemental Rods = 0 Combined Elemental Tria3 = 12328 Combined Elemental Quad4 = 0 Updating mesh element types based on properties input EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! 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 = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box1, index = 1 Name = point, index = 2 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 2168 Number of elements = 4332 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 4332 Elemental Quad4 = 0 Setting FEA Data Mesh for body = 1 Number of nodal coordinates = 4009 Number of elements = 8014 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 8014 Elemental Quad4 = 0 Setting FEA Data Mesh for body = 2 Number of nodal coordinates = 1 Number of elements = 1 Elemental Nodes = 1 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 0 Combining multiple FEA meshes! Combined Number of nodal coordinates = 6178 Combined Number of elements = 12347 Combined Elemental Nodes = 1 Combined Elemental Rods = 0 Combined Elemental Tria3 = 12346 Combined Elemental Quad4 = 0 Getting FEA materials....... Number of materials - 2 Material name - madeupium Material name - unobtainium Done getting FEA materials Getting FEA properties....... Number of properties - 2 Property name - box1 Property name - point Done getting FEA properties Updating mesh element types based on properties input CAPS Info: Hit last success -- going live! 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 = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box1, index = 1 Name = point, index = 2 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 2168 Number of elements = 4332 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 4332 Elemental Quad4 = 0 Setting FEA Data Mesh for body = 1 Number of nodal coordinates = 4009 Number of elements = 8014 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 8014 Elemental Quad4 = 0 Setting FEA Data Mesh for body = 2 Number of nodal coordinates = 1 Number of elements = 1 Elemental Nodes = 1 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 0 Combining multiple FEA meshes! Combined Number of nodal coordinates = 6178 Combined Number of elements = 12347 Combined Elemental Nodes = 1 Combined Elemental Rods = 0 Combined Elemental Tria3 = 12346 Combined Elemental Quad4 = 0 Getting FEA materials....... Number of materials - 2 Material name - madeupium Material name - unobtainium Done getting FEA materials Getting FEA properties....... Number of properties - 2 Property name - box1 Property name - point Done getting FEA properties Updating mesh element types based on properties input CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! 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 = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box1, index = 1 Name = point, index = 2 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 2168 Number of elements = 4332 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 4332 Elemental Quad4 = 0 Setting FEA Data Mesh for body = 1 Number of nodal coordinates = 4000 Number of elements = 7996 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 7996 Elemental Quad4 = 0 Setting FEA Data Mesh for body = 2 Number of nodal coordinates = 1 Number of elements = 1 Elemental Nodes = 1 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 0 Combining multiple FEA meshes! Combined Number of nodal coordinates = 6169 Combined Number of elements = 12329 Combined Elemental Nodes = 1 Combined Elemental Rods = 0 Combined Elemental Tria3 = 12328 Combined Elemental Quad4 = 0 Getting FEA materials....... Number of materials - 2 Material name - madeupium Material name - unobtainium Done getting FEA materials Getting FEA properties....... Number of properties - 2 Property name - box1 Property name - point Done getting FEA properties Updating mesh element types based on properties input CAPS Info: Hit last success -- going live! 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 = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box1, index = 1 Name = point, index = 2 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 2168 Number of elements = 4332 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 4332 Elemental Quad4 = 0 Setting FEA Data Mesh for body = 1 Number of nodal coordinates = 4000 Number of elements = 7996 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 7996 Elemental Quad4 = 0 Setting FEA Data Mesh for body = 2 Number of nodal coordinates = 1 Number of elements = 1 Elemental Nodes = 1 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 0 Combining multiple FEA meshes! Combined Number of nodal coordinates = 6169 Combined Number of elements = 12329 Combined Elemental Nodes = 1 Combined Elemental Rods = 0 Combined Elemental Tria3 = 12328 Combined Elemental Quad4 = 0 Getting FEA materials....... Number of materials - 2 Material name - madeupium Material name - unobtainium Done getting FEA materials Getting FEA properties....... Number of properties - 2 Property name - box1 Property name - point Done getting FEA properties Updating mesh element types based on properties input ok test_plate (test_masstran.TestMasstran.test_plate) ... 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 = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = box1, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 441 Number of elements = 400 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 400 Getting FEA properties....... Number of properties - 1 Property name - box1 Done getting FEA properties Updating mesh element types based on properties input Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 7 Design_Variable name - H Design_Variable name - L Design_Variable name - W Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Number of design variable relations - 3 Done getting FEA design variables ===> L 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 = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = box1, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 441 Number of elements = 400 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 400 Updating mesh element types based on properties input 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 = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = box1, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 441 Number of elements = 400 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 400 Updating mesh element types based on properties input ===> W 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 = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = box1, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 441 Number of elements = 400 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 400 Updating mesh element types based on properties input 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 = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = box1, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 441 Number of elements = 400 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 400 Updating mesh element types based on properties input ===> H 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 = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = box1, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 441 Number of elements = 400 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 400 Updating mesh element types based on properties input 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 = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = box1, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 441 Number of elements = 400 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 400 Updating mesh element types based on properties input ===> x0 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 = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = box1, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 441 Number of elements = 400 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 400 Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Number of design variable relations - 3 Done getting FEA design variables Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Number of design variable relations - 3 Done getting FEA design variables ===> x1 Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Number of design variable relations - 3 Done getting FEA design variables Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Number of design variable relations - 3 Done getting FEA design variables ===> m0 Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Number of design variable relations - 3 Done getting FEA design variables Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Number of design variable relations - 3 Done getting FEA design variables ===> m1 Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Number of design variable relations - 3 Done getting FEA design variables Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Number of design variable relations - 3 Done getting FEA design variables ok test_plate_point (test_masstran.TestMasstran.test_plate_point) ... 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 = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box1, index = 1 Name = point, index = 2 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 441 Number of elements = 400 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 400 Setting FEA Data Mesh for body = 1 Number of nodal coordinates = 1 Number of elements = 1 Elemental Nodes = 1 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 0 Combining multiple FEA meshes! Combined Number of nodal coordinates = 442 Combined Number of elements = 401 Combined Elemental Nodes = 1 Combined Elemental Rods = 0 Combined Elemental Tria3 = 0 Combined Elemental Quad4 = 400 Getting FEA properties....... Number of properties - 2 Property name - box1 Property name - point Done getting FEA properties Updating mesh element types based on properties input Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 7 Design_Variable name - H Design_Variable name - L Design_Variable name - W Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - mass_point Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Number of design variable relations - 4 Done getting FEA design variables ===> L 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 = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box1, index = 1 Name = point, index = 2 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 441 Number of elements = 400 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 400 Setting FEA Data Mesh for body = 1 Number of nodal coordinates = 1 Number of elements = 1 Elemental Nodes = 1 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 0 Combining multiple FEA meshes! Combined Number of nodal coordinates = 442 Combined Number of elements = 401 Combined Elemental Nodes = 1 Combined Elemental Rods = 0 Combined Elemental Tria3 = 0 Combined Elemental Quad4 = 400 Updating mesh element types based on properties input 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 = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box1, index = 1 Name = point, index = 2 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 441 Number of elements = 400 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 400 Setting FEA Data Mesh for body = 1 Number of nodal coordinates = 1 Number of elements = 1 Elemental Nodes = 1 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 0 Combining multiple FEA meshes! Combined Number of nodal coordinates = 442 Combined Number of elements = 401 Combined Elemental Nodes = 1 Combined Elemental Rods = 0 Combined Elemental Tria3 = 0 Combined Elemental Quad4 = 400 Updating mesh element types based on properties input ===> W 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 = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box1, index = 1 Name = point, index = 2 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 441 Number of elements = 400 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 400 Setting FEA Data Mesh for body = 1 Number of nodal coordinates = 1 Number of elements = 1 Elemental Nodes = 1 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 0 Combining multiple FEA meshes! Combined Number of nodal coordinates = 442 Combined Number of elements = 401 Combined Elemental Nodes = 1 Combined Elemental Rods = 0 Combined Elemental Tria3 = 0 Combined Elemental Quad4 = 400 Updating mesh element types based on properties input 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 = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box1, index = 1 Name = point, index = 2 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 441 Number of elements = 400 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 400 Setting FEA Data Mesh for body = 1 Number of nodal coordinates = 1 Number of elements = 1 Elemental Nodes = 1 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 0 Combining multiple FEA meshes! Combined Number of nodal coordinates = 442 Combined Number of elements = 401 Combined Elemental Nodes = 1 Combined Elemental Rods = 0 Combined Elemental Tria3 = 0 Combined Elemental Quad4 = 400 Updating mesh element types based on properties input ===> H 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 = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box1, index = 1 Name = point, index = 2 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 441 Number of elements = 400 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 400 Setting FEA Data Mesh for body = 1 Number of nodal coordinates = 1 Number of elements = 1 Elemental Nodes = 1 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 0 Combining multiple FEA meshes! Combined Number of nodal coordinates = 442 Combined Number of elements = 401 Combined Elemental Nodes = 1 Combined Elemental Rods = 0 Combined Elemental Tria3 = 0 Combined Elemental Quad4 = 400 Updating mesh element types based on properties input 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 = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box1, index = 1 Name = point, index = 2 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 441 Number of elements = 400 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 400 Setting FEA Data Mesh for body = 1 Number of nodal coordinates = 1 Number of elements = 1 Elemental Nodes = 1 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 0 Combining multiple FEA meshes! Combined Number of nodal coordinates = 442 Combined Number of elements = 401 Combined Elemental Nodes = 1 Combined Elemental Rods = 0 Combined Elemental Tria3 = 0 Combined Elemental Quad4 = 400 Updating mesh element types based on properties input ===> x0 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 = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box1, index = 1 Name = point, index = 2 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 441 Number of elements = 400 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 400 Setting FEA Data Mesh for body = 1 Number of nodal coordinates = 1 Number of elements = 1 Elemental Nodes = 1 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 0 Combining multiple FEA meshes! Combined Number of nodal coordinates = 442 Combined Number of elements = 401 Combined Elemental Nodes = 1 Combined Elemental Rods = 0 Combined Elemental Tria3 = 0 Combined Elemental Quad4 = 400 Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - mass_point Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Number of design variable relations - 4 Done getting FEA design variables Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - mass_point Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Number of design variable relations - 4 Done getting FEA design variables ===> x1 Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - mass_point Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Number of design variable relations - 4 Done getting FEA design variables Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - mass_point Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Number of design variable relations - 4 Done getting FEA design variables ===> m0 Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - mass_point Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Number of design variable relations - 4 Done getting FEA design variables Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - mass_point Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Number of design variable relations - 4 Done getting FEA design variables ===> m1 Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - mass_point Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Number of design variable relations - 4 Done getting FEA design variables Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - mass_point Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Number of design variable relations - 4 Done getting FEA design variables ok test_Cheby_Modes (test_mses.TestMSES_Kulfan.test_Cheby_Modes) ... Getting CFD design variables....... Number of design variables - 4 Design Variable name - alowervar Design Variable name - auppervar Design Variable name - classvar Design Variable name - ztailvar Done getting CFD design variables CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 ok test_Cheby_Modes_Symmetric (test_mses.TestMSES_Kulfan.test_Cheby_Modes_Symmetric) ... Getting CFD design variables....... Number of design variables - 1 Design Variable name - avar Done getting CFD design variables CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 ok test_allInputs (test_mses.TestMSES_Kulfan.test_allInputs) ... ok test_execute (test_mses.TestMSES_Kulfan.test_execute) ... ok test_sensitivity_AnalysisIn (test_mses.TestMSES_Kulfan.test_sensitivity_AnalysisIn) ... ok test_Cheby_Modes_Symmetric (test_mses.TestMSES_NACA.test_Cheby_Modes_Symmetric) ... Getting CFD design variables....... Number of design variables - 1 Design Variable name - thick Done getting CFD design variables ok test_geom_sensitivity_CL (test_mses.TestMSES_NACA.test_geom_sensitivity_CL) ... Getting CFD design variables....... Number of design variables - 2 Design Variable name - camber Design Variable name - thick Done getting CFD design variables ok test_journal (test_mses.TestMSES_NACA.test_journal) ... Getting CFD design variables....... Number of design variables - 1 Design Variable name - thick Done getting CFD design variables EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! Getting CFD design variables....... Number of design variables - 1 Design Variable name - thick Done getting CFD design variables CAPS Info: Hit last success -- going live! Getting CFD design variables....... Number of design variables - 1 Design Variable name - thick Done getting CFD design variables CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! Getting CFD design variables....... Number of design variables - 1 Design Variable name - thick Done getting CFD design variables CAPS Info: Hit last success -- going live! Getting CFD design variables....... Number of design variables - 1 Design Variable name - thick Done getting CFD design variables ok test_MultiBody (test_pointwise.TestPointwise.test_MultiBody) ... skipped 'No pointwise executable' test_SingleBody (test_pointwise.TestPointwise.test_SingleBody) ... skipped 'No pointwise executable' test_all (test_pointwise.TestPointwise.test_all) ... skipped 'No pointwise executable' test_box (test_pointwise.TestPointwise.test_box) ... skipped 'No pointwise executable' test_bullet (test_pointwise.TestPointwise.test_bullet) ... skipped 'No pointwise executable' test_cone (test_pointwise.TestPointwise.test_cone) ... skipped 'No pointwise executable' test_cylinder (test_pointwise.TestPointwise.test_cylinder) ... skipped 'No pointwise executable' test_executeError (test_pointwise.TestPointwise.test_executeError) ... skipped 'No pointwise executable' test_reenter (test_pointwise.TestPointwise.test_reenter) ... skipped 'No pointwise executable' test_sphere (test_pointwise.TestPointwise.test_sphere) ... skipped 'No pointwise executable' EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! test_Area_Mesh (test_refine.TestREFINE.test_Area_Mesh) ... Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 5 Name = 2DSlice, index = 1 Name = TunnelWall, index = 2 Name = OutFlow, index = 3 Name = InFlow, index = 4 Name = Airfoil, index = 5 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = TunnelWall, index = 1 Name = OutFlow, index = 2 Name = InFlow, index = 3 Name = Airfoil, index = 4 Getting 2D mesh for body 1 (of 1) AFLR2 : --------------------------------------- AFLR2 : AFLR2 LIBRARY AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR2 : TRIA/QUAD GRID GENERATOR AFLR2 : Version Number 9.17.15 AFLR2 : Version Date 04/23/24 @ 12:51AM AFLR2 : Compile OS Darwin 23.4.0 x86_64 AFLR2 : Compile Date 04/23/24 @ 11:49AM AFLR2 : Copyright 1994-2021, D.L. Marcum AFLR2 : --------------------------------------- AFLR2 IC : INPUT DATA CHECK AFLR2 IC : Nodes, Faces = 54 0 AFLR2 : CPU Time = 0.000 seconds AFLR2 EG : EDGE GRID RE-GENERATION AFLR2 EG : Nodes, Edges = 54 54 AFLR2 : CPU Time = 0.000 seconds AFLR2 IG : INITIAL GRID GENERATION AFLR2 IG : Nodes, Faces = 0 2 AFLR2 IG : Nodes, Faces = 12 26 AFLR2 IG : Nodes, Faces = 24 50 AFLR2 IG : Nodes, Faces = 36 74 AFLR2 IG : Nodes, Faces = 48 98 AFLR2 IG : Nodes, Faces = 52 106 AFLR2 IG : Nodes, Faces = 53 108 AFLR2 IG : Nodes, Faces = 54 110 AFLR2 IG : Nodes, Faces = 58 110 AFLR2 IG : Nodes, Faces = 54 54 AFLR2 : CPU Time = 0.000 seconds AFLR2 GG : FIELD GRID GENERATION AFLR2 GG : Nodes, Faces = 54 54 AFLR2 GG : Nodes, Faces = 100 146 AFLR2 GG : Nodes, Faces = 122 190 AFLR2 GG : Nodes, Faces = 138 222 AFLR2 GG : Nodes, Faces = 153 252 AFLR2 GG : Nodes, Faces = 168 282 AFLR2 GG : Nodes, Faces = 180 306 AFLR2 GG : Nodes, Faces = 192 330 AFLR2 GG : Nodes, Faces = 201 348 AFLR2 GG : Nodes, Faces = 210 366 AFLR2 GG : Nodes, Faces = 216 378 AFLR2 GG : Nodes, Faces = 221 388 AFLR2 GG : Nodes, Faces = 224 394 AFLR2 GG : Nodes, Faces = 225 396 AFLR2 : CPU Time = 0.002 seconds AFLR2 QI : QUALITY IMPROVEMENT AFLR2 QI : Nodes, Faces = 225 396 AFLR2 : CPU Time = 0.000 seconds AFLR2 : DONE Writing AFLR3 file .... Finished writing AFLR3 file Number of nodes = 225 Number of elements = 450 Number of tris = 396 Number of quad = 0 Writing Binary VTK file .... Finished writing Binary VTK file Writing vtk file .... Writing vtk general file .... Finished writing vtk file Writing FAST file .... Finished writing FAST file Writing SU2 file .... Finished writing SU2 file Writing Tecplot file .... Finished writing Tecplot file Writing ugrid file .... Finished writing ugrid file Writing Binary VTK file .... Finished writing Binary VTK file Writing vtk file .... Writing vtk general file .... Finished writing vtk file Writing FAST file .... Finished writing FAST file Writing SU2 file .... Finished writing SU2 file Writing Tecplot file .... Finished writing Tecplot file Writing ugrid file .... Finished writing ugrid file Writing Binary VTK file .... Finished writing Binary VTK file Writing vtk file .... Writing vtk general file .... Finished writing vtk file Writing FAST file .... Finished writing FAST file Writing SU2 file .... Finished writing SU2 file Writing Tecplot file .... Finished writing Tecplot file Writing ugrid file .... Finished writing ugrid file ok test_all (test_refine.TestREFINE.test_all) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = farfield, index = 1 Name = box, index = 2 Name = sphere, index = 3 Name = boxhole, index = 4 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = farfield, index = 1 Name = box, index = 2 Name = sphere, index = 3 Name = boxhole, index = 4 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 x86_64 AFLR2 : Compile Date 04/23/24 @ 11:49AM 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 x86_64 AFLR4 : Compile Date 04/23/24 @ 11:49AM AFLR4 : Copyright 1994-2021, D.L. Marcum AFLR4 : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 1602 Number of elements = 8758 Number of triangles = 1240 Number of quadrilatarals = 0 Number of tetrahedrals = 7518 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 ok test_box_volume (test_refine.TestREFINE.test_box_volume) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = farfield, index = 1 Name = box, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = farfield, index = 1 Name = box, index = 2 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 2600 Number of elements = 13864 Number of triangles = 2758 Number of quadrilatarals = 0 Number of tetrahedrals = 11106 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 ok test_boxhole (test_refine.TestREFINE.test_boxhole) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = farfield, index = 1 Name = boxhole, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = farfield, index = 1 Name = boxhole, index = 2 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 1071 Number of elements = 5705 Number of triangles = 998 Number of quadrilatarals = 0 Number of tetrahedrals = 4707 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 ok test_cfdSingleBody (test_refine.TestREFINE.test_cfdSingleBody) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 15544 Number of elements = 89331 Number of triangles = 4632 Number of quadrilatarals = 0 Number of tetrahedrals = 84699 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Binary VTK file .... Finished writing Binary VTK file Writing vtk file .... Writing vtk general file .... Finished writing vtk file Writing FAST file .... Finished writing FAST file Writing SU2 file .... Finished writing SU2 file Writing Tecplot file .... Finished writing Tecplot file Writing ugrid file .... Finished writing ugrid file Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Done getting CFD boundary conditions Writing boundary flags - bcProps.surfaceProp[0].surfaceType = 3 - bcProps.surfaceProp[1].surfaceType = 1 Done boundary flags Warning: The su2 cfg file will be overwritten! Write SU2 configuration file for version "Harrier (8.0.1)" Writing Binary VTK file .... Finished writing Binary VTK file Writing vtk file .... Writing vtk general file .... Finished writing vtk file Writing FAST file .... Finished writing FAST file Writing SU2 file .... Finished writing SU2 file Writing Tecplot file .... Finished writing Tecplot file Writing ugrid file .... Finished writing ugrid file Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Done getting CFD boundary conditions Writing boundary flags - bcProps.surfaceProp[0].surfaceType = 3 - bcProps.surfaceProp[1].surfaceType = 1 Done boundary flags Warning: The su2 cfg file will be overwritten! Write SU2 configuration file for version "Harrier (8.0.1)" Writing Binary VTK file .... Finished writing Binary VTK file Writing vtk file .... Writing vtk general file .... Finished writing vtk file Writing FAST file .... Finished writing FAST file Writing SU2 file .... Finished writing SU2 file Writing Tecplot file .... Finished writing Tecplot file Writing ugrid file .... Finished writing ugrid file Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Done getting CFD boundary conditions Writing boundary flags - bcProps.surfaceProp[0].surfaceType = 3 - bcProps.surfaceProp[1].surfaceType = 1 Done boundary flags Warning: The su2 cfg file will be overwritten! Write SU2 configuration file for version "Harrier (8.0.1)" ok test_fun3d (test_refine.TestREFINE.test_fun3d) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = farfield, index = 1 Name = box, index = 2 Name = sphere, index = 3 Name = boxhole, index = 4 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = farfield, index = 1 Name = box, index = 2 Name = sphere, index = 3 Name = boxhole, index = 4 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 1602 Number of elements = 8758 Number of triangles = 1240 Number of quadrilatarals = 0 Number of tetrahedrals = 7518 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 ok test_inputs (test_refine.TestREFINE.test_inputs) ... ok test_phase (test_refine.TestREFINE.test_phase) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = farfield, index = 1 Name = box, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = farfield, index = 1 Name = box, index = 2 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 438 Number of elements = 2179 Number of triangles = 644 Number of quadrilatarals = 0 Number of tetrahedrals = 1535 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = farfield, index = 1 Name = box, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = farfield, index = 1 Name = box, index = 2 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = farfield, index = 1 Name = box, index = 2 ok test_sphere (test_refine.TestREFINE.test_sphere) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = farfield, index = 1 Name = sphere, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = farfield, index = 1 Name = sphere, index = 2 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 936 Number of elements = 4999 Number of triangles = 758 Number of quadrilatarals = 0 Number of tetrahedrals = 4241 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 ok test_inputs (test_su2.TestSU2.test_inputs) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 AFLR4 : Proximity BG Surface Grid Generation Skipped AFLR4 : No Modifications Required Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Getting volume mesh UG PARAM : SETTING INPUT PARAMETERS FROM ARGUMENT VECTOR UG PARAM : mrecm = 3 UG PARAM : mrecqm = 3 UG PARAM : mpfrmt = 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 x86_64 AFLR2 : Compile Date 04/23/24 @ 11:49AM 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 x86_64 AFLR4 : Compile Date 04/23/24 @ 11:49AM AFLR4 : Copyright 1994-2021, D.L. Marcum AFLR4 : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : EGADS CAD Geometry Setup EGADS : Model has 3 Active Bodies EGADS : Body 0 is a SolidBody EGADS : Body 0 has 1 Shells EGADS : Body 0 has 8 Faces EGADS : Body 0 has 15 Edges EGADS : Body 0 has 8 Loops EGADS : Body 0 has 9 Nodes EGADS : Body 1 is a SolidBody EGADS : Body 1 has 1 Shells EGADS : Body 1 has 8 Faces EGADS : Body 1 has 15 Edges EGADS : Body 1 has 8 Loops EGADS : Body 1 has 9 Nodes EGADS : Body 2 is a SolidBody EGADS : Body 2 has 1 Shells EGADS : Body 2 has 2 Faces EGADS : Body 2 has 6 Edges EGADS : Body 2 has 2 Loops EGADS : Body 2 has 2 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 1 1 2 3 4 5 EGADS : 2 Yes 0 0 1 1 1 1 3 4 6 EGADS : 3 Yes 0 0 1 1 1 1 2 4 7 EGADS : 4 Yes 0 0 1 1 1 1 2 3 EGADS : 5 Yes 0 0 1 1 1 1 6 7 8 EGADS : 6 Yes 0 0 1 1 1 2 5 7 8 EGADS : 7 Yes 0 0 1 1 1 3 5 6 8 EGADS : 8 Yes 0 0 1 1 1 5 6 7 EGADS : 9 Yes 1 0 1 0 10 10 11 12 13 EGADS : 10 Yes 1 0 1 0 10 9 11 12 14 EGADS : 11 Yes 1 0 1 0 10 9 10 12 15 EGADS : 12 Yes 1 0 1 0 10 9 10 11 EGADS : 13 Yes 1 0 1 0 10 9 14 15 16 EGADS : 14 Yes 1 0 1 0 10 10 13 15 16 EGADS : 15 Yes 1 0 1 0 10 11 13 14 16 EGADS : 16 Yes 1 0 1 0 10 13 14 15 EGADS : 17 Yes 2 0 1 NA NA 18 EGADS : 18 Yes 2 0 1 NA NA 17 EGADS : Face Edges Information EGADS : Face Edges EGADS : 1 1 4 -3 -2 EGADS : 2 3 7 -6 -5 EGADS : 3 6 9 -1 -8 EGADS : 4 -4 -9 -7 EGADS : 5 -10 2 11 -12 EGADS : 6 -11 5 13 -14 EGADS : 7 -13 8 10 -15 EGADS : 8 12 14 15 EGADS : 9 16 19 -18 -17 EGADS : 10 18 22 -21 -20 EGADS : 11 21 24 -16 -23 EGADS : 12 -19 -24 -22 EGADS : 13 -25 17 26 -27 EGADS : 14 -26 20 28 -29 EGADS : 15 -28 23 25 -30 EGADS : 16 27 29 30 EGADS : 17 -31 -32 33 34 EGADS : 18 -35 -34 36 32 EGADS : Face Loops Information EGADS : Face Loops EGADS : 1 1 EGADS : 2 2 EGADS : 3 3 EGADS : 4 4 EGADS : 5 5 EGADS : 6 6 EGADS : 7 7 EGADS : 8 8 EGADS : 9 9 EGADS : 10 10 EGADS : 11 11 EGADS : 12 12 EGADS : 13 13 EGADS : 14 14 EGADS : 15 15 EGADS : 16 16 EGADS : 17 17 EGADS : 18 18 EGADS : Loop Edges Information EGADS : Loop Active Edges EGADS : 1 Yes 1 4 -3 -2 EGADS : 2 Yes 3 7 -6 -5 EGADS : 3 Yes 6 9 -1 -8 EGADS : 4 Yes -4 -9 -7 EGADS : 5 Yes -10 2 11 -12 EGADS : 6 Yes -11 5 13 -14 EGADS : 7 Yes -13 8 10 -15 EGADS : 8 Yes 12 14 15 EGADS : 9 Yes 16 19 -18 -17 EGADS : 10 Yes 18 22 -21 -20 EGADS : 11 Yes 21 24 -16 -23 EGADS : 12 Yes -19 -24 -22 EGADS : 13 Yes -25 17 26 -27 EGADS : 14 Yes -26 20 28 -29 EGADS : 15 Yes -28 23 25 -30 EGADS : 16 Yes 27 29 30 EGADS : 17 Yes -31 -32 33 34 EGADS : 18 Yes -35 -34 36 32 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 1 2 1 1 3 EGADS : 2 0 Yes 1 3 1 1 5 EGADS : 3 0 Yes 3 4 1 1 2 EGADS : 4 0 Yes 2 4 1 1 4 EGADS : 5 0 Yes 3 5 1 2 6 EGADS : 6 0 Yes 5 6 1 2 3 EGADS : 7 0 Yes 4 6 1 2 4 EGADS : 8 0 Yes 5 1 1 3 7 EGADS : 9 0 Yes 6 2 1 3 4 EGADS : 10 0 Yes 1 7 1 5 7 EGADS : 11 0 Yes 3 8 1 5 6 EGADS : 12 0 Yes 7 8 1 5 8 EGADS : 13 0 Yes 5 9 1 6 7 EGADS : 14 0 Yes 8 9 1 6 8 EGADS : 15 0 Yes 9 7 1 7 8 EGADS : 16 1 Yes 10 11 1 9 11 EGADS : 17 1 Yes 10 12 1 9 13 EGADS : 18 1 Yes 12 13 1 9 10 EGADS : 19 1 Yes 11 13 1 9 12 EGADS : 20 1 Yes 12 14 1 10 14 EGADS : 21 1 Yes 14 15 1 10 11 EGADS : 22 1 Yes 13 15 1 10 12 EGADS : 23 1 Yes 14 10 1 11 15 EGADS : 24 1 Yes 15 11 1 11 12 EGADS : 25 1 Yes 10 16 1 13 15 EGADS : 26 1 Yes 12 17 1 13 14 EGADS : 27 1 Yes 16 17 1 13 16 EGADS : 28 1 Yes 14 18 1 14 15 EGADS : 29 1 Yes 17 18 1 14 16 EGADS : 30 1 Yes 18 16 1 15 16 EGADS : 31 2 DEGEN 19 19 - 17 EGADS : 32 2 Yes 20 19 NA 17 18 EGADS : 33 2 DEGEN 20 20 - 17 EGADS : 34 2 Yes 20 19 NA 17 18 EGADS : 35 2 DEGEN 19 19 - 18 EGADS : 36 2 DEGEN 20 20 - 18 EGADS : Node Information EGADS : Node Active Coordinates EGADS : 1 Yes 3.77246052 0 0.00459131419 EGADS : 2 Yes 5.90487498 7.07106781 0 EGADS : 3 Yes 0 0 0 EGADS : 4 Yes 4.0824829 7.07106781 0.123425948 EGADS : 5 Yes 3.77001182 0 0 EGADS : 6 Yes 5.90282524 7.07106781 0 EGADS : 7 Yes 5.90487498 0 0 EGADS : 8 Yes 4.0824829 0 0.123425948 EGADS : 9 Yes 5.90282524 0 0 EGADS : 10 Yes 11.5089842 0 0.00183652568 EGADS : 11 Yes 12.36195 2.82842712 0 EGADS : 12 Yes 10 0 0 EGADS : 13 Yes 11.6329932 2.82842712 0.0493703791 EGADS : 14 Yes 11.5080047 0 0 EGADS : 15 Yes 12.3611301 2.82842712 0 EGADS : 16 Yes 12.36195 0 0 EGADS : 17 Yes 11.6329932 0 0.0493703791 EGADS : 18 Yes 12.3611301 0 0 EGADS : 19 Yes 0 0 80 EGADS : 20 Yes 0 0 0 EGADS : Face and Edge Match Information EGADS : No Face Matches Found AFLR4 : Surface Mesh Spacing Setup AFLR4 : Max Bounding Box Length = 160 AFLR4 : Min Bounding Box Length = 160 AFLR4 : Max Ref Bounding Box Length = 14.1421 AFLR4 : Min Ref Bounding Box Length = 0.890888 AFLR4 : Reference Length = 0.890888 AFLR4 : BL Thickness = 0 AFLR4 : FarField Spacing = 15.6122 AFLR4 : Abs Min Surf Spacing = 0.00222722 AFLR4 : Min Surf Spacing = 0.00445444 AFLR4 : Max Surf Spacing = 0.0890888 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 AFLR4 : 2 CAD geometry 0 STD AFLR4 : 3 CAD geometry 0 STD AFLR4 : 4 CAD geometry 0 STD AFLR4 : 5 CAD geometry 0 STD AFLR4 : 6 CAD geometry 0 STD AFLR4 : 7 CAD geometry 0 STD AFLR4 : 8 CAD geometry 0 STD AFLR4 : 9 CAD geometry 0 STD AFLR4 : 10 CAD geometry 0 STD AFLR4 : 11 CAD geometry 0 STD AFLR4 : 12 CAD geometry 0 STD AFLR4 : 13 CAD geometry 0 STD AFLR4 : 14 CAD geometry 0 STD AFLR4 : 15 CAD geometry 0 STD AFLR4 : 16 CAD geometry 0 STD AFLR4 : 17 CAD geometry 0 FARFIELD AFLR4 : 18 CAD geometry 0 FARFIELD AFLR4 : Case has 2 Proximity Checking Components AFLR4 : Component 1 includes Definitions 1 2 3 4 5 6 7 8 AFLR4 : Component 2 includes Definitions 9 10 11 12 13 14 15 16 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 : Define CAD surface definition 10 AFLR4 : Define CAD surface definition 11 AFLR4 : Define CAD surface definition 12 AFLR4 : Define CAD surface definition 13 AFLR4 : Define CAD surface definition 14 AFLR4 : Define CAD surface definition 15 AFLR4 : Define CAD surface definition 16 AFLR4 : Define CAD surface definition 17 AFLR4 : Define CAD surface definition 18 AFLR43 : INPUT SURFACE MESH FROM TESS AFLR43 : Quad Surface Faces= 0 AFLR43 : Tria Surface Faces= 12428 AFLR43 : Nodes = 6220 UG PARAM : SETTING INPUT PARAMETERS FROM ARGUMENT VECTOR UG PARAM : mrecm = 3 UG PARAM : mrecqm = 3 UG PARAM : mpfrmt = 0 AFLR3 : --------------------------------------- AFLR3 : AFLR3 LIBRARY AFLR3 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR3 : TETRAHEDRAL GRID GENERATOR AFLR3 : Version Number 16.32.50 AFLR3 : Version Date 10/31/23 @ 06:31PM AFLR3 : Compile OS Darwin 22.6.0 x86_64 AFLR3 : Compile Date 11/01/23 @ 12:19PM AFLR3 : Copyright 1994-2021, D.L. Marcum AFLR3 : --------------------------------------- AFLR3 IC : INPUT SURFACE GRID CHECK AFLR3 IC : Nodes, Elements = 6220 0 UG3 : Boundary Conditions UG3 : B-Face ID Boundary Condition UG3 : 1 Solid UG3 : 2 Solid UG3 : 3 Solid UG3 : 4 Solid UG3 : 5 Solid UG3 : 6 Solid UG3 : 7 Solid UG3 : 8 Solid UG3 : 9 Solid UG3 : 10 Solid UG3 : 11 Solid UG3 : 12 Solid UG3 : 13 Solid UG3 : 14 Solid UG3 : 15 Solid UG3 : 16 Solid UG3 : 17 FarField UG3 : 18 FarField AFLR3 : CPU Time = 0.019 seconds AFLR3 IG : INITIAL VOLUME GRID GENERATION AFLR3 IG : Nodes, Elements = 6220 0 AFLR3 IG : Nodes, Elements = 8 10 AFLR3 IG : Nodes, Elements = 1246 7333 AFLR3 IG : Nodes, Elements = 2492 16261 AFLR3 IG : Nodes, Elements = 3738 25021 AFLR3 IG : Nodes, Elements = 4984 34304 AFLR3 IG : Nodes, Elements = 6227 43518 AFLR3 IG : Nodes, Elements = 6227 43440 AFLR3 IG : Nodes, Elements = 6227 43474 AFLR3 IG : Nodes, Elements = 6227 43437 AFLR3 IG : Nodes, Elements = 6220 26107 AFLR3 IG : Nodes, Elements = 6220 26133 AFLR3 IG : Nodes, Elements = 6220 21538 AFLR3 IG : Nodes, Elements = 6220 19141 AFLR3 : CPU Time = 0.196 seconds AFLR3 GG : ISOTROPIC VOLUME GRID GENERATION AFLR3 GG : Nodes, Elements = 6220 19141 AFLR3 GG : Nodes, Elements = 9092 27970 AFLR3 GG : Nodes, Elements = 9092 39349 AFLR3 GG : Nodes, Elements = 9092 36380 AFLR3 GG : Nodes, Elements = 9092 34923 AFLR3 GG : Nodes, Elements = 11659 42981 AFLR3 GG : Nodes, Elements = 11659 53807 AFLR3 GG : Nodes, Elements = 11659 50702 AFLR3 GG : Nodes, Elements = 11659 49815 AFLR3 GG : Nodes, Elements = 14477 58553 AFLR3 GG : Nodes, Elements = 14477 70855 AFLR3 GG : Nodes, Elements = 14477 67465 AFLR3 GG : Nodes, Elements = 14477 66533 AFLR3 GG : Nodes, Elements = 17443 75634 AFLR3 GG : Nodes, Elements = 17443 88707 AFLR3 GG : Nodes, Elements = 17443 85026 AFLR3 GG : Nodes, Elements = 17443 84166 AFLR3 GG : Nodes, Elements = 20625 93912 AFLR3 GG : Nodes, Elements = 20625 107483 AFLR3 GG : Nodes, Elements = 20625 103837 AFLR3 GG : Nodes, Elements = 20625 103014 AFLR3 GG : Nodes, Elements = 23983 113245 AFLR3 GG : Nodes, Elements = 23983 127691 AFLR3 GG : Nodes, Elements = 23983 123762 AFLR3 GG : Nodes, Elements = 23983 122939 AFLR3 GG : Nodes, Elements = 27471 133562 AFLR3 GG : Nodes, Elements = 27471 148246 AFLR3 GG : Nodes, Elements = 27471 144367 AFLR3 GG : Nodes, Elements = 27471 143483 AFLR3 GG : Nodes, Elements = 31049 154330 AFLR3 GG : Nodes, Elements = 31049 169629 AFLR3 GG : Nodes, Elements = 31049 165573 AFLR3 GG : Nodes, Elements = 31049 164719 AFLR3 GG : Nodes, Elements = 34642 175591 AFLR3 GG : Nodes, Elements = 34642 190772 AFLR3 GG : Nodes, Elements = 34642 186857 AFLR3 GG : Nodes, Elements = 34642 186049 AFLR3 GG : Nodes, Elements = 38204 196811 AFLR3 GG : Nodes, Elements = 38204 211769 AFLR3 GG : Nodes, Elements = 38204 208011 AFLR3 GG : Nodes, Elements = 38204 207203 AFLR3 GG : Nodes, Elements = 41735 217867 AFLR3 GG : Nodes, Elements = 41735 232734 AFLR3 GG : Nodes, Elements = 41735 228893 AFLR3 GG : Nodes, Elements = 41735 228199 AFLR3 GG : Nodes, Elements = 45118 238407 AFLR3 GG : Nodes, Elements = 45118 252771 AFLR3 GG : Nodes, Elements = 45118 249083 AFLR3 GG : Nodes, Elements = 45118 248399 AFLR3 GG : Nodes, Elements = 48432 258383 AFLR3 GG : Nodes, Elements = 48432 272398 AFLR3 GG : Nodes, Elements = 48432 268767 AFLR3 GG : Nodes, Elements = 48432 268040 AFLR3 GG : Nodes, Elements = 51632 277673 AFLR3 GG : Nodes, Elements = 51632 291124 AFLR3 GG : Nodes, Elements = 51632 287737 AFLR3 GG : Nodes, Elements = 51632 287138 AFLR3 GG : Nodes, Elements = 54742 296489 AFLR3 GG : Nodes, Elements = 54742 309545 AFLR3 GG : Nodes, Elements = 54742 306294 AFLR3 GG : Nodes, Elements = 54742 305700 AFLR3 GG : Nodes, Elements = 57753 314750 AFLR3 GG : Nodes, Elements = 57753 327393 AFLR3 GG : Nodes, Elements = 57753 324205 AFLR3 GG : Nodes, Elements = 57753 323671 AFLR3 GG : Nodes, Elements = 60589 332185 AFLR3 GG : Nodes, Elements = 60589 344195 AFLR3 GG : Nodes, Elements = 60589 341132 AFLR3 GG : Nodes, Elements = 60589 340678 AFLR3 GG : Nodes, Elements = 63303 348823 AFLR3 GG : Nodes, Elements = 63303 360078 AFLR3 GG : Nodes, Elements = 63303 357259 AFLR3 GG : Nodes, Elements = 63303 356861 AFLR3 GG : Nodes, Elements = 65821 364418 AFLR3 GG : Nodes, Elements = 65821 375019 AFLR3 GG : Nodes, Elements = 65821 372315 AFLR3 GG : Nodes, Elements = 65821 371973 AFLR3 GG : Nodes, Elements = 68056 378682 AFLR3 GG : Nodes, Elements = 68056 387933 AFLR3 GG : Nodes, Elements = 68056 385584 AFLR3 GG : Nodes, Elements = 68056 385301 AFLR3 GG : Nodes, Elements = 69951 390988 AFLR3 GG : Nodes, Elements = 69951 398948 AFLR3 GG : Nodes, Elements = 69951 396934 AFLR3 GG : Nodes, Elements = 69951 396704 AFLR3 GG : Nodes, Elements = 71446 401190 AFLR3 GG : Nodes, Elements = 71446 407532 AFLR3 GG : Nodes, Elements = 71446 405836 AFLR3 GG : Nodes, Elements = 71446 405665 AFLR3 GG : Nodes, Elements = 72588 409091 AFLR3 GG : Nodes, Elements = 72588 414051 AFLR3 GG : Nodes, Elements = 72588 412698 AFLR3 GG : Nodes, Elements = 72588 412555 AFLR3 GG : Nodes, Elements = 73412 415028 AFLR3 GG : Nodes, Elements = 73412 418465 AFLR3 GG : Nodes, Elements = 73412 417560 AFLR3 GG : Nodes, Elements = 73412 417491 AFLR3 GG : Nodes, Elements = 73970 419165 AFLR3 GG : Nodes, Elements = 73970 421515 AFLR3 GG : Nodes, Elements = 73970 420850 AFLR3 GG : Nodes, Elements = 73970 420801 AFLR3 GG : Nodes, Elements = 74329 421878 AFLR3 GG : Nodes, Elements = 74329 423409 AFLR3 GG : Nodes, Elements = 74329 422967 AFLR3 GG : Nodes, Elements = 74329 422934 AFLR3 GG : Nodes, Elements = 74527 423528 AFLR3 GG : Nodes, Elements = 74527 424406 AFLR3 GG : Nodes, Elements = 74527 424145 AFLR3 GG : Nodes, Elements = 74527 424123 AFLR3 GG : Nodes, Elements = 74619 424399 AFLR3 GG : Nodes, Elements = 74619 424805 AFLR3 GG : Nodes, Elements = 74619 424686 AFLR3 GG : Nodes, Elements = 74619 424681 AFLR3 GG : Nodes, Elements = 74657 424795 AFLR3 GG : Nodes, Elements = 74657 424951 AFLR3 GG : Nodes, Elements = 74657 424897 AFLR3 GG : Nodes, Elements = 74672 424942 AFLR3 GG : Nodes, Elements = 74672 425006 AFLR3 GG : Nodes, Elements = 74672 424985 AFLR3 GG : Nodes, Elements = 74672 424986 AFLR3 GG : Nodes, Elements = 74673 424989 AFLR3 GG : Nodes, Elements = 74673 424992 AFLR3 GG : Nodes, Elements = 74673 424991 AFLR3 GG : Nodes, Elements = 74696 425060 AFLR3 GG : Nodes, Elements = 74696 425133 AFLR3 GG : Nodes, Elements = 74696 425114 AFLR3 GG : Nodes, Elements = 74696 425117 AFLR3 GG : Nodes, Elements = 74700 425129 AFLR3 GG : Nodes, Elements = 74700 425145 AFLR3 GG : Nodes, Elements = 74700 425140 AFLR3 GG : Nodes, Elements = 74702 425146 AFLR3 GG : Nodes, Elements = 74702 425155 AFLR3 GG : Nodes, Elements = 74702 425152 AFLR3 GG : Nodes, Elements = 74702 425150 AFLR3 : CPU Time = 6.577 seconds AFLR3 QI : QUALITY IMPROVEMENT AFLR3 QI : Nodes, Elements = 74702 425150 AFLR3 QI : Nodes, Elements = 73200 416638 AFLR3 QI : Nodes, Elements = 72976 415359 AFLR3 QI : Nodes, Elements = 72961 415273 AFLR3 QI : Nodes, Elements = 72960 415266 AFLR3 QI : Nodes, Elements = 72960 419161 AFLR3 QI : Nodes, Elements = 72960 415035 AFLR3 QI : Nodes, Elements = 72960 414621 AFLR3 QI : Nodes, Elements = 72960 415001 AFLR3 QI : Nodes, Elements = 72960 414373 AFLR3 QI : Nodes, Elements = 72960 414178 AFLR3 QI : Nodes, Elements = 72960 414472 AFLR3 QI : Nodes, Elements = 72960 414145 AFLR3 QI : Nodes, Elements = 72960 414045 AFLR3 QI : Nodes, Elements = 72960 414288 AFLR3 QI : Nodes, Elements = 72960 414039 AFLR3 QI : Nodes, Elements = 72960 413980 AFLR3 QI : Nodes, Elements = 72960 414224 AFLR3 QI : Nodes, Elements = 72960 413989 AFLR3 QI : Nodes, Elements = 72960 413938 AFLR3 QI : Nodes, Elements = 72966 413964 AFLR3 QI : Nodes, Elements = 72966 414196 AFLR3 QI : Nodes, Elements = 72966 413985 AFLR3 QI : Nodes, Elements = 72966 413966 AFLR3 QI : Nodes, Elements = 72966 414195 AFLR3 QI : Nodes, Elements = 72966 413976 AFLR3 QI : Nodes, Elements = 72966 413935 AFLR3 : CPU Time = 2.338 seconds AFLR3 QRG: QUALITY GRID RE-GENERATION AFLR3 QRG: Nodes, Elements = 72966 413935 AFLR3 QRG: Nodes, Elements = 72978 413998 AFLR3 QRG: Nodes, Elements = 72988 414052 AFLR3 QRG: Nodes, Elements = 72990 414061 AFLR3 QRG: Nodes, Elements = 72991 414065 AFLR3 QRG: Nodes, Elements = 72990 414059 AFLR3 QRG: Nodes, Elements = 72998 414101 AFLR3 QRG: Nodes, Elements = 72998 414099 AFLR3 QRG: Nodes, Elements = 73000 414112 AFLR3 QRG: Nodes, Elements = 73007 414152 AFLR3 : CPU Time = 0.077 seconds AFLR3 : DONE UG3 : DIHEDRAL ANGLE CHECK UG3 : No. Tet Elems = 414152 UG3 : Min, Max Ang = 1.137 170.9 UG3 : Average Angle = 70.2 UG3 : No. Angle>160.0 = 61 UG3 : No. Angle>179.9 = 0 UG3 : VOL CHECK UG3 : Total-Volume = 2.12e+06 UG3 : No. Tet Elems = 414152 UG3 : Min Vol = 6.36e-10 UG3 : Average Vol = 5.12 UG3 : Total-Tet-Vol = 2.12e+06 UG3 : No. Vol<TOL = 0 UG3 : Q VOL-LENGTH-RATIO CHECK 2/3 2 UG3 : Q = c * Vol / sum( L ) UG3 : 0 <= Q <= 1 UG3 : No. Tet Elems = 414152 UG3 : Min, Max Q = 0.0734 1 UG3 : Average Q = 0.894 UG3 : No. Q< 0.1 = 29 UG3 : No. Q< 0.01 = 0 OVERALL : CPU Time = 9.939 seconds UG3 : DIHEDRAL ANGLE CHECK UG3 : No. Tet Elems = 414152 UG3 : Min, Max Ang = 1.137 170.9 UG3 : Average Angle = 70.2 UG3 : No. Angle>160.0 = 61 UG3 : No. Angle>179.9 = 0 UG3 : VOL CHECK UG3 : Total-Volume = 2.12e+06 UG3 : No. Tet Elems = 414152 UG3 : Min Vol = 6.36e-10 UG3 : Average Vol = 5.12 UG3 : Total-Tet-Vol = 2.12e+06 UG3 : No. Vol<TOL = 0 UG3 : Q VOL-LENGTH-RATIO CHECK 2/3 2 UG3 : Q = c * Vol / sum( L ) UG3 : 0 <= Q <= 1 UG3 : Note that L includes scaling for BL-aspect=ratio UG3 : No. Tet Elems = 414152 UG3 : Min, Max Q = 0.223 1 UG3 : Average Q = 0.859 UG3 : No. Q< 0.1 = 0 UG3 : No. Q< 0.01 = 0 UG3 : CPU Time = 0.000 seconds EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : CREATE EGADS TESS FROM AFLR3 DATA EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 1 EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 2 EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 3 EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 4 EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 5 EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 6 EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 7 EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 8 EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 9 EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 10 EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 11 EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 12 EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 13 EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 14 EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 15 EGADS : CREATING TESSELLATION FOR BODY 0 FACE 1 EGADS : CREATING TESSELLATION FOR BODY 0 FACE 2 EGADS : CREATING TESSELLATION FOR BODY 0 FACE 3 EGADS : CREATING TESSELLATION FOR BODY 0 FACE 4 EGADS : CREATING TESSELLATION FOR BODY 0 FACE 5 EGADS : CREATING TESSELLATION FOR BODY 0 FACE 6 EGADS : CREATING TESSELLATION FOR BODY 0 FACE 7 EGADS : CREATING TESSELLATION FOR BODY 0 FACE 8 EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 16 EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 17 EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 18 EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 19 EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 20 EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 21 EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 22 EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 23 EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 24 EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 25 EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 26 EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 27 EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 28 EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 29 EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 30 EGADS : CREATING TESSELLATION FOR BODY 1 FACE 9 EGADS : CREATING TESSELLATION FOR BODY 1 FACE 10 EGADS : CREATING TESSELLATION FOR BODY 1 FACE 11 EGADS : CREATING TESSELLATION FOR BODY 1 FACE 12 EGADS : CREATING TESSELLATION FOR BODY 1 FACE 13 EGADS : CREATING TESSELLATION FOR BODY 1 FACE 14 EGADS : CREATING TESSELLATION FOR BODY 1 FACE 15 EGADS : CREATING TESSELLATION FOR BODY 1 FACE 16 EGADS : CREATING TESSELLATION FOR BODY 2 EDGE 32 EGADS : CREATING TESSELLATION FOR BODY 2 EDGE 34 EGADS : CREATING TESSELLATION FOR BODY 2 FACE 17 EGADS : CREATING TESSELLATION FOR BODY 2 FACE 18 EGADS : EGADS TESS CREATED EGADS : CHECK TESS FACE NODE MAP EGADS : CHECKING NODE MAP FOR BODY 0 FACE 1 EGADS : CHECKING NODE MAP FOR BODY 0 FACE 2 EGADS : CHECKING NODE MAP FOR BODY 0 FACE 3 EGADS : CHECKING NODE MAP FOR BODY 0 FACE 4 EGADS : CHECKING NODE MAP FOR BODY 0 FACE 5 EGADS : CHECKING NODE MAP FOR BODY 0 FACE 6 EGADS : CHECKING NODE MAP FOR BODY 0 FACE 7 EGADS : CHECKING NODE MAP FOR BODY 0 FACE 8 EGADS : CHECKING NODE MAP FOR BODY 1 FACE 9 EGADS : CHECKING NODE MAP FOR BODY 1 FACE 10 EGADS : CHECKING NODE MAP FOR BODY 1 FACE 11 EGADS : CHECKING NODE MAP FOR BODY 1 FACE 12 EGADS : CHECKING NODE MAP FOR BODY 1 FACE 13 EGADS : CHECKING NODE MAP FOR BODY 1 FACE 14 EGADS : CHECKING NODE MAP FOR BODY 1 FACE 15 EGADS : CHECKING NODE MAP FOR BODY 1 FACE 16 EGADS : CHECKING NODE MAP FOR BODY 2 FACE 17 EGADS : CHECKING NODE MAP FOR BODY 2 FACE 18 Volume mesh: Number of nodes = 73007 Number of elements = 426580 Number of triangles = 12428 Number of quadrilatarals = 0 Number of tetrahedrals = 414152 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 - Wing1 Boundary condition name - Wing2 Done getting CFD boundary conditions Writing boundary flags - bcProps.surfaceProp[0].surfaceType = 3 - bcProps.surfaceProp[1].surfaceType = 1 - bcProps.surfaceProp[2].surfaceType = 1 Done boundary flags Warning: The su2 cfg file will be overwritten! Write SU2 configuration file for version "Cardinal" Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - Wing2 Done getting CFD boundary conditions Writing boundary flags - bcProps.surfaceProp[0].surfaceType = 3 - bcProps.surfaceProp[1].surfaceType = 1 - bcProps.surfaceProp[2].surfaceType = 1 Done boundary flags Warning: The su2 cfg file will be overwritten! Write SU2 configuration file for version "Raven" Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - Wing2 Done getting CFD boundary conditions Writing boundary flags - bcProps.surfaceProp[0].surfaceType = 3 - bcProps.surfaceProp[1].surfaceType = 1 - bcProps.surfaceProp[2].surfaceType = 1 Done boundary flags Warning: The su2 cfg file will be overwritten! Write SU2 configuration file for version "Falcon" Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - Wing2 Done getting CFD boundary conditions Writing boundary flags - bcProps.surfaceProp[0].surfaceType = 3 - bcProps.surfaceProp[1].surfaceType = 1 - bcProps.surfaceProp[2].surfaceType = 1 Done boundary flags Warning: The su2 cfg file will be overwritten! Write SU2 configuration file for version "BlackBird (7.5.1) " ok test_invalidBoundary (test_su2.TestSU2.test_invalidBoundary) ... Getting CFD boundary conditions Boundary condition name - Wing1 ok test_invalidBoundaryName (test_su2.TestSU2.test_invalidBoundaryName) ... Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - X ok test_journal (test_su2.TestSU2.test_journal) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 AFLR4 : Proximity BG Surface Grid Generation Skipped AFLR4 : No Modifications Required Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 73007 Number of elements = 426580 Number of triangles = 12428 Number of quadrilatarals = 0 Number of tetrahedrals = 414152 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 - Wing1 Boundary condition name - Wing2 Done getting CFD boundary conditions Warning: The su2 cfg file will be overwritten! Write SU2 configuration file for version "Harrier (8.0.1)" Running SU2 1 Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - Wing2 Done getting CFD boundary conditions Writing boundary flags - bcProps.surfaceProp[0].surfaceType = 3 - bcProps.surfaceProp[1].surfaceType = 2 - bcProps.surfaceProp[2].surfaceType = 1 Done boundary flags Warning: The su2 cfg file will be overwritten! Write SU2 configuration file for version "Harrier (8.0.1)" Running SU2 2 EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 AFLR4 : Proximity BG Surface Grid Generation Skipped AFLR4 : No Modifications Required Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 73007 Number of elements = 426580 Number of triangles = 12428 Number of quadrilatarals = 0 Number of tetrahedrals = 414152 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 - Wing1 Boundary condition name - Wing2 Done getting CFD boundary conditions Warning: The su2 cfg file will be overwritten! Write SU2 configuration file for version "Harrier (8.0.1)" CAPS Info: Hit last success -- going live! Running SU2 1 CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - Wing2 Done getting CFD boundary conditions CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - Wing2 Done getting CFD boundary conditions Writing boundary flags - bcProps.surfaceProp[0].surfaceType = 3 - bcProps.surfaceProp[1].surfaceType = 2 - bcProps.surfaceProp[2].surfaceType = 1 Done boundary flags Warning: The su2 cfg file will be overwritten! Write SU2 configuration file for version "Harrier (8.0.1)" CAPS Info: Hit last success -- going live! Running SU2 2 CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - Wing2 Done getting CFD boundary conditions ok test_phase (test_su2.TestSU2.test_phase) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 AFLR4 : Proximity BG Surface Grid Generation Skipped AFLR4 : No Modifications Required Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 73007 Number of elements = 426580 Number of triangles = 12428 Number of quadrilatarals = 0 Number of tetrahedrals = 414152 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 - Wing1 Boundary condition name - Wing2 Done getting CFD boundary conditions Warning: The su2 cfg file will be overwritten! Write SU2 configuration file for version "Harrier (8.0.1)" Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - Wing2 Done getting CFD boundary conditions Writing boundary flags - bcProps.surfaceProp[0].surfaceType = 3 - bcProps.surfaceProp[1].surfaceType = 1 - bcProps.surfaceProp[2].surfaceType = 1 Done boundary flags Warning: The su2 cfg file will be overwritten! Write SU2 configuration file for version "Harrier (8.0.1)" ok test_reenter (test_su2.TestSU2.test_reenter) ... Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - Wing2 Done getting CFD boundary conditions Writing boundary flags - bcProps.surfaceProp[0].surfaceType = 3 - bcProps.surfaceProp[1].surfaceType = 1 - bcProps.surfaceProp[2].surfaceType = 1 Done boundary flags Warning: The su2 cfg file will be overwritten! Write SU2 configuration file for version "BlackBird (7.5.1) " Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - Wing2 Done getting CFD boundary conditions Writing boundary flags - bcProps.surfaceProp[0].surfaceType = 3 - bcProps.surfaceProp[1].surfaceType = 2 - bcProps.surfaceProp[2].surfaceType = 1 Done boundary flags Warning: The su2 cfg file will be overwritten! Write SU2 configuration file for version "BlackBird (7.5.1) " ok test_units (test_su2.TestSU2.test_units) ... Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - Wing2 Done getting CFD boundary conditions Warning: The su2 cfg file will be overwritten! Write SU2 configuration file for version "Harrier (8.0.1)" ok test_PlateSensFile (test_tacs.TestTACS.test_PlateSensFile) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Face 1 TFI quading disabled with attribute .qParams Getting surface mesh for body 1 (of 1) Body 1 (of 1) Number of nodes = 25 Number of elements = 16 Number of triangle elements = 0 Number of quadrilateral elements = 16 ---------------------------- Total number of nodes = 25 Total number of elements = 16 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Face 1 TFI quading disabled with attribute .qParams Getting surface mesh for body 1 (of 1) Body 1 (of 1) Number of nodes = 25 Number of elements = 16 Number of triangle elements = 0 Number of quadrilateral elements = 16 ---------------------------- Total number of nodes = 25 Total number of elements = 16 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 = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 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 = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate 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 - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 2 Design_Variable name - plateLength Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables 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 Writing Nastran grid and connectivity file (in small 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 Writing design variable cards Writing design variable relation cards 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 = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 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 = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate 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 - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 2 Design_Variable name - plateLength Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables 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 Writing Nastran grid and connectivity file (in small 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 Writing design variable cards Writing design variable relation cards 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 = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 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 = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate 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 - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 2 Design_Variable name - plateLength Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables 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 Writing Nastran grid and connectivity file (in small 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 Writing design variable cards Writing design variable relation cards 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 = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 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 = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate 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 - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 2 Design_Variable name - plateLength Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables 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 Writing Nastran grid and connectivity file (in small 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 Writing design variable cards Writing design variable relation cards 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 = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 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 = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate 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 - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 2 Design_Variable name - plateLength Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables 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 Writing Nastran grid and connectivity file (in small 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 Writing design variable cards Writing design variable relation cards 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 = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 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 = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate 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 - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 2 Design_Variable name - plateLength Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables 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 Writing Nastran grid and connectivity file (in small 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 Writing design variable cards Writing design variable relation cards 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 = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 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 = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate 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 - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 2 Design_Variable name - plateLength Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables 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 Writing Nastran grid and connectivity file (in small 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 Writing design variable cards Writing design variable relation cards 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 = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 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 = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate 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 - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 2 Design_Variable name - plateLength Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables 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 Writing Nastran grid and connectivity file (in small 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 Writing design variable cards Writing design variable relation cards 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 = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 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 = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate 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 - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 2 Design_Variable name - plateLength Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables 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 Writing Nastran grid and connectivity file (in small 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 Writing design variable cards Writing design variable relation cards 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 = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 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 = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate 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 - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 2 Design_Variable name - plateLength Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables 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 Writing Nastran grid and connectivity file (in small 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 Writing design variable cards Writing design variable relation cards 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 = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 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 = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate 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 - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 2 Design_Variable name - plateLength Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables 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 Writing Nastran grid and connectivity file (in small 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 Writing design variable cards Writing design variable relation cards 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 = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 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 = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate 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 - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 2 Design_Variable name - plateLength Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables 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 Writing Nastran grid and connectivity file (in small 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 Writing design variable cards Writing design variable relation cards 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 = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 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 = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate 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 - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 2 Design_Variable name - plateLength Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables 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 Writing Nastran grid and connectivity file (in small 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 Writing design variable cards Writing design variable relation cards 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 = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 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 = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate 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 - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 2 Design_Variable name - plateLength Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables 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 Writing Nastran grid and connectivity file (in small 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 Writing design variable cards Writing design variable relation cards 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 = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 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 = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate 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 - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 2 Design_Variable name - plateLength Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables 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 Writing Nastran grid and connectivity file (in small 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 Writing design variable cards Writing design variable relation cards 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 = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 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 = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate 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 - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 2 Design_Variable name - plateLength Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables 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 Writing Nastran grid and connectivity file (in small 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 Writing design variable cards Writing design variable relation cards 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 = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 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 = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate 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 - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 2 Design_Variable name - plateLength Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables 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 Writing Nastran grid and connectivity file (in small 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 Writing design variable cards Writing design variable relation cards 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 = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 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 = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate 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 - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 2 Design_Variable name - plateLength Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables 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 Writing Nastran grid and connectivity file (in small 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 Writing design variable cards Writing design variable relation cards 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 = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 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 = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate 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 - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 2 Design_Variable name - plateLength Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables 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 Writing Nastran grid and connectivity file (in small 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 Writing design variable cards Writing design variable relation cards 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 = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 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 = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate 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 - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 2 Design_Variable name - plateLength Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables 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 Writing Nastran grid and connectivity file (in small 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 Writing design variable cards Writing design variable relation cards 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 = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 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 = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate 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 - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 2 Design_Variable name - plateLength Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables 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 Writing Nastran grid and connectivity file (in small 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 Writing design variable cards Writing design variable relation cards 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 = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 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 = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate 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 - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 2 Design_Variable name - plateLength Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables 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 Writing Nastran grid and connectivity file (in small 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 Writing design variable cards Writing design variable relation cards 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 = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 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 = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate 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 - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 2 Design_Variable name - plateLength Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables 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 Writing Nastran grid and connectivity file (in small 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 Writing design variable cards Writing design variable relation cards 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 = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 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 = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate 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 - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 2 Design_Variable name - plateLength Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables 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 Writing Nastran grid and connectivity file (in small 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 Writing design variable cards Writing design variable relation cards 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 = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 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 = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate 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 - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 2 Design_Variable name - plateLength Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables 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 Writing Nastran grid and connectivity file (in small 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 Writing design variable cards Writing design variable relation cards 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 = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 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 = 1 Name = plate, index = 1 Projecting tessellation 1 (of 1) on to new body Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate 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 - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables 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 Writing Nastran grid and connectivity file (in small 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 Writing design variable cards 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 = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 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 = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate 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 - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables 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 Writing Nastran grid and connectivity file (in small 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 Writing design variable cards 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 = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 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 = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate 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 - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables 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 Writing Nastran grid and connectivity file (in small 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 Writing design variable cards 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 = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 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 = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate 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 - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables 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 Writing Nastran grid and connectivity file (in small 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 Writing design variable cards 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 = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 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 = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate 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 - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables 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 Writing Nastran grid and connectivity file (in small 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 Writing design variable cards 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 = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 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 = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate 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 - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables 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 Writing Nastran grid and connectivity file (in small 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 Writing design variable cards 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 = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 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 = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate 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 - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables 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 Writing Nastran grid and connectivity file (in small 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 Writing design variable cards 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 = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 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 = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate 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 - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables 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 Writing Nastran grid and connectivity file (in small 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 Writing design variable cards 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 = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 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 = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate 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 - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables 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 Writing Nastran grid and connectivity file (in small 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 Writing design variable cards 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 = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 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 = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate 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 - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables 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 Writing Nastran grid and connectivity file (in small 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 Writing design variable cards 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 = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 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 = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate 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 - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables 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 Writing Nastran grid and connectivity file (in small 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 Writing design variable cards 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 = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 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 = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate 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 - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables 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 Writing Nastran grid and connectivity file (in small 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 Writing design variable cards 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 = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 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 = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate 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 - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables 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 Writing Nastran grid and connectivity file (in small 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 Writing design variable cards 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 = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 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 = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate 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 - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables 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 Writing Nastran grid and connectivity file (in small 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 Writing design variable cards 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 = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 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 = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate 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 - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables 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 Writing Nastran grid and connectivity file (in small 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 Writing design variable cards 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 = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 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 = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate 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 - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables 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 Writing Nastran grid and connectivity file (in small 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 Writing design variable cards 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 = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 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 = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate 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 - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables 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 Writing Nastran grid and connectivity file (in small 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 Writing design variable cards 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 = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 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 = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate 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 - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables 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 Writing Nastran grid and connectivity file (in small 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 Writing design variable cards 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 = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 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 = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate 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 - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables 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 Writing Nastran grid and connectivity file (in small 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 Writing design variable cards 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 = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 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 = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate 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 - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables 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 Writing Nastran grid and connectivity file (in small 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 Writing design variable cards 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 = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 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 = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate 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 - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables 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 Writing Nastran grid and connectivity file (in small 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 Writing design variable cards 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 = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 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 = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate 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 - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables 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 Writing Nastran grid and connectivity file (in small 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 Writing design variable cards 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 = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 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 = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate 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 - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables 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 Writing Nastran grid and connectivity file (in small 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 Writing design variable cards 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 = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 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 = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate 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 - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables 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 Writing Nastran grid and connectivity file (in small 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 Writing design variable cards 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 = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 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 = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate 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 - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables 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 Writing Nastran grid and connectivity file (in small 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 Writing design variable cards 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 = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 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 = 1 Name = plate, index = 1 Projecting tessellation 1 (of 1) on to new body Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate 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 - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables 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 Writing Nastran grid and connectivity file (in small 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 Writing design variable cards 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 = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 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 = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate 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 - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables 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 Writing Nastran grid and connectivity file (in small 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 Writing design variable cards 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 = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 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 = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate 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 - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables 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 Writing Nastran grid and connectivity file (in small 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 Writing design variable cards 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 = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 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 = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate 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 - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables 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 Writing Nastran grid and connectivity file (in small 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 Writing design variable cards 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 = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 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 = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate 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 - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables 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 Writing Nastran grid and connectivity file (in small 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 Writing design variable cards 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 = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 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 = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate 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 - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables 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 Writing Nastran grid and connectivity file (in small 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 Writing design variable cards 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 = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 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 = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate 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 - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables 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 Writing Nastran grid and connectivity file (in small 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 Writing design variable cards 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 = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 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 = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate 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 - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables 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 Writing Nastran grid and connectivity file (in small 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 Writing design variable cards 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 = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 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 = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate 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 - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables 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 Writing Nastran grid and connectivity file (in small 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 Writing design variable cards 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 = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 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 = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate 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 - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables 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 Writing Nastran grid and connectivity file (in small 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 Writing design variable cards 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 = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 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 = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate 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 - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables 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 Writing Nastran grid and connectivity file (in small 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 Writing design variable cards 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 = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 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 = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate 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 - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables 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 Writing Nastran grid and connectivity file (in small 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 Writing design variable cards 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 = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 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 = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate 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 - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables 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 Writing Nastran grid and connectivity file (in small 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 Writing design variable cards 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 = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 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 = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate 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 - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables 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 Writing Nastran grid and connectivity file (in small 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 Writing design variable cards 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 = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 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 = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate 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 - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables 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 Writing Nastran grid and connectivity file (in small 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 Writing design variable cards 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 = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 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 = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate 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 - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables 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 Writing Nastran grid and connectivity file (in small 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 Writing design variable cards 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 = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 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 = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate 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 - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables 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 Writing Nastran grid and connectivity file (in small 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 Writing design variable cards 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 = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 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 = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate 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 - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables 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 Writing Nastran grid and connectivity file (in small 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 Writing design variable cards 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 = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 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 = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate 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 - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables 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 Writing Nastran grid and connectivity file (in small 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 Writing design variable cards 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 = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 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 = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate 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 - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables 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 Writing Nastran grid and connectivity file (in small 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 Writing design variable cards 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 = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 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 = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate 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 - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables 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 Writing Nastran grid and connectivity file (in small 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 Writing design variable cards 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 = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 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 = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate 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 - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables 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 Writing Nastran grid and connectivity file (in small 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 Writing design variable cards 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 = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 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 = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate 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 - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables 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 Writing Nastran grid and connectivity file (in small 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 Writing design variable cards 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 = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 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 = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate 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 - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables 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 Writing Nastran grid and connectivity file (in small 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 Writing design variable cards 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 = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 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 = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate 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 - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables 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 Writing Nastran grid and connectivity file (in small 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 Writing design variable cards 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 = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 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 = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate 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 - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables 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 Writing Nastran grid and connectivity file (in small 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 Writing design variable cards Writing design variable relation cards 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 = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 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 = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate 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 - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables 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 Writing Nastran grid and connectivity file (in small 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 Writing design variable cards Writing design variable relation cards 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 = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 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 = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate 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 - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables 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 Writing Nastran grid and connectivity file (in small 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 Writing design variable cards Writing design variable relation cards 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 = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 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 = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate 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 - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables 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 Writing Nastran grid and connectivity file (in small 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 Writing design variable cards Writing design variable relation cards 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 = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 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 = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate 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 - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables 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 Writing Nastran grid and connectivity file (in small 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 Writing design variable cards Writing design variable relation cards 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 = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 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 = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate 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 - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables 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 Writing Nastran grid and connectivity file (in small 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 Writing design variable cards Writing design variable relation cards 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 = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 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 = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate 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 - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables 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 Writing Nastran grid and connectivity file (in small 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 Writing design variable cards Writing design variable relation cards 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 = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 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 = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate 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 - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables 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 Writing Nastran grid and connectivity file (in small 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 Writing design variable cards Writing design variable relation cards 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 = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 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 = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate 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 - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables 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 Writing Nastran grid and connectivity file (in small 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 Writing design variable cards Writing design variable relation cards 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 = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 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 = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate 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 - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables 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 Writing Nastran grid and connectivity file (in small 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 Writing design variable cards Writing design variable relation cards 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 = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 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 = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate 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 - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables 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 Writing Nastran grid and connectivity file (in small 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 Writing design variable cards Writing design variable relation cards 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 = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 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 = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate 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 - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables 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 Writing Nastran grid and connectivity file (in small 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 Writing design variable cards Writing design variable relation cards 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 = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 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 = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate 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 - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables 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 Writing Nastran grid and connectivity file (in small 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 Writing design variable cards Writing design variable relation cards 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 = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 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 = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate 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 - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables 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 Writing Nastran grid and connectivity file (in small 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 Writing design variable cards Writing design variable relation cards 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 = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 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 = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate 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 - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables 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 Writing Nastran grid and connectivity file (in small 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 Writing design variable cards Writing design variable relation cards 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 = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 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 = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate 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 - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables 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 Writing Nastran grid and connectivity file (in small 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 Writing design variable cards Writing design variable relation cards 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 = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 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 = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate 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 - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables 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 Writing Nastran grid and connectivity file (in small 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 Writing design variable cards Writing design variable relation cards 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 = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 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 = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate 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 - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables 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 Writing Nastran grid and connectivity file (in small 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 Writing design variable cards Writing design variable relation cards 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 = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 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 = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate 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 - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables 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 Writing Nastran grid and connectivity file (in small 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 Writing design variable cards Writing design variable relation cards 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 = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 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 = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate 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 - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables 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 Writing Nastran grid and connectivity file (in small 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 Writing design variable cards Writing design variable relation cards 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 = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 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 = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate 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 - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables 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 Writing Nastran grid and connectivity file (in small 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 Writing design variable cards Writing design variable relation cards 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 = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 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 = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate 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 - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables 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 Writing Nastran grid and connectivity file (in small 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 Writing design variable cards Writing design variable relation cards 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 = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 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 = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate 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 - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables 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 Writing Nastran grid and connectivity file (in small 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 Writing design variable cards Writing design variable relation cards 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 = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 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 = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate 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 - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables 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 Writing Nastran grid and connectivity file (in small 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 Writing design variable cards Writing design variable relation cards 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 = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 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 = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate 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 - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables 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 Writing Nastran grid and connectivity file (in small 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 Writing design variable cards Writing design variable relation cards ok test_Multiple_Mesh (test_tetgen.TestTETGEN.test_Multiple_Mesh) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62031) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 7 Name = box, index = 1 Name = cylinder, index = 2 Name = cone, index = 3 Name = torus, index = 4 Name = sphere, index = 5 Name = boxhole, index = 6 Name = bullet, index = 7 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Getting surface mesh for body 1 (of 7) Getting surface mesh for body 2 (of 7) Getting surface mesh for body 3 (of 7) Getting surface mesh for body 4 (of 7) Getting surface mesh for body 5 (of 7) Getting surface mesh for body 6 (of 7) 112A55E00 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1! 700007FC5000 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1! 112A55E00 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1! 700007FC5000 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 4 7, sen = 1! Getting surface mesh for body 7 (of 7) Body 1 (of 7) Number of nodes = 98 Number of elements = 192 Number of triangle elements = 192 Number of quadrilateral elements = 0 Body 2 (of 7) Number of nodes = 294 Number of elements = 584 Number of triangle elements = 584 Number of quadrilateral elements = 0 Body 3 (of 7) Number of nodes = 488 Number of elements = 972 Number of triangle elements = 972 Number of quadrilateral elements = 0 Body 4 (of 7) Number of nodes = 2048 Number of elements = 4096 Number of triangle elements = 4096 Number of quadrilateral elements = 0 Body 5 (of 7) Number of nodes = 152 Number of elements = 300 Number of triangle elements = 300 Number of quadrilateral elements = 0 Body 6 (of 7) Number of nodes = 624 Number of elements = 1248 Number of triangle elements = 1248 Number of quadrilateral elements = 0 Body 7 (of 7) Number of nodes = 488 Number of elements = 972 Number of triangle elements = 972 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 4192 Total number of elements = 8364 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 7 Name = box, index = 1 Name = cylinder, index = 2 Name = cone, index = 3 Name = torus, index = 4 Name = sphere, index = 5 Name = boxhole, index = 6 Name = bullet, index = 7 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Body 1 number of surface: nodes - 98, elements - 192 Body 2 number of surface: nodes - 294, elements - 584 Body 3 number of surface: nodes - 488, elements - 972 Body 4 number of surface: nodes - 2048, elements - 4096 Body 5 number of surface: nodes - 152, elements - 300 Body 6 number of surface: nodes - 624, elements - 1248 Body 7 number of surface: nodes - 488, elements - 972 Getting volume mesh for body 1 (of 7) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = box, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Getting volume mesh for body 2 (of 7) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = cylinder, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Getting volume mesh for body 3 (of 7) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = cone, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Getting volume mesh for body 4 (of 7) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = torus, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Getting volume mesh for body 5 (of 7) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = sphere, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Getting volume mesh for body 6 (of 7) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = boxhole, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Getting volume mesh for body 7 (of 7) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = bullet, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 7 Name = box, index = 1 Name = cylinder, index = 2 Name = cone, index = 3 Name = torus, index = 4 Name = sphere, index = 5 Name = boxhole, index = 6 Name = bullet, index = 7 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Body 1 number of surface: nodes - 98, elements - 192 Body 2 number of surface: nodes - 294, elements - 584 Body 3 number of surface: nodes - 488, elements - 972 Body 4 number of surface: nodes - 2048, elements - 4096 Body 5 number of surface: nodes - 152, elements - 300 Body 6 number of surface: nodes - 624, elements - 1248 Body 7 number of surface: nodes - 488, elements - 972 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 7 Name = box, index = 1 Name = cylinder, index = 2 Name = cone, index = 3 Name = torus, index = 4 Name = sphere, index = 5 Name = boxhole, index = 6 Name = bullet, index = 7 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Number of surface: nodes - 4192, elements - 8364 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! ok test_faceMatch_MultiDomain (test_tetgen.TestTETGEN.test_faceMatch_MultiDomain) ... ../csmData/MultiDomain/example1.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting surface mesh for body 1 (of 2) Getting surface mesh for body 2 (of 2) Body 1 (of 2) Number of nodes = 374 Number of elements = 744 Number of triangle elements = 744 Number of quadrilateral elements = 0 Body 2 (of 2) Number of nodes = 98 Number of elements = 192 Number of triangle elements = 192 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 472 Total number of elements = 936 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Body 1 number of surface: nodes - 374, elements - 744 Body 2 number of surface: nodes - 98, elements - 192 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Body 1 number of surface: nodes - 374, elements - 744 Body 2 number of surface: nodes - 98, elements - 192 Getting volume mesh for body 1 (of 2) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Getting volume mesh for body 2 (of 2) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! ../csmData/MultiDomain/example2.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting surface mesh for body 1 (of 3) Getting surface mesh for body 2 (of 3) Getting surface mesh for body 3 (of 3) Body 1 (of 3) Number of nodes = 386 Number of elements = 768 Number of triangle elements = 768 Number of quadrilateral elements = 0 Body 2 (of 3) Number of nodes = 98 Number of elements = 192 Number of triangle elements = 192 Number of quadrilateral elements = 0 Body 3 (of 3) Number of nodes = 98 Number of elements = 192 Number of triangle elements = 192 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 582 Total number of elements = 1152 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Body 1 number of surface: nodes - 386, elements - 768 Body 2 number of surface: nodes - 98, elements - 192 Body 3 number of surface: nodes - 98, elements - 192 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Body 1 number of surface: nodes - 386, elements - 768 Body 2 number of surface: nodes - 98, elements - 192 Body 3 number of surface: nodes - 98, elements - 192 Getting volume mesh for body 1 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Getting volume mesh for body 2 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Getting volume mesh for body 3 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! ../csmData/MultiDomain/example3.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting surface mesh for body 1 (of 3) Getting surface mesh for body 2 (of 3) Getting surface mesh for body 3 (of 3) Body 1 (of 3) Number of nodes = 351 Number of elements = 698 Number of triangle elements = 698 Number of quadrilateral elements = 0 Body 2 (of 3) Number of nodes = 98 Number of elements = 192 Number of triangle elements = 192 Number of quadrilateral elements = 0 Body 3 (of 3) Number of nodes = 42 Number of elements = 80 Number of triangle elements = 80 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 491 Total number of elements = 970 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Body 1 number of surface: nodes - 351, elements - 698 Body 2 number of surface: nodes - 98, elements - 192 Body 3 number of surface: nodes - 42, elements - 80 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Body 1 number of surface: nodes - 351, elements - 698 Body 2 number of surface: nodes - 98, elements - 192 Body 3 number of surface: nodes - 42, elements - 80 Getting volume mesh for body 1 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Getting volume mesh for body 2 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Getting volume mesh for body 3 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! ../csmData/MultiDomain/example4.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting surface mesh for body 1 (of 3) Getting surface mesh for body 2 (of 3) Getting surface mesh for body 3 (of 3) Body 1 (of 3) Number of nodes = 376 Number of elements = 748 Number of triangle elements = 748 Number of quadrilateral elements = 0 Body 2 (of 3) Number of nodes = 98 Number of elements = 192 Number of triangle elements = 192 Number of quadrilateral elements = 0 Body 3 (of 3) Number of nodes = 42 Number of elements = 80 Number of triangle elements = 80 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 516 Total number of elements = 1020 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Body 1 number of surface: nodes - 376, elements - 748 Body 2 number of surface: nodes - 98, elements - 192 Body 3 number of surface: nodes - 42, elements - 80 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Body 1 number of surface: nodes - 376, elements - 748 Body 2 number of surface: nodes - 98, elements - 192 Body 3 number of surface: nodes - 42, elements - 80 Getting volume mesh for body 1 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Getting volume mesh for body 2 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Getting volume mesh for body 3 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! ../csmData/MultiDomain/example6.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting surface mesh for body 1 (of 3) Getting surface mesh for body 2 (of 3) Getting surface mesh for body 3 (of 3) Body 1 (of 3) Number of nodes = 370 Number of elements = 736 Number of triangle elements = 736 Number of quadrilateral elements = 0 Body 2 (of 3) Number of nodes = 42 Number of elements = 80 Number of triangle elements = 80 Number of quadrilateral elements = 0 Body 3 (of 3) Number of nodes = 42 Number of elements = 80 Number of triangle elements = 80 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 454 Total number of elements = 896 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Body 1 number of surface: nodes - 370, elements - 736 Body 2 number of surface: nodes - 42, elements - 80 Body 3 number of surface: nodes - 42, elements - 80 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Body 1 number of surface: nodes - 370, elements - 736 Body 2 number of surface: nodes - 42, elements - 80 Body 3 number of surface: nodes - 42, elements - 80 Getting volume mesh for body 1 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Getting volume mesh for body 2 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Getting volume mesh for body 3 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! ../csmData/MultiDomain/example7.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting surface mesh for body 1 (of 3) Getting surface mesh for body 2 (of 3) Getting surface mesh for body 3 (of 3) Body 1 (of 3) Number of nodes = 370 Number of elements = 736 Number of triangle elements = 736 Number of quadrilateral elements = 0 Body 2 (of 3) Number of nodes = 126 Number of elements = 252 Number of triangle elements = 252 Number of quadrilateral elements = 0 Body 3 (of 3) Number of nodes = 20 Number of elements = 36 Number of triangle elements = 36 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 516 Total number of elements = 1024 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Body 1 number of surface: nodes - 370, elements - 736 Body 2 number of surface: nodes - 126, elements - 252 Body 3 number of surface: nodes - 20, elements - 36 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Body 1 number of surface: nodes - 370, elements - 736 Body 2 number of surface: nodes - 126, elements - 252 Body 3 number of surface: nodes - 20, elements - 36 Getting volume mesh for body 1 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Getting volume mesh for body 2 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Getting volume mesh for body 3 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! ../csmData/MultiDomain/example8.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting surface mesh for body 1 (of 3) Getting surface mesh for body 2 (of 3) Getting surface mesh for body 3 (of 3) Body 1 (of 3) Number of nodes = 109 Number of elements = 214 Number of triangle elements = 214 Number of quadrilateral elements = 0 Body 2 (of 3) Number of nodes = 48 Number of elements = 96 Number of triangle elements = 96 Number of quadrilateral elements = 0 Body 3 (of 3) Number of nodes = 12 Number of elements = 20 Number of triangle elements = 20 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 169 Total number of elements = 330 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Body 1 number of surface: nodes - 109, elements - 214 Body 2 number of surface: nodes - 48, elements - 96 Body 3 number of surface: nodes - 12, elements - 20 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Body 1 number of surface: nodes - 109, elements - 214 Body 2 number of surface: nodes - 48, elements - 96 Body 3 number of surface: nodes - 12, elements - 20 Getting volume mesh for body 1 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Getting volume mesh for body 2 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Getting volume mesh for body 3 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! ../csmData/MultiDomain/example9.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting surface mesh for body 1 (of 2) Getting surface mesh for body 2 (of 2) Body 1 (of 2) Number of nodes = 536 Number of elements = 1072 Number of triangle elements = 1072 Number of quadrilateral elements = 0 Body 2 (of 2) Number of nodes = 544 Number of elements = 1084 Number of triangle elements = 1084 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 1080 Total number of elements = 2156 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Body 1 number of surface: nodes - 536, elements - 1072 Body 2 number of surface: nodes - 544, elements - 1084 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Body 1 number of surface: nodes - 536, elements - 1072 Body 2 number of surface: nodes - 544, elements - 1084 Getting volume mesh for body 1 (of 2) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Getting volume mesh for body 2 (of 2) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! ../csmData/MultiDomain/multi_prim.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting surface mesh for body 1 (of 5) Getting surface mesh for body 2 (of 5) Getting surface mesh for body 3 (of 5) Getting surface mesh for body 4 (of 5) Getting surface mesh for body 5 (of 5) Body 1 (of 5) Number of nodes = 1351 Number of elements = 2682 Number of triangle elements = 2682 Number of quadrilateral elements = 0 Body 2 (of 5) Number of nodes = 288 Number of elements = 572 Number of triangle elements = 572 Number of quadrilateral elements = 0 Body 3 (of 5) Number of nodes = 174 Number of elements = 344 Number of triangle elements = 344 Number of quadrilateral elements = 0 Body 4 (of 5) Number of nodes = 26 Number of elements = 48 Number of triangle elements = 48 Number of quadrilateral elements = 0 Body 5 (of 5) Number of nodes = 482 Number of elements = 960 Number of triangle elements = 960 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 2321 Total number of elements = 4606 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Body 1 number of surface: nodes - 1351, elements - 2682 Body 2 number of surface: nodes - 288, elements - 572 Body 3 number of surface: nodes - 174, elements - 344 Body 4 number of surface: nodes - 26, elements - 48 Body 5 number of surface: nodes - 482, elements - 960 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Body 1 number of surface: nodes - 1351, elements - 2682 Body 2 number of surface: nodes - 288, elements - 572 Body 3 number of surface: nodes - 174, elements - 344 Body 4 number of surface: nodes - 26, elements - 48 Body 5 number of surface: nodes - 482, elements - 960 Getting volume mesh for body 1 (of 5) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Getting volume mesh for body 2 (of 5) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Getting volume mesh for body 3 (of 5) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Getting volume mesh for body 4 (of 5) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Getting volume mesh for body 5 (of 5) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! ../csmData/MultiDomain/cyl_seam.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting surface mesh for body 1 (of 2) Getting surface mesh for body 2 (of 2) Body 1 (of 2) Number of nodes = 444 Number of elements = 884 Number of triangle elements = 884 Number of quadrilateral elements = 0 Body 2 (of 2) Number of nodes = 522 Number of elements = 1044 Number of triangle elements = 1044 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 966 Total number of elements = 1928 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Body 1 number of surface: nodes - 444, elements - 884 Body 2 number of surface: nodes - 522, elements - 1044 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Body 1 number of surface: nodes - 444, elements - 884 Body 2 number of surface: nodes - 522, elements - 1044 Getting volume mesh for body 1 (of 2) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Getting volume mesh for body 2 (of 2) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! ok test_journal (test_tetgen.TestTETGEN.test_journal) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Getting mesh sizing parameters Mesh sizing name - Farfield Done getting mesh sizing parameters Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Number of surface: nodes - 9601, elements - 19194 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Number of surface: nodes - 9601, elements - 19194 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq2.000/0.000QT1.00e-16A Done meshing using TetGen! EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Getting mesh sizing parameters Mesh sizing name - Farfield Done getting mesh sizing parameters Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Number of surface: nodes - 9601, elements - 19194 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Getting mesh sizing parameters Mesh sizing name - Farfield Done getting mesh sizing parameters Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Getting mesh sizing parameters Mesh sizing name - Farfield Done getting mesh sizing parameters Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Getting mesh sizing parameters Mesh sizing name - Farfield Done getting mesh sizing parameters Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Number of surface: nodes - 9601, elements - 19194 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq2.000/0.000QT1.00e-16A Done meshing using TetGen! CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Getting mesh sizing parameters Mesh sizing name - Farfield Done getting mesh sizing parameters Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 ok test_phase (test_tetgen.TestTETGEN.test_phase) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Getting mesh sizing parameters Mesh sizing name - Farfield Done getting mesh sizing parameters Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Number of surface: nodes - 9601, elements - 19194 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Getting mesh sizing parameters Mesh sizing name - Farfield Done getting mesh sizing parameters Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Getting mesh sizing parameters Mesh sizing name - Farfield Done getting mesh sizing parameters Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Number of surface: nodes - 7173, elements - 14338 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! ok test_reenter (test_tetgen.TestTETGEN.test_reenter) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Getting mesh sizing parameters Mesh sizing name - Farfield Done getting mesh sizing parameters Getting surface mesh for body 1 (of 1) Body 1 (of 1) Number of nodes = 9601 Number of elements = 19194 Number of triangle elements = 19194 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 9601 Total number of elements = 19194 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Number of surface: nodes - 9601, elements - 19194 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Writing Binary VTK file .... Finished writing Binary VTK file Writing vtk file .... Writing vtk general file .... Finished writing vtk file Writing FAST file .... Finished writing FAST file Writing SU2 file .... Finished writing SU2 file Writing Binary STL file .... Finished writing Binary STL file Writing ASCII STL file .... Finished writing ASCII STL file Writing Tecplot file .... Finished writing Tecplot file Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Number of surface: nodes - 9601, elements - 19194 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq2.000/0.000QT1.00e-16A Done meshing using TetGen! Writing Binary VTK file .... Finished writing Binary VTK file Writing vtk file .... Writing vtk general file .... Finished writing vtk file Writing FAST file .... Finished writing FAST file Writing SU2 file .... Finished writing SU2 file Writing Binary STL file .... Finished writing Binary STL file Writing ASCII STL file .... Finished writing ASCII STL file Writing Tecplot file .... Finished writing Tecplot file ok test_setInput (test_tetgen.TestTETGEN.test_setInput) ... ok EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! test_Cl (test_xfoil.Testxfoil_Kulfan.test_Cl) ... ok test_alpha_custom_increment (test_xfoil.Testxfoil_Kulfan.test_alpha_custom_increment) ... ok test_CL_uniform_increment (test_xfoil.Testxfoil_NACA.test_CL_uniform_increment) ... ok test_Cl (test_xfoil.Testxfoil_NACA.test_Cl) ... ok test_alpha_custom_increment (test_xfoil.Testxfoil_NACA.test_alpha_custom_increment) ... ok test_alpha_uniform_inrement (test_xfoil.Testxfoil_NACA.test_alpha_uniform_inrement) ... ok test_append (test_xfoil.Testxfoil_NACA.test_append) ... ok test_normalize (test_xfoil.Testxfoil_NACA.test_normalize) ... ok test_phase (test_xfoil.Testxfoil_NACA.test_phase) ... ok test_Output (test_zaero.TestZAERO.test_Output) ... ok test_inputs (test_zaero.TestZAERO.test_inputs) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 6 Name = Ribs, index = 1 Name = Skin, index = 2 Name = Spar1, index = 3 Name = Rib_Root, index = 4 Name = Spar2, index = 5 Name = Rib_Root_Point, index = 6 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 2 Name = LeadingEdge, index = 1 Name = TrailingEdge, index = 2 Getting surface mesh for body 1 (of 2) Getting surface mesh for body 2 (of 2) Body 1 (of 2) Number of nodes = 1220 Number of elements = 2680 Number of triangle elements = 2680 Number of quadrilateral elements = 0 Body 2 (of 2) Number of nodes = 1 Number of elements = 0 Number of triangle elements = 0 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 1221 Total number of elements = 2680 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_Point, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 1 Name = Skin_Top, index = 1 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 1 Name = Rib_Root, index = 1 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 6 Name = Ribs, index = 1 Name = Skin, index = 2 Name = Spar1, index = 3 Name = Rib_Root, index = 4 Name = Spar2, index = 5 Name = Rib_Root_Point, index = 6 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 1220 Number of elements = 2680 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 2680 Elemental Quad4 = 0 Setting FEA Data Mesh for body = 1 Number of nodal coordinates = 1 Number of elements = 1 Elemental Nodes = 1 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 0 Combining multiple FEA meshes! Combined Number of nodal coordinates = 1221 Combined Number of elements = 2681 Combined Elemental Nodes = 1 Combined Elemental Rods = 0 Combined Elemental Tria3 = 2680 Combined Elemental Quad4 = 0 Getting FEA materials....... Number of materials - 1 Material name - madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 6 Property name - Rib_Root Property name - Rib_Root_Point Property name - Ribs Property name - Skin Property name - Spar1 Property name - Spar2 Done getting FEA properties Updating mesh element types based on properties input 'Smart_Restart' is ON Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = Wing, index = 1 Getting vortex lattice surface data VLM surface name - WingSurface Done getting vortex lattice surface data Getting vortex lattice control surface data VLM control surface name - CntrlLE VLM control surface name - CntrlTE Done getting vortex lattice control surface data Getting FEA vortex lattice mesh Getting ZAERO UAIC Configurations....... Number of UAIC Configurations - 2 UAIC Configuration: climb, id = 1 - Mach Number : 0.200000 - Reduced Freq: [0.020000, ... , 0.250000] UAIC Configuration: cruise, id = 2 - Mach Number : 0.700000 - Reduced Freq: [0.040000, ... , 0.350000] Getting ZAERO Analysis Subcases....... Number of Analysis Subcases - 2 Analysis Subcase: FlutterCruise, id = 1 - Discipline : flutter - UAIC : cruise Analysis Subcase: Trim, id = 2 - Discipline : Trim - UAIC : climb Getting ZAERO Trim Variables....... Number of Trim Variables - 2 Trim Variable: ANGLEA - Label : ALPHA - Value : free Trim Variable: URDD3 - Label : NZ - Value : 1.0 Updating StaticAeroelastic subcase: Trim - vectorToCG -> [0.345898, 1.652951, -0.041403] - weight -> 476456.149985 - weightMomentOfInertia -> [304902.643270, 98963.803820, 69822.813290, 6179.981375, 19723.152207, 370546.335523] ok ---------------------------------------------------------------------- Ran 143 tests in 1015.431s OK (skipped=15) /Library/Developer/CommandLineTools/usr/bin/make -C legacy/aim/pyCAPS test python --version Python 3.11.5 python -u -m unittest discover Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 5 Name = 2DSlice, index = 1 Name = TunnelWall, index = 2 Name = OutFlow, index = 3 Name = InFlow, index = 4 Name = Airfoil, index = 5 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = TunnelWall, index = 1 Name = OutFlow, index = 2 Name = InFlow, index = 3 Name = Airfoil, index = 4 Getting mesh sizing parameters Mesh sizing name - 2DSlice Mesh sizing name - Airfoil Mesh sizing name - InFlow Mesh sizing name - OutFlow Mesh sizing name - TunnelWall Done getting mesh sizing parameters Getting 2D mesh for body 1 (of 1) AFLR2 : --------------------------------------- AFLR2 : AFLR2 LIBRARY AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR2 : TRIA/QUAD GRID GENERATOR AFLR2 : Version Number 9.17.15 AFLR2 : Version Date 04/23/24 @ 12:51AM AFLR2 : Compile OS Darwin 23.4.0 x86_64 AFLR2 : Compile Date 04/23/24 @ 11:49AM AFLR2 : Copyright 1994-2021, D.L. Marcum AFLR2 : --------------------------------------- AFLR2 IC : INPUT DATA CHECK AFLR2 IC : Nodes, Faces = 344 0 AFLR2 : CPU Time = 0.000 seconds AFLR2 EG : EDGE GRID RE-GENERATION AFLR2 EG : Nodes, Edges = 344 344 AFLR2 : CPU Time = 0.000 seconds AFLR2 IG : INITIAL GRID GENERATION AFLR2 IG : Nodes, Faces = 0 2 AFLR2 IG : Nodes, Faces = 70 142 AFLR2 IG : Nodes, Faces = 140 282 AFLR2 IG : Nodes, Faces = 210 422 AFLR2 IG : Nodes, Faces = 280 562 AFLR2 IG : Nodes, Faces = 316 634 AFLR2 IG : Nodes, Faces = 344 690 AFLR2 IG : Nodes, Faces = 348 690 AFLR2 IG : Nodes, Faces = 344 344 AFLR2 : CPU Time = 0.001 seconds AFLR2 GG : FIELD GRID GENERATION AFLR2 GG : Nodes, Faces = 344 344 AFLR2 GG : Nodes, Faces = 680 1016 AFLR2 GG : Nodes, Faces = 1009 1674 AFLR2 GG : Nodes, Faces = 1333 2322 AFLR2 GG : Nodes, Faces = 1650 2956 AFLR2 GG : Nodes, Faces = 1957 3570 AFLR2 GG : Nodes, Faces = 2258 4172 AFLR2 GG : Nodes, Faces = 2548 4752 AFLR2 GG : Nodes, Faces = 2831 5318 AFLR2 GG : Nodes, Faces = 3102 5860 AFLR2 GG : Nodes, Faces = 3364 6384 AFLR2 GG : Nodes, Faces = 3614 6884 AFLR2 GG : Nodes, Faces = 3830 7316 AFLR2 GG : Nodes, Faces = 4037 7730 AFLR2 GG : Nodes, Faces = 4229 8114 AFLR2 GG : Nodes, Faces = 4415 8486 AFLR2 GG : Nodes, Faces = 4594 8844 AFLR2 GG : Nodes, Faces = 4763 9182 AFLR2 GG : Nodes, Faces = 4926 9508 AFLR2 GG : Nodes, Faces = 5086 9828 AFLR2 GG : Nodes, Faces = 5239 10134 AFLR2 GG : Nodes, Faces = 5385 10426 AFLR2 GG : Nodes, Faces = 5529 10714 AFLR2 GG : Nodes, Faces = 5669 10994 AFLR2 GG : Nodes, Faces = 5812 11280 AFLR2 GG : Nodes, Faces = 5943 11542 AFLR2 GG : Nodes, Faces = 6070 11796 AFLR2 GG : Nodes, Faces = 6189 12034 AFLR2 GG : Nodes, Faces = 6307 12270 AFLR2 GG : Nodes, Faces = 6415 12486 AFLR2 GG : Nodes, Faces = 6510 12676 AFLR2 GG : Nodes, Faces = 6595 12846 AFLR2 GG : Nodes, Faces = 6665 12986 AFLR2 GG : Nodes, Faces = 6727 13110 AFLR2 GG : Nodes, Faces = 6772 13200 AFLR2 GG : Nodes, Faces = 6806 13268 AFLR2 GG : Nodes, Faces = 6831 13318 AFLR2 GG : Nodes, Faces = 6850 13356 AFLR2 GG : Nodes, Faces = 6864 13384 AFLR2 GG : Nodes, Faces = 6872 13400 AFLR2 GG : Nodes, Faces = 6875 13406 AFLR2 GG : Nodes, Faces = 6876 13408 AFLR2 : CPU Time = 0.018 seconds AFLR2 QI : QUALITY IMPROVEMENT AFLR2 QI : Nodes, Faces = 6876 13408 AFLR2 : CPU Time = 0.002 seconds AFLR2 : DONE Writing AFLR3 file .... Finished writing AFLR3 file Number of nodes = 6876 Number of elements = 13752 Number of tris = 13408 Number of quad = 0 Writing Tecplot file .... Tecplot expects 2D meshes in the x-y plane... attempting to rotate mesh! Swapping z and y coordinates! Finished writing Tecplot file Getting mesh sizing parameters Mesh sizing name - 2DSlice Mesh sizing name - Airfoil Mesh sizing name - InFlow Mesh sizing name - OutFlow Mesh sizing name - TunnelWall Done getting mesh sizing parameters Getting 2D mesh for body 1 (of 1) UG PARAM : SETTING INPUT PARAMETERS FROM ARGUMENT VECTOR UG PARAM : mquad = 1 UG PARAM : mpp = 3 AFLR2 IC : INPUT DATA CHECK AFLR2 IC : Nodes, Faces = 344 0 AFLR2 : CPU Time = 0.000 seconds AFLR2 EG : EDGE GRID RE-GENERATION AFLR2 EG : Nodes, Edges = 344 344 AFLR2 : CPU Time = 0.000 seconds AFLR2 IG : INITIAL GRID GENERATION AFLR2 IG : Nodes, Faces = 0 2 AFLR2 IG : Nodes, Faces = 70 142 AFLR2 IG : Nodes, Faces = 140 282 AFLR2 IG : Nodes, Faces = 210 422 AFLR2 IG : Nodes, Faces = 280 562 AFLR2 IG : Nodes, Faces = 316 634 AFLR2 IG : Nodes, Faces = 344 690 AFLR2 IG : Nodes, Faces = 348 690 AFLR2 IG : Nodes, Faces = 344 344 AFLR2 : CPU Time = 0.001 seconds AFLR2 GG : FIELD GRID GENERATION AFLR2 GGp: Nodes, Faces = 344 344 AFLR2 GGp: Nodes, Faces = 681 1018 AFLR2 GGp: Nodes, Faces = 1013 1682 AFLR2 GGp: Nodes, Faces = 1339 2334 AFLR2 GGp: Nodes, Faces = 1652 2960 AFLR2 GGp: Nodes, Faces = 1957 3570 AFLR2 GGp: Nodes, Faces = 2252 4160 AFLR2 GGp: Nodes, Faces = 2526 4708 AFLR2 GGp: Nodes, Faces = 2809 5274 AFLR2 GGp: Nodes, Faces = 3083 5822 AFLR2 GGp: Nodes, Faces = 3327 6310 AFLR2 GGp: Nodes, Faces = 3564 6784 AFLR2 GGp: Nodes, Faces = 3788 7232 AFLR2 GGp: Nodes, Faces = 3995 7646 AFLR2 GGp: Nodes, Faces = 4194 8044 AFLR2 GGp: Nodes, Faces = 4394 8444 AFLR2 GGp: Nodes, Faces = 4585 8826 AFLR2 GGp: Nodes, Faces = 4772 9200 AFLR2 GGp: Nodes, Faces = 4943 9542 AFLR2 GGp: Nodes, Faces = 5129 9914 AFLR2 GGp: Nodes, Faces = 5293 10242 AFLR2 GGp: Nodes, Faces = 5447 10550 AFLR2 GGp: Nodes, Faces = 5594 10844 AFLR2 GGp: Nodes, Faces = 5716 11088 AFLR2 GGp: Nodes, Faces = 5830 11316 AFLR2 GGp: Nodes, Faces = 5909 11474 AFLR2 GGp: Nodes, Faces = 5964 11584 AFLR2 GGp: Nodes, Faces = 6006 11668 AFLR2 GGp: Nodes, Faces = 6025 11706 AFLR2 GGp: Nodes, Faces = 6034 11724 AFLR2 : CPU Time = 0.023 seconds AFLR2 QI : QUALITY IMPROVEMENT AFLR2 QI : Nodes, Faces = 6034 11724 AFLR2 QI : Nodes, Faces = 6033 454 AFLR2 QI : Nodes, Faces = 6033 5634 AFLR2 QI : Nodes, Faces = 6033 11722 AFLR2 QI : Nodes, Faces = 6032 462 AFLR2 QI : Nodes, Faces = 6032 5629 AFLR2 QI : Nodes, Faces = 6032 11720 AFLR2 QI : Nodes, Faces = 6032 456 AFLR2 QI : Nodes, Faces = 6032 5632 AFLR2 QI : Nodes, Faces = 6032 11720 AFLR2 QI : Nodes, Faces = 6032 474 AFLR2 QI : Nodes, Faces = 6032 5623 AFLR2 QI : Nodes, Faces = 6032 11720 AFLR2 QI : Nodes, Faces = 6031 486 AFLR2 QI : Nodes, Faces = 6031 5616 AFLR2 QI : Nodes, Faces = 6031 488 AFLR2 QI : Nodes, Faces = 6031 5616 AFLR2 : CPU Time = 0.011 seconds AFLR2 : DONE EGADS Internal: Face 1, Side 4741 4722 complete [but 7915] (EG_makeConnect)! EGADS Internal: Face 1, Side 4741 4912 complete [but 7916] (EG_makeConnect)! EGADS Internal: Face 1, Side 5850 5858 complete [but 8742] (EG_makeConnect)! EGADS Internal: Face 1, Side 5850 5851 complete [but 8742] (EG_makeConnect)! EGADS Internal: Face 1, Side 5858 5851 complete [but 8791] (EG_makeConnect)! EGADS Internal: Face 1, Side 4912 4722 complete [but 9417] (EG_makeConnect)! Writing AFLR3 file .... Finished writing AFLR3 file Number of nodes = 6031 Number of elements = 6448 Number of tris = 488 Number of quad = 5616 EGADS Internal: Face 1, Side 4741 4722 complete [but 7915] (EG_makeConnect)! EGADS Internal: Face 1, Side 4741 4912 complete [but 7916] (EG_makeConnect)! EGADS Internal: Face 1, Side 5850 5858 complete [but 8742] (EG_makeConnect)! EGADS Internal: Face 1, Side 5850 5851 complete [but 8742] (EG_makeConnect)! EGADS Internal: Face 1, Side 5858 5851 complete [but 8791] (EG_makeConnect)! EGADS Internal: Face 1, Side 4912 4722 complete [but 9417] (EG_makeConnect)! EGADS Internal: Face 1, Side 4741 4722 complete [but 7915] (EG_makeConnect)! EGADS Internal: Face 1, Side 4741 4912 complete [but 7916] (EG_makeConnect)! EGADS Internal: Face 1, Side 5850 5858 complete [but 8742] (EG_makeConnect)! EGADS Internal: Face 1, Side 5850 5851 complete [but 8742] (EG_makeConnect)! EGADS Internal: Face 1, Side 5858 5851 complete [but 8791] (EG_makeConnect)! EGADS Internal: Face 1, Side 4912 4722 complete [but 9417] (EG_makeConnect)! Writing Tecplot file .... Tecplot expects 2D meshes in the x-y plane... attempting to rotate mesh! Swapping z and y coordinates! Finished writing Tecplot file .Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 5 Name = 2DSlice, index = 1 Name = TunnelWall, index = 2 Name = OutFlow, index = 3 Name = InFlow, index = 4 Name = Airfoil, index = 5 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = TunnelWall, index = 1 Name = OutFlow, index = 2 Name = InFlow, index = 3 Name = Airfoil, index = 4 Getting mesh sizing parameters Mesh sizing name - 2DSlice Mesh sizing name - Airfoil Mesh sizing name - InFlow Mesh sizing name - OutFlow Mesh sizing name - TunnelWall Done getting mesh sizing parameters Getting 2D mesh for body 1 (of 1) AFLR2 : --------------------------------------- AFLR2 : AFLR2 LIBRARY AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR2 : TRIA/QUAD GRID GENERATOR AFLR2 : Version Number 9.17.15 AFLR2 : Version Date 04/23/24 @ 12:51AM AFLR2 : Compile OS Darwin 23.4.0 x86_64 AFLR2 : Compile Date 04/23/24 @ 11:49AM AFLR2 : Copyright 1994-2021, D.L. Marcum AFLR2 : --------------------------------------- AFLR2 IC : INPUT DATA CHECK AFLR2 IC : Nodes, Faces = 344 0 AFLR2 : CPU Time = 0.001 seconds AFLR2 EG : EDGE GRID RE-GENERATION AFLR2 EG : Nodes, Edges = 344 344 AFLR2 : CPU Time = 0.000 seconds AFLR2 IG : INITIAL GRID GENERATION AFLR2 IG : Nodes, Faces = 0 2 AFLR2 IG : Nodes, Faces = 70 142 AFLR2 IG : Nodes, Faces = 140 282 AFLR2 IG : Nodes, Faces = 210 422 AFLR2 IG : Nodes, Faces = 280 562 AFLR2 IG : Nodes, Faces = 316 634 AFLR2 IG : Nodes, Faces = 344 690 AFLR2 IG : Nodes, Faces = 348 690 AFLR2 IG : Nodes, Faces = 344 344 AFLR2 : CPU Time = 0.002 seconds AFLR2 GG : FIELD GRID GENERATION AFLR2 GGp: Nodes, Faces = 344 344 AFLR2 GGp: Nodes, Faces = 681 1018 AFLR2 GGp: Nodes, Faces = 1013 1682 AFLR2 GGp: Nodes, Faces = 1339 2334 AFLR2 GGp: Nodes, Faces = 1652 2960 AFLR2 GGp: Nodes, Faces = 1957 3570 AFLR2 GGp: Nodes, Faces = 2252 4160 AFLR2 GGp: Nodes, Faces = 2526 4708 AFLR2 GGp: Nodes, Faces = 2809 5274 AFLR2 GGp: Nodes, Faces = 3083 5822 AFLR2 GGp: Nodes, Faces = 3327 6310 AFLR2 GGp: Nodes, Faces = 3564 6784 AFLR2 GGp: Nodes, Faces = 3788 7232 AFLR2 GGp: Nodes, Faces = 3995 7646 AFLR2 GGp: Nodes, Faces = 4194 8044 AFLR2 GGp: Nodes, Faces = 4394 8444 AFLR2 GGp: Nodes, Faces = 4585 8826 AFLR2 GGp: Nodes, Faces = 4772 9200 AFLR2 GGp: Nodes, Faces = 4943 9542 AFLR2 GGp: Nodes, Faces = 5129 9914 AFLR2 GGp: Nodes, Faces = 5293 10242 AFLR2 GGp: Nodes, Faces = 5447 10550 AFLR2 GGp: Nodes, Faces = 5594 10844 AFLR2 GGp: Nodes, Faces = 5716 11088 AFLR2 GGp: Nodes, Faces = 5830 11316 AFLR2 GGp: Nodes, Faces = 5909 11474 AFLR2 GGp: Nodes, Faces = 5964 11584 AFLR2 GGp: Nodes, Faces = 6006 11668 AFLR2 GGp: Nodes, Faces = 6025 11706 AFLR2 GGp: Nodes, Faces = 6034 11724 AFLR2 : CPU Time = 0.021 seconds AFLR2 QI : QUALITY IMPROVEMENT AFLR2 QI : Nodes, Faces = 6034 11724 AFLR2 QI : Nodes, Faces = 6033 454 AFLR2 QI : Nodes, Faces = 6033 5634 AFLR2 QI : Nodes, Faces = 6033 11722 AFLR2 QI : Nodes, Faces = 6032 462 AFLR2 QI : Nodes, Faces = 6032 5629 AFLR2 QI : Nodes, Faces = 6032 11720 AFLR2 QI : Nodes, Faces = 6032 456 AFLR2 QI : Nodes, Faces = 6032 5632 AFLR2 QI : Nodes, Faces = 6032 11720 AFLR2 QI : Nodes, Faces = 6032 474 AFLR2 QI : Nodes, Faces = 6032 5623 AFLR2 QI : Nodes, Faces = 6032 11720 AFLR2 QI : Nodes, Faces = 6031 486 AFLR2 QI : Nodes, Faces = 6031 5616 AFLR2 QI : Nodes, Faces = 6031 488 AFLR2 QI : Nodes, Faces = 6031 5616 AFLR2 : CPU Time = 0.011 seconds AFLR2 : DONE EGADS Internal: Face 1, Side 4741 4722 complete [but 7915] (EG_makeConnect)! EGADS Internal: Face 1, Side 4741 4912 complete [but 7916] (EG_makeConnect)! EGADS Internal: Face 1, Side 5850 5858 complete [but 8742] (EG_makeConnect)! EGADS Internal: Face 1, Side 5850 5851 complete [but 8742] (EG_makeConnect)! EGADS Internal: Face 1, Side 5858 5851 complete [but 8791] (EG_makeConnect)! EGADS Internal: Face 1, Side 4912 4722 complete [but 9417] (EG_makeConnect)! Writing AFLR3 file .... Finished writing AFLR3 file Number of nodes = 6031 Number of elements = 6448 Number of tris = 488 Number of quad = 5616 EGADS Internal: Face 1, Side 4741 4722 complete [but 7915] (EG_makeConnect)! EGADS Internal: Face 1, Side 4741 4912 complete [but 7916] (EG_makeConnect)! EGADS Internal: Face 1, Side 5850 5858 complete [but 8742] (EG_makeConnect)! EGADS Internal: Face 1, Side 5850 5851 complete [but 8742] (EG_makeConnect)! EGADS Internal: Face 1, Side 5858 5851 complete [but 8791] (EG_makeConnect)! EGADS Internal: Face 1, Side 4912 4722 complete [but 9417] (EG_makeConnect)! EGADS Internal: Face 1, Side 4741 4722 complete [but 7915] (EG_makeConnect)! EGADS Internal: Face 1, Side 4741 4912 complete [but 7916] (EG_makeConnect)! EGADS Internal: Face 1, Side 5850 5858 complete [but 8742] (EG_makeConnect)! EGADS Internal: Face 1, Side 5850 5851 complete [but 8742] (EG_makeConnect)! EGADS Internal: Face 1, Side 5858 5851 complete [but 8791] (EG_makeConnect)! EGADS Internal: Face 1, Side 4912 4722 complete [but 9417] (EG_makeConnect)! Writing Tecplot file .... Tecplot expects 2D meshes in the x-y plane... attempting to rotate mesh! Swapping z and y coordinates! Finished writing Tecplot file .Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 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 x86_64 AFLR2 : Compile Date 04/23/24 @ 11:49AM 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 x86_64 AFLR4 : Compile Date 04/23/24 @ 11:49AM AFLR4 : Copyright 1994-2021, D.L. Marcum AFLR4 : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : EGADS CAD Geometry Setup EGADS : Model has 3 Active Bodies EGADS : Body 0 is a SolidBody EGADS : Body 0 has 1 Shells EGADS : Body 0 has 8 Faces EGADS : Body 0 has 15 Edges EGADS : Body 0 has 8 Loops EGADS : Body 0 has 9 Nodes EGADS : Body 1 is a SolidBody EGADS : Body 1 has 1 Shells EGADS : Body 1 has 8 Faces EGADS : Body 1 has 15 Edges EGADS : Body 1 has 8 Loops EGADS : Body 1 has 9 Nodes EGADS : Body 2 is a SolidBody EGADS : Body 2 has 1 Shells EGADS : Body 2 has 2 Faces EGADS : Body 2 has 6 Edges EGADS : Body 2 has 2 Loops EGADS : Body 2 has 2 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 1 1 2 3 4 5 EGADS : 2 Yes 0 0 1 1 1 1 3 4 6 EGADS : 3 Yes 0 0 1 1 1 1 2 4 7 EGADS : 4 Yes 0 0 1 1 1 1 2 3 EGADS : 5 Yes 0 0 1 1 1 1 6 7 8 EGADS : 6 Yes 0 0 1 1 1 2 5 7 8 EGADS : 7 Yes 0 0 1 1 1 3 5 6 8 EGADS : 8 Yes 0 0 1 1 1 5 6 7 EGADS : 9 Yes 1 0 1 0 10 10 11 12 13 EGADS : 10 Yes 1 0 1 0 10 9 11 12 14 EGADS : 11 Yes 1 0 1 0 10 9 10 12 15 EGADS : 12 Yes 1 0 1 0 10 9 10 11 EGADS : 13 Yes 1 0 1 0 10 9 14 15 16 EGADS : 14 Yes 1 0 1 0 10 10 13 15 16 EGADS : 15 Yes 1 0 1 0 10 11 13 14 16 EGADS : 16 Yes 1 0 1 0 10 13 14 15 EGADS : 17 Yes 2 0 1 NA NA 18 EGADS : 18 Yes 2 0 1 NA NA 17 EGADS : Face Edges Information EGADS : Face Edges EGADS : 1 1 4 -3 -2 EGADS : 2 3 7 -6 -5 EGADS : 3 6 9 -1 -8 EGADS : 4 -4 -9 -7 EGADS : 5 -10 2 11 -12 EGADS : 6 -11 5 13 -14 EGADS : 7 -13 8 10 -15 EGADS : 8 12 14 15 EGADS : 9 16 19 -18 -17 EGADS : 10 18 22 -21 -20 EGADS : 11 21 24 -16 -23 EGADS : 12 -19 -24 -22 EGADS : 13 -25 17 26 -27 EGADS : 14 -26 20 28 -29 EGADS : 15 -28 23 25 -30 EGADS : 16 27 29 30 EGADS : 17 -31 -32 33 34 EGADS : 18 -35 -34 36 32 EGADS : Face Loops Information EGADS : Face Loops EGADS : 1 1 EGADS : 2 2 EGADS : 3 3 EGADS : 4 4 EGADS : 5 5 EGADS : 6 6 EGADS : 7 7 EGADS : 8 8 EGADS : 9 9 EGADS : 10 10 EGADS : 11 11 EGADS : 12 12 EGADS : 13 13 EGADS : 14 14 EGADS : 15 15 EGADS : 16 16 EGADS : 17 17 EGADS : 18 18 EGADS : Loop Edges Information EGADS : Loop Active Edges EGADS : 1 Yes 1 4 -3 -2 EGADS : 2 Yes 3 7 -6 -5 EGADS : 3 Yes 6 9 -1 -8 EGADS : 4 Yes -4 -9 -7 EGADS : 5 Yes -10 2 11 -12 EGADS : 6 Yes -11 5 13 -14 EGADS : 7 Yes -13 8 10 -15 EGADS : 8 Yes 12 14 15 EGADS : 9 Yes 16 19 -18 -17 EGADS : 10 Yes 18 22 -21 -20 EGADS : 11 Yes 21 24 -16 -23 EGADS : 12 Yes -19 -24 -22 EGADS : 13 Yes -25 17 26 -27 EGADS : 14 Yes -26 20 28 -29 EGADS : 15 Yes -28 23 25 -30 EGADS : 16 Yes 27 29 30 EGADS : 17 Yes -31 -32 33 34 EGADS : 18 Yes -35 -34 36 32 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 1 2 1 1 3 EGADS : 2 0 Yes 1 3 1 1 5 EGADS : 3 0 Yes 3 4 1 1 2 EGADS : 4 0 Yes 2 4 1 1 4 EGADS : 5 0 Yes 3 5 1 2 6 EGADS : 6 0 Yes 5 6 1 2 3 EGADS : 7 0 Yes 4 6 1 2 4 EGADS : 8 0 Yes 5 1 1 3 7 EGADS : 9 0 Yes 6 2 1 3 4 EGADS : 10 0 Yes 1 7 1 5 7 EGADS : 11 0 Yes 3 8 1 5 6 EGADS : 12 0 Yes 7 8 1 5 8 EGADS : 13 0 Yes 5 9 1 6 7 EGADS : 14 0 Yes 8 9 1 6 8 EGADS : 15 0 Yes 9 7 1 7 8 EGADS : 16 1 Yes 10 11 1 9 11 EGADS : 17 1 Yes 10 12 1 9 13 EGADS : 18 1 Yes 12 13 1 9 10 EGADS : 19 1 Yes 11 13 1 9 12 EGADS : 20 1 Yes 12 14 1 10 14 EGADS : 21 1 Yes 14 15 1 10 11 EGADS : 22 1 Yes 13 15 1 10 12 EGADS : 23 1 Yes 14 10 1 11 15 EGADS : 24 1 Yes 15 11 1 11 12 EGADS : 25 1 Yes 10 16 1 13 15 EGADS : 26 1 Yes 12 17 1 13 14 EGADS : 27 1 Yes 16 17 1 13 16 EGADS : 28 1 Yes 14 18 1 14 15 EGADS : 29 1 Yes 17 18 1 14 16 EGADS : 30 1 Yes 18 16 1 15 16 EGADS : 31 2 DEGEN 19 19 - 17 EGADS : 32 2 Yes 20 19 NA 17 18 EGADS : 33 2 DEGEN 20 20 - 17 EGADS : 34 2 Yes 20 19 NA 17 18 EGADS : 35 2 DEGEN 19 19 - 18 EGADS : 36 2 DEGEN 20 20 - 18 EGADS : Node Information EGADS : Node Active Coordinates EGADS : 1 Yes 3.77246052 0 0.00459131419 EGADS : 2 Yes 5.90487498 7.07106781 0 EGADS : 3 Yes 0 0 0 EGADS : 4 Yes 4.0824829 7.07106781 0.123425948 EGADS : 5 Yes 3.77001182 0 0 EGADS : 6 Yes 5.90282524 7.07106781 0 EGADS : 7 Yes 5.90487498 0 0 EGADS : 8 Yes 4.0824829 0 0.123425948 EGADS : 9 Yes 5.90282524 0 0 EGADS : 10 Yes 11.5089842 0 0.00183652568 EGADS : 11 Yes 12.36195 2.82842712 0 EGADS : 12 Yes 10 0 0 EGADS : 13 Yes 11.6329932 2.82842712 0.0493703791 EGADS : 14 Yes 11.5080047 0 0 EGADS : 15 Yes 12.3611301 2.82842712 0 EGADS : 16 Yes 12.36195 0 0 EGADS : 17 Yes 11.6329932 0 0.0493703791 EGADS : 18 Yes 12.3611301 0 0 EGADS : 19 Yes 0 0 80 EGADS : 20 Yes 0 0 0 EGADS : Face and Edge Match Information EGADS : No Face Matches Found AFLR4 : Surface Mesh Spacing Setup AFLR4 : Max Bounding Box Length = 160 AFLR4 : Min Bounding Box Length = 160 AFLR4 : Max Ref Bounding Box Length = 14.1421 AFLR4 : Min Ref Bounding Box Length = 0.890888 AFLR4 : Reference Length = 2.82843 AFLR4 : BL Thickness = 0 AFLR4 : FarField Spacing = 15.6197 AFLR4 : Abs Min Surf Spacing = 0.00707107 AFLR4 : Min Surf Spacing = 0.0141421 AFLR4 : Max Surf Spacing = 0.282843 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 : 10 CAD geometry 0 STD w/BL AFLR4 : 11 CAD geometry 0 STD w/BL AFLR4 : 12 CAD geometry 0 STD w/BL AFLR4 : 13 CAD geometry 0 STD w/BL AFLR4 : 14 CAD geometry 0 STD w/BL AFLR4 : 15 CAD geometry 0 STD w/BL AFLR4 : 16 CAD geometry 0 STD w/BL AFLR4 : 17 CAD geometry 0 FARFIELD AFLR4 : 18 CAD geometry 0 FARFIELD AFLR4 : Case has 2 Proximity Checking Components AFLR4 : Component 1 includes Definitions 1 2 3 4 5 6 7 8 AFLR4 : Component 2 includes Definitions 9 10 11 12 13 14 15 16 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 : Define CAD surface definition 10 AFLR4 : Define CAD surface definition 11 AFLR4 : Define CAD surface definition 12 AFLR4 : Define CAD surface definition 13 AFLR4 : Define CAD surface definition 14 AFLR4 : Define CAD surface definition 15 AFLR4 : Define CAD surface definition 16 AFLR4 : Define CAD surface definition 17 AFLR4 : Define CAD surface definition 18 AFLR4 : Surface Grid Generation AFLR4 : Generate optimal mesh on surface definition 1 AFLR2 : Nodes, Trias,Quads= 17154 33578 0 AFLR4 : Nodes, Trias,Quads= 7368 14006 0 AFLR4 : Generate optimal mesh on surface definition 2 AFLR2 : Nodes, Trias,Quads= 14793 28857 0 AFLR4 : Nodes, Trias,Quads= 6844 12959 0 AFLR4 : Generate optimal mesh on surface definition 3 AFLR2 : Nodes, Trias,Quads= 182 241 0 AFLR4 : Nodes, Trias,Quads= 122 121 0 AFLR4 : Generate optimal mesh on surface definition 4 AFLR2 : Nodes, Trias,Quads= 328 542 0 AFLR4 : Nodes, Trias,Quads= 324 534 0 AFLR4 : Generate optimal mesh on surface definition 5 AFLR2 : Nodes, Trias,Quads= 17058 33386 0 AFLR4 : Nodes, Trias,Quads= 7507 14284 0 AFLR4 : Generate optimal mesh on surface definition 6 AFLR2 : Nodes, Trias,Quads= 14987 29245 0 AFLR4 : Nodes, Trias,Quads= 6879 13029 0 AFLR4 : Generate optimal mesh on surface definition 7 AFLR2 : Nodes, Trias,Quads= 182 241 0 AFLR4 : Nodes, Trias,Quads= 122 121 0 AFLR4 : Generate optimal mesh on surface definition 8 AFLR2 : Nodes, Trias,Quads= 330 546 0 AFLR4 : Nodes, Trias,Quads= 322 530 0 AFLR4 : Generate optimal mesh on surface definition 9 AFLR2 : Nodes, Trias,Quads= 740 1354 0 AFLR4 : Nodes, Trias,Quads= 602 1078 0 AFLR4 : Generate optimal mesh on surface definition 10 AFLR2 : Nodes, Trias,Quads= 757 1388 0 AFLR4 : Nodes, Trias,Quads= 591 1056 0 AFLR4 : Generate optimal mesh on surface definition 11 AFLR2 : Nodes, Trias,Quads= 180 251 0 AFLR4 : Nodes, Trias,Quads= 108 107 0 AFLR4 : Generate optimal mesh on surface definition 12 AFLR2 : Nodes, Trias,Quads= 182 282 0 AFLR4 : Nodes, Trias,Quads= 181 280 0 AFLR4 : Generate optimal mesh on surface definition 13 AFLR2 : Nodes, Trias,Quads= 737 1348 0 AFLR4 : Nodes, Trias,Quads= 602 1078 0 AFLR4 : Generate optimal mesh on surface definition 14 AFLR2 : Nodes, Trias,Quads= 755 1384 0 AFLR4 : Nodes, Trias,Quads= 596 1066 0 AFLR4 : Generate optimal mesh on surface definition 15 AFLR2 : Nodes, Trias,Quads= 180 251 0 AFLR4 : Nodes, Trias,Quads= 108 107 0 AFLR4 : Generate optimal mesh on surface definition 16 AFLR2 : Nodes, Trias,Quads= 182 282 0 AFLR4 : Nodes, Trias,Quads= 181 280 0 AFLR4 : Generate optimal mesh on surface definition 17 AFLR2 : Nodes, Trias,Quads= 92 150 0 AFLR4 : Nodes, Trias,Quads= 215 396 0 AFLR4 : Generate optimal mesh on surface definition 18 AFLR2 : Nodes, Trias,Quads= 92 150 0 AFLR4 : Nodes, Trias,Quads= 210 386 0 DGEOM : Add surface definitions to composite definition 0 DGEOM : Glue composite surface definition 0 DGEOM : Nodes,Faces,BEdges= 30715 61418 4310 AFLR4 : Curvature BG Surface Grid Generation AFLR4 : Nodes, Faces = 30715 61418 AFLR4 : Surface Grid Generation AFLR4 : Generate optimal mesh on surface definition 1 AFLR2 : Nodes, Trias,Quads= 24469 47607 0 AFLR4 : Nodes, Trias,Quads= 14850 28369 0 AFLR4 : Generate optimal mesh on surface definition 2 AFLR2 : Nodes, Trias,Quads= 25078 48855 0 AFLR4 : Nodes, Trias,Quads= 14477 27653 0 AFLR4 : Generate optimal mesh on surface definition 3 AFLR2 : Nodes, Trias,Quads= 1589 2117 0 AFLR4 : Nodes, Trias,Quads= 1059 1057 0 AFLR4 : Generate optimal mesh on surface definition 4 AFLR2 : Nodes, Trias,Quads= 2646 5000 0 AFLR4 : Nodes, Trias,Quads= 1543 2794 0 AFLR4 : Generate optimal mesh on surface definition 5 AFLR2 : Nodes, Trias,Quads= 25468 49604 0 AFLR4 : Nodes, Trias,Quads= 14818 28304 0 AFLR4 : Generate optimal mesh on surface definition 6 AFLR2 : Nodes, Trias,Quads= 24060 46818 0 AFLR4 : Nodes, Trias,Quads= 14427 27552 0 AFLR4 : Generate optimal mesh on surface definition 7 AFLR2 : Nodes, Trias,Quads= 1589 2117 0 AFLR4 : Nodes, Trias,Quads= 1059 1057 0 AFLR4 : Generate optimal mesh on surface definition 8 AFLR2 : Nodes, Trias,Quads= 2642 4992 0 AFLR4 : Nodes, Trias,Quads= 1532 2772 0 AFLR4 : Generate optimal mesh on surface definition 9 AFLR2 : Nodes, Trias,Quads= 863 1589 0 AFLR4 : Nodes, Trias,Quads= 712 1287 0 AFLR4 : Generate optimal mesh on surface definition 10 AFLR2 : Nodes, Trias,Quads= 864 1593 0 AFLR4 : Nodes, Trias,Quads= 696 1257 0 AFLR4 : Generate optimal mesh on surface definition 11 AFLR2 : Nodes, Trias,Quads= 218 316 0 AFLR4 : Nodes, Trias,Quads= 118 116 0 AFLR4 : Generate optimal mesh on surface definition 12 AFLR2 : Nodes, Trias,Quads= 188 294 0 AFLR4 : Nodes, Trias,Quads= 183 284 0 AFLR4 : Generate optimal mesh on surface definition 13 AFLR2 : Nodes, Trias,Quads= 861 1585 0 AFLR4 : Nodes, Trias,Quads= 713 1289 0 AFLR4 : Generate optimal mesh on surface definition 14 AFLR2 : Nodes, Trias,Quads= 868 1601 0 AFLR4 : Nodes, Trias,Quads= 693 1251 0 AFLR4 : Generate optimal mesh on surface definition 15 AFLR2 : Nodes, Trias,Quads= 218 316 0 AFLR4 : Nodes, Trias,Quads= 118 116 0 AFLR4 : Generate optimal mesh on surface definition 16 AFLR2 : Nodes, Trias,Quads= 186 290 0 AFLR4 : Nodes, Trias,Quads= 183 284 0 AFLR4 : Generate optimal mesh on surface definition 17 AFLR2 : Nodes, Trias,Quads= 82 132 0 AFLR4 : Nodes, Trias,Quads= 208 384 0 AFLR4 : Generate optimal mesh on surface definition 18 AFLR2 : Nodes, Trias,Quads= 80 128 0 AFLR4 : Nodes, Trias,Quads= 205 378 0 DGEOM : Add surface definitions to composite definition 0 DGEOM : Glue composite surface definition 0 DGEOM : Nodes,Faces,BEdges= 63108 126204 8948 AFLR4 : Proximity BG Surface Grid Generation AFLR4 : Proximity BG Surface Grid Generation Skipped AFLR4 : No Modifications Required OVERALL : CPU Time = 3.360 seconds Body 1 (of 3) Number of nodes = 59781 Number of elements = 119558 Number of triangle elements = 119558 Number of quadrilateral elements = 0 Body 2 (of 3) Number of nodes = 2944 Number of elements = 5884 Number of triangle elements = 5884 Number of quadrilateral elements = 0 Body 3 (of 3) Number of nodes = 383 Number of elements = 762 Number of triangle elements = 762 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 63108 Total number of elements = 126204 .Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 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 x86_64 AFLR2 : Compile Date 04/23/24 @ 11:49AM 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 x86_64 AFLR4 : Compile Date 04/23/24 @ 11:49AM AFLR4 : Copyright 1994-2021, D.L. Marcum AFLR4 : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : EGADS CAD Geometry Setup EGADS : Model has 1 Active Bodies EGADS : Body 0 is a SolidBody EGADS : Body 0 has 2 Shells EGADS : Body 0 has 14 Faces EGADS : Body 0 has 27 Edges EGADS : Body 0 has 14 Loops EGADS : Body 0 has 17 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 NA NA 2 3 4 5 EGADS : 2 Yes 0 0 1 NA NA 1 3 5 6 EGADS : 3 Yes 0 0 1 NA NA 1 2 4 6 EGADS : 4 Yes 0 0 1 NA NA 1 3 5 6 EGADS : 5 Yes 0 0 1 NA NA 1 2 4 6 EGADS : 6 Yes 0 0 1 NA NA 2 3 4 5 EGADS : 7 Yes 0 0 1 0 1 8 9 10 11 EGADS : 8 Yes 0 0 1 0 1 7 10 11 12 EGADS : 9 Yes 0 0 1 0 1 7 12 13 14 EGADS : 10 Yes 0 0 1 0 1 7 8 11 13 EGADS : 11 Yes 0 0 1 0 1 7 8 10 EGADS : 12 Yes 0 0 1 0 1 8 9 13 14 EGADS : 13 Yes 0 0 1 0 1 9 10 12 14 EGADS : 14 Yes 0 0 1 0 1 9 12 13 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 EGADS : 4 -10 3 8 -11 EGADS : 5 4 10 -12 -5 EGADS : 6 -6 12 11 -9 EGADS : 7 -13 14 15 -16 EGADS : 8 -17 18 13 -19 EGADS : 9 20 22 -21 -14 EGADS : 10 -15 23 17 -24 EGADS : 11 16 24 19 EGADS : 12 25 26 -20 -18 EGADS : 13 21 27 -25 -23 EGADS : 14 -22 -26 -27 EGADS : Face Loops Information EGADS : Face Loops EGADS : 1 1 EGADS : 2 2 EGADS : 3 3 EGADS : 4 4 EGADS : 5 5 EGADS : 6 6 EGADS : 7 7 EGADS : 8 8 EGADS : 9 9 EGADS : 10 10 EGADS : 11 11 EGADS : 12 12 EGADS : 13 13 EGADS : 14 14 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 3 8 -11 EGADS : 5 Yes 4 10 -12 -5 EGADS : 6 Yes -6 12 11 -9 EGADS : 7 Yes -13 14 15 -16 EGADS : 8 Yes -17 18 13 -19 EGADS : 9 Yes 20 22 -21 -14 EGADS : 10 Yes -15 23 17 -24 EGADS : 11 Yes 16 24 19 EGADS : 12 Yes 25 26 -20 -18 EGADS : 13 Yes 21 27 -25 -23 EGADS : 14 Yes -22 -26 -27 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 NA 1 2 EGADS : 2 0 Yes 1 3 NA 1 3 EGADS : 3 0 Yes 4 3 NA 1 4 EGADS : 4 0 Yes 2 4 NA 1 5 EGADS : 5 0 Yes 2 5 NA 2 5 EGADS : 6 0 Yes 5 6 NA 2 6 EGADS : 7 0 Yes 1 6 NA 2 3 EGADS : 8 0 Yes 3 7 NA 3 4 EGADS : 9 0 Yes 6 7 NA 3 6 EGADS : 10 0 Yes 4 8 NA 4 5 EGADS : 11 0 Yes 8 7 NA 4 6 EGADS : 12 0 Yes 5 8 NA 5 6 EGADS : 13 0 Yes 9 10 1 7 8 EGADS : 14 0 Yes 9 11 1 7 9 EGADS : 15 0 Yes 11 12 1 7 10 EGADS : 16 0 Yes 10 12 1 7 11 EGADS : 17 0 Yes 13 14 1 8 10 EGADS : 18 0 Yes 13 9 1 8 12 EGADS : 19 0 Yes 14 10 1 8 11 EGADS : 20 0 Yes 9 15 1 9 12 EGADS : 21 0 Yes 11 16 1 9 13 EGADS : 22 0 Yes 15 16 1 9 14 EGADS : 23 0 Yes 11 13 1 10 13 EGADS : 24 0 Yes 12 14 1 10 11 EGADS : 25 0 Yes 13 17 1 12 13 EGADS : 26 0 Yes 17 15 1 12 14 EGADS : 27 0 Yes 16 17 1 13 14 EGADS : Node Information EGADS : Node Active Coordinates EGADS : 1 Yes 0 0 40 EGADS : 2 Yes 0 0 0 EGADS : 3 Yes 0 40 40 EGADS : 4 Yes 0 40 0 EGADS : 5 Yes 40 0 0 EGADS : 6 Yes 40 0 40 EGADS : 7 Yes 40 40 40 EGADS : 8 Yes 40 40 0 EGADS : 9 Yes 3.77246052 0 0.00459131419 EGADS : 10 Yes 5.90487498 7.07106781 0 EGADS : 11 Yes 0 0 0 EGADS : 12 Yes 4.0824829 7.07106781 0.123425948 EGADS : 13 Yes 3.77001182 0 0 EGADS : 14 Yes 5.90282524 7.07106781 0 EGADS : 15 Yes 5.90487498 0 0 EGADS : 16 Yes 4.0824829 0 0.123425948 EGADS : 17 Yes 5.90282524 0 0 EGADS : Face and Edge Match Information EGADS : No Face Matches Found AFLR4 : Surface Mesh Spacing Setup AFLR4 : Max Bounding Box Length = 80 AFLR4 : Min Bounding Box Length = 80 AFLR4 : Max Ref Bounding Box Length = 14.1421 AFLR4 : Min Ref Bounding Box Length = 0.890888 AFLR4 : Reference Length = 2.82843 AFLR4 : BL Thickness = 0 AFLR4 : FarField Spacing = 7.60986 AFLR4 : Abs Min Surf Spacing = 0.00707107 AFLR4 : Min Surf Spacing = 0.0141421 AFLR4 : Max Surf Spacing = 0.282843 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 FARFIELD AFLR4 : 2 CAD geometry 0 FARFIELD AFLR4 : 3 CAD geometry 0 FARFIELD AFLR4 : 4 CAD geometry 0 FARFIELD AFLR4 : 5 CAD geometry 0 FARFIELD AFLR4 : 6 CAD geometry 0 FARFIELD 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 : 10 CAD geometry 0 STD w/BL AFLR4 : 11 CAD geometry 0 STD w/BL AFLR4 : 12 CAD geometry 0 STD w/BL AFLR4 : 13 CAD geometry 0 STD w/BL AFLR4 : 14 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 : Define CAD surface definition 10 AFLR4 : Define CAD surface definition 11 AFLR4 : Define CAD surface definition 12 AFLR4 : Define CAD surface definition 13 AFLR4 : Define CAD surface definition 14 AFLR4 : Surface Grid Generation AFLR4 : Generate optimal mesh on surface definition 1 AFLR2 : Nodes, Trias,Quads= 136 230 0 AFLR4 : Nodes, Trias,Quads= 132 222 0 AFLR4 : Generate optimal mesh on surface definition 2 AFLR2 : Nodes, Trias,Quads= 136 230 0 AFLR4 : Nodes, Trias,Quads= 132 222 0 AFLR4 : Generate optimal mesh on surface definition 3 AFLR2 : Nodes, Trias,Quads= 136 230 0 AFLR4 : Nodes, Trias,Quads= 132 222 0 AFLR4 : Generate optimal mesh on surface definition 4 AFLR2 : Nodes, Trias,Quads= 136 230 0 AFLR4 : Nodes, Trias,Quads= 132 222 0 AFLR4 : Generate optimal mesh on surface definition 5 AFLR2 : Nodes, Trias,Quads= 136 230 0 AFLR4 : Nodes, Trias,Quads= 132 222 0 AFLR4 : Generate optimal mesh on surface definition 6 AFLR2 : Nodes, Trias,Quads= 136 230 0 AFLR4 : Nodes, Trias,Quads= 132 222 0 AFLR4 : Generate optimal mesh on surface definition 7 AFLR2 : Nodes, Trias,Quads= 17058 33386 0 AFLR4 : Nodes, Trias,Quads= 7507 14284 0 AFLR4 : Generate optimal mesh on surface definition 8 AFLR2 : Nodes, Trias,Quads= 182 241 0 AFLR4 : Nodes, Trias,Quads= 122 121 0 AFLR4 : Generate optimal mesh on surface definition 9 AFLR2 : Nodes, Trias,Quads= 17154 33578 0 AFLR4 : Nodes, Trias,Quads= 7368 14006 0 AFLR4 : Generate optimal mesh on surface definition 10 AFLR2 : Nodes, Trias,Quads= 14987 29245 0 AFLR4 : Nodes, Trias,Quads= 6879 13029 0 AFLR4 : Generate optimal mesh on surface definition 11 AFLR2 : Nodes, Trias,Quads= 330 546 0 AFLR4 : Nodes, Trias,Quads= 322 530 0 AFLR4 : Generate optimal mesh on surface definition 12 AFLR2 : Nodes, Trias,Quads= 182 241 0 AFLR4 : Nodes, Trias,Quads= 122 121 0 AFLR4 : Generate optimal mesh on surface definition 13 AFLR2 : Nodes, Trias,Quads= 14793 28857 0 AFLR4 : Nodes, Trias,Quads= 6844 12959 0 AFLR4 : Generate optimal mesh on surface definition 14 AFLR2 : Nodes, Trias,Quads= 328 542 0 AFLR4 : Nodes, Trias,Quads= 324 534 0 DGEOM : Add surface definitions to composite definition 0 DGEOM : Glue composite surface definition 0 DGEOM : Nodes,Faces,BEdges= 28462 56916 3616 AFLR4 : Curvature BG Surface Grid Generation AFLR4 : Nodes, Faces = 28462 56916 AFLR4 : Surface Grid Generation AFLR4 : Generate optimal mesh on surface definition 1 AFLR2 : Nodes, Trias,Quads= 136 230 0 AFLR4 : Nodes, Trias,Quads= 132 222 0 AFLR4 : Generate optimal mesh on surface definition 2 AFLR2 : Nodes, Trias,Quads= 137 232 0 AFLR4 : Nodes, Trias,Quads= 132 222 0 AFLR4 : Generate optimal mesh on surface definition 3 AFLR2 : Nodes, Trias,Quads= 137 232 0 AFLR4 : Nodes, Trias,Quads= 132 222 0 AFLR4 : Generate optimal mesh on surface definition 4 AFLR2 : Nodes, Trias,Quads= 136 230 0 AFLR4 : Nodes, Trias,Quads= 132 222 0 AFLR4 : Generate optimal mesh on surface definition 5 AFLR2 : Nodes, Trias,Quads= 137 232 0 AFLR4 : Nodes, Trias,Quads= 132 222 0 AFLR4 : Generate optimal mesh on surface definition 6 AFLR2 : Nodes, Trias,Quads= 137 232 0 AFLR4 : Nodes, Trias,Quads= 132 222 0 AFLR4 : Generate optimal mesh on surface definition 7 AFLR2 : Nodes, Trias,Quads= 15590 30449 0 AFLR4 : Nodes, Trias,Quads= 9447 18163 0 AFLR4 : Generate optimal mesh on surface definition 8 AFLR2 : Nodes, Trias,Quads= 254 370 0 AFLR4 : Nodes, Trias,Quads= 136 134 0 AFLR4 : Generate optimal mesh on surface definition 9 AFLR2 : Nodes, Trias,Quads= 15870 31009 0 AFLR4 : Nodes, Trias,Quads= 9439 18147 0 AFLR4 : Generate optimal mesh on surface definition 10 AFLR2 : Nodes, Trias,Quads= 14689 28649 0 AFLR4 : Nodes, Trias,Quads= 9247 17765 0 AFLR4 : Generate optimal mesh on surface definition 11 AFLR2 : Nodes, Trias,Quads= 346 577 0 AFLR4 : Nodes, Trias,Quads= 359 603 0 AFLR4 : Generate optimal mesh on surface definition 12 AFLR2 : Nodes, Trias,Quads= 254 370 0 AFLR4 : Nodes, Trias,Quads= 136 134 0 AFLR4 : Generate optimal mesh on surface definition 13 AFLR2 : Nodes, Trias,Quads= 14582 28435 0 AFLR4 : Nodes, Trias,Quads= 9309 17889 0 AFLR4 : Generate optimal mesh on surface definition 14 AFLR2 : Nodes, Trias,Quads= 348 581 0 AFLR4 : Nodes, Trias,Quads= 361 607 0 DGEOM : Add surface definitions to composite definition 0 DGEOM : Glue composite surface definition 0 DGEOM : Nodes,Faces,BEdges= 37391 74774 3650 OVERALL : CPU Time = 1.684 seconds Body 1 (of 1) Number of nodes = 37391 Number of elements = 74774 Number of triangle elements = 74774 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 37391 Total number of elements = 74774 .ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62031) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 6 Name = box, index = 1 Name = cylinder, index = 2 Name = cone, index = 3 Name = torus, index = 4 Name = sphere, index = 5 Name = farfield, index = 6 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 x86_64 AFLR2 : Compile Date 04/23/24 @ 11:49AM 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 x86_64 AFLR4 : Compile Date 04/23/24 @ 11:49AM AFLR4 : Copyright 1994-2021, D.L. Marcum AFLR4 : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : EGADS CAD Geometry Setup EGADS : Model has 6 Active Bodies EGADS : Body 0 is a SolidBody EGADS : Body 0 has 1 Shells EGADS : Body 0 has 6 Faces EGADS : Body 0 has 12 Edges EGADS : Body 0 has 6 Loops EGADS : Body 0 has 8 Nodes EGADS : Body 1 is a SolidBody EGADS : Body 1 has 1 Shells EGADS : Body 1 has 3 Faces EGADS : Body 1 has 3 Edges EGADS : Body 1 has 3 Loops EGADS : Body 1 has 2 Nodes EGADS : Body 2 is a SolidBody EGADS : Body 2 has 1 Shells EGADS : Body 2 has 3 Faces EGADS : Body 2 has 6 Edges EGADS : Body 2 has 3 Loops EGADS : Body 2 has 3 Nodes EGADS : Body 3 is a SolidBody EGADS : Body 3 has 1 Shells EGADS : Body 3 has 1 Faces EGADS : Body 3 has 2 Edges EGADS : Body 3 has 1 Loops EGADS : Body 3 has 1 Nodes EGADS : Body 4 is a SolidBody EGADS : Body 4 has 1 Shells EGADS : Body 4 has 2 Faces EGADS : Body 4 has 6 Edges EGADS : Body 4 has 2 Loops EGADS : Body 4 has 2 Nodes EGADS : Body 5 is a SolidBody EGADS : Body 5 has 1 Shells EGADS : Body 5 has 6 Faces EGADS : Body 5 has 12 Edges EGADS : Body 5 has 6 Loops EGADS : Body 5 has 8 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 3 4 5 6 EGADS : 2 Yes 0 0 1 0 1 3 4 5 6 EGADS : 3 Yes 0 0 1 0 1 1 2 5 6 EGADS : 4 Yes 0 0 1 0 1 1 2 5 6 EGADS : 5 Yes 0 0 1 0 1 1 2 3 4 EGADS : 6 Yes 0 0 1 0 1 1 2 3 4 EGADS : 7 Yes 1 0 1 0 1 8 EGADS : 8 Yes 1 0 1 0 1 7 9 EGADS : 9 Yes 1 0 1 0 1 8 EGADS : 10 Yes 2 0 1 0 1 11 12 EGADS : 11 Yes 2 0 1 0 1 10 12 EGADS : 12 Yes 2 0 1 0 1 10 11 EGADS : 13 Yes 3 0 1 0 1 EGADS : 14 Yes 4 0 1 0 1 15 EGADS : 15 Yes 4 0 1 0 1 14 EGADS : 16 Yes 5 0 1 NA NA 18 19 20 21 EGADS : 17 Yes 5 0 1 NA NA 18 19 20 21 EGADS : 18 Yes 5 0 1 NA NA 16 17 20 21 EGADS : 19 Yes 5 0 1 NA NA 16 17 20 21 EGADS : 20 Yes 5 0 1 NA NA 16 17 18 19 EGADS : 21 Yes 5 0 1 NA NA 16 17 18 19 EGADS : Face Edges Information EGADS : Face Edges EGADS : 1 1 2 -3 -4 EGADS : 2 -5 8 7 -6 EGADS : 3 9 5 -10 -1 EGADS : 4 -11 3 12 -7 EGADS : 5 4 11 -8 -9 EGADS : 6 -2 10 6 -12 EGADS : 7 -13 EGADS : 8 13 15 -14 -15 EGADS : 9 14 EGADS : 10 -16 -17 18 19 EGADS : 11 20 17 -21 -19 EGADS : 12 16 21 EGADS : 13 -22 23 22 -23 EGADS : 14 -24 -25 26 27 EGADS : 15 -28 -27 29 25 EGADS : 16 30 31 -32 -33 EGADS : 17 -34 37 36 -35 EGADS : 18 38 34 -39 -30 EGADS : 19 -40 32 41 -36 EGADS : 20 33 40 -37 -38 EGADS : 21 -31 39 35 -41 EGADS : Face Loops Information EGADS : Face Loops EGADS : 1 1 EGADS : 2 2 EGADS : 3 3 EGADS : 4 4 EGADS : 5 5 EGADS : 6 6 EGADS : 7 7 EGADS : 8 8 EGADS : 9 9 EGADS : 10 10 EGADS : 11 11 EGADS : 12 12 EGADS : 13 13 EGADS : 14 14 EGADS : 15 15 EGADS : 16 16 EGADS : 17 17 EGADS : 18 18 EGADS : 19 19 EGADS : 20 20 EGADS : 21 21 EGADS : Loop Edges Information EGADS : Loop Active Edges EGADS : 1 Yes 1 2 -3 -4 EGADS : 2 Yes -5 8 7 -6 EGADS : 3 Yes 9 5 -10 -1 EGADS : 4 Yes -11 3 12 -7 EGADS : 5 Yes 4 11 -8 -9 EGADS : 6 Yes -2 10 6 -12 EGADS : 7 Yes -13 EGADS : 8 Yes 13 15 -14 -15 EGADS : 9 Yes 14 EGADS : 10 Yes -16 -17 18 19 EGADS : 11 Yes 20 17 -21 -19 EGADS : 12 Yes 16 21 EGADS : 13 Yes -22 23 22 -23 EGADS : 14 Yes -24 -25 26 27 EGADS : 15 Yes -28 -27 29 25 EGADS : 16 Yes 30 31 -32 -33 EGADS : 17 Yes -34 37 36 -35 EGADS : 18 Yes 38 34 -39 -30 EGADS : 19 Yes -40 32 41 -36 EGADS : 20 Yes 33 40 -37 -38 EGADS : 21 Yes -31 39 35 -41 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 3 EGADS : 2 0 Yes 1 3 1 1 6 EGADS : 3 0 Yes 4 3 1 1 4 EGADS : 4 0 Yes 2 4 1 1 5 EGADS : 5 0 Yes 6 5 1 2 3 EGADS : 6 0 Yes 5 7 1 2 6 EGADS : 7 0 Yes 8 7 1 2 4 EGADS : 8 0 Yes 6 8 1 2 5 EGADS : 9 0 Yes 2 6 1 3 5 EGADS : 10 0 Yes 1 5 1 3 6 EGADS : 11 0 Yes 4 8 1 4 5 EGADS : 12 0 Yes 3 7 1 4 6 EGADS : 13 1 Yes 9 9 1 7 8 EGADS : 14 1 Yes 10 10 1 8 9 EGADS : 15 1 Yes 9 10 1 8 8 EGADS : 16 2 Yes 12 11 1 10 12 EGADS : 17 2 Yes 13 12 1 10 11 EGADS : 18 2 DEGEN 13 13 - 10 EGADS : 19 2 Yes 13 11 1 10 11 EGADS : 20 2 DEGEN 13 13 - 11 EGADS : 21 2 Yes 11 12 1 11 12 EGADS : 22 3 Yes 14 14 1 13 13 EGADS : 23 3 Yes 14 14 1 13 13 EGADS : 24 4 DEGEN 15 15 - 14 EGADS : 25 4 Yes 16 15 1 14 15 EGADS : 26 4 DEGEN 16 16 - 14 EGADS : 27 4 Yes 16 15 1 14 15 EGADS : 28 4 DEGEN 15 15 - 15 EGADS : 29 4 DEGEN 16 16 - 15 EGADS : 30 5 Yes 18 17 NA 16 18 EGADS : 31 5 Yes 17 19 NA 16 21 EGADS : 32 5 Yes 20 19 NA 16 19 EGADS : 33 5 Yes 18 20 NA 16 20 EGADS : 34 5 Yes 22 21 NA 17 18 EGADS : 35 5 Yes 21 23 NA 17 21 EGADS : 36 5 Yes 24 23 NA 17 19 EGADS : 37 5 Yes 22 24 NA 17 20 EGADS : 38 5 Yes 18 22 NA 18 20 EGADS : 39 5 Yes 17 21 NA 18 21 EGADS : 40 5 Yes 20 24 NA 19 20 EGADS : 41 5 Yes 19 23 NA 19 21 EGADS : Node Information EGADS : Node Active Coordinates EGADS : 1 Yes 0 0 0.5 EGADS : 2 Yes 0 0 0 EGADS : 3 Yes 0 0.5 0.5 EGADS : 4 Yes 0 0.5 0 EGADS : 5 Yes 1 0 0.5 EGADS : 6 Yes 1 0 0 EGADS : 7 Yes 1 0.5 0.5 EGADS : 8 Yes 1 0.5 0 EGADS : 9 Yes 2 0 0.5 EGADS : 10 Yes 3 0 0.5 EGADS : 11 Yes 5 0 0 EGADS : 12 Yes 5 0 0.5 EGADS : 13 Yes 4 0 0 EGADS : 14 Yes 7.25 0 0 EGADS : 15 Yes 8.5 0 0.5 EGADS : 16 Yes 8.5 0 0 EGADS : 17 Yes 0 0 2 EGADS : 18 Yes 0 0 0 EGADS : 19 Yes 0 2 2 EGADS : 20 Yes 0 2 0 EGADS : 21 Yes 14 0 2 EGADS : 22 Yes 14 0 0 EGADS : 23 Yes 14 2 2 EGADS : 24 Yes 14 2 0 EGADS : Face and Edge Match Information EGADS : No Face Matches Found AFLR4 : Surface Mesh Spacing Setup AFLR4 : Max Bounding Box Length = 15 AFLR4 : Min Bounding Box Length = 4 AFLR4 : Max Ref Bounding Box Length = 9 AFLR4 : Min Ref Bounding Box Length = 1 AFLR4 : Reference Length = 1 AFLR4 : BL Thickness = 0 AFLR4 : FarField Spacing = 0.5 AFLR4 : Abs Min Surf Spacing = 0.0025 AFLR4 : Min Surf Spacing = 0.1 AFLR4 : Max Surf Spacing = 0.5 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 : 10 CAD geometry 0 STD w/BL AFLR4 : 11 CAD geometry 0 STD w/BL AFLR4 : 12 CAD geometry 0 STD w/BL AFLR4 : 13 CAD geometry 0 STD w/BL AFLR4 : 14 CAD geometry 0 STD w/BL AFLR4 : 15 CAD geometry 0 STD w/BL AFLR4 : 16 CAD geometry 0 FARFIELD AFLR4 : 17 CAD geometry 0 FARFIELD AFLR4 : 18 CAD geometry 0 FARFIELD AFLR4 : 19 CAD geometry 0 FARFIELD AFLR4 : 20 CAD geometry 0 FARFIELD AFLR4 : 21 CAD geometry 0 FARFIELD AFLR4 : Case has 5 Proximity Checking Components AFLR4 : Component 1 includes Definitions 1 2 3 4 5 6 AFLR4 : Component 2 includes Definitions 7 8 9 AFLR4 : Component 3 includes Definitions 10 11 12 AFLR4 : Component 4 includes Definitions 13 AFLR4 : Component 5 includes Definitions 14 15 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 : Define CAD surface definition 10 AFLR4 : Define CAD surface definition 11 AFLR4 : Define CAD surface definition 12 AFLR4 : Define CAD surface definition 13 AFLR4 : Define CAD surface definition 14 AFLR4 : Define CAD surface definition 15 AFLR4 : Define CAD surface definition 16 AFLR4 : Define CAD surface definition 17 AFLR4 : Define CAD surface definition 18 AFLR4 : Define CAD surface definition 19 AFLR4 : Define CAD surface definition 20 AFLR4 : Define CAD surface definition 21 AFLR4 : Surface Grid Generation AFLR4 : Generate optimal mesh on surface definition 1 AFLR2 : Nodes, Trias,Quads= 12 14 0 AFLR4 : Nodes, Trias,Quads= 8 6 0 AFLR4 : Generate optimal mesh on surface definition 2 AFLR2 : Nodes, Trias,Quads= 12 14 0 AFLR4 : Nodes, Trias,Quads= 8 6 0 AFLR4 : Generate optimal mesh on surface definition 3 AFLR2 : Nodes, Trias,Quads= 12 14 0 AFLR4 : Nodes, Trias,Quads= 8 6 0 AFLR4 : Generate optimal mesh on surface definition 4 AFLR2 : Nodes, Trias,Quads= 12 14 0 AFLR4 : Nodes, Trias,Quads= 8 6 0 AFLR4 : Generate optimal mesh on surface definition 5 AFLR2 : Nodes, Trias,Quads= 12 14 0 AFLR4 : Nodes, Trias,Quads= 8 6 0 AFLR4 : Generate optimal mesh on surface definition 6 AFLR2 : Nodes, Trias,Quads= 12 14 0 AFLR4 : Nodes, Trias,Quads= 8 6 0 AFLR4 : Generate optimal mesh on surface definition 7 AFLR2 : Nodes, Trias,Quads= 103 173 0 AFLR4 : Nodes, Trias,Quads= 100 167 0 AFLR4 : Generate optimal mesh on surface definition 8 AFLR2 : Nodes, Trias,Quads= 388 692 0 AFLR4 : Nodes, Trias,Quads= 388 692 0 AFLR4 : Generate optimal mesh on surface definition 9 AFLR2 : Nodes, Trias,Quads= 105 177 0 AFLR4 : Nodes, Trias,Quads= 103 173 0 AFLR4 : Generate optimal mesh on surface definition 10 AFLR2 : Nodes, Trias,Quads= 104 168 0 AFLR4 : Nodes, Trias,Quads= 124 208 0 AFLR4 : Generate optimal mesh on surface definition 11 AFLR2 : Nodes, Trias,Quads= 104 168 0 AFLR4 : Nodes, Trias,Quads= 123 206 0 AFLR4 : Generate optimal mesh on surface definition 12 AFLR2 : Nodes, Trias,Quads= 112 190 0 AFLR4 : Nodes, Trias,Quads= 95 156 0 AFLR4 : Generate optimal mesh on surface definition 13 AFLR2 : Nodes, Trias,Quads= 919 1710 0 AFLR4 : Nodes, Trias,Quads= 675 1222 0 AFLR4 : Generate optimal mesh on surface definition 14 AFLR2 : Nodes, Trias,Quads= 94 154 0 AFLR4 : Nodes, Trias,Quads= 202 370 0 AFLR4 : Generate optimal mesh on surface definition 15 AFLR2 : Nodes, Trias,Quads= 94 154 0 AFLR4 : Nodes, Trias,Quads= 201 368 0 AFLR4 : Generate optimal mesh on surface definition 16 AFLR2 : Nodes, Trias,Quads= 92 150 0 AFLR4 : Nodes, Trias,Quads= 88 142 0 AFLR4 : Generate optimal mesh on surface definition 17 AFLR2 : Nodes, Trias,Quads= 92 150 0 AFLR4 : Nodes, Trias,Quads= 87 140 0 AFLR4 : Generate optimal mesh on surface definition 18 AFLR2 : Nodes, Trias,Quads= 312 546 0 AFLR4 : Nodes, Trias,Quads= 308 538 0 AFLR4 : Generate optimal mesh on surface definition 19 AFLR2 : Nodes, Trias,Quads= 312 546 0 AFLR4 : Nodes, Trias,Quads= 308 538 0 AFLR4 : Generate optimal mesh on surface definition 20 AFLR2 : Nodes, Trias,Quads= 311 544 0 AFLR4 : Nodes, Trias,Quads= 308 538 0 AFLR4 : Generate optimal mesh on surface definition 21 AFLR2 : Nodes, Trias,Quads= 311 544 0 AFLR4 : Nodes, Trias,Quads= 308 538 0 DGEOM : Add surface definitions to composite definition 0 DGEOM : Glue composite surface definition 0 DGEOM : Nodes,Faces,BEdges= 3026 6032 858 AFLR4 : Auto Mode Turned OFF OVERALL : CPU Time = 0.151 seconds Body 1 (of 6) Number of nodes = 20 Number of elements = 36 Number of triangle elements = 36 Number of quadrilateral elements = 0 Body 2 (of 6) Number of nodes = 518 Number of elements = 1032 Number of triangle elements = 1032 Number of quadrilateral elements = 0 Body 3 (of 6) Number of nodes = 287 Number of elements = 570 Number of triangle elements = 570 Number of quadrilateral elements = 0 Body 4 (of 6) Number of nodes = 611 Number of elements = 1222 Number of triangle elements = 1222 Number of quadrilateral elements = 0 Body 5 (of 6) Number of nodes = 371 Number of elements = 738 Number of triangle elements = 738 Number of quadrilateral elements = 0 Body 6 (of 6) Number of nodes = 1219 Number of elements = 2434 Number of triangle elements = 2434 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 3026 Total number of elements = 6032 . Analysis object with the name, aflr4AIM, has already been initilized An altName of aflr4AIM_1 will be used! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : EGADS CAD Geometry Setup EGADS : Model has 2 Active Bodies EGADS : Body 0 is a SolidBody EGADS : Body 0 has 1 Shells EGADS : Body 0 has 6 Faces EGADS : Body 0 has 12 Edges EGADS : Body 0 has 6 Loops EGADS : Body 0 has 8 Nodes EGADS : Body 1 is a SolidBody EGADS : Body 1 has 1 Shells EGADS : Body 1 has 6 Faces EGADS : Body 1 has 12 Edges EGADS : Body 1 has 6 Loops EGADS : Body 1 has 8 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 3 4 5 6 EGADS : 2 Yes 0 0 1 0 1 3 4 5 6 EGADS : 3 Yes 0 0 1 0 1 1 2 5 6 EGADS : 4 Yes 0 0 1 0 1 1 2 5 6 EGADS : 5 Yes 0 0 1 0 1 1 2 3 4 EGADS : 6 Yes 0 0 1 0 1 1 2 3 4 EGADS : 7 Yes 1 0 1 NA NA 9 10 11 12 EGADS : 8 Yes 1 0 1 NA NA 9 10 11 12 EGADS : 9 Yes 1 0 1 NA NA 7 8 11 12 EGADS : 10 Yes 1 0 1 NA NA 7 8 11 12 EGADS : 11 Yes 1 0 1 NA NA 7 8 9 10 EGADS : 12 Yes 1 0 1 NA NA 7 8 9 10 EGADS : Face Edges Information EGADS : Face Edges EGADS : 1 1 2 -3 -4 EGADS : 2 -5 8 7 -6 EGADS : 3 9 5 -10 -1 EGADS : 4 -11 3 12 -7 EGADS : 5 4 11 -8 -9 EGADS : 6 -2 10 6 -12 EGADS : 7 13 14 -15 -16 EGADS : 8 -17 20 19 -18 EGADS : 9 21 17 -22 -13 EGADS : 10 -23 15 24 -19 EGADS : 11 16 23 -20 -21 EGADS : 12 -14 22 18 -24 EGADS : Face Loops Information EGADS : Face Loops EGADS : 1 1 EGADS : 2 2 EGADS : 3 3 EGADS : 4 4 EGADS : 5 5 EGADS : 6 6 EGADS : 7 7 EGADS : 8 8 EGADS : 9 9 EGADS : 10 10 EGADS : 11 11 EGADS : 12 12 EGADS : Loop Edges Information EGADS : Loop Active Edges EGADS : 1 Yes 1 2 -3 -4 EGADS : 2 Yes -5 8 7 -6 EGADS : 3 Yes 9 5 -10 -1 EGADS : 4 Yes -11 3 12 -7 EGADS : 5 Yes 4 11 -8 -9 EGADS : 6 Yes -2 10 6 -12 EGADS : 7 Yes 13 14 -15 -16 EGADS : 8 Yes -17 20 19 -18 EGADS : 9 Yes 21 17 -22 -13 EGADS : 10 Yes -23 15 24 -19 EGADS : 11 Yes 16 23 -20 -21 EGADS : 12 Yes -14 22 18 -24 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 3 EGADS : 2 0 Yes 1 3 1 1 6 EGADS : 3 0 Yes 4 3 1 1 4 EGADS : 4 0 Yes 2 4 1 1 5 EGADS : 5 0 Yes 6 5 1 2 3 EGADS : 6 0 Yes 5 7 1 2 6 EGADS : 7 0 Yes 8 7 1 2 4 EGADS : 8 0 Yes 6 8 1 2 5 EGADS : 9 0 Yes 2 6 1 3 5 EGADS : 10 0 Yes 1 5 1 3 6 EGADS : 11 0 Yes 4 8 1 4 5 EGADS : 12 0 Yes 3 7 1 4 6 EGADS : 13 1 Yes 10 9 NA 7 9 EGADS : 14 1 Yes 9 11 NA 7 12 EGADS : 15 1 Yes 12 11 NA 7 10 EGADS : 16 1 Yes 10 12 NA 7 11 EGADS : 17 1 Yes 14 13 NA 8 9 EGADS : 18 1 Yes 13 15 NA 8 12 EGADS : 19 1 Yes 16 15 NA 8 10 EGADS : 20 1 Yes 14 16 NA 8 11 EGADS : 21 1 Yes 10 14 NA 9 11 EGADS : 22 1 Yes 9 13 NA 9 12 EGADS : 23 1 Yes 12 16 NA 10 11 EGADS : 24 1 Yes 11 15 NA 10 12 EGADS : Node Information EGADS : Node Active Coordinates EGADS : 1 Yes 0 0 0.5 EGADS : 2 Yes 0 0 0 EGADS : 3 Yes 0 0.5 0.5 EGADS : 4 Yes 0 0.5 0 EGADS : 5 Yes 1 0 0.5 EGADS : 6 Yes 1 0 0 EGADS : 7 Yes 1 0.5 0.5 EGADS : 8 Yes 1 0.5 0 EGADS : 9 Yes 0 0 2 EGADS : 10 Yes 0 0 0 EGADS : 11 Yes 0 2 2 EGADS : 12 Yes 0 2 0 EGADS : 13 Yes 14 0 2 EGADS : 14 Yes 14 0 0 EGADS : 15 Yes 14 2 2 EGADS : 16 Yes 14 2 0 EGADS : Face and Edge Match Information EGADS : No Face Matches Found AFLR4 : Surface Mesh Spacing Setup AFLR4 : Max Bounding Box Length = 15 AFLR4 : Min Bounding Box Length = 4 AFLR4 : Max Ref Bounding Box Length = 1 AFLR4 : Min Ref Bounding Box Length = 1 AFLR4 : Reference Length = 1 AFLR4 : BL Thickness = 0 AFLR4 : FarField Spacing = 0.5 AFLR4 : Abs Min Surf Spacing = 0.0025 AFLR4 : Min Surf Spacing = 0.1 AFLR4 : Max Surf Spacing = 0.5 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 FARFIELD AFLR4 : 8 CAD geometry 0 FARFIELD AFLR4 : 9 CAD geometry 0 FARFIELD AFLR4 : 10 CAD geometry 0 FARFIELD AFLR4 : 11 CAD geometry 0 FARFIELD AFLR4 : 12 CAD geometry 0 FARFIELD 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 : Define CAD surface definition 10 AFLR4 : Define CAD surface definition 11 AFLR4 : Define CAD surface definition 12 AFLR4 : Surface Grid Generation AFLR4 : Generate optimal mesh on surface definition 1 AFLR2 : Nodes, Trias,Quads= 12 14 0 AFLR4 : Nodes, Trias,Quads= 8 6 0 AFLR4 : Generate optimal mesh on surface definition 2 AFLR2 : Nodes, Trias,Quads= 12 14 0 AFLR4 : Nodes, Trias,Quads= 8 6 0 AFLR4 : Generate optimal mesh on surface definition 3 AFLR2 : Nodes, Trias,Quads= 12 14 0 AFLR4 : Nodes, Trias,Quads= 8 6 0 AFLR4 : Generate optimal mesh on surface definition 4 AFLR2 : Nodes, Trias,Quads= 12 14 0 AFLR4 : Nodes, Trias,Quads= 8 6 0 AFLR4 : Generate optimal mesh on surface definition 5 AFLR2 : Nodes, Trias,Quads= 12 14 0 AFLR4 : Nodes, Trias,Quads= 8 6 0 AFLR4 : Generate optimal mesh on surface definition 6 AFLR2 : Nodes, Trias,Quads= 12 14 0 AFLR4 : Nodes, Trias,Quads= 8 6 0 AFLR4 : Generate optimal mesh on surface definition 7 AFLR2 : Nodes, Trias,Quads= 92 150 0 AFLR4 : Nodes, Trias,Quads= 88 142 0 AFLR4 : Generate optimal mesh on surface definition 8 AFLR2 : Nodes, Trias,Quads= 92 150 0 AFLR4 : Nodes, Trias,Quads= 87 140 0 AFLR4 : Generate optimal mesh on surface definition 9 AFLR2 : Nodes, Trias,Quads= 312 546 0 AFLR4 : Nodes, Trias,Quads= 308 538 0 AFLR4 : Generate optimal mesh on surface definition 10 AFLR2 : Nodes, Trias,Quads= 312 546 0 AFLR4 : Nodes, Trias,Quads= 308 538 0 AFLR4 : Generate optimal mesh on surface definition 11 AFLR2 : Nodes, Trias,Quads= 311 544 0 AFLR4 : Nodes, Trias,Quads= 308 538 0 AFLR4 : Generate optimal mesh on surface definition 12 AFLR2 : Nodes, Trias,Quads= 311 544 0 AFLR4 : Nodes, Trias,Quads= 308 538 0 DGEOM : Add surface definitions to composite definition 0 DGEOM : Glue composite surface definition 0 DGEOM : Nodes,Faces,BEdges= 1239 2470 416 AFLR4 : Auto Mode Turned OFF OVERALL : CPU Time = 0.061 seconds Body 1 (of 2) Number of nodes = 20 Number of elements = 36 Number of triangle elements = 36 Number of quadrilateral elements = 0 Body 2 (of 2) Number of nodes = 1219 Number of elements = 2434 Number of triangle elements = 2434 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 1239 Total number of elements = 2470 . Analysis object with the name, aflr4AIM, has already been initilized An altName of aflr4AIM_2 will be used! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = bullet, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : EGADS CAD Geometry Setup EGADS : Model has 2 Active Bodies EGADS : Body 0 is a SolidBody EGADS : Body 0 has 1 Shells EGADS : Body 0 has 3 Faces EGADS : Body 0 has 5 Edges EGADS : Body 0 has 3 Loops EGADS : Body 0 has 3 Nodes EGADS : Body 1 is a SolidBody EGADS : Body 1 has 1 Shells EGADS : Body 1 has 6 Faces EGADS : Body 1 has 12 Edges EGADS : Body 1 has 6 Loops EGADS : Body 1 has 8 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 EGADS : 2 Yes 0 0 1 0 1 1 3 EGADS : 3 Yes 0 0 1 0 1 2 EGADS : 4 Yes 1 0 1 NA NA 6 7 8 9 EGADS : 5 Yes 1 0 1 NA NA 6 7 8 9 EGADS : 6 Yes 1 0 1 NA NA 4 5 8 9 EGADS : 7 Yes 1 0 1 NA NA 4 5 8 9 EGADS : 8 Yes 1 0 1 NA NA 4 5 6 7 EGADS : 9 Yes 1 0 1 NA NA 4 5 6 7 EGADS : Face Edges Information EGADS : Face Edges EGADS : 1 1 3 -2 -3 EGADS : 2 2 5 -4 -5 EGADS : 3 4 EGADS : 4 6 7 -8 -9 EGADS : 5 -10 13 12 -11 EGADS : 6 14 10 -15 -6 EGADS : 7 -16 8 17 -12 EGADS : 8 9 16 -13 -14 EGADS : 9 -7 15 11 -17 EGADS : Face Loops Information EGADS : Face Loops EGADS : 1 1 EGADS : 2 2 EGADS : 3 3 EGADS : 4 4 EGADS : 5 5 EGADS : 6 6 EGADS : 7 7 EGADS : 8 8 EGADS : 9 9 EGADS : Loop Edges Information EGADS : Loop Active Edges EGADS : 1 Yes 1 3 -2 -3 EGADS : 2 Yes 2 5 -4 -5 EGADS : 3 Yes 4 EGADS : 4 Yes 6 7 -8 -9 EGADS : 5 Yes -10 13 12 -11 EGADS : 6 Yes 14 10 -15 -6 EGADS : 7 Yes -16 8 17 -12 EGADS : 8 Yes 9 16 -13 -14 EGADS : 9 Yes -7 15 11 -17 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 DEGEN 1 1 - 1 EGADS : 2 0 Yes 2 2 1 1 2 EGADS : 3 0 Yes 1 2 1 1 1 EGADS : 4 0 Yes 3 3 1 2 3 EGADS : 5 0 Yes 2 3 1 2 2 EGADS : 6 1 Yes 5 4 NA 4 6 EGADS : 7 1 Yes 4 6 NA 4 9 EGADS : 8 1 Yes 7 6 NA 4 7 EGADS : 9 1 Yes 5 7 NA 4 8 EGADS : 10 1 Yes 9 8 NA 5 6 EGADS : 11 1 Yes 8 10 NA 5 9 EGADS : 12 1 Yes 11 10 NA 5 7 EGADS : 13 1 Yes 9 11 NA 5 8 EGADS : 14 1 Yes 5 9 NA 6 8 EGADS : 15 1 Yes 4 8 NA 6 9 EGADS : 16 1 Yes 7 11 NA 7 8 EGADS : 17 1 Yes 6 10 NA 7 9 EGADS : Node Information EGADS : Node Active Coordinates EGADS : 1 Yes 12 0 0 EGADS : 2 Yes 12.18062 0 0 EGADS : 3 Yes 13.3304132 0 0 EGADS : 4 Yes 0 0 2 EGADS : 5 Yes 0 0 0 EGADS : 6 Yes 0 2 2 EGADS : 7 Yes 0 2 0 EGADS : 8 Yes 14 0 2 EGADS : 9 Yes 14 0 0 EGADS : 10 Yes 14 2 2 EGADS : 11 Yes 14 2 0 EGADS : Face and Edge Match Information EGADS : No Face Matches Found AFLR4 : Surface Mesh Spacing Setup AFLR4 : Max Bounding Box Length = 15 AFLR4 : Min Bounding Box Length = 4 AFLR4 : Max Ref Bounding Box Length = 1.33041 AFLR4 : Min Ref Bounding Box Length = 1 AFLR4 : Reference Length = 1 AFLR4 : BL Thickness = 0 AFLR4 : FarField Spacing = 0.5 AFLR4 : Abs Min Surf Spacing = 0.0025 AFLR4 : Min Surf Spacing = 0.1 AFLR4 : Max Surf Spacing = 0.5 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 FARFIELD AFLR4 : 5 CAD geometry 0 FARFIELD AFLR4 : 6 CAD geometry 0 FARFIELD AFLR4 : 7 CAD geometry 0 FARFIELD AFLR4 : 8 CAD geometry 0 FARFIELD AFLR4 : 9 CAD geometry 0 FARFIELD 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= 37 48 0 AFLR4 : Nodes, Trias,Quads= 56 86 0 AFLR4 : Generate optimal mesh on surface definition 2 AFLR2 : Nodes, Trias,Quads= 304 535 0 AFLR4 : Nodes, Trias,Quads= 366 659 0 AFLR4 : Generate optimal mesh on surface definition 3 AFLR2 : Nodes, Trias,Quads= 103 173 0 AFLR4 : Nodes, Trias,Quads= 102 171 0 AFLR4 : Generate optimal mesh on surface definition 4 AFLR2 : Nodes, Trias,Quads= 92 150 0 AFLR4 : Nodes, Trias,Quads= 88 142 0 AFLR4 : Generate optimal mesh on surface definition 5 AFLR2 : Nodes, Trias,Quads= 92 150 0 AFLR4 : Nodes, Trias,Quads= 87 140 0 AFLR4 : Generate optimal mesh on surface definition 6 AFLR2 : Nodes, Trias,Quads= 312 546 0 AFLR4 : Nodes, Trias,Quads= 308 538 0 AFLR4 : Generate optimal mesh on surface definition 7 AFLR2 : Nodes, Trias,Quads= 312 546 0 AFLR4 : Nodes, Trias,Quads= 308 538 0 AFLR4 : Generate optimal mesh on surface definition 8 AFLR2 : Nodes, Trias,Quads= 311 544 0 AFLR4 : Nodes, Trias,Quads= 308 538 0 AFLR4 : Generate optimal mesh on surface definition 9 AFLR2 : Nodes, Trias,Quads= 311 544 0 AFLR4 : Nodes, Trias,Quads= 308 538 0 DGEOM : Add surface definitions to composite definition 0 DGEOM : Glue composite surface definition 0 DGEOM : Nodes,Faces,BEdges= 1679 3350 494 AFLR4 : Curvature BG Surface Grid Generation AFLR4 : Nodes, Faces = 1679 3350 AFLR4 : Surface Grid Generation AFLR4 : Generate optimal mesh on surface definition 1 AFLR2 : Nodes, Trias,Quads= 40 53 0 AFLR4 : Nodes, Trias,Quads= 55 83 0 AFLR4 : Generate optimal mesh on surface definition 2 AFLR2 : Nodes, Trias,Quads= 320 564 0 AFLR4 : Nodes, Trias,Quads= 381 686 0 AFLR4 : Generate optimal mesh on surface definition 3 AFLR2 : Nodes, Trias,Quads= 104 175 0 AFLR4 : Nodes, Trias,Quads= 99 165 0 AFLR4 : Generate optimal mesh on surface definition 4 AFLR2 : Nodes, Trias,Quads= 91 148 0 AFLR4 : Nodes, Trias,Quads= 88 142 0 AFLR4 : Generate optimal mesh on surface definition 5 AFLR2 : Nodes, Trias,Quads= 92 150 0 AFLR4 : Nodes, Trias,Quads= 87 140 0 AFLR4 : Generate optimal mesh on surface definition 6 AFLR2 : Nodes, Trias,Quads= 313 548 0 AFLR4 : Nodes, Trias,Quads= 308 538 0 AFLR4 : Generate optimal mesh on surface definition 7 AFLR2 : Nodes, Trias,Quads= 314 550 0 AFLR4 : Nodes, Trias,Quads= 308 538 0 AFLR4 : Generate optimal mesh on surface definition 8 AFLR2 : Nodes, Trias,Quads= 310 542 0 AFLR4 : Nodes, Trias,Quads= 308 538 0 AFLR4 : Generate optimal mesh on surface definition 9 AFLR2 : Nodes, Trias,Quads= 314 550 0 AFLR4 : Nodes, Trias,Quads= 308 538 0 DGEOM : Add surface definitions to composite definition 0 DGEOM : Glue composite surface definition 0 DGEOM : Nodes,Faces,BEdges= 1688 3368 498 OVERALL : CPU Time = 0.116 seconds Body 1 (of 2) Number of nodes = 469 Number of elements = 934 Number of triangle elements = 934 Number of quadrilateral elements = 0 Body 2 (of 2) Number of nodes = 1219 Number of elements = 2434 Number of triangle elements = 2434 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 1688 Total number of elements = 3368 . Analysis object with the name, aflr4AIM, has already been initilized An altName of aflr4AIM_3 will be used! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = cone, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : EGADS CAD Geometry Setup EGADS : Model has 2 Active Bodies EGADS : Body 0 is a SolidBody EGADS : Body 0 has 1 Shells EGADS : Body 0 has 3 Faces EGADS : Body 0 has 6 Edges EGADS : Body 0 has 3 Loops EGADS : Body 0 has 3 Nodes EGADS : Body 1 is a SolidBody EGADS : Body 1 has 1 Shells EGADS : Body 1 has 6 Faces EGADS : Body 1 has 12 Edges EGADS : Body 1 has 6 Loops EGADS : Body 1 has 8 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 EGADS : 2 Yes 0 0 1 0 1 1 3 EGADS : 3 Yes 0 0 1 0 1 1 2 EGADS : 4 Yes 1 0 1 NA NA 6 7 8 9 EGADS : 5 Yes 1 0 1 NA NA 6 7 8 9 EGADS : 6 Yes 1 0 1 NA NA 4 5 8 9 EGADS : 7 Yes 1 0 1 NA NA 4 5 8 9 EGADS : 8 Yes 1 0 1 NA NA 4 5 6 7 EGADS : 9 Yes 1 0 1 NA NA 4 5 6 7 EGADS : Face Edges Information EGADS : Face Edges EGADS : 1 -1 -2 3 4 EGADS : 2 5 2 -6 -4 EGADS : 3 1 6 EGADS : 4 7 8 -9 -10 EGADS : 5 -11 14 13 -12 EGADS : 6 15 11 -16 -7 EGADS : 7 -17 9 18 -13 EGADS : 8 10 17 -14 -15 EGADS : 9 -8 16 12 -18 EGADS : Face Loops Information EGADS : Face Loops EGADS : 1 1 EGADS : 2 2 EGADS : 3 3 EGADS : 4 4 EGADS : 5 5 EGADS : 6 6 EGADS : 7 7 EGADS : 8 8 EGADS : 9 9 EGADS : Loop Edges Information EGADS : Loop Active Edges EGADS : 1 Yes -1 -2 3 4 EGADS : 2 Yes 5 2 -6 -4 EGADS : 3 Yes 1 6 EGADS : 4 Yes 7 8 -9 -10 EGADS : 5 Yes -11 14 13 -12 EGADS : 6 Yes 15 11 -16 -7 EGADS : 7 Yes -17 9 18 -13 EGADS : 8 Yes 10 17 -14 -15 EGADS : 9 Yes -8 16 12 -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 3 EGADS : 2 0 Yes 3 2 1 1 2 EGADS : 3 0 DEGEN 3 3 - 1 EGADS : 4 0 Yes 3 1 1 1 2 EGADS : 5 0 DEGEN 3 3 - 2 EGADS : 6 0 Yes 1 2 1 2 3 EGADS : 7 1 Yes 5 4 NA 4 6 EGADS : 8 1 Yes 4 6 NA 4 9 EGADS : 9 1 Yes 7 6 NA 4 7 EGADS : 10 1 Yes 5 7 NA 4 8 EGADS : 11 1 Yes 9 8 NA 5 6 EGADS : 12 1 Yes 8 10 NA 5 9 EGADS : 13 1 Yes 11 10 NA 5 7 EGADS : 14 1 Yes 9 11 NA 5 8 EGADS : 15 1 Yes 5 9 NA 6 8 EGADS : 16 1 Yes 4 8 NA 6 9 EGADS : 17 1 Yes 7 11 NA 7 8 EGADS : 18 1 Yes 6 10 NA 7 9 EGADS : Node Information EGADS : Node Active Coordinates EGADS : 1 Yes 5 0 0 EGADS : 2 Yes 5 0 0.5 EGADS : 3 Yes 4 0 0 EGADS : 4 Yes 0 0 2 EGADS : 5 Yes 0 0 0 EGADS : 6 Yes 0 2 2 EGADS : 7 Yes 0 2 0 EGADS : 8 Yes 14 0 2 EGADS : 9 Yes 14 0 0 EGADS : 10 Yes 14 2 2 EGADS : 11 Yes 14 2 0 EGADS : Face and Edge Match Information EGADS : No Face Matches Found AFLR4 : Surface Mesh Spacing Setup AFLR4 : Max Bounding Box Length = 15 AFLR4 : Min Bounding Box Length = 4 AFLR4 : Max Ref Bounding Box Length = 1 AFLR4 : Min Ref Bounding Box Length = 1 AFLR4 : Reference Length = 1 AFLR4 : BL Thickness = 0 AFLR4 : FarField Spacing = 0.5 AFLR4 : Abs Min Surf Spacing = 0.0025 AFLR4 : Min Surf Spacing = 0.1 AFLR4 : Max Surf Spacing = 0.5 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 FARFIELD AFLR4 : 5 CAD geometry 0 FARFIELD AFLR4 : 6 CAD geometry 0 FARFIELD AFLR4 : 7 CAD geometry 0 FARFIELD AFLR4 : 8 CAD geometry 0 FARFIELD AFLR4 : 9 CAD geometry 0 FARFIELD 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= 104 168 0 AFLR4 : Nodes, Trias,Quads= 124 208 0 AFLR4 : Generate optimal mesh on surface definition 2 AFLR2 : Nodes, Trias,Quads= 104 168 0 AFLR4 : Nodes, Trias,Quads= 123 206 0 AFLR4 : Generate optimal mesh on surface definition 3 AFLR2 : Nodes, Trias,Quads= 112 190 0 AFLR4 : Nodes, Trias,Quads= 95 156 0 AFLR4 : Generate optimal mesh on surface definition 4 AFLR2 : Nodes, Trias,Quads= 92 150 0 AFLR4 : Nodes, Trias,Quads= 88 142 0 AFLR4 : Generate optimal mesh on surface definition 5 AFLR2 : Nodes, Trias,Quads= 92 150 0 AFLR4 : Nodes, Trias,Quads= 87 140 0 AFLR4 : Generate optimal mesh on surface definition 6 AFLR2 : Nodes, Trias,Quads= 312 546 0 AFLR4 : Nodes, Trias,Quads= 308 538 0 AFLR4 : Generate optimal mesh on surface definition 7 AFLR2 : Nodes, Trias,Quads= 312 546 0 AFLR4 : Nodes, Trias,Quads= 308 538 0 AFLR4 : Generate optimal mesh on surface definition 8 AFLR2 : Nodes, Trias,Quads= 311 544 0 AFLR4 : Nodes, Trias,Quads= 308 538 0 AFLR4 : Generate optimal mesh on surface definition 9 AFLR2 : Nodes, Trias,Quads= 311 544 0 AFLR4 : Nodes, Trias,Quads= 308 538 0 DGEOM : Add surface definitions to composite definition 0 DGEOM : Glue composite surface definition 0 DGEOM : Nodes,Faces,BEdges= 1506 3004 476 AFLR4 : Curvature BG Surface Grid Generation AFLR4 : Nodes, Faces = 1506 3004 AFLR4 : Surface Grid Generation AFLR4 : Generate optimal mesh on surface definition 1 AFLR2 : Nodes, Trias,Quads= 101 162 0 AFLR4 : Nodes, Trias,Quads= 129 218 0 AFLR4 : Generate optimal mesh on surface definition 2 AFLR2 : Nodes, Trias,Quads= 102 164 0 AFLR4 : Nodes, Trias,Quads= 127 214 0 AFLR4 : Generate optimal mesh on surface definition 3 AFLR2 : Nodes, Trias,Quads= 111 188 0 AFLR4 : Nodes, Trias,Quads= 103 172 0 AFLR4 : Generate optimal mesh on surface definition 4 AFLR2 : Nodes, Trias,Quads= 91 148 0 AFLR4 : Nodes, Trias,Quads= 88 142 0 AFLR4 : Generate optimal mesh on surface definition 5 AFLR2 : Nodes, Trias,Quads= 92 150 0 AFLR4 : Nodes, Trias,Quads= 87 140 0 AFLR4 : Generate optimal mesh on surface definition 6 AFLR2 : Nodes, Trias,Quads= 313 548 0 AFLR4 : Nodes, Trias,Quads= 308 538 0 AFLR4 : Generate optimal mesh on surface definition 7 AFLR2 : Nodes, Trias,Quads= 314 550 0 AFLR4 : Nodes, Trias,Quads= 308 538 0 AFLR4 : Generate optimal mesh on surface definition 8 AFLR2 : Nodes, Trias,Quads= 310 542 0 AFLR4 : Nodes, Trias,Quads= 308 538 0 AFLR4 : Generate optimal mesh on surface definition 9 AFLR2 : Nodes, Trias,Quads= 314 550 0 AFLR4 : Nodes, Trias,Quads= 308 538 0 DGEOM : Add surface definitions to composite definition 0 DGEOM : Glue composite surface definition 0 DGEOM : Nodes,Faces,BEdges= 1523 3038 476 OVERALL : CPU Time = 0.143 seconds Body 1 (of 2) Number of nodes = 304 Number of elements = 604 Number of triangle elements = 604 Number of quadrilateral elements = 0 Body 2 (of 2) Number of nodes = 1219 Number of elements = 2434 Number of triangle elements = 2434 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 1523 Total number of elements = 3038 . Analysis object with the name, aflr4AIM, has already been initilized An altName of aflr4AIM_4 will be used! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = cylinder, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : EGADS CAD Geometry Setup EGADS : Model has 2 Active Bodies EGADS : Body 0 is a SolidBody EGADS : Body 0 has 1 Shells EGADS : Body 0 has 3 Faces EGADS : Body 0 has 3 Edges EGADS : Body 0 has 3 Loops EGADS : Body 0 has 2 Nodes EGADS : Body 1 is a SolidBody EGADS : Body 1 has 1 Shells EGADS : Body 1 has 6 Faces EGADS : Body 1 has 12 Edges EGADS : Body 1 has 6 Loops EGADS : Body 1 has 8 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 EGADS : 2 Yes 0 0 1 0 1 1 3 EGADS : 3 Yes 0 0 1 0 1 2 EGADS : 4 Yes 1 0 1 NA NA 6 7 8 9 EGADS : 5 Yes 1 0 1 NA NA 6 7 8 9 EGADS : 6 Yes 1 0 1 NA NA 4 5 8 9 EGADS : 7 Yes 1 0 1 NA NA 4 5 8 9 EGADS : 8 Yes 1 0 1 NA NA 4 5 6 7 EGADS : 9 Yes 1 0 1 NA NA 4 5 6 7 EGADS : Face Edges Information EGADS : Face Edges EGADS : 1 -1 EGADS : 2 1 3 -2 -3 EGADS : 3 2 EGADS : 4 4 5 -6 -7 EGADS : 5 -8 11 10 -9 EGADS : 6 12 8 -13 -4 EGADS : 7 -14 6 15 -10 EGADS : 8 7 14 -11 -12 EGADS : 9 -5 13 9 -15 EGADS : Face Loops Information EGADS : Face Loops EGADS : 1 1 EGADS : 2 2 EGADS : 3 3 EGADS : 4 4 EGADS : 5 5 EGADS : 6 6 EGADS : 7 7 EGADS : 8 8 EGADS : 9 9 EGADS : Loop Edges Information EGADS : Loop Active Edges EGADS : 1 Yes -1 EGADS : 2 Yes 1 3 -2 -3 EGADS : 3 Yes 2 EGADS : 4 Yes 4 5 -6 -7 EGADS : 5 Yes -8 11 10 -9 EGADS : 6 Yes 12 8 -13 -4 EGADS : 7 Yes -14 6 15 -10 EGADS : 8 Yes 7 14 -11 -12 EGADS : 9 Yes -5 13 9 -15 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 1 1 1 1 2 EGADS : 2 0 Yes 2 2 1 2 3 EGADS : 3 0 Yes 1 2 1 2 2 EGADS : 4 1 Yes 4 3 NA 4 6 EGADS : 5 1 Yes 3 5 NA 4 9 EGADS : 6 1 Yes 6 5 NA 4 7 EGADS : 7 1 Yes 4 6 NA 4 8 EGADS : 8 1 Yes 8 7 NA 5 6 EGADS : 9 1 Yes 7 9 NA 5 9 EGADS : 10 1 Yes 10 9 NA 5 7 EGADS : 11 1 Yes 8 10 NA 5 8 EGADS : 12 1 Yes 4 8 NA 6 8 EGADS : 13 1 Yes 3 7 NA 6 9 EGADS : 14 1 Yes 6 10 NA 7 8 EGADS : 15 1 Yes 5 9 NA 7 9 EGADS : Node Information EGADS : Node Active Coordinates EGADS : 1 Yes 2 0 0.5 EGADS : 2 Yes 3 0 0.5 EGADS : 3 Yes 0 0 2 EGADS : 4 Yes 0 0 0 EGADS : 5 Yes 0 2 2 EGADS : 6 Yes 0 2 0 EGADS : 7 Yes 14 0 2 EGADS : 8 Yes 14 0 0 EGADS : 9 Yes 14 2 2 EGADS : 10 Yes 14 2 0 EGADS : Face and Edge Match Information EGADS : No Face Matches Found AFLR4 : Surface Mesh Spacing Setup AFLR4 : Max Bounding Box Length = 15 AFLR4 : Min Bounding Box Length = 4 AFLR4 : Max Ref Bounding Box Length = 1 AFLR4 : Min Ref Bounding Box Length = 1 AFLR4 : Reference Length = 1 AFLR4 : BL Thickness = 0 AFLR4 : FarField Spacing = 0.5 AFLR4 : Abs Min Surf Spacing = 0.0025 AFLR4 : Min Surf Spacing = 0.1 AFLR4 : Max Surf Spacing = 0.5 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 FARFIELD AFLR4 : 5 CAD geometry 0 FARFIELD AFLR4 : 6 CAD geometry 0 FARFIELD AFLR4 : 7 CAD geometry 0 FARFIELD AFLR4 : 8 CAD geometry 0 FARFIELD AFLR4 : 9 CAD geometry 0 FARFIELD 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= 103 173 0 AFLR4 : Nodes, Trias,Quads= 100 167 0 AFLR4 : Generate optimal mesh on surface definition 2 AFLR2 : Nodes, Trias,Quads= 388 692 0 AFLR4 : Nodes, Trias,Quads= 388 692 0 AFLR4 : Generate optimal mesh on surface definition 3 AFLR2 : Nodes, Trias,Quads= 105 177 0 AFLR4 : Nodes, Trias,Quads= 103 173 0 AFLR4 : Generate optimal mesh on surface definition 4 AFLR2 : Nodes, Trias,Quads= 92 150 0 AFLR4 : Nodes, Trias,Quads= 88 142 0 AFLR4 : Generate optimal mesh on surface definition 5 AFLR2 : Nodes, Trias,Quads= 92 150 0 AFLR4 : Nodes, Trias,Quads= 87 140 0 AFLR4 : Generate optimal mesh on surface definition 6 AFLR2 : Nodes, Trias,Quads= 312 546 0 AFLR4 : Nodes, Trias,Quads= 308 538 0 AFLR4 : Generate optimal mesh on surface definition 7 AFLR2 : Nodes, Trias,Quads= 312 546 0 AFLR4 : Nodes, Trias,Quads= 308 538 0 AFLR4 : Generate optimal mesh on surface definition 8 AFLR2 : Nodes, Trias,Quads= 311 544 0 AFLR4 : Nodes, Trias,Quads= 308 538 0 AFLR4 : Generate optimal mesh on surface definition 9 AFLR2 : Nodes, Trias,Quads= 311 544 0 AFLR4 : Nodes, Trias,Quads= 308 538 0 DGEOM : Add surface definitions to composite definition 0 DGEOM : Glue composite surface definition 0 DGEOM : Nodes,Faces,BEdges= 1737 3466 512 AFLR4 : Curvature BG Surface Grid Generation AFLR4 : Nodes, Faces = 1737 3466 AFLR4 : Surface Grid Generation AFLR4 : Generate optimal mesh on surface definition 1 AFLR2 : Nodes, Trias,Quads= 104 175 0 AFLR4 : Nodes, Trias,Quads= 99 165 0 AFLR4 : Generate optimal mesh on surface definition 2 AFLR2 : Nodes, Trias,Quads= 388 692 0 AFLR4 : Nodes, Trias,Quads= 391 698 0 AFLR4 : Generate optimal mesh on surface definition 3 AFLR2 : Nodes, Trias,Quads= 102 171 0 AFLR4 : Nodes, Trias,Quads= 102 171 0 AFLR4 : Generate optimal mesh on surface definition 4 AFLR2 : Nodes, Trias,Quads= 91 148 0 AFLR4 : Nodes, Trias,Quads= 88 142 0 AFLR4 : Generate optimal mesh on surface definition 5 AFLR2 : Nodes, Trias,Quads= 92 150 0 AFLR4 : Nodes, Trias,Quads= 87 140 0 AFLR4 : Generate optimal mesh on surface definition 6 AFLR2 : Nodes, Trias,Quads= 313 548 0 AFLR4 : Nodes, Trias,Quads= 308 538 0 AFLR4 : Generate optimal mesh on surface definition 7 AFLR2 : Nodes, Trias,Quads= 314 550 0 AFLR4 : Nodes, Trias,Quads= 308 538 0 AFLR4 : Generate optimal mesh on surface definition 8 AFLR2 : Nodes, Trias,Quads= 310 542 0 AFLR4 : Nodes, Trias,Quads= 308 538 0 AFLR4 : Generate optimal mesh on surface definition 9 AFLR2 : Nodes, Trias,Quads= 314 550 0 AFLR4 : Nodes, Trias,Quads= 308 538 0 DGEOM : Add surface definitions to composite definition 0 DGEOM : Glue composite surface definition 0 DGEOM : Nodes,Faces,BEdges= 1738 3468 512 OVERALL : CPU Time = 0.100 seconds Body 1 (of 2) Number of nodes = 519 Number of elements = 1034 Number of triangle elements = 1034 Number of quadrilateral elements = 0 Body 2 (of 2) Number of nodes = 1219 Number of elements = 2434 Number of triangle elements = 2434 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 1738 Total number of elements = 3468 .Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 .Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : EGADS CAD Geometry Setup EGADS : Model has 1 Active Bodies EGADS : Body 0 is a SolidBody EGADS : Body 0 has 2 Shells EGADS : Body 0 has 14 Faces EGADS : Body 0 has 27 Edges EGADS : Body 0 has 14 Loops EGADS : Body 0 has 17 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 NA NA 2 3 4 5 EGADS : 2 Yes 0 0 1 NA NA 1 3 5 6 EGADS : 3 Yes 0 0 1 NA NA 1 2 4 6 EGADS : 4 Yes 0 0 1 NA NA 1 3 5 6 EGADS : 5 Yes 0 0 1 NA NA 1 2 4 6 EGADS : 6 Yes 0 0 1 NA NA 2 3 4 5 EGADS : 7 Yes 0 0 1 0 1 8 9 10 11 EGADS : 8 Yes 0 0 1 0 1 7 10 11 12 EGADS : 9 Yes 0 0 1 0 1 7 12 13 14 EGADS : 10 Yes 0 0 1 0 1 7 8 11 13 EGADS : 11 Yes 0 0 1 0 1 7 8 10 EGADS : 12 Yes 0 0 1 0 1 8 9 13 14 EGADS : 13 Yes 0 0 1 0 1 9 10 12 14 EGADS : 14 Yes 0 0 1 0 1 9 12 13 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 EGADS : 4 -10 3 8 -11 EGADS : 5 4 10 -12 -5 EGADS : 6 -6 12 11 -9 EGADS : 7 -13 14 15 -16 EGADS : 8 -17 18 13 -19 EGADS : 9 20 22 -21 -14 EGADS : 10 -15 23 17 -24 EGADS : 11 16 24 19 EGADS : 12 25 26 -20 -18 EGADS : 13 21 27 -25 -23 EGADS : 14 -22 -26 -27 EGADS : Face Loops Information EGADS : Face Loops EGADS : 1 1 EGADS : 2 2 EGADS : 3 3 EGADS : 4 4 EGADS : 5 5 EGADS : 6 6 EGADS : 7 7 EGADS : 8 8 EGADS : 9 9 EGADS : 10 10 EGADS : 11 11 EGADS : 12 12 EGADS : 13 13 EGADS : 14 14 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 3 8 -11 EGADS : 5 Yes 4 10 -12 -5 EGADS : 6 Yes -6 12 11 -9 EGADS : 7 Yes -13 14 15 -16 EGADS : 8 Yes -17 18 13 -19 EGADS : 9 Yes 20 22 -21 -14 EGADS : 10 Yes -15 23 17 -24 EGADS : 11 Yes 16 24 19 EGADS : 12 Yes 25 26 -20 -18 EGADS : 13 Yes 21 27 -25 -23 EGADS : 14 Yes -22 -26 -27 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 NA 1 2 EGADS : 2 0 Yes 1 3 NA 1 3 EGADS : 3 0 Yes 4 3 NA 1 4 EGADS : 4 0 Yes 2 4 NA 1 5 EGADS : 5 0 Yes 2 5 NA 2 5 EGADS : 6 0 Yes 5 6 NA 2 6 EGADS : 7 0 Yes 1 6 NA 2 3 EGADS : 8 0 Yes 3 7 NA 3 4 EGADS : 9 0 Yes 6 7 NA 3 6 EGADS : 10 0 Yes 4 8 NA 4 5 EGADS : 11 0 Yes 8 7 NA 4 6 EGADS : 12 0 Yes 5 8 NA 5 6 EGADS : 13 0 Yes 9 10 1 7 8 EGADS : 14 0 Yes 9 11 1 7 9 EGADS : 15 0 Yes 11 12 1 7 10 EGADS : 16 0 Yes 10 12 1 7 11 EGADS : 17 0 Yes 13 14 1 8 10 EGADS : 18 0 Yes 13 9 1 8 12 EGADS : 19 0 Yes 14 10 1 8 11 EGADS : 20 0 Yes 9 15 1 9 12 EGADS : 21 0 Yes 11 16 1 9 13 EGADS : 22 0 Yes 15 16 1 9 14 EGADS : 23 0 Yes 11 13 1 10 13 EGADS : 24 0 Yes 12 14 1 10 11 EGADS : 25 0 Yes 13 17 1 12 13 EGADS : 26 0 Yes 17 15 1 12 14 EGADS : 27 0 Yes 16 17 1 13 14 EGADS : Node Information EGADS : Node Active Coordinates EGADS : 1 Yes 0 0 40 EGADS : 2 Yes 0 0 0 EGADS : 3 Yes 0 40 40 EGADS : 4 Yes 0 40 0 EGADS : 5 Yes 40 0 0 EGADS : 6 Yes 40 0 40 EGADS : 7 Yes 40 40 40 EGADS : 8 Yes 40 40 0 EGADS : 9 Yes 3.77246052 0 0.00459131419 EGADS : 10 Yes 5.90487498 7.07106781 0 EGADS : 11 Yes 0 0 0 EGADS : 12 Yes 4.0824829 7.07106781 0.123425948 EGADS : 13 Yes 3.77001182 0 0 EGADS : 14 Yes 5.90282524 7.07106781 0 EGADS : 15 Yes 5.90487498 0 0 EGADS : 16 Yes 4.0824829 0 0.123425948 EGADS : 17 Yes 5.90282524 0 0 EGADS : Face and Edge Match Information EGADS : No Face Matches Found AFLR4 : Surface Mesh Spacing Setup AFLR4 : Max Bounding Box Length = 80 AFLR4 : Min Bounding Box Length = 80 AFLR4 : Max Ref Bounding Box Length = 14.1421 AFLR4 : Min Ref Bounding Box Length = 0.890888 AFLR4 : Reference Length = 2.82843 AFLR4 : BL Thickness = 0 AFLR4 : FarField Spacing = 7.60986 AFLR4 : Abs Min Surf Spacing = 0.00707107 AFLR4 : Min Surf Spacing = 0.0141421 AFLR4 : Max Surf Spacing = 0.282843 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 FARFIELD AFLR4 : 2 CAD geometry 0 FARFIELD AFLR4 : 3 CAD geometry 0 FARFIELD AFLR4 : 4 CAD geometry 0 FARFIELD AFLR4 : 5 CAD geometry 0 FARFIELD AFLR4 : 6 CAD geometry 0 FARFIELD 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 : 10 CAD geometry 0 STD w/BL AFLR4 : 11 CAD geometry 0 STD w/BL AFLR4 : 12 CAD geometry 0 STD w/BL AFLR4 : 13 CAD geometry 0 STD w/BL AFLR4 : 14 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 : Define CAD surface definition 10 AFLR4 : Define CAD surface definition 11 AFLR4 : Define CAD surface definition 12 AFLR4 : Define CAD surface definition 13 AFLR4 : Define CAD surface definition 14 AFLR4 : Surface Grid Generation AFLR4 : Generate optimal mesh on surface definition 1 AFLR2 : Nodes, Trias,Quads= 136 230 0 AFLR4 : Nodes, Trias,Quads= 132 222 0 AFLR4 : Generate optimal mesh on surface definition 2 AFLR2 : Nodes, Trias,Quads= 136 230 0 AFLR4 : Nodes, Trias,Quads= 132 222 0 AFLR4 : Generate optimal mesh on surface definition 3 AFLR2 : Nodes, Trias,Quads= 136 230 0 AFLR4 : Nodes, Trias,Quads= 132 222 0 AFLR4 : Generate optimal mesh on surface definition 4 AFLR2 : Nodes, Trias,Quads= 136 230 0 AFLR4 : Nodes, Trias,Quads= 132 222 0 AFLR4 : Generate optimal mesh on surface definition 5 AFLR2 : Nodes, Trias,Quads= 136 230 0 AFLR4 : Nodes, Trias,Quads= 132 222 0 AFLR4 : Generate optimal mesh on surface definition 6 AFLR2 : Nodes, Trias,Quads= 136 230 0 AFLR4 : Nodes, Trias,Quads= 132 222 0 AFLR4 : Generate optimal mesh on surface definition 7 AFLR2 : Nodes, Trias,Quads= 17058 33386 0 AFLR4 : Nodes, Trias,Quads= 7507 14284 0 AFLR4 : Generate optimal mesh on surface definition 8 AFLR2 : Nodes, Trias,Quads= 182 241 0 AFLR4 : Nodes, Trias,Quads= 122 121 0 AFLR4 : Generate optimal mesh on surface definition 9 AFLR2 : Nodes, Trias,Quads= 17154 33578 0 AFLR4 : Nodes, Trias,Quads= 7368 14006 0 AFLR4 : Generate optimal mesh on surface definition 10 AFLR2 : Nodes, Trias,Quads= 14987 29245 0 AFLR4 : Nodes, Trias,Quads= 6879 13029 0 AFLR4 : Generate optimal mesh on surface definition 11 AFLR2 : Nodes, Trias,Quads= 330 546 0 AFLR4 : Nodes, Trias,Quads= 322 530 0 AFLR4 : Generate optimal mesh on surface definition 12 AFLR2 : Nodes, Trias,Quads= 182 241 0 AFLR4 : Nodes, Trias,Quads= 122 121 0 AFLR4 : Generate optimal mesh on surface definition 13 AFLR2 : Nodes, Trias,Quads= 14793 28857 0 AFLR4 : Nodes, Trias,Quads= 6844 12959 0 AFLR4 : Generate optimal mesh on surface definition 14 AFLR2 : Nodes, Trias,Quads= 328 542 0 AFLR4 : Nodes, Trias,Quads= 324 534 0 DGEOM : Add surface definitions to composite definition 0 DGEOM : Glue composite surface definition 0 DGEOM : Nodes,Faces,BEdges= 28462 56916 3616 AFLR4 : Curvature BG Surface Grid Generation AFLR4 : Nodes, Faces = 28462 56916 AFLR4 : Surface Grid Generation AFLR4 : Generate optimal mesh on surface definition 1 AFLR2 : Nodes, Trias,Quads= 136 230 0 AFLR4 : Nodes, Trias,Quads= 132 222 0 AFLR4 : Generate optimal mesh on surface definition 2 AFLR2 : Nodes, Trias,Quads= 137 232 0 AFLR4 : Nodes, Trias,Quads= 132 222 0 AFLR4 : Generate optimal mesh on surface definition 3 AFLR2 : Nodes, Trias,Quads= 137 232 0 AFLR4 : Nodes, Trias,Quads= 132 222 0 AFLR4 : Generate optimal mesh on surface definition 4 AFLR2 : Nodes, Trias,Quads= 136 230 0 AFLR4 : Nodes, Trias,Quads= 132 222 0 AFLR4 : Generate optimal mesh on surface definition 5 AFLR2 : Nodes, Trias,Quads= 137 232 0 AFLR4 : Nodes, Trias,Quads= 132 222 0 AFLR4 : Generate optimal mesh on surface definition 6 AFLR2 : Nodes, Trias,Quads= 137 232 0 AFLR4 : Nodes, Trias,Quads= 132 222 0 AFLR4 : Generate optimal mesh on surface definition 7 AFLR2 : Nodes, Trias,Quads= 15590 30449 0 AFLR4 : Nodes, Trias,Quads= 9447 18163 0 AFLR4 : Generate optimal mesh on surface definition 8 AFLR2 : Nodes, Trias,Quads= 254 370 0 AFLR4 : Nodes, Trias,Quads= 136 134 0 AFLR4 : Generate optimal mesh on surface definition 9 AFLR2 : Nodes, Trias,Quads= 15870 31009 0 AFLR4 : Nodes, Trias,Quads= 9439 18147 0 AFLR4 : Generate optimal mesh on surface definition 10 AFLR2 : Nodes, Trias,Quads= 14689 28649 0 AFLR4 : Nodes, Trias,Quads= 9247 17765 0 AFLR4 : Generate optimal mesh on surface definition 11 AFLR2 : Nodes, Trias,Quads= 346 577 0 AFLR4 : Nodes, Trias,Quads= 359 603 0 AFLR4 : Generate optimal mesh on surface definition 12 AFLR2 : Nodes, Trias,Quads= 254 370 0 AFLR4 : Nodes, Trias,Quads= 136 134 0 AFLR4 : Generate optimal mesh on surface definition 13 AFLR2 : Nodes, Trias,Quads= 14582 28435 0 AFLR4 : Nodes, Trias,Quads= 9309 17889 0 AFLR4 : Generate optimal mesh on surface definition 14 AFLR2 : Nodes, Trias,Quads= 348 581 0 AFLR4 : Nodes, Trias,Quads= 361 607 0 DGEOM : Add surface definitions to composite definition 0 DGEOM : Glue composite surface definition 0 DGEOM : Nodes,Faces,BEdges= 37391 74774 3650 OVERALL : CPU Time = 1.707 seconds Body 1 (of 1) Number of nodes = 37391 Number of elements = 74774 Number of triangle elements = 74774 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 37391 Total number of elements = 74774 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : EGADS CAD Geometry Setup EGADS : Model has 1 Active Bodies EGADS : Body 0 is a SolidBody EGADS : Body 0 has 2 Shells EGADS : Body 0 has 14 Faces EGADS : Body 0 has 27 Edges EGADS : Body 0 has 14 Loops EGADS : Body 0 has 17 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 NA NA 2 3 4 5 EGADS : 2 Yes 0 0 1 NA NA 1 3 5 6 EGADS : 3 Yes 0 0 1 NA NA 1 2 4 6 EGADS : 4 Yes 0 0 1 NA NA 1 3 5 6 EGADS : 5 Yes 0 0 1 NA NA 1 2 4 6 EGADS : 6 Yes 0 0 1 NA NA 2 3 4 5 EGADS : 7 Yes 0 0 1 0 1 8 9 10 11 EGADS : 8 Yes 0 0 1 0 1 7 10 11 12 EGADS : 9 Yes 0 0 1 0 1 7 12 13 14 EGADS : 10 Yes 0 0 1 0 1 7 8 11 13 EGADS : 11 Yes 0 0 1 0 1 7 8 10 EGADS : 12 Yes 0 0 1 0 1 8 9 13 14 EGADS : 13 Yes 0 0 1 0 1 9 10 12 14 EGADS : 14 Yes 0 0 1 0 1 9 12 13 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 EGADS : 4 -10 3 8 -11 EGADS : 5 4 10 -12 -5 EGADS : 6 -6 12 11 -9 EGADS : 7 -13 14 15 -16 EGADS : 8 -17 18 13 -19 EGADS : 9 20 22 -21 -14 EGADS : 10 -15 23 17 -24 EGADS : 11 16 24 19 EGADS : 12 25 26 -20 -18 EGADS : 13 21 27 -25 -23 EGADS : 14 -22 -26 -27 EGADS : Face Loops Information EGADS : Face Loops EGADS : 1 1 EGADS : 2 2 EGADS : 3 3 EGADS : 4 4 EGADS : 5 5 EGADS : 6 6 EGADS : 7 7 EGADS : 8 8 EGADS : 9 9 EGADS : 10 10 EGADS : 11 11 EGADS : 12 12 EGADS : 13 13 EGADS : 14 14 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 3 8 -11 EGADS : 5 Yes 4 10 -12 -5 EGADS : 6 Yes -6 12 11 -9 EGADS : 7 Yes -13 14 15 -16 EGADS : 8 Yes -17 18 13 -19 EGADS : 9 Yes 20 22 -21 -14 EGADS : 10 Yes -15 23 17 -24 EGADS : 11 Yes 16 24 19 EGADS : 12 Yes 25 26 -20 -18 EGADS : 13 Yes 21 27 -25 -23 EGADS : 14 Yes -22 -26 -27 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 NA 1 2 EGADS : 2 0 Yes 1 3 NA 1 3 EGADS : 3 0 Yes 4 3 NA 1 4 EGADS : 4 0 Yes 2 4 NA 1 5 EGADS : 5 0 Yes 2 5 NA 2 5 EGADS : 6 0 Yes 5 6 NA 2 6 EGADS : 7 0 Yes 1 6 NA 2 3 EGADS : 8 0 Yes 3 7 NA 3 4 EGADS : 9 0 Yes 6 7 NA 3 6 EGADS : 10 0 Yes 4 8 NA 4 5 EGADS : 11 0 Yes 8 7 NA 4 6 EGADS : 12 0 Yes 5 8 NA 5 6 EGADS : 13 0 Yes 9 10 1 7 8 EGADS : 14 0 Yes 9 11 1 7 9 EGADS : 15 0 Yes 11 12 1 7 10 EGADS : 16 0 Yes 10 12 1 7 11 EGADS : 17 0 Yes 13 14 1 8 10 EGADS : 18 0 Yes 13 9 1 8 12 EGADS : 19 0 Yes 14 10 1 8 11 EGADS : 20 0 Yes 9 15 1 9 12 EGADS : 21 0 Yes 11 16 1 9 13 EGADS : 22 0 Yes 15 16 1 9 14 EGADS : 23 0 Yes 11 13 1 10 13 EGADS : 24 0 Yes 12 14 1 10 11 EGADS : 25 0 Yes 13 17 1 12 13 EGADS : 26 0 Yes 17 15 1 12 14 EGADS : 27 0 Yes 16 17 1 13 14 EGADS : Node Information EGADS : Node Active Coordinates EGADS : 1 Yes 0 0 40 EGADS : 2 Yes 0 0 0 EGADS : 3 Yes 0 40 40 EGADS : 4 Yes 0 40 0 EGADS : 5 Yes 40 0 0 EGADS : 6 Yes 40 0 40 EGADS : 7 Yes 40 40 40 EGADS : 8 Yes 40 40 0 EGADS : 9 Yes 3.77246052 0 0.00459131419 EGADS : 10 Yes 5.90487498 7.07106781 0 EGADS : 11 Yes 0 0 0 EGADS : 12 Yes 4.0824829 7.07106781 0.123425948 EGADS : 13 Yes 3.77001182 0 0 EGADS : 14 Yes 5.90282524 7.07106781 0 EGADS : 15 Yes 5.90487498 0 0 EGADS : 16 Yes 4.0824829 0 0.123425948 EGADS : 17 Yes 5.90282524 0 0 EGADS : Face and Edge Match Information EGADS : No Face Matches Found AFLR4 : Surface Mesh Spacing Setup AFLR4 : Max Bounding Box Length = 80 AFLR4 : Min Bounding Box Length = 80 AFLR4 : Max Ref Bounding Box Length = 14.1421 AFLR4 : Min Ref Bounding Box Length = 0.890888 AFLR4 : Reference Length = 2.82843 AFLR4 : BL Thickness = 0 AFLR4 : FarField Spacing = 15.2197 AFLR4 : Abs Min Surf Spacing = 0.00707107 AFLR4 : Min Surf Spacing = 0.0141421 AFLR4 : Max Surf Spacing = 0.282843 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 FARFIELD AFLR4 : 2 CAD geometry 0 FARFIELD AFLR4 : 3 CAD geometry 0 FARFIELD AFLR4 : 4 CAD geometry 0 FARFIELD AFLR4 : 5 CAD geometry 0 FARFIELD AFLR4 : 6 CAD geometry 0 FARFIELD 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 : 10 CAD geometry 0 STD w/BL AFLR4 : 11 CAD geometry 0 STD w/BL AFLR4 : 12 CAD geometry 0 STD w/BL AFLR4 : 13 CAD geometry 0 STD w/BL AFLR4 : 14 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 : Define CAD surface definition 10 AFLR4 : Define CAD surface definition 11 AFLR4 : Define CAD surface definition 12 AFLR4 : Define CAD surface definition 13 AFLR4 : Define CAD surface definition 14 AFLR4 : Surface Grid Generation AFLR4 : Generate optimal mesh on surface definition 1 AFLR2 : Nodes, Trias,Quads= 41 60 0 AFLR4 : Nodes, Trias,Quads= 37 52 0 AFLR4 : Generate optimal mesh on surface definition 2 AFLR2 : Nodes, Trias,Quads= 41 60 0 AFLR4 : Nodes, Trias,Quads= 37 52 0 AFLR4 : Generate optimal mesh on surface definition 3 AFLR2 : Nodes, Trias,Quads= 41 60 0 AFLR4 : Nodes, Trias,Quads= 37 52 0 AFLR4 : Generate optimal mesh on surface definition 4 AFLR2 : Nodes, Trias,Quads= 41 60 0 AFLR4 : Nodes, Trias,Quads= 37 52 0 AFLR4 : Generate optimal mesh on surface definition 5 AFLR2 : Nodes, Trias,Quads= 41 60 0 AFLR4 : Nodes, Trias,Quads= 37 52 0 AFLR4 : Generate optimal mesh on surface definition 6 AFLR2 : Nodes, Trias,Quads= 41 60 0 AFLR4 : Nodes, Trias,Quads= 37 52 0 AFLR4 : Generate optimal mesh on surface definition 7 AFLR2 : Nodes, Trias,Quads= 6308 12196 0 AFLR4 : Nodes, Trias,Quads= 3150 5880 0 AFLR4 : Generate optimal mesh on surface definition 8 AFLR2 : Nodes, Trias,Quads= 192 273 0 AFLR4 : Nodes, Trias,Quads= 110 109 0 AFLR4 : Generate optimal mesh on surface definition 9 AFLR2 : Nodes, Trias,Quads= 6486 12552 0 AFLR4 : Nodes, Trias,Quads= 3253 6086 0 AFLR4 : Generate optimal mesh on surface definition 10 AFLR2 : Nodes, Trias,Quads= 5848 11277 0 AFLR4 : Nodes, Trias,Quads= 3043 5667 0 AFLR4 : Generate optimal mesh on surface definition 11 AFLR2 : Nodes, Trias,Quads= 250 400 0 AFLR4 : Nodes, Trias,Quads= 245 390 0 AFLR4 : Generate optimal mesh on surface definition 12 AFLR2 : Nodes, Trias,Quads= 192 273 0 AFLR4 : Nodes, Trias,Quads= 110 109 0 AFLR4 : Generate optimal mesh on surface definition 13 AFLR2 : Nodes, Trias,Quads= 5864 11309 0 AFLR4 : Nodes, Trias,Quads= 3002 5585 0 AFLR4 : Generate optimal mesh on surface definition 14 AFLR2 : Nodes, Trias,Quads= 249 398 0 AFLR4 : Nodes, Trias,Quads= 244 388 0 DGEOM : Add surface definitions to composite definition 0 DGEOM : Glue composite surface definition 0 DGEOM : Nodes,Faces,BEdges= 12267 24526 2204 AFLR4 : Curvature BG Surface Grid Generation AFLR4 : Nodes, Faces = 12267 24526 AFLR4 : Surface Grid Generation AFLR4 : Generate optimal mesh on surface definition 1 AFLR2 : Nodes, Trias,Quads= 41 60 0 AFLR4 : Nodes, Trias,Quads= 36 50 0 AFLR4 : Generate optimal mesh on surface definition 2 AFLR2 : Nodes, Trias,Quads= 41 60 0 AFLR4 : Nodes, Trias,Quads= 36 50 0 AFLR4 : Generate optimal mesh on surface definition 3 AFLR2 : Nodes, Trias,Quads= 41 60 0 AFLR4 : Nodes, Trias,Quads= 36 50 0 AFLR4 : Generate optimal mesh on surface definition 4 AFLR2 : Nodes, Trias,Quads= 41 60 0 AFLR4 : Nodes, Trias,Quads= 36 50 0 AFLR4 : Generate optimal mesh on surface definition 5 AFLR2 : Nodes, Trias,Quads= 41 60 0 AFLR4 : Nodes, Trias,Quads= 36 50 0 AFLR4 : Generate optimal mesh on surface definition 6 AFLR2 : Nodes, Trias,Quads= 41 60 0 AFLR4 : Nodes, Trias,Quads= 36 50 0 AFLR4 : Generate optimal mesh on surface definition 7 AFLR2 : Nodes, Trias,Quads= 6119 11815 0 AFLR4 : Nodes, Trias,Quads= 4216 8009 0 AFLR4 : Generate optimal mesh on surface definition 8 AFLR2 : Nodes, Trias,Quads= 226 328 0 AFLR4 : Nodes, Trias,Quads= 122 120 0 AFLR4 : Generate optimal mesh on surface definition 9 AFLR2 : Nodes, Trias,Quads= 6177 11933 0 AFLR4 : Nodes, Trias,Quads= 4307 8193 0 AFLR4 : Generate optimal mesh on surface definition 10 AFLR2 : Nodes, Trias,Quads= 5886 11351 0 AFLR4 : Nodes, Trias,Quads= 4129 7837 0 AFLR4 : Generate optimal mesh on surface definition 11 AFLR2 : Nodes, Trias,Quads= 250 401 0 AFLR4 : Nodes, Trias,Quads= 252 405 0 AFLR4 : Generate optimal mesh on surface definition 12 AFLR2 : Nodes, Trias,Quads= 225 326 0 AFLR4 : Nodes, Trias,Quads= 122 120 0 AFLR4 : Generate optimal mesh on surface definition 13 AFLR2 : Nodes, Trias,Quads= 5948 11476 0 AFLR4 : Nodes, Trias,Quads= 4168 7916 0 AFLR4 : Generate optimal mesh on surface definition 14 AFLR2 : Nodes, Trias,Quads= 246 394 0 AFLR4 : Nodes, Trias,Quads= 244 390 0 DGEOM : Add surface definitions to composite definition 0 DGEOM : Glue composite surface definition 0 DGEOM : Nodes,Faces,BEdges= 16649 33290 2234 OVERALL : CPU Time = 0.766 seconds Body 1 (of 1) Number of nodes = 16649 Number of elements = 33290 Number of triangle elements = 33290 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 16649 Total number of elements = 33290 .. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! Analysis object with the name, aflr4AIM, has already been initilized An altName of aflr4AIM_5 will be used! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = sphere, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : EGADS CAD Geometry Setup EGADS : Model has 2 Active Bodies EGADS : Body 0 is a SolidBody EGADS : Body 0 has 1 Shells EGADS : Body 0 has 2 Faces EGADS : Body 0 has 6 Edges EGADS : Body 0 has 2 Loops EGADS : Body 0 has 2 Nodes EGADS : Body 1 is a SolidBody EGADS : Body 1 has 1 Shells EGADS : Body 1 has 6 Faces EGADS : Body 1 has 12 Edges EGADS : Body 1 has 6 Loops EGADS : Body 1 has 8 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 EGADS : 2 Yes 0 0 1 0 1 1 EGADS : 3 Yes 1 0 1 NA NA 5 6 7 8 EGADS : 4 Yes 1 0 1 NA NA 5 6 7 8 EGADS : 5 Yes 1 0 1 NA NA 3 4 7 8 EGADS : 6 Yes 1 0 1 NA NA 3 4 7 8 EGADS : 7 Yes 1 0 1 NA NA 3 4 5 6 EGADS : 8 Yes 1 0 1 NA NA 3 4 5 6 EGADS : Face Edges Information EGADS : Face Edges EGADS : 1 -1 -2 3 4 EGADS : 2 -5 -4 6 2 EGADS : 3 7 8 -9 -10 EGADS : 4 -11 14 13 -12 EGADS : 5 15 11 -16 -7 EGADS : 6 -17 9 18 -13 EGADS : 7 10 17 -14 -15 EGADS : 8 -8 16 12 -18 EGADS : Face Loops Information EGADS : Face Loops EGADS : 1 1 EGADS : 2 2 EGADS : 3 3 EGADS : 4 4 EGADS : 5 5 EGADS : 6 6 EGADS : 7 7 EGADS : 8 8 EGADS : Loop Edges Information EGADS : Loop Active Edges EGADS : 1 Yes -1 -2 3 4 EGADS : 2 Yes -5 -4 6 2 EGADS : 3 Yes 7 8 -9 -10 EGADS : 4 Yes -11 14 13 -12 EGADS : 5 Yes 15 11 -16 -7 EGADS : 6 Yes -17 9 18 -13 EGADS : 7 Yes 10 17 -14 -15 EGADS : 8 Yes -8 16 12 -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 DEGEN 1 1 - 1 EGADS : 2 0 Yes 2 1 1 1 2 EGADS : 3 0 DEGEN 2 2 - 1 EGADS : 4 0 Yes 2 1 1 1 2 EGADS : 5 0 DEGEN 1 1 - 2 EGADS : 6 0 DEGEN 2 2 - 2 EGADS : 7 1 Yes 4 3 NA 3 5 EGADS : 8 1 Yes 3 5 NA 3 8 EGADS : 9 1 Yes 6 5 NA 3 6 EGADS : 10 1 Yes 4 6 NA 3 7 EGADS : 11 1 Yes 8 7 NA 4 5 EGADS : 12 1 Yes 7 9 NA 4 8 EGADS : 13 1 Yes 10 9 NA 4 6 EGADS : 14 1 Yes 8 10 NA 4 7 EGADS : 15 1 Yes 4 8 NA 5 7 EGADS : 16 1 Yes 3 7 NA 5 8 EGADS : 17 1 Yes 6 10 NA 6 7 EGADS : 18 1 Yes 5 9 NA 6 8 EGADS : Node Information EGADS : Node Active Coordinates EGADS : 1 Yes 8.5 0 0.5 EGADS : 2 Yes 8.5 0 0 EGADS : 3 Yes 0 0 2 EGADS : 4 Yes 0 0 0 EGADS : 5 Yes 0 2 2 EGADS : 6 Yes 0 2 0 EGADS : 7 Yes 14 0 2 EGADS : 8 Yes 14 0 0 EGADS : 9 Yes 14 2 2 EGADS : 10 Yes 14 2 0 EGADS : Face and Edge Match Information EGADS : No Face Matches Found AFLR4 : Surface Mesh Spacing Setup AFLR4 : Max Bounding Box Length = 15 AFLR4 : Min Bounding Box Length = 4 AFLR4 : Max Ref Bounding Box Length = 1 AFLR4 : Min Ref Bounding Box Length = 1 AFLR4 : Reference Length = 1 AFLR4 : BL Thickness = 0 AFLR4 : FarField Spacing = 0.5 AFLR4 : Abs Min Surf Spacing = 0.0025 AFLR4 : Min Surf Spacing = 0.1 AFLR4 : Max Surf Spacing = 0.5 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 FARFIELD AFLR4 : 4 CAD geometry 0 FARFIELD AFLR4 : 5 CAD geometry 0 FARFIELD AFLR4 : 6 CAD geometry 0 FARFIELD AFLR4 : 7 CAD geometry 0 FARFIELD AFLR4 : 8 CAD geometry 0 FARFIELD 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 : Surface Grid Generation AFLR4 : Generate optimal mesh on surface definition 1 AFLR2 : Nodes, Trias,Quads= 94 154 0 AFLR4 : Nodes, Trias,Quads= 202 370 0 AFLR4 : Generate optimal mesh on surface definition 2 AFLR2 : Nodes, Trias,Quads= 94 154 0 AFLR4 : Nodes, Trias,Quads= 201 368 0 AFLR4 : Generate optimal mesh on surface definition 3 AFLR2 : Nodes, Trias,Quads= 92 150 0 AFLR4 : Nodes, Trias,Quads= 88 142 0 AFLR4 : Generate optimal mesh on surface definition 4 AFLR2 : Nodes, Trias,Quads= 92 150 0 AFLR4 : Nodes, Trias,Quads= 87 140 0 AFLR4 : Generate optimal mesh on surface definition 5 AFLR2 : Nodes, Trias,Quads= 312 546 0 AFLR4 : Nodes, Trias,Quads= 308 538 0 AFLR4 : Generate optimal mesh on surface definition 6 AFLR2 : Nodes, Trias,Quads= 312 546 0 AFLR4 : Nodes, Trias,Quads= 308 538 0 AFLR4 : Generate optimal mesh on surface definition 7 AFLR2 : Nodes, Trias,Quads= 311 544 0 AFLR4 : Nodes, Trias,Quads= 308 538 0 AFLR4 : Generate optimal mesh on surface definition 8 AFLR2 : Nodes, Trias,Quads= 311 544 0 AFLR4 : Nodes, Trias,Quads= 308 538 0 DGEOM : Add surface definitions to composite definition 0 DGEOM : Glue composite surface definition 0 DGEOM : Nodes,Faces,BEdges= 1590 3172 432 AFLR4 : Curvature BG Surface Grid Generation AFLR4 : Nodes, Faces = 1590 3172 AFLR4 : Surface Grid Generation AFLR4 : Generate optimal mesh on surface definition 1 AFLR2 : Nodes, Trias,Quads= 81 130 0 AFLR4 : Nodes, Trias,Quads= 203 374 0 AFLR4 : Generate optimal mesh on surface definition 2 AFLR2 : Nodes, Trias,Quads= 81 130 0 AFLR4 : Nodes, Trias,Quads= 199 366 0 AFLR4 : Generate optimal mesh on surface definition 3 AFLR2 : Nodes, Trias,Quads= 91 148 0 AFLR4 : Nodes, Trias,Quads= 88 142 0 AFLR4 : Generate optimal mesh on surface definition 4 AFLR2 : Nodes, Trias,Quads= 92 150 0 AFLR4 : Nodes, Trias,Quads= 87 140 0 AFLR4 : Generate optimal mesh on surface definition 5 AFLR2 : Nodes, Trias,Quads= 313 548 0 AFLR4 : Nodes, Trias,Quads= 308 538 0 AFLR4 : Generate optimal mesh on surface definition 6 AFLR2 : Nodes, Trias,Quads= 314 550 0 AFLR4 : Nodes, Trias,Quads= 308 538 0 AFLR4 : Generate optimal mesh on surface definition 7 AFLR2 : Nodes, Trias,Quads= 310 542 0 AFLR4 : Nodes, Trias,Quads= 308 538 0 AFLR4 : Generate optimal mesh on surface definition 8 AFLR2 : Nodes, Trias,Quads= 314 550 0 AFLR4 : Nodes, Trias,Quads= 308 538 0 DGEOM : Add surface definitions to composite definition 0 DGEOM : Glue composite surface definition 0 DGEOM : Nodes,Faces,BEdges= 1591 3174 428 OVERALL : CPU Time = 0.114 seconds Body 1 (of 2) Number of nodes = 372 Number of elements = 740 Number of triangle elements = 740 Number of quadrilateral elements = 0 Body 2 (of 2) Number of nodes = 1219 Number of elements = 2434 Number of triangle elements = 2434 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 1591 Total number of elements = 3174 . Analysis object with the name, aflr4AIM, has already been initilized An altName of aflr4AIM_6 will be used! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = torus, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : EGADS CAD Geometry Setup EGADS : Model has 2 Active Bodies EGADS : Body 0 is a SolidBody EGADS : Body 0 has 1 Shells EGADS : Body 0 has 1 Faces EGADS : Body 0 has 2 Edges EGADS : Body 0 has 1 Loops EGADS : Body 0 has 1 Nodes EGADS : Body 1 is a SolidBody EGADS : Body 1 has 1 Shells EGADS : Body 1 has 6 Faces EGADS : Body 1 has 12 Edges EGADS : Body 1 has 6 Loops EGADS : Body 1 has 8 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 EGADS : 2 Yes 1 0 1 NA NA 4 5 6 7 EGADS : 3 Yes 1 0 1 NA NA 4 5 6 7 EGADS : 4 Yes 1 0 1 NA NA 2 3 6 7 EGADS : 5 Yes 1 0 1 NA NA 2 3 6 7 EGADS : 6 Yes 1 0 1 NA NA 2 3 4 5 EGADS : 7 Yes 1 0 1 NA NA 2 3 4 5 EGADS : Face Edges Information EGADS : Face Edges EGADS : 1 -1 2 1 -2 EGADS : 2 3 4 -5 -6 EGADS : 3 -7 10 9 -8 EGADS : 4 11 7 -12 -3 EGADS : 5 -13 5 14 -9 EGADS : 6 6 13 -10 -11 EGADS : 7 -4 12 8 -14 EGADS : Face Loops Information EGADS : Face Loops EGADS : 1 1 EGADS : 2 2 EGADS : 3 3 EGADS : 4 4 EGADS : 5 5 EGADS : 6 6 EGADS : 7 7 EGADS : Loop Edges Information EGADS : Loop Active Edges EGADS : 1 Yes -1 2 1 -2 EGADS : 2 Yes 3 4 -5 -6 EGADS : 3 Yes -7 10 9 -8 EGADS : 4 Yes 11 7 -12 -3 EGADS : 5 Yes -13 5 14 -9 EGADS : 6 Yes 6 13 -10 -11 EGADS : 7 Yes -4 12 8 -14 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 1 1 1 1 1 EGADS : 2 0 Yes 1 1 1 1 1 EGADS : 3 1 Yes 3 2 NA 2 4 EGADS : 4 1 Yes 2 4 NA 2 7 EGADS : 5 1 Yes 5 4 NA 2 5 EGADS : 6 1 Yes 3 5 NA 2 6 EGADS : 7 1 Yes 7 6 NA 3 4 EGADS : 8 1 Yes 6 8 NA 3 7 EGADS : 9 1 Yes 9 8 NA 3 5 EGADS : 10 1 Yes 7 9 NA 3 6 EGADS : 11 1 Yes 3 7 NA 4 6 EGADS : 12 1 Yes 2 6 NA 4 7 EGADS : 13 1 Yes 5 9 NA 5 6 EGADS : 14 1 Yes 4 8 NA 5 7 EGADS : Node Information EGADS : Node Active Coordinates EGADS : 1 Yes 7.25 0 0 EGADS : 2 Yes 0 0 2 EGADS : 3 Yes 0 0 0 EGADS : 4 Yes 0 2 2 EGADS : 5 Yes 0 2 0 EGADS : 6 Yes 14 0 2 EGADS : 7 Yes 14 0 0 EGADS : 8 Yes 14 2 2 EGADS : 9 Yes 14 2 0 EGADS : Face and Edge Match Information EGADS : No Face Matches Found AFLR4 : Surface Mesh Spacing Setup AFLR4 : Max Bounding Box Length = 15 AFLR4 : Min Bounding Box Length = 4 AFLR4 : Max Ref Bounding Box Length = 1.5 AFLR4 : Min Ref Bounding Box Length = 0.5 AFLR4 : Reference Length = 1 AFLR4 : BL Thickness = 0 AFLR4 : FarField Spacing = 0.5 AFLR4 : Abs Min Surf Spacing = 0.0025 AFLR4 : Min Surf Spacing = 0.1 AFLR4 : Max Surf Spacing = 0.5 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 FARFIELD AFLR4 : 3 CAD geometry 0 FARFIELD AFLR4 : 4 CAD geometry 0 FARFIELD AFLR4 : 5 CAD geometry 0 FARFIELD AFLR4 : 6 CAD geometry 0 FARFIELD AFLR4 : 7 CAD geometry 0 FARFIELD 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 : Surface Grid Generation AFLR4 : Generate optimal mesh on surface definition 1 AFLR2 : Nodes, Trias,Quads= 919 1710 0 AFLR4 : Nodes, Trias,Quads= 675 1222 0 AFLR4 : Generate optimal mesh on surface definition 2 AFLR2 : Nodes, Trias,Quads= 92 150 0 AFLR4 : Nodes, Trias,Quads= 88 142 0 AFLR4 : Generate optimal mesh on surface definition 3 AFLR2 : Nodes, Trias,Quads= 92 150 0 AFLR4 : Nodes, Trias,Quads= 87 140 0 AFLR4 : Generate optimal mesh on surface definition 4 AFLR2 : Nodes, Trias,Quads= 312 546 0 AFLR4 : Nodes, Trias,Quads= 308 538 0 AFLR4 : Generate optimal mesh on surface definition 5 AFLR2 : Nodes, Trias,Quads= 312 546 0 AFLR4 : Nodes, Trias,Quads= 308 538 0 AFLR4 : Generate optimal mesh on surface definition 6 AFLR2 : Nodes, Trias,Quads= 311 544 0 AFLR4 : Nodes, Trias,Quads= 308 538 0 AFLR4 : Generate optimal mesh on surface definition 7 AFLR2 : Nodes, Trias,Quads= 311 544 0 AFLR4 : Nodes, Trias,Quads= 308 538 0 DGEOM : Add surface definitions to composite definition 0 DGEOM : Glue composite surface definition 0 DGEOM : Nodes,Faces,BEdges= 1830 3656 494 AFLR4 : Curvature BG Surface Grid Generation AFLR4 : Nodes, Faces = 1830 3656 AFLR4 : Surface Grid Generation AFLR4 : Generate optimal mesh on surface definition 1 AFLR2 : Nodes, Trias,Quads= 930 1730 0 AFLR4 : Nodes, Trias,Quads= 728 1326 0 AFLR4 : Generate optimal mesh on surface definition 2 AFLR2 : Nodes, Trias,Quads= 91 148 0 AFLR4 : Nodes, Trias,Quads= 88 142 0 AFLR4 : Generate optimal mesh on surface definition 3 AFLR2 : Nodes, Trias,Quads= 92 150 0 AFLR4 : Nodes, Trias,Quads= 87 140 0 AFLR4 : Generate optimal mesh on surface definition 4 AFLR2 : Nodes, Trias,Quads= 313 548 0 AFLR4 : Nodes, Trias,Quads= 308 538 0 AFLR4 : Generate optimal mesh on surface definition 5 AFLR2 : Nodes, Trias,Quads= 314 550 0 AFLR4 : Nodes, Trias,Quads= 308 538 0 AFLR4 : Generate optimal mesh on surface definition 6 AFLR2 : Nodes, Trias,Quads= 310 542 0 AFLR4 : Nodes, Trias,Quads= 308 538 0 AFLR4 : Generate optimal mesh on surface definition 7 AFLR2 : Nodes, Trias,Quads= 314 550 0 AFLR4 : Nodes, Trias,Quads= 308 538 0 DGEOM : Add surface definitions to composite definition 0 DGEOM : Glue composite surface definition 0 DGEOM : Nodes,Faces,BEdges= 1882 3760 496 OVERALL : CPU Time = 0.143 seconds Body 1 (of 2) Number of nodes = 663 Number of elements = 1326 Number of triangle elements = 1326 Number of quadrilateral elements = 0 Body 2 (of 2) Number of nodes = 1219 Number of elements = 2434 Number of triangle elements = 2434 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 1882 Total number of elements = 3760 .No analysis directory provided - defaulting to altName Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Rib_Root, index = 1 Name = Skin, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting surface mesh for body 1 (of 2) Getting surface mesh for body 2 (of 2) Body 1 (of 2) Number of nodes = 1 Number of elements = 0 Number of triangle elements = 0 Number of quadrilateral elements = 0 Body 2 (of 2) Number of nodes = 46 Number of elements = 44 Number of triangle elements = 0 Number of quadrilateral elements = 44 ---------------------------- Total number of nodes = 47 Total number of elements = 44 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_Point, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 1 Name = Skin_Top, index = 1 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 1 Name = Rib_Root, index = 1 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 = Rib_Root, index = 1 Name = Skin, index = 2 Name = Wing, index = 3 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Rib_Root, index = 1 Name = Skin, index = 2 Name = Wing, index = 3 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 1 Number of elements = 1 Elemental Nodes = 1 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 0 Setting FEA Data Mesh for body = 1 Number of nodal coordinates = 46 Number of elements = 44 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 44 Combining multiple FEA meshes! Combined Number of nodal coordinates = 47 Combined Number of elements = 45 Combined Elemental Nodes = 1 Combined Elemental Rods = 0 Combined Elemental Tria3 = 0 Combined Elemental Quad4 = 44 Getting vortex lattice surface data VLM surface name - Skin_Top Done getting vortex lattice surface data Getting FEA vortex lattice mesh Surface 1: Number of points found for aero-spline = 3 Surface 2: Number of points found for aero-spline = 6 (Re-)Combining all aerodynamic surfaces into a 'Wing', 'Canard', and/or 'Fin' single surfaces ! Aero_Reference value is NULL - No aero reference parameters set Getting FEA materials....... Number of materials - 1 Material name - Unobtainium No "materialType" specified for Material tuple Unobtainium, defaulting to "Isotropic" Done getting FEA materials Getting FEA properties....... Number of properties - 2 Property name - Rib_Root No "material" specified for Property tuple Rib_Root, defaulting to an index of 1 Property name - Skin No "material" specified for Property tuple Skin, defaulting to an index of 1 Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - ribConstraint No "constraintType" specified for Constraint tuple ribConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Getting FEA supports....... Number of supports - 1 Support name - ribSupport Done getting FEA supports Getting FEA connections....... Number of connection tuples - 1 Connection name - Rib_Root No "groupName" specified for Connection tuple Rib_Root! Looking for automatic connections from the use of capsConnectLink for Rib_Root 8 automatic connections were made for capsConnect Rib_Root (node id 1) Done getting FEA connections Load tuple is NULL - No loads applied 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 Getting FEA analyses....... Number of analyses - 1 Analysis name - Trim1 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 connection cards - appending mesh file Writing Astros instruction file.... Writing aeros card Writing analysis cards Writing constraint cards--each subcase individually Writing support cards Writing material cards Writing property cards Writing aeroelastic cards Running Astros...... Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG IEEE_DENORMAL Done running Astros! .No analysis directory provided - defaulting to altName Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting surface mesh for body 1 (of 1) Body 1 (of 1) Number of nodes = 25 Number of elements = 16 Number of triangle elements = 0 Number of quadrilateral elements = 16 ---------------------------- Total number of nodes = 25 Total number of elements = 16 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 = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 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 = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 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 - 1 Property name - plate 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 - appliedPressure 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 .... 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 IEEE_DENORMAL Done running Astros! 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 - 1 Property name - plate 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 - appliedPressure 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 large 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 IEEE_DENORMAL Done running Astros! 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 - 1 Property name - plate 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 - appliedPressure 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 IEEE_DENORMAL Done running Astros! .Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 5 Name = Wing, index = 1 Name = hTail, index = 2 Name = vTail, index = 3 Name = VTail1, index = 4 Name = VTail2, index = 5 Getting vortex lattice surface data VLM surface name - Wing Done getting vortex lattice surface data Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 5 Name = Wing, index = 1 Name = hTail, index = 2 Name = vTail, index = 3 Name = VTail1, index = 4 Name = VTail2, index = 5 Getting vortex lattice surface data VLM surface name - Wing Done getting vortex lattice surface data Writing surface - Wing (ID = 0) Section 1 of 4 (ID = 3) Section 2 of 4 (ID = 2) Section 3 of 4 (ID = 1) Section 4 of 4 (ID = 0) Writing mass properties file: caps.mass Parsing MassProp Writing mass properties file: caps.mass Parsing MassProp Writing mass properties file: caps.mass Parsing MassProp Writing mass properties file: caps.mass Parsing MassProp Writing mass properties file: caps.mass Parsing MassProp Writing mass properties file: caps.mass Parsing MassProp . Analysis object with the name, avlAIM, has already been initilized An altName of avlAIM_1 will be used! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 5 Name = Wing, index = 1 Name = hTail, index = 2 Name = vTail, index = 3 Name = VTail1, index = 4 Name = VTail2, index = 5 Getting vortex lattice surface data VLM surface name - Wing Done getting vortex lattice surface data Writing surface - Wing (ID = 0) Section 1 of 4 (ID = 3) Section 2 of 4 (ID = 2) Section 3 of 4 (ID = 1) Section 4 of 4 (ID = 0) Running avl...... Running avl...... Running avl...... . Analysis object with the name, avlAIM, has already been initilized An altName of avlAIM_2 will be used! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 5 Name = Wing, index = 1 Name = hTail, index = 2 Name = vTail, index = 3 Name = VTail1, index = 4 Name = VTail2, index = 5 Getting vortex lattice surface data VLM surface name - Wing Done getting vortex lattice surface data Writing surface - Wing (ID = 0) Section 1 of 4 (ID = 3) Section 2 of 4 (ID = 2) Section 3 of 4 (ID = 1) Section 4 of 4 (ID = 0) Running avl...... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 5 Name = Wing, index = 1 Name = hTail, index = 2 Name = vTail, index = 3 Name = VTail1, index = 4 Name = VTail2, index = 5 Getting vortex lattice surface data VLM surface name - Wing Done getting vortex lattice surface data Writing surface - Wing (ID = 0) Section 1 of 4 (ID = 3) Section 2 of 4 (ID = 2) Section 3 of 4 (ID = 1) Section 4 of 4 (ID = 0) Running avl...... . Analysis object with the name, avlAIM, has already been initilized An altName of avlAIM_3 will be used! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 5 Name = Wing, index = 1 Name = hTail, index = 2 Name = vTail, index = 3 Name = VTail1, index = 4 Name = VTail2, index = 5 Getting vortex lattice surface data VLM surface name - Wing Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 5 Name = Wing, index = 1 Name = hTail, index = 2 Name = vTail, index = 3 Name = VTail1, index = 4 Name = VTail2, index = 5 Getting vortex lattice surface data VLM surface name - Wing . Analysis object with the name, avlAIM, has already been initilized An altName of avlAIM_4 will be used! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 5 Name = Wing, index = 1 Name = hTail, index = 2 Name = vTail, index = 3 Name = VTail1, index = 4 Name = VTail2, index = 5 Getting vortex lattice surface data VLM surface name - VTail1 No "groupName" variable provided or no matches found, going to use tuple name VLM surface name - VTail2 No "groupName" variable provided or no matches found, going to use tuple name VLM surface name - Wing Done getting vortex lattice surface data Writing surface - VTail1 (ID = 0) Section 1 of 2 (ID = 1) Section 2 of 2 (ID = 0) Writing surface - VTail2 (ID = 1) Section 1 of 2 (ID = 0) Section 2 of 2 (ID = 1) Writing surface - Wing (ID = 2) Section 1 of 4 (ID = 3) Section 2 of 4 (ID = 2) Section 3 of 4 (ID = 1) Section 4 of 4 (ID = 0) Running avl...... . Analysis object with the name, avlAIM, has already been initilized An altName of avlAIM_5 will be used! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 5 Name = Wing, index = 1 Name = hTail, index = 2 Name = vTail, index = 3 Name = VTail1, index = 4 Name = VTail2, index = 5 Getting vortex lattice surface data VLM surface name - Wing VLM surface name - hTail VLM surface name - vTail No "groupName" variable provided or no matches found, going to use tuple name Done getting vortex lattice surface data Writing surface - Wing (ID = 0) Section 1 of 4 (ID = 3) Section 2 of 4 (ID = 2) Section 3 of 4 (ID = 1) Section 4 of 4 (ID = 0) Writing surface - hTail (ID = 1) Section 1 of 3 (ID = 2) Section 2 of 3 (ID = 1) Section 3 of 3 (ID = 0) Writing surface - vTail (ID = 2) Section 1 of 2 (ID = 0) Section 2 of 2 (ID = 1) Running avl...... .Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Getting mesh sizing parameters Mesh sizing name - Farfield Done getting mesh sizing parameters Getting surface mesh for body 1 (of 3) Getting surface mesh for body 2 (of 3) Getting surface mesh for body 3 (of 3) Body 1 (of 3) Number of nodes = 9618 Number of elements = 19232 Number of triangle elements = 19232 Number of quadrilateral elements = 0 Body 2 (of 3) Number of nodes = 6142 Number of elements = 12280 Number of triangle elements = 12280 Number of quadrilateral elements = 0 Body 3 (of 3) Number of nodes = 123 Number of elements = 242 Number of triangle elements = 242 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 15883 Total number of elements = 31754 .Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Getting mesh sizing parameters Mesh sizing name - Farfield Done getting mesh sizing parameters Getting surface mesh for body 1 (of 1) Body 1 (of 1) Number of nodes = 9601 Number of elements = 19194 Number of triangle elements = 19194 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 9601 Total number of elements = 19194 .ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62031) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 8 Name = box, index = 1 Name = cylinder, index = 2 Name = cone, index = 3 Name = torus, index = 4 Name = sphere, index = 5 Name = boxhole, index = 6 Name = bullet, index = 7 Name = farfield, index = 8 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting surface mesh for body 1 (of 8) Getting surface mesh for body 2 (of 8) Getting surface mesh for body 3 (of 8) Getting surface mesh for body 4 (of 8) Getting surface mesh for body 5 (of 8) Getting surface mesh for body 6 (of 8) 70000F631000 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1! 70000F631000 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1! 111FFCE00 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1! 111FFCE00 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 4 7, sen = 1! Getting surface mesh for body 7 (of 8) Getting surface mesh for body 8 (of 8) Body 1 (of 8) Number of nodes = 1538 Number of elements = 3072 Number of triangle elements = 3072 Number of quadrilateral elements = 0 Body 2 (of 8) Number of nodes = 906 Number of elements = 1808 Number of triangle elements = 1808 Number of quadrilateral elements = 0 Body 3 (of 8) Number of nodes = 1332 Number of elements = 2660 Number of triangle elements = 2660 Number of quadrilateral elements = 0 Body 4 (of 8) Number of nodes = 2048 Number of elements = 4096 Number of triangle elements = 4096 Number of quadrilateral elements = 0 Body 5 (of 8) Number of nodes = 824 Number of elements = 1644 Number of triangle elements = 1644 Number of quadrilateral elements = 0 Body 6 (of 8) Number of nodes = 1958 Number of elements = 3916 Number of triangle elements = 3916 Number of quadrilateral elements = 0 Body 7 (of 8) Number of nodes = 946 Number of elements = 1888 Number of triangle elements = 1888 Number of quadrilateral elements = 0 Body 8 (of 8) Number of nodes = 73730 Number of elements = 147456 Number of triangle elements = 147456 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 83282 Total number of elements = 166540 . Analysis object with the name, egadsTessAIM, has already been initilized An altName of egadsTessAIM_1 will be used! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting surface mesh for body 1 (of 2) Getting surface mesh for body 2 (of 2) Body 1 (of 2) Number of nodes = 1538 Number of elements = 3072 Number of triangle elements = 3072 Number of quadrilateral elements = 0 Body 2 (of 2) Number of nodes = 73730 Number of elements = 147456 Number of triangle elements = 147456 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 75268 Total number of elements = 150528 . Analysis object with the name, egadsTessAIM, has already been initilized An altName of egadsTessAIM_2 will be used! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = boxhole, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting surface mesh for body 1 (of 2) 70000F631000 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1! 70000F631000 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1! 111FFCE00 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1! 111FFCE00 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 4 7, sen = 1! Getting surface mesh for body 2 (of 2) Body 1 (of 2) Number of nodes = 1958 Number of elements = 3916 Number of triangle elements = 3916 Number of quadrilateral elements = 0 Body 2 (of 2) Number of nodes = 73730 Number of elements = 147456 Number of triangle elements = 147456 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 75688 Total number of elements = 151372 . Analysis object with the name, egadsTessAIM, has already been initilized An altName of egadsTessAIM_3 will be used! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = bullet, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting surface mesh for body 1 (of 2) Getting surface mesh for body 2 (of 2) Body 1 (of 2) Number of nodes = 946 Number of elements = 1888 Number of triangle elements = 1888 Number of quadrilateral elements = 0 Body 2 (of 2) Number of nodes = 73730 Number of elements = 147456 Number of triangle elements = 147456 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 74676 Total number of elements = 149344 . Analysis object with the name, egadsTessAIM, has already been initilized An altName of egadsTessAIM_4 will be used! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = cone, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting surface mesh for body 1 (of 2) Getting surface mesh for body 2 (of 2) Body 1 (of 2) Number of nodes = 1332 Number of elements = 2660 Number of triangle elements = 2660 Number of quadrilateral elements = 0 Body 2 (of 2) Number of nodes = 73730 Number of elements = 147456 Number of triangle elements = 147456 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 75062 Total number of elements = 150116 . Analysis object with the name, egadsTessAIM, has already been initilized An altName of egadsTessAIM_5 will be used! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = cylinder, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting surface mesh for body 1 (of 2) Getting surface mesh for body 2 (of 2) Body 1 (of 2) Number of nodes = 906 Number of elements = 1808 Number of triangle elements = 1808 Number of quadrilateral elements = 0 Body 2 (of 2) Number of nodes = 73730 Number of elements = 147456 Number of triangle elements = 147456 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 74636 Total number of elements = 149264 .Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 .Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Getting mesh sizing parameters Mesh sizing name - Farfield Done getting mesh sizing parameters Getting surface mesh for body 1 (of 1) Body 1 (of 1) Number of nodes = 9601 Number of elements = 19194 Number of triangle elements = 19194 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 9601 Total number of elements = 19194 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Getting mesh sizing parameters Mesh sizing name - Farfield Done getting mesh sizing parameters Getting surface mesh for body 1 (of 1) Body 1 (of 1) Number of nodes = 7173 Number of elements = 14338 Number of triangle elements = 14338 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 7173 Total number of elements = 14338 . EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! . Analysis object with the name, egadsTessAIM, has already been initilized An altName of egadsTessAIM_6 will be used! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = sphere, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting surface mesh for body 1 (of 2) Getting surface mesh for body 2 (of 2) Body 1 (of 2) Number of nodes = 824 Number of elements = 1644 Number of triangle elements = 1644 Number of quadrilateral elements = 0 Body 2 (of 2) Number of nodes = 73730 Number of elements = 147456 Number of triangle elements = 147456 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 74554 Total number of elements = 149100 . Analysis object with the name, egadsTessAIM, has already been initilized An altName of egadsTessAIM_7 will be used! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = torus, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting surface mesh for body 1 (of 2) Getting surface mesh for body 2 (of 2) Body 1 (of 2) Number of nodes = 2048 Number of elements = 4096 Number of triangle elements = 4096 Number of quadrilateral elements = 0 Body 2 (of 2) Number of nodes = 73730 Number of elements = 147456 Number of triangle elements = 147456 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 75778 Total number of elements = 151552 .Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Getting mesh sizing parameters Mesh sizing name - Farfield Done getting mesh sizing parameters Getting surface mesh for body 1 (of 3) Getting surface mesh for body 2 (of 3) Getting surface mesh for body 3 (of 3) Body 1 (of 3) Number of nodes = 7820 Number of elements = 15636 Number of triangle elements = 15636 Number of quadrilateral elements = 0 Body 2 (of 3) Number of nodes = 5889 Number of elements = 11774 Number of triangle elements = 11774 Number of quadrilateral elements = 0 Body 3 (of 3) Number of nodes = 524 Number of elements = 1044 Number of triangle elements = 1044 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 14233 Total number of elements = 28454 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Number of surface: nodes - 14233, elements - 28454 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000T1.00e-16A Delaunizing vertices... Delaunay seconds: 0.251537 Creating surface mesh ... Surface mesh seconds: 0.051958 Recovering boundaries... Boundary recovery seconds: 0.15309 Removing exterior tetrahedra ... Spreading region attributes. Exterior tets removal seconds: 0.072203 Recovering Delaunayness... Delaunay recovery seconds: 0.084059 Refining mesh... 18972 insertions, added 13254 points, 701278 tetrahedra in queue. 6317 insertions, added 2883 points, 614952 tetrahedra in queue. 8421 insertions, added 2047 points, 103425 tetrahedra in queue. Refinement seconds: 3.32272 Smoothing vertices... Mesh smoothing seconds: 3.23018 Improving mesh... Mesh improvement seconds: 0.06842 Writing nodes. Writing elements. Writing faces. Writing edges. Output seconds: 0.022506 Total running seconds: 7.25749 Statistics: Input points: 14233 Input facets: 28454 Input segments: 42681 Input holes: 2 Input regions: 0 Mesh points: 33078 Mesh tetrahedra: 159812 Mesh faces: 333851 Mesh faces on exterior boundary: 28454 Mesh faces on input facets: 28454 Mesh edges on input segments: 42681 Steiner points inside domain: 18845 Done meshing using TetGen! Analysis object with the name, fun3dAIM, has already been initilized An altName of fun3dAIM_1 will be used! Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - Wing2 Done getting CFD boundary conditions Writing MAPBC file .... Finished writing MAPBC file Using Python to write FUN3D namelist (fun3d.nml) Reading /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/CAPS/legacy/aim/pyCAPS/__main__/Scratch/workDir_fun3dTest4_fun3dAIM/fun3d.nml ..... Appending namelist Done writing nml file with Python Info: No recognized data transfer names found. . Analysis object with the name, fun3dAIM, has already been initilized An altName of fun3dAIM_2 will be used! Getting CFD boundary conditions Boundary condition name - Wing1 Warning: No boundary condition specified for capsGroup Wing2! Warning: No boundary condition specified for capsGroup Farfield! Done getting CFD boundary conditions Writing MAPBC file .... Finished writing MAPBC file Using Python to write FUN3D namelist (fun3d.nml) Reading /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/CAPS/legacy/aim/pyCAPS/__main__/Scratch/workDir_fun3dTest5_fun3dAIM/fun3d.nml ..... Traceback (most recent call last): Error: Python error occurred while writing namelist file File "/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/venv/lib/python3.11/site-packages/f90nml/parser.py", line 378, in _readstream self._update_tokens() File "/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/venv/lib/python3.11/site-packages/f90nml/parser.py", line 797, in _update_tokens next_token = next(self.tokens) ^^^^^^^^^^^^^^^^^ StopIteration During handling of the above exception, another exception occurred: Traceback (most recent call last): File "fun3dNamelist.pyx", line 103, in fun3dNamelist.fun3d_writeNMLPython File "fun3dNamelist.pyx", line 65, in fun3dNamelist.read_fun3d_nml File "/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/venv/lib/python3.11/site-packages/f90nml/__init__.py", line 31, in read return parser.read(nml_path) ^^^^^^^^^^^^^^^^^^^^^ File "/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/venv/lib/python3.11/site-packages/f90nml/parser.py", line 281, in read return self._readstream(nml_file, nml_patch) ^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^ File "/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/venv/lib/python3.11/site-packages/f90nml/parser.py", line 380, in _readstream raise ValueError( ValueError: End-of-file before end of namelist group: '&badNamelist' . Analysis object with the name, fun3dAIM, has already been initilized An altName of fun3dAIM_3 will be used! Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - Wing2 Done getting CFD boundary conditions Writing MAPBC file .... Finished writing MAPBC file Using Python to write FUN3D namelist (fun3d.nml) /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/CAPS/legacy/aim/pyCAPS/__main__/Scratch/workDir_fun3dTest6_fun3dAIM/fun3d.nml not found! Creating namelist Done writing nml file with Python Info: No recognized data transfer names found. Writing MAPBC file .... Finished writing MAPBC file Using Python to write FUN3D namelist (fun3d.nml) Reading /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/CAPS/legacy/aim/pyCAPS/__main__/Scratch/workDir_fun3dTest6_fun3dAIM/fun3d.nml ..... Appending namelist Done writing nml file with Python Info: No recognized data transfer names found. . Analysis object with the name, fun3dAIM, has already been initilized An altName of fun3dAIM_4 will be used! Getting CFD boundary conditions Boundary condition name - Wing1 . Analysis object with the name, fun3dAIM, has already been initilized An altName of fun3dAIM_5 will be used! Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - X . Analysis object with the name, fun3dAIM, has already been initilized An altName of fun3dAIM_6 will be used! Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - Wing2 Done getting CFD boundary conditions Python library was linked, but will not be used! Writing MAPBC file .... Finished writing MAPBC file Since Python was not linked and/or being used, the "Overwrite_NML" input needs to be set to "True" to give permission to create a new fun3d.nml. fun3d.nml will NOT be updated!! Info: No recognized data transfer names found. .Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - Wing2 Done getting CFD boundary conditions Python library was linked, but will not be used! Writing MAPBC file .... Finished writing MAPBC file Warning: The fun3d.nml file will be overwritten! Writing fun3d.nml Info: No recognized data transfer names found. Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - Wing2 Done getting CFD boundary conditions Python library was linked, but will not be used! Writing MAPBC file .... Finished writing MAPBC file Warning: The fun3d.nml file will be overwritten! Writing fun3d.nml Info: No recognized data transfer names found. . Analysis object with the name, fun3dAIM, has already been initilized An altName of fun3dAIM_7 will be used! Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - Wing2 Done getting CFD boundary conditions Getting CFD design variables....... Number of design variables - 1 Design Variable name - Alpha Done getting CFD design variables Getting CFD functional....... Number of design variables - 1 Objective name - LoD Done getting CFD functional Python library was linked, but will not be used! Creating FUN3D directory tree Writing rubber.data Writing MAPBC file .... Finished writing MAPBC file Since Python was not linked and/or being used, the "Overwrite_NML" input needs to be set to "True" to give permission to create a new fun3d.nml. fun3d.nml will NOT be updated!! Info: No recognized data transfer names found. Reading rubber.data .Closing fun3d!!!! No analysis directory provided - defaulting to altName 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 = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = box1, index = 1 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 2168 Number of elements = 2166 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 2166 Getting FEA materials....... Number of materials - 2 Material name - madeupium Material name - unobtainium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - box1 Done getting FEA properties Updating mesh element types based on properties input .No analysis directory provided - defaulting to altName 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 = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = box1, index = 1 Face 3 TFI quading disabled with attribute .qParams Face 6 TFI quading disabled with attribute .qParams Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 4009 Number of elements = 6570 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 5126 Elemental Quad4 = 1444 Getting FEA materials....... Number of materials - 2 Material name - madeupium Material name - unobtainium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - box1 Done getting FEA properties Updating mesh element types based on properties input .No analysis directory provided - defaulting to altName 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 = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box1, index = 1 Name = box2, index = 2 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 2168 Number of elements = 2166 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 2166 Getting FEA materials....... Number of materials - 2 Material name - madeupium Material name - unobtainium Done getting FEA materials Getting FEA properties....... Number of properties - 2 Property name - box1 Property name - box2 Done getting FEA properties Updating mesh element types based on properties input .No analysis directory provided - defaulting to altName 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 = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = box1, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 400 Number of elements = 361 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 361 Getting FEA materials....... Number of materials - 2 Material name - madeupium Material name - unobtainium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - box1 Done getting FEA properties Updating mesh element types based on properties input .ssssssssss EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Getting mesh sizing parameters Mesh sizing name - Farfield Done getting mesh sizing parameters Getting surface mesh for body 1 (of 3) Getting surface mesh for body 2 (of 3) Getting surface mesh for body 3 (of 3) Body 1 (of 3) Number of nodes = 7820 Number of elements = 15636 Number of triangle elements = 15636 Number of quadrilateral elements = 0 Body 2 (of 3) Number of nodes = 5889 Number of elements = 11774 Number of triangle elements = 11774 Number of quadrilateral elements = 0 Body 3 (of 3) Number of nodes = 524 Number of elements = 1044 Number of triangle elements = 1044 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 14233 Total number of elements = 28454 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Number of surface: nodes - 14233, elements - 28454 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000T1.00e-16A Delaunizing vertices... Delaunay seconds: 0.24339 Creating surface mesh ... Surface mesh seconds: 0.050953 Recovering boundaries... Boundary recovery seconds: 0.154373 Removing exterior tetrahedra ... Spreading region attributes. Exterior tets removal seconds: 0.072393 Recovering Delaunayness... Delaunay recovery seconds: 0.072245 Refining mesh... 18972 insertions, added 13254 points, 701278 tetrahedra in queue. 6317 insertions, added 2883 points, 614952 tetrahedra in queue. 8421 insertions, added 2047 points, 103425 tetrahedra in queue. Refinement seconds: 3.32981 Smoothing vertices... Mesh smoothing seconds: 3.17064 Improving mesh... Mesh improvement seconds: 0.073434 Writing nodes. Writing elements. Writing faces. Writing edges. Output seconds: 0.022393 Total running seconds: 7.19047 Statistics: Input points: 14233 Input facets: 28454 Input segments: 42681 Input holes: 2 Input regions: 0 Mesh points: 33078 Mesh tetrahedra: 159812 Mesh faces: 333851 Mesh faces on exterior boundary: 28454 Mesh faces on input facets: 28454 Mesh edges on input segments: 42681 Steiner points inside domain: 18845 Done meshing using TetGen! Analysis object with the name, su2AIM, has already been initilized An altName of su2AIM_1 will be used! Writing SU2 file .... Finished writing SU2 file Getting CFD boundary conditions Boundary condition name - Wing1 . Analysis object with the name, su2AIM, has already been initilized An altName of su2AIM_2 will be used! Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - X .Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - Wing2 Done getting CFD boundary conditions Warning: The su2 cfg file will be overwritten! Write SU2 configuration file for version "Harrier (8.0.1)" Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - Wing2 Done getting CFD boundary conditions Warning: The su2 cfg file will be overwritten! Write SU2 configuration file for version "Harrier (8.0.1)" . Running xFoil...... . Running xFoil...... . Running xFoil...... . Running xFoil...... . Running xFoil...... . Running xFoil...... . Running xFoil...... Running xFoil...... . ---------------------------------------------------------------------- Ran 67 tests in 89.596s OK (skipped=10) WARNING: 'capsProblem.loadCAPS' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsGeometry.__init__' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsProblem.setVerbosity' is deprecated. Please use 'Problem.setOutLevel'! WARNING: 'capsProblem.loadAIM' is deprecated. Please use 'Problem.analysis.create'! WARNING: 'capsAnalysis.__init__' is deprecated. Please use 'Problem.analysis.create'! WARNING: 'capsAnalysis.setAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'! WARNING: 'capsAnalysis.getAnalysisOutVal' is deprecated. Please use 'Analysis.output["varname"].value'! WARNING: 'capsProblem.__init__' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsAnalysis.aimName' is deprecated. Please use 'name'! WARNING: 'capsAnalysis.getAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'! WARNING: 'capsGeometry.getGeometryVal' is deprecated. Please use 'Problem.geometry.despmtr["varname"].value'! WARNING: 'capsGeometry.setGeometryVal' is deprecated. Please use 'Problem.geometry.despmtr["varname"].value'! Legacy AIM unit testing done! (cd test; ./runUnitTest.sh) EGADS Info: 0 Objects, 0 Reference in Use (of 84) at Close! EGADS Info: 0 Objects, 0 Reference in Use (of 84) at Close! EGADS Info: 0 Objects, 0 Reference in Use (of 84) at Close! EGADS Info: 0 Objects, 0 Reference in Use (of 84) at Close! EGADS Info: 0 Objects, 0 Reference in Use (of 84) at Close! EGADS Info: 0 Objects, 0 Reference in Use (of 84) at Close! EGADS Info: 0 Objects, 0 Reference in Use (of 84) at Close! EGADS Info: 0 Objects, 0 Reference in Use (of 84) at Close! EGADS Info: 0 Objects, 0 Reference in Use (of 84) at Close! EGADS Info: 0 Objects, 0 Reference in Use (of 84) at Close! EGADS Info: 0 Objects, 0 Reference in Use (of 84) at Close! EGADS Info: 0 Objects, 0 Reference in Use (of 84) at Close! EGADS Info: 0 Objects, 0 Reference in Use (of 84) at Close! EGADS Info: 0 Objects, 0 Reference in Use (of 84) at Close! EGADS Info: 0 Objects, 0 Reference in Use (of 84) at Close! EGADS Info: 0 Objects, 0 Reference in Use (of 84) at Close! EGADS Info: 0 Objects, 0 Reference in Use (of 84) at Close! EGADS Info: 0 Objects, 0 Reference in Use (of 84) at Close! aimTransferUtil Tests passed! real 0m0.190s user 0m0.046s sys 0m0.014s ============================================= CAPS test (using c-executables) case /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/test/aimTransferUtilTest passed (as expected) ============================================= + expectCSuccess /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/test/miscUtilsTest + /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/test/miscUtilsTest Error in convert_doubleToString: Input fieldWidth of 1 must be greater than 1 for the input value 0.000000E+00 Returning a 'NaN' string. Error in convert_doubleToString: Input fieldWidth of -2 must be greater than 1 for the input value 9.000000E+00 Returning a 'NaN' string. Error in convert_doubleToString: Input fieldWidth of 0 must be greater than 1 for the input value 9.000000E+00 Returning a 'NaN' string. Error in convert_doubleToString: Cannot write -1.000000E+100 with field with 7! Returning a 'NaN' string. Error in convert_doubleToString: Cannot write -9.900000E+99 with field with 7! Returning a 'NaN' string. Error in convert_doubleToString: Input fieldWidth of 2 must be greater than 2 for the input value -1.000000E+00 Returning a 'NaN' string. Error in convert_doubleToString: Input fieldWidth of 1 must be greater than 1 for the input value 1.000000E+00 Returning a 'NaN' string. Error in convert_integerToString: Input 9999999 fails with requested fieldWidth of 6 Returning a 'NaN' string. Error in convert_integerToString: Input -999999 fails with requested fieldWidth of 6 Returning a 'NaN' string. Error in convert_integerToString: fieldWidth > 15 not verified Returning a 'NaN' string. Error in convert_integerToString: fieldWidth <= 0 Returning a 'NaN' string. Error in convert_integerToString: fieldWidth <= 0 Returning a 'NaN' string. miscUtils Tests passed! real 0m0.144s user 0m0.027s sys 0m0.012s + set +x + expectCSuccess /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/test/vlmUtilsTest ============================================= CAPS test (using c-executables) case /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/test/miscUtilsTest passed (as expected) ============================================= + /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/test/vlmUtilsTest vlmUtils Tests passed! real 0m0.141s user 0m0.027s sys 0m0.012s + set +x + rm -rf aimTest ============================================= CAPS test (using c-executables) case /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/test/vlmUtilsTest passed (as expected) ============================================= + expectCSuccess '/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/test/aim testingAIM.csm' + /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/test/aim testingAIM.csm Root Path = /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/CAPS/test/aimTest/Scratch testingAIM/aimInitialize instance = -1 unitSys = (null)! caps_queryAnalysis = 0 4 3 1 testingAIM/aimInputs instance = -1 index = 1! in 1: testingAIMin 0 testingAIM/aimInputs instance = -1 index = 2! in 2: table 0 testingAIM/aimInputs instance = -1 index = 3! in 3: tessIn 0 testingAIM/aimInputs instance = -1 index = 4! in 4: meshFile 0 testingAIM/aimOutputs instance = -1 index = 1! out 1: testingAIMout 0 testingAIM/aimOutputs instance = -1 index = 2! out 2: tessOut 0 testingAIM/aimOutputs instance = -1 index = 3! out 3: meshFile 0 testingAIM/aimInitialize instance = 0 unitSys = m! testingAIM/aimInputs instance = 0 index = 1! testingAIM/aimInputs instance = 0 index = 2! testingAIM/aimInputs instance = 0 index = 3! testingAIM/aimInputs instance = 0 index = 4! testingAIM/aimOutputs instance = 0 index = 1! testingAIM/aimOutputs instance = 0 index = 2! testingAIM/aimOutputs instance = 0 index = 3! testingAIM/aimBackdoor instance = 0: Input String! Backdoor return string = aimBackdoor Output testingAIM/aimInitialize instance = 1 unitSys = (null)! testingAIM/aimInputs instance = 1 index = 1! testingAIM/aimInputs instance = 1 index = 2! testingAIM/aimInputs instance = 1 index = 3! testingAIM/aimInputs instance = 1 index = 4! testingAIM/aimOutputs instance = 1 index = 1! testingAIM/aimOutputs instance = 1 index = 2! testingAIM/aimOutputs instance = 1 index = 3! Intent = child APath = /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/CAPS/test/aimTest/Scratch/testingAIM1 UnitSys = (null) Exec = 1 Fields = scalar (1 1) vector (3 1) scalar (1 0) vector (3 0) Dirty = 3 Problem: # Dirty Analyses = 2! Bound: # Dirty Analyses = 2! Analys0: # Dirty Analyses = 0! Analys1: # Dirty Analyses = 1! testingAIM/aimUpdateState instance = 0! tess is NULL! testingAIM/aimPreAnalysis instance = 0! testingAIM/aimPreAnalysis aim_getBounds = 0 Analysis in Bound = Interface aim_newGeometry = 0! getDiscr = 0 getDataSet = 0, rank = 1, method = 0 0 scalars! meshRef = NULL testingAIM/aimExecute instance = 0! testingAIM/aimPostAnalysis instance = 0 restart = 0! testingAIM/aimPostAnalysis: 0 -- 1 is Config Parameter After Execute on Parent Problem: # Dirty Analyses = 1! Bound: # Dirty Analyses = 1! Analys0: # Dirty Analyses = 0! Analys1: # Dirty Analyses = 0! testingAIM/aimCalcOutput instance = 0 index = 2 tessOut 0! tessPtr = 0 testingAIM/aimUpdateState instance = 1! tess is NULL! testingAIM/aimDiscr: tname = Interface, instance = 1! testingAIM/aimDiscr: Tessellation set! testingAIM/aimDiscr: Body 1/Face 3 matches Interface! testingAIM/aimDiscr: ntris = 1962! testingAIM/aimDiscr: npts = 1040! testingAIM/aimDiscr: tname = Interface, instance = 0! testingAIM/aimDiscr: Tessellation set! testingAIM/aimDiscr: Body 1/Face 6 matches Interface! testingAIM/aimDiscr: ntris = 790! testingAIM/aimDiscr: npts = 442! testingAIM/aimTransfer name = scalar instance = 0 npts = 442/1! CAPS Info: Bound 'Interface' Normalized Integrated 'scalar' Rank 0: src = 6.547926e+01, tgt = 6.547926e+01, diff = 3.844036e-11 testingAIM/aimPreAnalysis instance = 1! testingAIM/aimPreAnalysis aim_getBounds = 0 Analysis in Bound = Interface aim_newGeometry = 0! getDiscr = 0 getDataSet = -303, rank = 0, method = 0 vectors not setup yet! testingAIM/aimExecute instance = 1! testingAIM/aimPostAnalysis instance = 1 restart = 0! Dirty = 0 Problem: # Dirty Analyses = 0! Bound: # Dirty Analyses = 0! Analys0: # Dirty Analyses = 0! Analys1: # Dirty Analyses = 0! Body 1 has length units = cm Body 2 has length units = cm aimTest has type PROBLEM, subtype PARAMETRIC with 0 attributes last: aimTest macys-VM:57388 jenkins 2024/05/19 01:28:04 1 hist: (null) -> Initial Phase aimTest macys-VM:57388 jenkins 2024/05/19 01:28:04 1 2 Bodies, 2 Parameters, 6 GeomIns, 2 GeomOuts, 2 Analyses, 1 Bounds ParamName has type VALUE, subtype PARAMETER with 0 attributes last: aimTest macys-VM:57388 jenkins 2024/05/19 01:28:04 2 hist: (null) -> Starting aimTest macys-VM:57388 jenkins 2024/05/19 01:28:04 2 value = 0.000000 (null) Param has type VALUE, subtype PARAMETER with 0 attributes last: aimTest macys-VM:57388 jenkins 2024/05/19 01:28:04 3 hist: (null) -> Starting aimTest macys-VM:57388 jenkins 2024/05/19 01:28:04 3 value = 99 (null) num has type VALUE, subtype GEOMETRYIN with 0 attributes last: aimTest macys-VM:57388 jenkins 2024/05/19 01:28:04 6 hist: (null) -> Initial Phase aimTest macys-VM:57388 jenkins 2024/05/19 01:28:04 1 hist: (null) -> Starting aimTest macys-VM:57388 jenkins 2024/05/19 01:28:04 6 value = 8.000000 (null) x has type VALUE, subtype GEOMETRYIN with 0 attributes last: aimTest macys-VM:57388 jenkins 2024/05/19 01:28:04 1 hist: (null) -> Initial Phase aimTest macys-VM:57388 jenkins 2024/05/19 01:28:04 1 value (8x1) = 7.300000 8.400000 10.400000 11.300000 12.300000 13.800000 14.400000 17.200000 (null) ymin has type VALUE, subtype GEOMETRYIN with 0 attributes last: aimTest macys-VM:57388 jenkins 2024/05/19 01:28:04 1 hist: (null) -> Initial Phase aimTest macys-VM:57388 jenkins 2024/05/19 01:28:04 1 value (8x1) = -1.250000 -1.900000 -2.100000 -2.100000 -2.100000 -2.100000 -2.100000 -2.100000 (null) zmin has type VALUE, subtype GEOMETRYIN with 0 attributes last: aimTest macys-VM:57388 jenkins 2024/05/19 01:28:04 1 hist: (null) -> Initial Phase aimTest macys-VM:57388 jenkins 2024/05/19 01:28:04 1 value (8x1) = -0.825000 -0.812500 -0.800000 -0.775000 -0.750000 -0.700000 -0.690000 -0.100000 (null) zmax has type VALUE, subtype GEOMETRYIN with 0 attributes last: aimTest macys-VM:57388 jenkins 2024/05/19 01:28:04 1 hist: (null) -> Initial Phase aimTest macys-VM:57388 jenkins 2024/05/19 01:28:04 1 value (8x1) = 0.825000 0.812500 0.800000 0.775000 0.750000 0.700000 0.690000 0.100000 (null) unused has type VALUE, subtype GEOMETRYIN with 0 attributes last: aimTest macys-VM:57388 jenkins 2024/05/19 01:28:04 7 hist: (null) -> Initial Phase aimTest macys-VM:57388 jenkins 2024/05/19 01:28:04 1 hist: (null) -> Starting aimTest macys-VM:57388 jenkins 2024/05/19 01:28:04 7 linked to ParamName pVol has type VALUE, subtype GEOMETRYOUT with 0 attributes last: aimTest macys-VM:57388 jenkins 2024/05/19 01:28:04 16 hist: (null) -> Starting aimTest macys-VM:57388 jenkins 2024/05/19 01:28:04 16 value = 34.641525 (null) cVol has type VALUE, subtype GEOMETRYOUT with 0 attributes last: aimTest macys-VM:57388 jenkins 2024/05/19 01:28:04 16 hist: (null) -> Starting aimTest macys-VM:57388 jenkins 2024/05/19 01:28:04 16 value = 7.296560 (null) testingAIM0 has type ANALYSIS, subtype NONE with 0 attributes last: aimTest macys-VM:57388 jenkins 2024/05/19 01:28:04 18 hist: (null) -> Starting aimTest macys-VM:57388 jenkins 2024/05/19 01:28:04 18 4 AnalysisIns, 3 AnalysisOuts, 1 AnalysisDynOs 1 Bodies, 1 Tessellations testingAIMin has type VALUE, subtype ANALYSISIN with 0 attributes last: aimTest macys-VM:57388 jenkins 2024/05/19 01:28:04 8 hist: (null) -> Starting aimTest macys-VM:57388 jenkins 2024/05/19 01:28:04 8 value = 5.000000 cm table has type VALUE, subtype ANALYSISIN with 0 attributes last: aimTest macys-VM:57388 jenkins 2024/05/19 01:28:04 8 hist: (null) -> Starting aimTest macys-VM:57388 jenkins 2024/05/19 01:28:04 8 value (1x3) = 1: Entry1 -> Value1 2: Entry2 -> Value2 3: Entry3 -> Value3 tessIn has type VALUE, subtype ANALYSISIN with 0 attributes last: aimTest macys-VM:57388 jenkins 2024/05/19 01:28:04 8 hist: (null) -> Starting aimTest macys-VM:57388 jenkins 2024/05/19 01:28:04 8 value (0x0) = NULL with len = 0 ego meshFile has type VALUE, subtype ANALYSISIN with 0 attributes last: aimTest macys-VM:57388 jenkins 2024/05/19 01:28:04 8 hist: (null) -> Starting aimTest macys-VM:57388 jenkins 2024/05/19 01:28:04 8 value (0x0) = NULL with len = 0 meter testingAIMout has type VALUE, subtype ANALYSISOUT with 0 attributes last: aimTest macys-VM:57388 jenkins 2024/05/19 01:28:04 9 testingAIM/aimCalcOutput instance = 0 index = 1 testingAIMout 0! aim_getDiscr 0 on Interface = 0 aim_getDataSet 0 on Interface = -329 value = 12.340000 cm lazy: aimTest macys-VM:57388 jenkins 2024/05/19 01:28:24 18 tessOut has type VALUE, subtype ANALYSISOUT with 0 attributes last: aimTest macys-VM:57388 jenkins 2024/05/19 01:28:04 18 hist: (null) -> Child Execute aimTest macys-VM:57388 jenkins 2024/05/19 01:28:04 18 value (0x0) = NULL with len = 0 ego meshFile has type VALUE, subtype ANALYSISOUT with 0 attributes last: aimTest macys-VM:57388 jenkins 2024/05/19 01:28:04 9 testingAIM/aimCalcOutput instance = 0 index = 3 meshFile 0! value (0x0) = NULL with len = 0 writer lazy: aimTest macys-VM:57388 jenkins 2024/05/19 01:28:24 18 Everything has type VALUE, subtype ANALYSISDYNO with 0 attributes last: aimTest macys-VM:57388 jenkins 2024/05/19 01:28:04 18 hist: (null) -> Starting aimTest macys-VM:57388 jenkins 2024/05/19 01:28:04 18 value = 42 (null) testingAIM1 has type ANALYSIS, subtype NONE with 0 attributes last: aimTest macys-VM:57388 jenkins 2024/05/19 01:28:24 28 hist: (null) -> Starting aimTest macys-VM:57388 jenkins 2024/05/19 01:28:04 0 hist: (null) -> Child Execute aimTest macys-VM:57388 jenkins 2024/05/19 01:28:24 28 4 AnalysisIns, 3 AnalysisOuts, 1 AnalysisDynOs 1 Bodies, 1 Tessellations testingAIMin has type VALUE, subtype ANALYSISIN with 0 attributes last: aimTest macys-VM:57388 jenkins 2024/05/19 01:28:04 10 hist: (null) -> Starting aimTest macys-VM:57388 jenkins 2024/05/19 01:28:04 10 value = 6.000000 cm table has type VALUE, subtype ANALYSISIN with 0 attributes last: aimTest macys-VM:57388 jenkins 2024/05/19 01:28:04 12 hist: (null) -> Starting aimTest macys-VM:57388 jenkins 2024/05/19 01:28:04 12 value (1x3) = 1: Entry1 -> newValue1 2: Entry2 -> newValue2 3: Entry3 -> newValue3 tessIn has type VALUE, subtype ANALYSISIN with 0 attributes last: aimTest macys-VM:57388 jenkins 2024/05/19 01:28:04 18 hist: (null) -> Starting aimTest macys-VM:57388 jenkins 2024/05/19 01:28:04 13 hist: (null) -> Child Execute aimTest macys-VM:57388 jenkins 2024/05/19 01:28:04 23 linked to tessOut meshFile has type VALUE, subtype ANALYSISIN with 0 attributes last: aimTest macys-VM:57388 jenkins 2024/05/19 01:28:04 10 hist: (null) -> Starting aimTest macys-VM:57388 jenkins 2024/05/19 01:28:04 10 value (0x0) = NULL with len = 0 meter testingAIMout has type VALUE, subtype ANALYSISOUT with 0 attributes last: aimTest macys-VM:57388 jenkins 2024/05/19 01:28:04 11 testingAIM/aimCalcOutput instance = 1 index = 1 testingAIMout 0! aim_getDiscr 1 on Interface = 0 aim_getDataSet 1 on Interface = -329 value = 12.340000 cm lazy: aimTest macys-VM:57388 jenkins 2024/05/19 01:28:24 28 tessOut has type VALUE, subtype ANALYSISOUT with 0 attributes last: aimTest macys-VM:57388 jenkins 2024/05/19 01:28:04 11 testingAIM/aimCalcOutput instance = 1 index = 2 tessOut 0! tessPtr = 7feb2ba079a0 value = 7feb2ba079a0 ego lazy: aimTest macys-VM:57388 jenkins 2024/05/19 01:28:24 28 meshFile has type VALUE, subtype ANALYSISOUT with 0 attributes last: aimTest macys-VM:57388 jenkins 2024/05/19 01:28:04 11 testingAIM/aimCalcOutput instance = 1 index = 3 meshFile 0! value (0x0) = NULL with len = 0 writer lazy: aimTest macys-VM:57388 jenkins 2024/05/19 01:28:24 28 Everything has type VALUE, subtype ANALYSISDYNO with 0 attributes last: aimTest macys-VM:57388 jenkins 2024/05/19 01:28:24 28 hist: (null) -> Child Execute aimTest macys-VM:57388 jenkins 2024/05/19 01:28:24 28 value = 42 (null) Interface has type BOUND, subtype NONE with 0 attributes last: aimTest macys-VM:57388 jenkins 2024/05/19 01:28:05 23 hist: (null) -> Starting aimTest macys-VM:57388 jenkins 2024/05/19 01:28:04 14 hist: (null) -> Child Execute aimTest macys-VM:57388 jenkins 2024/05/19 01:28:05 23 2 Connecteds, 0 UnConnecteds testingAIM1 has type VERTEXSET, subtype CONNECTED with 0 attributes last: aimTest macys-VM:57388 jenkins 2024/05/19 01:28:04 23 hist: (null) -> Starting aimTest macys-VM:57388 jenkins 2024/05/19 01:28:04 0 hist: (null) -> Child Execute aimTest macys-VM:57388 jenkins 2024/05/19 01:28:04 23 5 DataSets xyz has type DATASET, subtype NONE with 0 attributes last: aimTest macys-VM:57388 jenkins 2024/05/19 01:28:05 23 hist: (null) -> Starting aimTest macys-VM:57388 jenkins 2024/05/19 01:28:04 0 hist: (null) -> Child Execute aimTest macys-VM:57388 jenkins 2024/05/19 01:28:05 23 1040 points, rank=3, units=cm xyzd has type DATASET, subtype NONE with 0 attributes last: aimTest macys-VM:57388 jenkins 2024/05/19 01:28:04 0 hist: (null) -> Starting aimTest macys-VM:57388 jenkins 2024/05/19 01:28:04 0 0 points, rank=3, units=(null) param has type DATASET, subtype NONE with 0 attributes last: aimTest macys-VM:57388 jenkins 2024/05/19 01:28:05 23 hist: (null) -> Starting aimTest macys-VM:57388 jenkins 2024/05/19 01:28:04 0 hist: (null) -> Child Execute aimTest macys-VM:57388 jenkins 2024/05/19 01:28:05 23 1040 points, rank=2, units=(null) paramd has type DATASET, subtype NONE with 0 attributes last: aimTest macys-VM:57388 jenkins 2024/05/19 01:28:04 0 hist: (null) -> Starting aimTest macys-VM:57388 jenkins 2024/05/19 01:28:04 0 0 points, rank=2, units=(null) scalar has type DATASET, subtype NONE with 0 attributes last: aimTest macys-VM:57388 jenkins 2024/05/19 01:28:24 26 hist: (null) -> Starting aimTest macys-VM:57388 jenkins 2024/05/19 01:28:04 15 hist: (null) -> Child Execute aimTest macys-VM:57388 jenkins 2024/05/19 01:28:24 26 1040 points, rank=1, units=(null) testingAIM0 has type VERTEXSET, subtype CONNECTED with 0 attributes last: aimTest macys-VM:57388 jenkins 2024/05/19 01:28:05 23 hist: (null) -> Starting aimTest macys-VM:57388 jenkins 2024/05/19 01:28:04 0 hist: (null) -> Child Execute aimTest macys-VM:57388 jenkins 2024/05/19 01:28:05 23 6 DataSets xyz has type DATASET, subtype NONE with 0 attributes last: aimTest macys-VM:57388 jenkins 2024/05/19 01:28:05 23 hist: (null) -> Starting aimTest macys-VM:57388 jenkins 2024/05/19 01:28:04 0 hist: (null) -> Child Execute aimTest macys-VM:57388 jenkins 2024/05/19 01:28:05 23 442 points, rank=3, units=cm xyzd has type DATASET, subtype NONE with 0 attributes last: aimTest macys-VM:57388 jenkins 2024/05/19 01:28:04 0 hist: (null) -> Starting aimTest macys-VM:57388 jenkins 2024/05/19 01:28:04 0 0 points, rank=3, units=(null) param has type DATASET, subtype NONE with 0 attributes last: aimTest macys-VM:57388 jenkins 2024/05/19 01:28:05 23 hist: (null) -> Starting aimTest macys-VM:57388 jenkins 2024/05/19 01:28:04 0 hist: (null) -> Child Execute aimTest macys-VM:57388 jenkins 2024/05/19 01:28:05 23 442 points, rank=2, units=(null) paramd has type DATASET, subtype NONE with 0 attributes last: aimTest macys-VM:57388 jenkins 2024/05/19 01:28:04 0 hist: (null) -> Starting aimTest macys-VM:57388 jenkins 2024/05/19 01:28:04 0 0 points, rank=2, units=(null) scalar has type DATASET, subtype NONE with 0 attributes last: aimTest macys-VM:57388 jenkins 2024/05/19 01:28:05 25 hist: (null) -> Starting aimTest macys-VM:57388 jenkins 2024/05/19 01:28:04 0 hist: (null) -> Child Execute aimTest macys-VM:57388 jenkins 2024/05/19 01:28:05 25 442 points, rank=1, units=(null) vector has type DATASET, subtype NONE with 0 attributes last: aimTest macys-VM:57388 jenkins 2024/05/19 01:28:04 0 hist: (null) -> Starting aimTest macys-VM:57388 jenkins 2024/05/19 01:28:04 0 testingAIM/aimTransfer name = vector instance = 0 npts = 442/3! 442 points, rank=3, units=(null) 1: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 8: 14.400000 14.400000 14.400000 14.400000 14.400000 14.381076 14.400000 15: 14.400000 14.385654 14.400000 14.386399 14.400000 14.400000 14.400000 22: 14.400000 14.400000 14.400000 14.383470 14.400000 14.400000 14.400000 29: 14.400000 14.390663 14.400000 14.400000 14.400000 14.400000 14.400000 36: 14.400000 14.400000 14.390526 14.400000 14.400000 14.400000 14.400000 43: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 50: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 57: 14.400000 14.400000 14.400000 14.400000 14.377038 14.400000 14.377947 64: 14.400000 14.378370 14.400000 14.380439 14.400000 14.400000 14.400000 71: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 78: 14.390431 14.400000 14.400000 14.400000 14.391064 14.400000 14.384912 85: 14.400000 14.400000 14.400000 14.400000 14.400000 14.390113 14.400000 92: 14.400000 14.400000 14.400000 14.400000 14.388870 14.400000 14.400000 99: 14.400000 14.400000 14.386035 14.400000 14.384898 14.400000 14.400000 106: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 113: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 120: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 127: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 134: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 141: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 148: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 155: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 162: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 169: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 176: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 183: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 190: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 197: 14.400000 14.400000 14.400000 14.400000 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14.378848 14.384694 14.382523 14.382981 source getTriangles = 0, nGtris = 1962, nGsegs = 5886, Ds = 0 0 destin getTriangles = 0, nGtris = 790, nGsegs = 2370, Ds = 0 0 In caps_outputObjects: 2 Analyses found 1 Bounds found testingAIM/aimCleanup instance = 0! testingAIM/aimCleanup instance = 1! real 0m20.832s user 0m16.641s sys 0m0.561s + set +x + rm -rf source.vs destin.vs ============================================= CAPS test (using c-executables) case /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/test/aim testingAIM.csm passed (as expected) ============================================= + expectCSuccess '/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/test/autoExec testingAIM.csm' + /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/test/autoExec testingAIM.csm testingAIM/aimInitialize instance = 0 unitSys = m! testingAIM/aimInputs instance = 0 index = 1! testingAIM/aimInputs instance = 0 index = 2! testingAIM/aimInputs instance = 0 index = 3! testingAIM/aimInputs instance = 0 index = 4! testingAIM/aimOutputs instance = 0 index = 1! testingAIM/aimOutputs instance = 0 index = 2! testingAIM/aimOutputs instance = 0 index = 3! testingAIM/aimInitialize instance = 1 unitSys = (null)! testingAIM/aimInputs instance = 1 index = 1! testingAIM/aimInputs instance = 1 index = 2! testingAIM/aimInputs instance = 1 index = 3! testingAIM/aimInputs instance = 1 index = 4! testingAIM/aimOutputs instance = 1 index = 1! testingAIM/aimOutputs instance = 1 index = 2! testingAIM/aimOutputs instance = 1 index = 3! Intent = child APath = /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/CAPS/test/autoExecTest/Scratch/testingAIM1 UnitSys = (null) Exec = 2 Fields = scalar (1 1) vector (3 1) scalar (1 0) vector (3 0) Dirty = 3 real 0m0.945s user 0m0.624s sys 0m0.151s + set +x testingAIM/aimUpdateState instance = 0! tess is NULL! testingAIM/aimPreAnalysis instance = 0! testingAIM/aimPreAnalysis aim_getBounds = 0 aim_newGeometry = 0! getDiscr = -303 meshRef = NULL testingAIM/aimExecute instance = 0! testingAIM/aimPostAnalysis instance = 0 restart = 0! testingAIM/aimPostAnalysis: 0 -- 1 is Config Parameter testingAIM/aimCalcOutput instance = 0 index = 1 testingAIMout 0! aim_getDiscr 0 on Interface = -303 testingAIM/aimCalcOutput instance = 0 index = 3 meshFile 0! testingAIM/aimUpdateState instance = 1! tess is NULL! testingAIM/aimPreAnalysis instance = 1! testingAIM/aimPreAnalysis aim_getBounds = 0 aim_newGeometry = 0! mesh file = /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/CAPS/test/autoExecTest/Scratch/testingAIM0/meshFile symLink = 0 getDiscr = -303 testingAIM/aimExecute instance = 1! testingAIM/aimPostAnalysis instance = 1 restart = 0! testingAIM/aimCalcOutput instance = 1 index = 1 testingAIMout 0! aim_getDiscr 1 on Interface = -303 *** testingAIMout (child) = 12.340000 1 1 *** testingAIM/aimCleanup instance = 0! testingAIM/aimCleanup instance = 1! ============================================= CAPS test (using c-executables) case /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/test/autoExec testingAIM.csm passed (as expected) ============================================= ++ set +x [Execution node] check if [macys_VM] 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/7.8/CAPS/unit/DARWIN64') [GNU C Compiler (gcc)] Successfully parsed console log [GNU C Compiler (gcc)] -> found 0 issues (skipped 0 duplicates) [GNU C Compiler (gcc)] Skipping post processing [GNU C Compiler (gcc)] No filter has been set, publishing all 0 issues [GNU C Compiler (gcc)] Repository miner is not configured, skipping repository mining [Clang] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64') [Clang] -> found 0 issues (skipped 0 duplicates) [Clang] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64') [Clang] -> found 0 issues (skipped 0 duplicates) [Clang] Successfully parsed console log [Clang] -> found 0 issues (skipped 0 duplicates) [Clang] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64') [Clang] Skipping post processing [Clang] No filter has been set, publishing all 0 issues [Clang] Repository miner is not configured, skipping repository mining [Static Analysis] Successfully parsed console log [Static Analysis] -> found 0 issues (skipped 0 duplicates) [Static Analysis] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64') [Static Analysis] Successfully parsed console log [Static Analysis] -> found 0 issues (skipped 0 duplicates) [Static Analysis] Skipping post processing [Static Analysis] No filter has been set, publishing all 0 issues [Static Analysis] Repository miner is not configured, skipping repository mining [Static Analysis] Successfully parsed console log [Static Analysis] -> found 0 issues (skipped 0 duplicates) [Static Analysis] Successfully parsed console log [Static Analysis] -> found 0 issues (skipped 0 duplicates) [Static Analysis] Successfully parsed console log [Static Analysis] -> found 0 issues (skipped 0 duplicates) [Static Analysis] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN64') [Static Analysis] Skipping post processing [Static Analysis] No filter has been set, publishing all 0 issues [Static Analysis] Repository miner is not configured, skipping repository mining [Static Analysis] Reference build recorder is not configured [Static Analysis] 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=7.8,ESPTEST=CAPS/unit,ESP_ARCH=DARWIN64,buildnode=macys_VM #650'. [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